AVIONIC B-system
SYSTEM I-system
DESCRIPTION O
( O
Example O
document O
for O
LSA O
applicants O
– O
v1 O
of O
17 O
. O

02 O
. O

16 O
) O
Introduction O
This O
document O
describes O
the O
Avionic B-system
System I-system
of O
the O
ABCD O
aircraft B-asset
according O
to O
the O
requirements O
as O
referenced O
in O
the O
certification O
programme O
( O
ref O
. O

1 O
) O
. O

The O
aim O
of O
this O
document O
to O
describe O
the O
avionic B-system
system I-system
of O
the O
aeroplane B-asset
and O
demonstrate O
compliance O
to O
the O
requirements O
. O

This O
document O
is O
essential O
, O

when O
the O
applicant O
’ O
s O
design O
contains O
non O
- O
certified O
elements O
. O

( O
e O
. O

g O
. O

instruments O
what O
aren O
’ O
t O
ETSO O
certified O
) O
References O
Certification O
Programme O
ABCD O
- O
CP O
- O
00 O
List O
of O
Abbreviations O
A O
/ O
C O
– O
Aircraft B-asset
A O
/ O
D O
– O
Analog B-parameter
/ I-parameter
Digital I-parameter
AC O
– O
Alternate B-parameter
Current I-parameter
AC O
( O
2 O
) O
Advisory O
Circular O
( O
FAA O
) O
ADC O
– O
Air B-module
Data I-module
Computer I-module
ALT O
– O
Altitude B-parameter
indicator I-module
Amp O
– O
Amperes B-measurement
AOA O
– O
Angle B-parameter
of I-parameter
Attack I-parameter
AP O
– O
Alternative O
Procedures O
of O
Design O
Organization O
ASI O
– O
Airspeed B-module
Indicator I-module
ASTM O
– O
American O
Society O
for O
Testing O
and O
Materials O
ATM O
– O
Air O
Traffic O
Management O
CB O
– O
Circuit B-component
Breakers I-component
CDI O
– O
Course B-module
Deviation I-module
Indicator I-module
CHT O
– O
Cylinder B-parameter
Head I-parameter
Temperature I-parameter
COM O
– O
Communication O
CS O
– O
Certification O
Specifications O
CS O
- O
LSA O
– O
Certification O
Specifications O
for O
Light O
Sport O
Aircraft O
DC O
– O
Direct B-parameter
Current I-parameter
DOA O
– O
Design O
Organization O
Approval O
EASA O
– O
European O
Aviation O
Safety O
Agency O
EFIS O
– O
Electronic B-system
Flight I-system
Instrument I-system
System I-system
ELA O
– O
European O
Light O
Aircraft B-asset
ETSO O
– O
European O
Technical O
Standard O
Order O
FAA O
– O
Federal O
Aviation O
Administration O
FOV O
– O
Field B-parameter
- I-parameter
of I-parameter
- I-parameter
View I-parameter
GNSS O
– O
Global B-module
Navigation I-module
Satellite I-module
System I-module
GPS O
– O
Global B-module
Positioning I-module
System I-module
HSI O
– O
Horizontal B-module
Situation I-module
Indicator I-module
Hg O
In O
– O
Inches I-parameter
of I-parameter
Mercury I-parameter
IC O
– O
Intercom B-module
ILS O
– O
Instrument B-module
Landing I-module
System I-module
LH O
– O
Left B-location
Hand I-location
( I-location
side I-location
) I-location
MFD O
– O
multi B-module
- I-module
function I-module
display I-module
NAV O
– O
Navigation B-module
OAT O
– O
Outside B-parameter
Air I-parameter
Temperature I-parameter
OP O
– O
Oil B-parameter
Pressure I-parameter
OT O
– O
Oil B-parameter
Temperature I-parameter
P O
/ O
N O
– O
Part O
Number O
PFD O
– O
Primary B-module
Flight I-module
Display I-module
PMA O
– O
Parts O
Manufacturer O
Approval O
RH O
– O
Right B-location
Hand I-location
( I-location
side I-location
) I-location
RPM O
– O
Revolution B-parameter
per I-parameter
minute I-parameter
S O
/ O
N O
– O
Serial O
Number O
SAE O
– O
Society O
of O
Automotive O
Engineers O
TSO O
– O
Technical O
Standard O
Order O
V O
– O
Volts B-parameter
VHF O
– O
Very B-parameter
High I-parameter
Frequency I-parameter
VOR O
– O
VHF B-module
Omnidirectional I-module
Range I-module
W O
– O
Watts B-parameter
Description O
The O
aircraft B-asset
ABCD O
has O
a O
semi B-system
- I-system
conventional I-system
instrument I-system
panel I-system
, I-system

intended O
for O
Day O
- O
VFR O
operation O
. O

The O
conventional O
“ O
sixpack O
” O
is O
replaced O
with O
an O
EFIS B-system
display I-system
on O
the O
pilot O
side O
, O

and O
contains O
the O
necessary O
flight O
data O
and O
engine O
data O
. O

The O
display B-module
has O
controls B-system
for O
the O
remote B-module
- I-module
controlled I-module
VHF I-module
radio I-module
, O

and O
NAV B-module
radio I-module
including O
VOR B-module
/ I-module
ILS I-module
, O

GNSS B-module
. O

The O
ignition B-component
switch I-component
is O
located O
on O
the O
left B-location
side I-location
of O
the O
panel B-system
. O

The O
master B-control
switch I-control
and O
the O
electrical B-control
switches I-control
( O
lights B-component
, O

avionic B-component
master I-component
, O

fuel B-component
pump I-component
, O

etc O
. O

) O
are O
located O
below B-location
the O
display B-module
. O

Above B-location
the O
display B-module
, O

a O
placard B-component
shows O
the O
applicable O
limitations B-parameter
( O
MTOW O
, O

Operational O
limitations O
, O

manoeuvring B-parameter
speed I-parameter
, O

manoeuvres O
, O

IMC O
limitations O
) O
. O

The O
instrument B-system
panel I-system
is O
divided O
into O
five O
sections O
: O
LH B-location
, O

centre B-location
, O

RH B-location
, O

instrument B-component
panel I-component
cover I-component
, O

and O
centre B-component
console I-component
. O

The O
EFIS B-system
display I-system
is O
located O
on O
the O
LH B-location
section O
together O
with O
the O
analogue B-module
indicators I-module
for O
airspeed B-parameter
and O
altitude B-parameter
. O

The O
stack O
for O
radio B-module
, O

transponder B-module
, O

navigation B-module
and O
GPS B-module
are O
located O
on O
the O
centre B-system
panel I-system
. O

Engine B-module
analogue I-module
instruments I-module
are O
located O
to O
the O
right B-location
. O

Location O
of O
circuit B-module
breakers I-module
( O
CB O
) O
are O
divided O
. O

The O
primary O
C O
/ O
B O
’ O
s O
, O

such O
as O
battery B-component
master I-component
, O

avionic B-component
master I-component
, O

flaps B-module
, O

etc O
. O

are O
placed O
in B-location
front I-location
of I-location
the O
pilot O
, O

the O
secondary O
circuit B-module
breakers I-module
, O

such O
as O
C O
/ O
B O
’ O
s O
for O
the O
conventional B-component
engine I-component
instruments I-component
are O
placed O
to O
the O
right B-location
side O
. O

Requirements O
The O
applicable O
requirements O
of O
CS O
- O
LSA O
. O

15 O
( O
Reference O
standard O
: O
ASTM O
F2245 O
- O
12d O
) O
as O
defined O
in O
the O
Certification O
programme O
( O
Ref O
. O

1 O
) O
, O

are O
shown O
in O
the O
table O
below O
. O

( O
NOTE O
: O
at O
the O
time O
of O
issue O
of O
this O
template O
, O

the O
CS O
- O
LSA O
amdt O
1 O
is O
in O
place O
which O
includes O
the O
ASTM O
F2245 O
- O
12d O
. O

If O
later O
amendments O
of O
the O
CS O
- O
LSA O
or O
ASTM O
are O
in O
place O
, O

they O
should O
be O
considered O
. O

The O
structure O
of O
the O
document O
remains O
the O
same O
, O

but O
the O
requirements O
defined O
in O
the O
certification O
basis O
agreed O
with O
the O
Agency O
shall O
be O
considered O
) O
Table O
1 O
– O
Cross O
reference O
table O
for O
CS O
- O
LSA O
requirements O
The O
design O
of O
the O
avionic B-system
system I-system
of O
the O
Airplane B-asset
ABCD O
meets O
also O
the O
standards O
provided O
by O
the O
certification O
memo O
“ O
Acceptance O
of O
Electronic B-module
Flight I-module
Instrument I-module
Systems I-module
without O
own O
equipment O
approval O
in O
Small O
Aeroplanes O
( O
ELA1 O
) O
” O
. O

A O
cross O
reference O
table O
is O
provided O
in O
Appendix O
1 O
. O

NOTE O
: O
at O
the O
date O
of O
issue O
of O
this O
template O
, O

the O
certification O
memo O
is O
still O
in O
consultation O
. O

Since O
the O
certification O
memo O
is O
not O
published O
yet O
, O

It O
might O
happen O
that O
the O
final O
version O
of O
the O
Certification O
Memo O
will O
differ O
in O
some O
aspects O
, O

nevertheless O
the O
intent O
of O
the O
certification O
memo O
is O
expected O
to O
remain O
the O
same O
. O

Instrument O
panel O
layout O
( O
NOTE O
: O
this O
document O
has O
been O
written O
considering O
a O
typical O
hybrid O
digital O
/ O
analog O
solution O
of O
the O
instrument B-system
panel I-system
. O

This O
is O
not O
aimed O
to O
suggest O
a O
“ O
desirable O
” O
solution O
by O
the O
Agency O
. O

Any O
solution O
, O

as O
long O
as O
it O
complies O
to O
the O
requirements O
, O

can O
be O
proposed O
and O
should O
be O
evaluated O
with O
the O
approach O
shown O
in O
this O
document O
) O
Figure O
1 O
– O
Instrument B-module
Panel I-module
Layout I-module
EFIS B-module
screen I-module
details O
The O
display B-module
is O
an O
8 O
” O
, O

high O
resolution O
VGA O
screen O
, O

with O
built O
- O
in O
features O
: O
Air B-module
data I-module
computer I-module
VOR B-module
and I-module
ILS I-module
LOC I-module
radio I-module
COM B-module
radio I-module
GPS B-module
receiver I-module
Glideslope B-module
receiver I-module
Solid B-module
- I-module
state I-module
attitude I-module
and I-module
heading I-module
reference I-module
system I-module
A B-module
/ I-module
D I-module
converter I-module
An O
audio B-module
panel I-module
is O
installed O
in O
the O
central O
section O
of O
the O
instrument B-system
panel I-system
. O

It O
contains O
controls B-system
for O
the O
pilot O
’ O
s O
and O
the O
passenger O
’ O
s O
audio O
output O
. O

The O
audio B-module
panel I-module
communicates O
with O
the O
avionics B-module
unit I-module
using O
RS B-parameter
- I-parameter
232 I-parameter
digital I-parameter
interface I-parameter
. O

Each O
microphone B-module
input O
has O
a O
dedicated O
VOX B-module
circuit I-module
to O
ensure O
that O
only O
the O
active O
microphone B-module
( O
s O
) O
is O
/ O
are O
heard O
when O
squelch B-control
is O
broken O
. O

After O
the O
operator O
has O
stopped O
talking O
, O

the O
intercom O
channel O
remains O
momentarily O
open O
to O
avoid O
closure O
between O
words O
or O
normal O
pauses O
. O

Remote O
VHF B-module
NAV I-module
/ I-module
COM I-module
receiver I-module
is O
located O
in O
the O
avionics B-module
rack I-module
, O

behind O
the O
co O
- O
pilot O
’ O
s O
seat B-system
. I-system

Panel B-module
- I-module
mounted I-module
VHF I-module
NAV I-module
/ I-module
COM I-module
/ I-module
GPS I-module
receiver I-module
is O
located O
in O
the O
central B-location
section O
of O
instrument B-system
panel I-system
. O

Both O
COM B-module
radios I-module
are O
able O
for O
8 O
. O

33 O
kHz O
channel O
spacing O
. O

The O
frequencies O
can O
be O
displayed O
additionally O
on O
the O
PFD B-module
. O

The O
COM B-module
radio I-module
is O
able O
for O
8 O
. O

33 O
kHz B-measurement
channel O
spacing O
. O

Parts O
of O
the O
EFIS B-module
screen I-module
Attitude B-parameter
indicator I-module
is O
located O
in O
the O
centre B-location
of O
the O
screen O
. O

Airspeed B-parameter
tape O
is O
located O
on O
the O
left B-location
side O
of O
the O
attitude B-module
indicator I-module
. O

True O
airspeed B-parameter
is O
digitally O
displayed O
in O
a O
small O
window O
below O
the O
airspeed B-parameter
tape O
. O

The O
airspeed B-module
indicator I-module
also O
displays O
speed B-parameter
ranges O
for O
different O
airplane B-asset
configurations O
( O
flaps O
retracted O
or O
extended O
) O
, O

airspeed B-parameter
trends O
and O
‘ B-parameter
V I-parameter
’ I-parameter
speeds I-parameter
. O

If O
the O
airspeed B-module
indicator I-module
fails O
, O

the O
display B-module
marks O
the O
airspeed B-parameter
display O
area O
with O
a O
red O
’ O
X O
’ O
and O
red O
text O
spelling O
out O
‘ O
AIRSPEED B-parameter
FAILURE O
’ O
. O

The O
altimeter B-module
is O
located O
on O
the O
RH B-location
side O
of O
the O
attitude B-module
indicator I-module
. O

The O
altimeter B-module
displays O
the O
airplane B-asset
altitude B-parameter
in O
feet O
on O
a O
rolling O
number O
gauge O
( O
like O
a O
drum O
- O
pointer O
altimeter O
) O
using O
a O
moving O
tape O
. O

The O
altimeter B-module
also O
shows O
an O
‘ O
altitude O
bug O
’ O
at O
the O
selected O
altitude B-parameter
or O
on O
the O
top O
or O
bottom O
of O
the O
tape O
. O

If O
the O
altitude B-module
indicator I-module
fails O
, O

the O
display O
marks O
the O
tape O
display O
area O
with O
a O
red O
’ O
X O
’ O
and O
red O
text O
spelling O
out O
‘ O
ALTITUDE B-parameter
FAILURE O
’ O
. O

The O
vertical B-module
speed I-module
indicator I-module
is O
located O
to O
the O
right B-location
of O
the O
altitude B-parameter
indicator I-module
. O

The O
indicator B-module
displays O
the O
airplane B-asset
vertical B-parameter
speed I-parameter
in O
feet B-measurement
/ I-measurement
min I-measurement
. O

A O
numeric B-component
pointer I-component
moves O
vertically O
up O
/ O
down O
a O
fixed B-component
tape I-component
. O

The O
vertical B-parameter
speed I-parameter
indication O
is O
shown O
digitally O
on O
the O
pointer B-component
. O

The O
scale O
on O
the O
tape O
gives O
the O
positive O
or O
negative O
multiplication O
factor O
on O
a O
1000 O
feet B-measurement
/ I-measurement
min I-measurement
ticks O
scale O
. O

A O
negative O
sign O
is O
shown O
on O
the O
pointer B-component
to O
indicate O
negative O
vertical B-parameter
speeds I-parameter
( O
airplane B-asset
descending O
) O
. O

If O
the O
VSI O
fails O
the O
display O
marks O
the O
tape O
display O
area O
with O
a O
red O
’ O
X O
’ O
and O
yellow O
text O
spelling O
out O
‘ O
VERT O
SPEED B-parameter
FAIL O
’ O
. O

Horizontal B-module
situation I-module
indicator I-module
( O
HSI O
) O
. O

The O
HSI O
is O
located O
in O
the O
center B-location
of O
the O
screen B-module
at O
the O
bottom O
. O

The O
HSI B-module
displays O
a O
rotating O
circular O
compass O
with O
heading O
markings O
. O

The O
HSI O
shows O
the O
following O
information O
: O
Heading B-parameter
information I-parameter
, O

as O
a O
direct O
reading O
compass O
. O

The O
heading O
is O
shown O
digitally O
in O
a O
window O
at O
the O
top B-location
of O
the O
rotating O
compass O
. O

Turn B-component
rate I-component
indicator I-component
. O

A O
turn B-component
rate I-component
indicator I-component
is O
located O
between O
the O
digital O
heading O
window O
and O
the O
rotating O
compass O
. O

Course B-component
deviation I-component
indicator I-component
( O
CDI O
) O
. O

The O
CDI O
is O
a O
line O
with O
an O
arrowhead O
that O
points O
to O
the O
airplane B-asset
heading O
on O
the O
rotating O
compass O
. O

The O
line O
can O
slide O
left O
or O
right O
of O
the O
center O
marking O
to O
show O
the O
deviation O
of O
the O
actual O
course O
being O
flown O
to O
the O
required O
course O
. O

Course O
data O
can O
be O
supplied O
from O
the O
airplane B-asset
VOR B-module
, O

LOC B-module
or O
GPS B-module
system I-module
. O

If O
the O
heading O
data O
is O
invalid O
the O
digital O
heading O
display O
window O
is O
marked O
with O
a O
red O
cross O
and O
yellow O
text O
spelling O
‘ O
HEADING O
ERROR O
’ O
. O

Vertical B-component
deviation I-component
( I-component
glideslope I-component
) I-component
indicator I-component
. O

The O
glideslope B-component
indicator I-component
is O
located O
to O
the O
left B-location
of O
the O
vertical B-module
speed I-module
indicator I-module
. O

Alerts B-component
window I-component
. O

The O
alerts B-component
window I-component
is O
located O
on O
the O
right I-location
side O
of O
the O
screen B-module
. O

This O
window B-component
opens O
when O
an O
alert O
is O
activated O
. O

( O
NOTE O
: O
the O
list O
of O
alerts O
should O
be O
provided O
) O
Warnings B-component
and I-component
cautions I-component
window I-component
. O

The O
warnings B-component
and I-component
cautions I-component
window I-component
is O
located O
above B-location
the O
alerts B-component
window I-component
. O

When O
an O
alert O
occurs O
, O

it O
supersedes O
the O
cautions O
and O
warnings O
. O

( O
NOTE O
: O
the O
list O
of O
warning O
/ O
caution O
messages O
should O
be O
provided O
) O
The O
navigation B-component
map I-component
( I-component
moving I-component
map I-component
) I-component
window I-component
is O
located O
in O
the O
lower O
left B-location
of O
the O
screen B-module
. O

The O
window O
shows O
a O
pictorial O
view O
of O
the O
airplane B-asset
on O
a O
moving O
map O
. O

Small B-component
bezels I-component
in O
the O
top B-location
left B-location
corner O
of O
the O
screen B-module
show O
active O
and O
standby O
NAV B-parameter
frequencies I-parameter
. O

Small B-component
windows I-component
in O
the O
top B-location
right B-location
of O
the O
PFD B-module
show O
active O
and O
standby O
COM B-parameter
frequencies I-parameter
. O

A O
larger O
horizontal O
band O
in O
the O
top B-location
centre B-location
of O
the O
PFD B-module
shows O
flight O
planning O
data O
when O
activated O
. O

A O
small B-component
window I-component
in O
the O
bottom B-location
left B-location
of O
the O
PFD B-module
shows O
the O
outside B-parameter
air I-parameter
temperature I-parameter
( O
OAT O
) O
. O

A O
small B-component
windows I-component
on O
the O
bottom B-location
right B-location
of O
the O
PFD B-module
shows O
the O
transponder B-parameter
settings I-parameter
and O
operational B-parameter
state I-parameter
. O

Another O
small B-component
window I-component
in O
the O
right B-location
bottom B-location
corner O
of O
the O
PFD B-module
shows O
a O
digital B-parameter
clock I-parameter
. O

A O
set O
of O
labels O
along O
the O
very O
bottom B-location
of O
the O
PFD B-module
identifies O
the O
function O
of O
the O
softkeys O
for O
the O
current O
page O
being O
displayed O
on O
the O
PFD B-module
. O

The O
engine B-component
indication I-component
system I-component
window I-component
is O
on O
the O
right B-location
side O
of O
the O
screen B-module
, O

that O
displays O
a O
full O
- O
time O
dedicated O
display O
of O
these O
engine B-system
parameters O
( O
backup O
engine O
instruments O
are O
placed O
on O
the O
right O
side O
of O
the O
instrument B-system
panel I-system
) O
: O
NOTE O
: O
in O
this O
example O
, O

the O
primary O
source O
of O
information O
is O
provided O
by O
the O
EFIS B-system
display I-system
. O

Engine B-parameter
RPM I-parameter
. O

The O
engine B-component
RPM I-component
indicator I-component
is O
located O
on O
the O
top O
of O
the O
engine B-system
parameters O
side O
. O

A O
pointer B-component
on O
a O
gauge O
- O
like O
circle O
moves O
to O
show O
the O
engine B-parameter
rpm I-parameter
. O

If O
the O
system O
fails O
the O
display B-module
shows O
a O
red O
cross O
on O
the O
rpm O
indicator O
. O

Manifold B-parameter
pressure I-parameter
( O
MP O
) O
The O
manifold B-component
pressure I-component
indicator I-component
is O
a O
horizontal O
bar O
below B-location
the O
RPM B-component
indicator I-component
, O

with O
an O
arrow O
- O
like O
pointer O
. O

The O
exact O
MP B-parameter
value I-parameter
in O
inches O
of O
mercury O
is O
displayed O
above O
the O
horizontal B-component
bar I-component
. O

The O
operating O
range O
of O
MP B-parameter
values I-parameter
is O
marked O
with O
a O
green O
band O
. O

The O
pointer O
moves O
from O
left O
to O
right O
to O
show O
the O
increasing O
manifold B-parameter
pressure I-parameter
. O

Cylinder B-parameter
- I-parameter
head I-parameter
temperature I-parameter
( I-parameter
CHT I-parameter
) I-parameter
indicator I-component
. O

This O
indicator O
is O
found O
below B-location
the O
MP B-component
indicator I-component
. O

This O
is O
also O
a O
horizontal O
bar O
, O

with O
an O
arrow O
- O
like O
pointer O
. O

The O
operating O
range O
of O
CHT B-parameter
values I-parameter
is O
marked O
with O
a O
small O
green O
band O
, O

the O
caution O
areas O
are O
marked O
with O
bigger O
yellow O
bands O
. O

The O
exact O
value O
of O
CHT B-parameter
is O
shown O
on O
the O
right O
side O
of O
the O
indicator O
in O
◦ O
C O
. O

Oil B-component
temperature I-component
indicator I-component
( O
OT O
) O
. O

This O
indicator O
is O
placed O
below B-location
the O
CHT B-component
indicator I-component
, O

and O
this O
is O
also O
a O
horizontal O
bar O
, O

with O
a O
pointer O
, O

with O
green O
- O
marked O
operating O
range O
. O

The O
exact O
value O
in O
◦ I-measurement
C I-measurement
. O

Oil B-component
pressure I-component
indicator I-component
( O
OP O
) O
is O
located O
below B-location
the O
oil B-component
temperature I-component
indicator I-component
. O

This O
indicator O
is O
a O
horizontal O
bar O
, O

with O
an O
arrow O
- O
like O
pointer O
. O

A O
small O
number O
on O
the O
right O
side O
shows O
the O
oil B-parameter
pressure I-parameter
digitally O
( O
in O
bars O
) O
. O

If O
the O
OP O
drops O
suddenly O
, O

a O
yellow O
bezel O
is O
shown O
around O
the O
indicator O
to O
get O
the O
pilot O
’ O
s O
attention O
. O

The O
main B-parameter
bus I-parameter
voltage I-parameter
is O
displayed O
below O
the O
RPM B-component
indicator I-component
. O

A O
pointer O
above O
a O
horizontal B-component
range I-component
bar I-component
shows O
the O
main B-parameter
bus I-parameter
voltage I-parameter
. O

The O
horizontal B-component
range I-component
bar I-component
is O
color O
coded O
, O

too O
. O

The O
green O
central O
section O
of O
the O
bar O
indicates O
that O
the O
voltage B-parameter
is O
within O
limits O
. O

The O
red O
section O
at O
the O
left O
end O
of O
the O
range O
bar O
indicates O
too O
low O
a O
voltage B-parameter
. O

The O
red O
section O
at O
the O
right O
end O
of O
the O
range O
bar O
indicates O
too O
high O
a O
voltage B-parameter
. O

Above O
the O
range O
bar O
is O
a O
window O
displaying O
the O
main B-parameter
bus I-parameter
voltage I-parameter
digitally O
. O

Amps B-measurement
. O

The O
generator O
load O
is O
shown O
by O
an O
indicator O
located O
below O
the O
Volts B-component
indicator I-component
. O

A O
pointer O
above O
a O
horizontal B-component
range I-component
bar I-component
shows O
the O
generator O
load O
. O

The O
pointer O
moves O
from O
left O
to O
right O
to O
show O
the O
load O
on O
the O
generator O
. O

When O
the O
generator B-parameter
output I-parameter
and O
the O
electric O
demands O
is O
in O
balance O
, O

the O
pointer O
remains O
in O
middle O
. O

When O
the O
pointer O
moves O
to O
right O
, O

it O
means O
the O
generator O
charges O
the O
battery B-module
. O

When O
the O
pointer O
moves O
to O
left O
, O

it O
means O
the O
generator O
’ O
s O
performance O
is O
insufficient O
to O
supply O
the O
electrical O
demands O
, O

so O
the O
battery O
energizes O
the O
electrical B-system
system I-system
. O

Fuel B-parameter
quantity I-parameter
. O

The O
fuel B-parameter
quantity I-parameter
indication O
is O
located O
at O
the O
bottom B-location
of O
the O
engine B-module
parameters I-module
annunciator I-module
. O

Pointers O
above O
and O
below O
a O
range O
bar O
indicate O
the O
fuel B-parameter
quantities I-parameter
. O

The O
pointers O
move O
from O
left O
( O
low O
) O
to O
right O
( O
full O
) O
to O
indicate O
the O
fuel B-parameter
quantity I-parameter
. O

The O
pointer O
above O
the O
range O
bar O
indicates O
the O
quantity O
of O
fuel O
in O
the O
left O
fuel B-component
tank I-component
and O
the O
pointer O
below O
the O
range O
bar O
indicates O
the O
quantity O
of O
fuel O
in O
the O
right O
fuel B-component
tank I-component
. O

The O
indicator O
is O
color O
- O
coded O
, O

when O
the O
fuel O
- O
quantity O
reaches O
the O
amount O
of O
11 O
liters B-measurement
( O
the O
fuel O
needed O
for O
30 O
minutes B-measurement
flight O
+ O
10 O
% O
safety O
margin O
at O
1500 O
’ O
above O
sea O
level O
+ O
the O
unusable O
fuel O
amount O
) O
the O
indicator O
becomes O
red O
. O

The O
11 O
liter B-measurement
( O
2 O
. O

9 O
USG O
) O
total O
fuel O
quantity O
( O
5 O
. O

5 O
liters B-measurement
/ O
1 O
. O

45 O
USG O
for O
each O
fuel O
tank O
) O
is O
marked O
with O
a O
red O
band O
on O
the O
horizontal O
bars O
. O

The O
exact O
fuel O
amount O
is O
shown O
on O
the O
top O
of O
the O
fuel O
bar O
. O

( O
Left O
and O
Right O
side O
tanks O
) O
. O

Field O
of O
view O
Because O
of O
the O
absence O
of O
more O
precise O
requirements O
within O
CS O
- O
LSA O
/ O
ASTM O
F2245 O
- O
12d O
for O
the O
visibility O
of O
instrumentation O
, O

an O
analysis O
of O
the O
primary O
field O
of O
view O
has O
been O
performed O
following O
AC O
23 O
. O

1311 O
- O
1C O
. O

The O
aim O
is O
to O
give O
to O
the O
pilot O
the O
ability O
to O
use O
all O
the O
required O
instruments O
with O
“ O
minimum O
head O
and O
eye O
movement O
” O
. O

The O
definitions O
below O
of O
AC O
23 O
. O

1311 O
- O
1C O
are O
considered O
. O

The O
definition O
of O
the O
Primary O
Maximum O
Field O
- O
of O
- O
View O
of O
AC O
23 O
. O

1311 O
- O
1C O
has O
been O
considered O
with O
one O
exception O
: O
a O
Field O
of O
View O
larger O
than O
+ O
/ O
– O
35 O
degrees O
horizontal O
and O
including O
almost O
the O
whole O
instrument B-system
panel I-system
has O
been O
considered O
acceptable O
. O

The O
justification O
is O
based O
on O
the O
reduced O
size O
of O
the O
instrument B-system
panel I-system
and O
the O
reduced O
number O
of O
needed O
information O
for O
a O
VFR O
- O
DAY O
airplane B-asset
. O

This O
has O
been O
assessed O
through O
an O
in O
- O
flight O
review O
and O
pilot O
assessment O
, O

which O
is O
recorded O
in O
document O
ABCD O
- O
FTR O
- O
00B O
“ O
Qualitative O
pilot O
statements O
” O
, O

where O
it O
is O
shown O
that O
all O
the O
displayed O
info O
, O

including O
engine B-system
analog O
instruments O
, O

are O
visible O
through O
pilot O
’ O
s O
visual O
scan O
and O
minimized O
head O
rotation O
. O

Note O
: O
the O
assessment O
above O
is O
very O
specific O
but O
it O
can O
be O
acceptable O
after O
review O
of O
EASA O
Flight O
test O
pilot O
. O

Figure O
3 O
– O
Field O
of O
View O
The O
table O
below O
shows O
the O
location O
of O
the O
equipment O
with O
respect O
to O
the O
above O
definitions O
of O
the O
Field O
of O
Views O
. O

Table O
2 O
– O
location O
of O
the O
displayed O
information O
on O
the O
instrument B-system
panel I-system
System O
schematics O
Flight O
instrumentation O
This O
sections O
provide O
a O
more O
detailed O
description O
of O
the O
individual O
equipment O
( O
information O
displayed O
, O

type O
of O
calibration O
performed O
, O

level O
of O
qualification O
, O

environmental O
conditions O
, O

scale O
range O
, O

etc O
. O

) O
. O

It O
is O
important O
to O
consider O
that O
the O
primary O
source O
of O
information O
for O
flight O
data O
is O
the O
EFIS O
. O

Thus O
the O
analogue O
serves O
as O
backup O
. O

Pitot B-module
- I-module
static I-module
instruments I-module
Navigation B-component
instruments I-component
Backup B-component
engine I-component
instruments I-component
Warning B-component
lights I-component
Main B-component
switches I-component
Circuit B-component
Breakers I-component
Other B-component
instruments I-component
and I-component
switches I-component
Transponder B-module
The O
XPNDR O
123 O
is O
a O
solid O
state O
Mode O
- O
S O
transponder O
. O

The O
transponder B-module
provides O
modes O
A O
, O

C O
and O
S O
functions O
. O

The O
unit O
is O
operated O
directly O
through O
the O
display B-component
’ I-component
s I-component
softkeys I-component
or O
the O
panel B-system
. O

The O
transponder B-module
is O
linked O
to O
the O
avionics B-module
unit I-module
via O
RS O
- O
232 O
digital B-parameter
interface I-parameter
. O

The O
transponder B-module
is O
installed O
in O
the O
bottom O
part O
of O
the O
middle O
instrument B-system
panel I-system
. O

Flap B-component
switch I-component
, O

and O
flap B-component
position I-component
indicator I-component
The O
flap B-component
switch I-component
and O
position B-component
indicator I-component
have O
been O
integrated O
into O
one O
unit O
. O

The O
positions O
are O
shown O
by O
LEDs O
for O
each O
flap O
position O
. O

One O
for O
the O
UP O
, O

one O
for O
the O
15 O
° O
, O

and O
one O
for O
the O
30 O
° O
position O
. O

Units O
integrated O
into O
the O
EFIS B-system
display I-system
AHRS B-module
: O
it O
provides O
airplane B-parameter
attitude I-parameter
and O
related O
flight O
data O
to O
the O
display O
. O

It O
receives O
data O
from O
the O
air O
data O
computer O
, O

the O
magnetometer B-module
and O
GPS B-component
signals I-component
. O

The O
Air B-module
Data I-module
Computer I-module
( O
ADC O
) O
receives O
data O
from O
the O
Pitot B-system
/ I-system
static I-system
system I-system
and O
an O
OAT B-parameter
sensor O
. O

The O
ADC O
uses O
this O
data O
to O
provide O
pressure B-parameter
altitude I-parameter
, O

airspeed B-parameter
, O

vertical B-parameter
speed I-parameter
and O
outside B-parameter
air I-parameter
temperature I-parameter
data O
to O
the O
EFIS B-system
system I-system
. O

Software O
and O
configuration O
data O
is O
received O
through O
RS O
- O
232 O
digital B-parameter
interface I-parameter
. O

The O
ADC O
is O
located O
inside O
the O
EFIS B-module
display I-module
unit I-module
. O

Integrated B-module
avionics I-module
unit I-module
processes O
all O
the O
data O
that O
is O
shown O
on O
the O
EFIS B-system
display I-system
. O

Engine B-module
I I-module
/ I-module
O I-module
unit I-module
is O
integrated O
into O
the O
EFIS B-module
display I-module
unit I-module
itself O
. O

It O
is O
a O
microprocessor B-module
based I-module
unit I-module
that O
receives O
and O
processes B-parameter
signals I-parameter
from O
airframe B-system
and O
engine B-component
sensors I-component
. O

( O
CHT B-component
sensor I-component
, O

RPM B-component
sensor I-component
, O

OAT B-parameter
, O

etc O
. O

) O
Magnetometer B-component
: O
it O
senses O
magnetic B-parameter
field I-parameter
information I-parameter
. O

Data O
is O
sent O
to O
the O
AHRS O
for O
processing O
. O

The O
magnetometer B-module
receives O
power O
from O
the O
AHRS O
and O
communicates O
with O
it O
using O
RS O
- O
485 O
digital B-parameter
interface I-parameter
. O

The O
magnetometer B-module
is O
located O
in O
the O
left O
outer O
wing B-system
and O
can O
accessed O
through O
a O
panel B-system
in O
the O
lower B-location
surface O
of O
the O
wing B-system
. O

Antenna O
and O
sensor O
locations O
The O
GPS B-module
antenna I-module
is O
located O
on O
the O
upper B-location
side O
of O
the O
fuselage B-system
. O

The O
COM B-module
antenna I-module
is O
located O
on O
the O
top B-location
of O
the O
vertical B-module
stabilizer I-module
. O

The O
NAV B-module
antenna I-module
is O
located O
underside B-location
of O
the O
fuselage B-system
. O

The O
pitot B-module
- I-module
static I-module
tube I-module
is O
located O
on O
the O
left O
wing B-system
. I-system

The O
magnetometer B-module
is O
located O
inside B-location
of O
the O
left O
wing B-system
. O

Antenna O
types O
Antenna B-component
and O
sensor B-module
location O
layout O
Figure O
4 O
– O
Antenna B-component
and O
sensor B-module
locations O
Qualification O
of O
the O
equipment O
The O
general O
approach O
for O
the O
qualification O
of O
the O
equipment O
is O
described O
in O
the O
following O
table O
. O

Three O
type O
of O
equipment O
are O
identified O
: O
Approved O
equipment O
: O
identifies O
an O
equipment O
whose O
design O
meets O
an O
ETSO O
standard O
; O
Standardized O
equipment O
: O
identifies O
an O
equipment O
whose O
design O
meets O
an O
industry O
standard O
; O
Accepted O
equipment O
: O
identifies O
an O
equipment O
which O
meets O
a O
certain O
specification O
defined O
by O
the O
equipment O
manufacturer O
; O
Note O
: O
the O
above O
definitions O
have O
a O
meaning O
limited O
to O
this O
document O
and O
should O
not O
be O
read O
in O
the O
context O
of O
other O
similar O
definitions O
given O
in O
EU O
regulations O
( O
e O
. O

g O
. O

: O
approved O
equipment O
has O
a O
different O
meaning O
here O
than O
the O
meaning O
in O
EU O
748 O
/ O
2012 O
- O
part O
21 O
) O
. O

Table O
3 O
– O
Qualifications O
level O
Note O
: O
the O
aim O
of O
this O
section O
is O
to O
define O
the O
criteria O
for O
acceptance O
. O

In O
the O
scope O
of O
this O
template O
, O

for O
most O
of O
the O
equipment O
in O
chapter O
9 O
, O

the O
information O
related O
to O
the O
qualification O
of O
each O
equipment O
just O
refer O
to O
Table O
3 O
without O
adding O
further O
information O
( O
only O
in O
some O
cases O
some O
additional O
info O
are O
provided O
) O
. O

When O
the O
applicant O
produces O
this O
document O
, O

she O
/ O
he O
will O
have O
to O
provide O
more O
details O
, O

explaining O
how O
the O
criteria O
above O
are O
used O
in O
each O
single O
case O
. O

This O
is O
mainly O
needed O
in O
case O
of O
“ O
accepted O
” O
equipment O
. O

Assessment O
of O
failures O
of O
the O
PFD O
This O
Safety O
Assessment O
( O
SA O
) O
is O
based O
on O
SAE O
Aerospace O
Recommended O
Practice O
( O
ARP O
) O
No O
. O

ARP4761 O
“ O
Guidelines O
And O
Methods O
For O
Conducting O
The O
Safety O
Assessment O
Process O
On O
Civil O
Airborne O
Systems O
And O
Equipment O
” O
issued O
on O
12 O
- O
1996 O
( O
as O
amended O
) O
. O

It O
follows O
the O
method O
of O
Failure O
Mode O
and O
Effect O
Analysis O
( O
FMEA O
) O
. O

Table O
4 O
– O
Safety O
assessment O
Note O
: O
this O
chapter O
is O
aimed O
to O
provide O
the O
assessment O
of O
the O
failures O
as O
required O
by O
the O
Certification O
memo O
on O
non O
ETSO O
EFIS O
. O

In O
this O
case O
it O
is O
limited O
to O
the O
PFD O
since O
it O
is O
the O
only O
( O
non O
ETSO O
) O
source O
of O
safety O
information O
. O

In O
general O
, O

such O
analysis O
can O
be O
used O
to O
support O
the O
suitability O
of O
a O
certain O
equipment O
and O
the O
acceptability O
of O
the O
corresponding O
qualification O
level O
. O

Instrument O
panel O
Hazard O
Assessment O
The O
aim O
of O
this O
chapter O
is O
to O
assess O
the O
potential O
hazards O
that O
might O
be O
placed O
to O
the O
occupants O
by O
the O
equipment O
in O
the O
instrument O
panel O
. O

This O
is O
aimed O
to O
support O
compliance O
to O
ASTM O
F2245 O
- O
12d O
chapters O
8 O
. O

6 O
. O

Table O
5 O
– O
Safety O
assessment O
Compliance O
statements O
Compliance O
statements O
are O
shown O
below O
. O

Appendix O
I O
See O
Certification O
Memo O
of O
“ O
Acceptance O
of O
non O
ETSO O
’ O
d O
Electronic O
Flight O
Instrument O
Systems O
in O
Small O
Airplanes B-asset
( O
ELA1 O
) O
” O

{ O
" O
extra O
" O
: O
{ O
} O
, O

" O
name O
" O
: O
" O
design O
_ O
12028 O
_ O
e437c0c4835841a99d48808aa8734bc7 O
_ O
s O
" O
, O

" O
parameters O
" O
: O
[ O
{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
413 O
. O

5996130739701 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
BODY B-parameter
_ I-parameter
ROT I-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
45 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
BOTTOM O
_ O
CONNECTOR O
_ O
ROTATION B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Z O
_ O
ANGLE B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoCaseRotation B-parameter
" O
, O

" O
value O
" O
: O
" O
315 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Rotation B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoMass B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
property O
" O
: O
" O
WEIGHT B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
ControlChannelAuto B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
AUTOPILOT O
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
AUTOPILOT O
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
44 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
BATTERY B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
BATTERY B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
6 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT O
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
5 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT O
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
80 O
. O

65 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
5 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
FLOOR B-module
_ O
HEIGHT B-parameter
" O
, O

" O
value O
" O
: O
" O
8 O
. O

75 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ O
HEIGHT B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
floor B-module
_ O
height B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
7 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
40 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
7 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
HORZ B-parameter
_ I-parameter
DIAMETER I-parameter
" O
, O

" O
value O
" O
: O
" O
332 O
. O

4 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
HORZ B-parameter
_ I-parameter
DIAMETER I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
horz O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
LENGTH B-parameter
" O
, O

" O
value O
" O
: O
" O
106 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FUSE O
_ O
CYL O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
3 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
100 O
. O

8 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
3 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
76 O
. O

65 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
, O

" O
value O
" O
: O
" O
52 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
vert O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
6 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
98 O
. O

3 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
6 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
1 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
2 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
3 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
4 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
] O
} O
] O
, O

" O
components O
" O
: O
[ O
{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube B-component
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube B-component
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube B-component
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube B-component
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube B-component
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube B-component
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube B-component
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube B-component
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
BatteryController B-control
_ O
6695 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
BatteryController B-control
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
BatteryController B-control
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Battery B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
TurnigyGraphene2200mAh3S75C O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Cargo B-system
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
type O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
CargoCase B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
UAV O
_ O
Fuselage B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
capsule O
_ O
fuselage B-system
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
MainHub O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Para O
_ O
Hub O
_ O
4 O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394od O
_ O
para O
_ O
hub O
_ O
4 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
AT3530KV580 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
AT3530KV580 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
AT3530KV580 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
AT3530KV580 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Orient O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Orient O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Orient O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
18x8 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
18x8 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
18x8 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
18x8 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
RpmTemp B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Autopilot B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Current B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Voltage B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
GPS B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Variometer B-parameter
" O
} O
] O
, O

" O
connections O
" O
: O
[ O
{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
6695 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
6695 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
6695 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
6695 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
6695 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector3 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector1 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Case2HubConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Orient B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
ORIENTCONN B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Orient B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
6695 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
6695 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
6695 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
6695 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
6695 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3327 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-component
_ O
3327 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector3 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector1 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Case2HubConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
10403 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop O
_ O
Connector O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Orient B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Orient B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
ORIENTCONN B-component
" O
} O
] O
} O

WING B-parameter
LOAD I-parameter
CALCULATION O
( O
Example O
document O
for O
LSA O
applicants O
– O
v1 O
of O
08 O
. O

03 O
. O

16 O
) O
Introduction O
This O
document O
calculates O
the O
flight B-parameter
loads I-parameter
on O
the O
wings B-system
of O
the O
ABCD O
aircraft B-asset
. O

The O
requirements O
are O
referenced O
in O
the O
compliance O
checklist O
of O
the O
certification O
programme O
ABCD O
- O
CP O
- O
00 O
. O

Within O
this O
document O
the O
loads O
on O
the O
wings B-system
are O
determined O
throughout O
the O
whole O
flight B-parameter
envelope I-parameter
and O
for O
the O
design B-parameter
weights I-parameter
as O
determined O
in O
under O
all O
loading B-parameter
conditions O
. O

The O
simplified O
criteria O
of O
requirement O
X O
. O

1 O
have O
not O
been O
used O
for O
these O
calculations O
. O

The O
Loads B-parameter
are O
calculated O
using O
literature O
methods O
taken O
from O
the O
documents O
referenced O
in O
chapter O
1 O
. O

The O
following O
assumptions O
are O
made O
: O
Applicable O
to O
LSA O
only O
; O
no O
compressibility O
effects O
; O
conventional O
configuration O
( O
e O
. O

g O
. O

no O
tandem O
aircraft B-asset
, O

bi O
- O
plane O
or O
canard O
) O
; O
no O
pitching O
moment O
of O
the O
horizontal B-system
tail I-system
( O
symmetrical O
profile O
) O
; O
no O
winglets O
, O

no O
wing B-component
tip I-component
tanks I-component
; O
no O
sweep B-parameter
, O

straight O
leading O
edge O
, O

no O
twist O
, O

constant O
profile B-parameter
, O

no O
dihedral B-parameter
; O
effect O
of O
the O
wing B-parameter
deformation I-parameter
on O
the O
loads B-parameter
not O
considered O
; O
no O
spoilers B-component
or O
airbrakes B-component
; O
landing B-system
gear I-system
attached O
to O
fuselage B-system
; O
no O
wing B-component
struts I-component
( O
cantilever B-system
wing I-system
) O
; O
References O
List O
of O
Abbreviations O
CG O
centre B-parameter
of I-parameter
gravity I-parameter
LE O
leading B-location
edge I-location
ISA O
international O
standard O
atmosphere O
by O
International O
Organisation O
for O
Standardisation O
KEAS O
knots B-parameter
equivalent I-parameter
airspeed I-parameter
MAC O
mean I-parameter
aerodynamic I-parameter
chord I-parameter
MTOW O
maximum B-parameter
take I-parameter
- I-parameter
off I-parameter
weight I-parameter
SI O
international O
system O
of O
units O
angle B-parameter
of I-parameter
attack I-parameter
of O
the O
wing B-system
[ O
deg O
] O
local B-parameter
angle I-parameter
of I-parameter
attack I-parameter
of O
the O
station O
i O
[ O
deg O
] O
wing B-parameter
zero I-parameter
lift I-parameter
angle I-parameter
of I-parameter
attack I-parameter
[ O
deg O
] O
profile B-parameter
zero I-parameter
lift I-parameter
angle I-parameter
of I-parameter
attack I-parameter
[ O
deg O
] O
a O
lift O
curve O
slope O
[ O
1 O
/ O
deg O
] O
AR O
wing B-parameter
aspect I-parameter
ratio I-parameter
calculated O
by O
[ O
] O
b O
wing B-parameter
span I-parameter
[ O
m O
] O
average B-parameter
wing I-parameter
span I-parameter
at O
station O
i O
( O
mid O
span O
position O
of O
station O
) O
[ O
m O
] O
wing B-parameter
span I-parameter
position I-parameter
of O
MAC O
[ O
m O
] O
average B-parameter
fuselage I-parameter
width I-parameter
at O
wing O
section O
[ O
m O
] O
maximum B-parameter
fuselage I-parameter
width I-parameter
( O
equals O
) O
[ O
m O
] O
local I-parameter
angle I-parameter
between O
resulting O
force O
and O
normal O
force O
at O
station O
[ O
deg O
] O
average B-parameter
chord I-parameter
at O
station O
i O
[ O
m O
] O
mean B-parameter
aerodynamic I-parameter
chord I-parameter
[ O
m O
] O
chord B-parameter
at I-parameter
wing I-parameter
root I-parameter
[ O
m O
] O
chord B-parameter
at I-parameter
wing I-parameter
tip I-parameter
[ O
m O
] O
shear O
axis O
relative O
position O
as O
a O
fraction O
of O
local B-component
wing I-component
chord I-component
[ O
] O
drag B-parameter
coefficient I-parameter
[ O
] O
lift I-parameter
coefficient I-parameter
[ O
] O
fuselage B-parameter
pitching I-parameter
moment I-parameter
coefficient I-parameter
[ O
] O
zero B-parameter
lift I-parameter
profile I-parameter
pitching I-parameter
moment I-parameter
coefficient I-parameter
[ O
] O
zero B-parameter
lift I-parameter
wing I-parameter
pitching I-parameter
moment I-parameter
coefficient I-parameter
[ O
] O
D O
drag B-parameter
force I-parameter
on O
the O
wings B-system
[ O
N B-measurement
] O
d O
span B-parameter
wise I-parameter
drag I-parameter
line I-parameter
loading I-parameter
[ O
] O
wing B-parameter
sweep I-parameter
of O
the O
quarter O
chord O
line O
[ O
deg O
] O
g O
gravity B-parameter
acceleration I-parameter
[ O
m B-measurement
/ I-measurement
s2 I-measurement
] O
fuselage I-parameter
moment I-parameter
factor I-parameter
[ O
] O
total B-parameter
wing I-parameter
lift I-parameter
force I-parameter
( O
on O
both O
wings O
) O
[ O
N B-measurement
] O
local B-parameter
lift I-parameter
at O
station O
i O
[ O
N B-measurement
] O
lift B-parameter
line I-parameter
loading I-parameter
on O
the O
wing B-system
[ O
N B-measurement
/ I-measurement
m I-measurement
] O
total B-parameter
horizontal B-system
tail I-system
lift I-parameter
force I-parameter
[ O
N B-measurement
] O
total B-parameter
fuselage B-system
length I-parameter
[ O
m B-measurement
] O
fuselage B-parameter
length I-parameter
in O
front O
of O
wing O
quarter O
mean O
aerodynamic O
chord O
point O
[ O
m B-measurement
] O
taper B-parameter
ratio I-parameter
( O
equals O
) O
[ O
] O
wing B-parameter
pitching I-parameter
moment I-parameter
with O
lift O
acting O
on O
its O
aerodynamic B-parameter
centre I-parameter
[ O
N B-measurement
] O
moments B-parameter
around O
y O
axis O
[ O
Nm B-measurement
] O
normal B-parameter
force I-parameter
[ O
N B-measurement
] O
n O
load I-parameter
factor I-parameter
[ O
] O
num O
total O
number O
of O
stations O
of O
a O
single O
wing B-system
; O
num O
= O
10 O
[ O
] O
density B-parameter
of I-parameter
ambient I-parameter
air I-parameter
at O
a O
specific O
altitude B-parameter
[ O
] O
running B-parameter
horizontal I-parameter
shear I-parameter
force I-parameter
at O
station O
i O
( O
direction O
parallel O
to O
drag O
force O
) O
[ O
N B-measurement
] O
incremental B-parameter
horizontal I-parameter
shear I-parameter
force I-parameter
at O
station O
i O
( O
direction O
parallel O
to O
drag O
force O
) O
[ O
N B-measurement
] O
running I-parameter
vertical I-parameter
shear I-parameter
force I-parameter
at O
station O
I O
( O
direction O
parallel O
to O
lift O
force O
) O
[ O
N B-measurement
] O
incremental I-parameter
vertical I-parameter
shear I-parameter
force I-parameter
at O
station O
i O
( O
direction O
parallel O
to O
lift O
force O
) O
[ O
N B-measurement
] O
local B-parameter
resulting I-parameter
force I-parameter
at O
station O
i O
[ O
N B-measurement
] O
S O
wing B-parameter
area I-parameter
( O
not O
including O
wing B-system
carry O
- O
through O
) O
[ O
] O
local B-parameter
tangential I-parameter
force I-parameter
at O
station O
i O
[ O
N B-measurement
] O
total O
torsion O
around O
elastic O
axis O
of O
the O
wing O
( O
at O
wing O
root O
) O
[ O
mN B-measurement
] O
local O
torsion O
around O
elastic O
axis O
of O
the O
wing O
at O
station O
i O
[ O
mN B-measurement
] O
incremental O
torsion O
around O
elastic O
axis O
of O
the O
wing O
at O
station O
i O
[ O
mN B-measurement
] O
dynamic O
viscosity O
( O
for O
Reynolds O
number O
) O
[ O
] O
v O
airspeed B-parameter
[ O
m O
/ O
s O
] O
W O
total I-parameter
aircraft I-parameter
weight I-parameter
[ O
kg O
] O
local B-parameter
weight I-parameter
of I-parameter
the I-parameter
wing I-parameter
at O
station O
i O
( O
with O
no O
fuel O
or O
payload O
) O
[ O
kg B-measurement
/ I-measurement
m2 I-measurement
] O
total I-parameter
weight I-parameter
of I-parameter
a I-parameter
single I-parameter
wing I-parameter
( O
with O
no O
fuel O
or O
payload O
) O
[ O
kg B-measurement
] O
local B-parameter
weight I-parameter
of I-parameter
the I-parameter
wing I-parameter
at O
station O
i O
( O
with O
no O
fuel O
or O
payload O
) O
[ O
kg B-measurement
/ I-measurement
m2 I-measurement
] O
x O
longitudinal O
axis O
of O
the O
aircraft I-asset
[ O
m B-measurement
] O
distance O
to O
HT O
quarter O
chord O
line O
from O
wing O
LE O
( O
at O
mean O
aerodynamic O
chord O
) O
[ O
m B-measurement
] O
distance B-parameter
to O
aircraft O
centre O
of O
gravity O
from O
wing B-system
LE O
( O
at O
mean O
aerodynamic O
chord O
) O
[ O
m B-measurement
] O
distance B-parameter
to O
fuel O
centre O
of O
gravity O
from O
wing B-system
LE O
( O
at O
mean O
aerodynamic O
chord O
) O
[ O
m B-measurement
] O
distance B-parameter
to O
wing O
centre O
of O
gravity O
from O
wing B-system
LE O
( O
at O
mean O
aerodynamic O
chord O
) O
[ O
m B-measurement
] O
local O
distance O
to O
wing B-system
centre O
of O
gravity O
from O
wing B-system
LE O
at O
station O
i O
[ O
m B-measurement
] O
aerodynamic O
centre O
shift O
due O
to O
fuselage O
pitching O
moment O
[ O
m B-measurement
] O
aerodynamic O
centre O
of O
the O
wing B-system
with O
respect O
to O
wing O
LE O
( O
at O
mean O
aerodynamic O
chord O
) O
[ O
m B-measurement
] O
aerodynamic O
centre O
of O
the O
wing O
- O
fuselage O
combination O
with O
respect O
to O
wing B-system
LE O
( O
at O
mean O
aerodynamic O
chord O
) O
[ O
m B-measurement
] O
local O
aerodynamic O
centre O
of O
the O
wing B-system
with O
respect O
to O
wing B-system
LE O
at O
station O
i O
[ O
m B-measurement
] O
centre O
of O
pressure O
of O
the O
wing O
from O
wing O
LE O
( O
at O
mean O
aerodynamic O
chord O
) O
[ O
m B-measurement
] O
local O
centre O
of O
pressure O
of O
the O
wing O
from O
wing O
LE O
at O
station O
i O
[ O
m B-measurement
] O
centre O
of O
pressure O
of O
the O
wing O
fuselage O
combination O
from O
wing O
LE O
( O
at O
mean O
aerodynamic O
chord O
) O
[ O
m B-measurement
] O
shear O
axis O
of O
the O
wing B-system
from O
wing O
LE O
( O
at O
mean O
aerodynamic O
chord O
) O
[ O
m B-measurement
] O
y O
lateral O
axis O
of O
the O
aircraft O
( O
span O
wise O
direction O
) O
[ O
m B-measurement
] O
average O
wing O
span O
position O
at O
station O
i O
[ O
m B-measurement
] O
spanwise O
width O
of O
station O
i O
[ O
m B-measurement
] O
z O
vertical O
axis O
of O
the O
aircraft O
[ O
m B-measurement
] O
Throughout O
this O
document O
SI O
- O
units O
are O
used O
with O
speeds O
expected O
as O
m B-measurement
/ I-measurement
s I-measurement
and O
angles O
in O
degrees O
if O
not O
stated O
otherwise O
. O

Requirements O
This O
document O
covers O
the O
following O
certification O
specifications O
requirements O
: O
Table O
1 O
– O
Requirements O
Input O
data O
The O
values O
shown O
below O
are O
derived O
from O
design O
data O
or O
other O
compliance O
documents O
for O
this O
particular O
aeroplane B-asset
. O

Load O
Calculation O
The O
following O
steps O
have O
been O
followed O
: O
Load B-parameter
cases O
: O
First O
, O

the O
load O
cases O
have O
been O
identified O
in O
, O

in O
terms O
of O
weight B-parameter
, O

centre O
of O
gravity O
, O

speed B-parameter
, O

load B-parameter
factor I-parameter
, O

flap B-parameter
/ I-parameter
aileron I-parameter
position I-parameter
, O

Altitude B-parameter
. O

External B-parameter
Loads I-parameter
on I-parameter
the I-parameter
wing I-parameter
: O
for O
all O
load O
cases O
, O

the O
loads O
on O
the O
wing B-system
are O
calculated O
; O
Internal B-parameter
Loads I-parameter
in I-parameter
the I-parameter
wing I-parameter
: O
for O
the O
same O
load B-parameter
cases O
the O
internal O
loads O
in O
the O
wing B-system
( O
shear B-parameter
, O

bending B-parameter
moment I-parameter
, O

torsion B-parameter
) O
are O
calculated O
considering O
also O
the O
effect O
of O
the O
inertia B-parameter
of O
the O
wing B-system
; O
Load O
cases O
Table O
3 O
comprises O
all O
load O
cases O
corresponding O
to O
the O
points O
of O
the O
flight B-parameter
envelope I-parameter
and O
design B-parameter
weights I-parameter
and O
centres B-parameter
of I-parameter
gravity I-parameter
. O

Important O
: O
Loads O
corresponding O
to O
flap O
deflected O
are O
considered O
not O
critical O
for O
the O
wing B-system
and O
will O
not O
be O
calculated O
in O
this O
document O
( O
flap B-system
loads I-parameter
will O
be O
calculated O
instead O
for O
the O
flap B-system
verification I-parameter
) O
. O

Loads O
corresponding O
to O
landing O
conditions O
are O
considered O
not O
critical O
for O
the O
wing B-system
( O
since O
the O
landing B-system
gear I-system
is O
attached O
to O
the O
fuselage B-system
and O
no O
tip B-component
tanks I-component
or O
other O
large O
masses O
under O
the O
wing B-system
) O
and O
will O
not O
be O
calculated O
in O
this O
document O
. O

For O
the O
gust B-parameter
load I-parameter
calculations O
the O
wing B-system
and O
horizontal B-system
tail I-system
are O
treated O
together O
according O
to O
X3 O
. O

1 O
in O
ref O
. O

. O

The O
resulting O
gust B-parameter
load I-parameter
accelerations O
are O
therefore O
calculated O
using O
the O
slope O
of O
the O
lift O
curve O
of O
the O
aeroplane B-asset
( O
see O
also O
) O
and O
treated O
as O
balanced O
flight O
conditions O
within O
this O
document O
. O

Note O
: O
These O
assumptions O
have O
been O
considered O
realistic O
for O
this O
aeroplane B-asset
but O
they O
are O
not O
of O
generic O
validity O
. O

It O
is O
the O
responsibility O
of O
the O
applicant O
to O
define O
the O
set O
of O
assumptions O
which O
can O
be O
acceptable O
for O
the O
particular O
aeroplane B-asset
. O

Altitude B-parameter
: O
The O
maximum B-parameter
permissible I-parameter
operational I-parameter
altitude I-parameter
is O
13000ft O
. O

Despite O
the O
CS O
- O
LSA O
requirements O
do O
not O
require O
to O
accounts O
for O
the O
effects O
of O
altitude B-parameter
, O

such O
effects O
have O
been O
considered O
up O
to O
10000 O
ft B-measurement
. O

in O
fact O
the O
gust B-parameter
load I-parameter
factor O
have O
been O
calculated O
at O
such O
altitude B-parameter
. O

This O
is O
considered O
acceptable O
since O
it O
covers O
the O
operational O
range O
within O
which O
the O
aeroplane B-asset
will O
fly O
most O
of O
the O
time O
. O

( O
Note O
: O
the O
CS O
- O
LSA O
requirement O
does O
not O
require O
to O
account O
for O
the O
effects O
of O
altitude B-parameter
. O

Calculating O
the O
loads B-parameter
at O
sea O
level O
would O
be O
acceptable O
. O

In O
this O
case O
, O

the O
choice O
to O
consider O
such O
effect O
up O
to O
10000 O
ft B-measurement
is O
a O
decision O
of O
a O
designer O
, O

which O
would O
be O
accepted O
by O
the O
team O
. O

) O
Figure O
1 O
– O
Reference O
flight B-parameter
envelope I-parameter
( O
WMTOW O
, O

FL O
100 O
) O
Table O
2 O
– O
Design B-parameter
weights I-parameter
( O
explained O
in O
ref O
. O

) O
Table O
3 O
– O
Load B-parameter
cases O
Note O
: O
For O
this O
revision O
of O
this O
example O
document O
, O

asymmetric O
load O
cases O
have O
not O
been O
calculated O
. O

Loads B-parameter
on O
the O
aeroplane B-asset
Reference O
axes O
and O
sign O
convention O
Figure O
2 O
– O
Aeroplane B-asset
reference O
axes O
The O
origin O
is O
located O
at O
the O
airplane B-asset
axis O
of O
symmetry O
( O
x O
axis O
) O
with O
the O
y O
axis O
passing O
through O
the O
leading B-location
edge I-location
of O
the O
mean B-parameter
aerodynamic I-parameter
chord I-parameter
section I-parameter
of O
the O
wing B-system
. O

Symmetrical O
flight O
conditions O
The O
loads B-parameter
on O
the O
wing B-module
structure I-module
arising O
from O
symmetrical O
flight O
manoeuvres O
according O
to O
requirements O
5 O
. O

2 O
. O

2 O
and O
5 O
. O

2 O
. O

3 O
are O
determined O
within O
this O
chapter O
. O

The O
following O
abbreviations O
are O
used O
within O
this O
chapter O
( O
all O
measurements O
with O
respect O
to O
wing B-parameter
leading I-parameter
edge I-parameter
at O
wing B-parameter
mean I-parameter
aerodynamic I-parameter
chord I-parameter
, O

forces O
acting O
according O
to O
arrows O
are O
positive O
) O
x O
longitudinal B-parameter
axis I-parameter
of I-parameter
the I-parameter
aircraft I-parameter
z O
vertical B-parameter
axis I-parameter
of I-parameter
the I-parameter
aircraft I-parameter
CG O
aircraft B-parameter
centre I-parameter
of I-parameter
gravity I-parameter
HT O
horizontal B-system
tail I-system
L O
lift B-parameter
force I-parameter
on O
the O
wings B-system
horizontal B-parameter
tail I-parameter
balancing I-parameter
force I-parameter
( O
HT B-parameter
lift I-parameter
force I-parameter
) O
zero B-parameter
lift I-parameter
wing I-parameter
pitching I-parameter
moment I-parameter
coefficient I-parameter
( O
lift O
force O
assumed O
to O
act O
on O
) O
total B-parameter
pitching I-parameter
moment I-parameter
( O
must O
be O
zero O
for O
equilibrium O
) O
n O
W O
aircraft B-parameter
total I-parameter
weight I-parameter
force I-parameter
( O
= O
m B-measurement
* I-measurement
n I-measurement
* I-measurement
g I-measurement
) O
distance B-parameter
to O
HT O
quarter O
chord O
line O
( O
of O
HT O
MAC O
as O
quarter O
chord O
line O
) O
distance B-parameter
to O
aircraft B-asset
centre O
of O
gravity O
distance B-parameter
to O
wing B-component
fuselage I-component
combination I-component
centre I-component
of O
pressure B-parameter
( O
lift B-parameter
force I-parameter
acting O
on O
not O
generating O
any O
pitching O
moment O
) O
distance B-parameter
to O
wing B-component
fuselage I-component
combination I-component
aerodynamic I-component
centre I-component
( O
lift B-parameter
force I-parameter
acting O
on O
generating O
constant O
pitching O
moment O
) O
The O
external B-parameter
forces I-parameter
and O
moments B-parameter
acting O
on O
the O
aeroplane B-asset
in O
a O
balanced O
flight O
condition O
have O
been O
determined O
. O

The O
simplified O
scheme O
in O
Figure O
3 O
is O
considered O
. O

The O
aeroplane B-asset
is O
reduced O
to O
the O
wing B-system
and O
the O
Horizontal B-system
tail I-system
. O

Figure O
3 O
– O
Aeroplane B-asset
simplified O
scheme O
The O
following O
forces B-parameter
are O
considered O
and O
placed O
in O
equilibrium O
: O
Lift B-parameter
on O
the O
wing B-system
; O
Horizontal B-system
tail I-system
balancing B-parameter
load I-parameter
according O
to O
requirement O
5 O
. O

2 O
. O

2 O
. O

1 O
; O
Weight B-parameter
of O
the O
aeroplane B-asset
; O
For O
the O
calculation O
of O
the O
equilibrium O
, O

the O
z B-parameter
- I-parameter
axis I-parameter
of O
the O
aeroplane B-asset
is O
assumed O
aligned O
with O
the O
direction O
of O
the O
gravity B-parameter
. O

In O
a O
second O
stage O
( O
section O
6 O
. O

4 O
) O
, O

once O
the O
forces B-parameter
are O
calculated O
, O

the O
corresponding O
angle O
of O
attack O
will O
be O
considered O
for O
the O
calculation O
of O
the O
correct O
direction O
of O
the O
forces B-parameter
on O
the O
wing B-system
; O
Influence O
of O
thrust B-parameter
and O
drag B-parameter
( O
of O
the O
total O
airplane B-asset
) O
are O
considered O
negligible O
at O
this O
stage O
of O
calculation O
of O
the O
vertical B-parameter
forces I-parameter
. O

The O
effect O
of O
the O
drag B-parameter
will O
be O
considered O
in O
a O
second O
stage O
on O
the O
wing B-system
only O
; O
The O
wing B-parameter
lift I-parameter
is O
assumed O
to O
act O
on O
the O
aerodynamic B-parameter
centre I-parameter
of O
the O
wing B-system
as O
a O
starting O
point O
. O

The O
contribution O
of O
the O
fuselage B-system
is O
accounted O
for O
as O
a O
shift O
of O
the O
point O
of O
aerodynamic B-parameter
centre I-parameter
. O

This O
is O
better O
explained O
in O
section O
6 O
. O

1 O
. O

5 O
. O

The O
HT B-parameter
lift I-parameter
is O
applied O
at O
25 O
% O
of O
the O
chord O
; O
Effects O
of O
structural O
flexure O
are O
considered O
negligible O
; O
Angular B-parameter
accelerations I-parameter
are O
disregarded O
until O
the O
aeroplane B-asset
has O
attained O
the O
prescribed O
load B-parameter
factor I-parameter
( O
according O
to O
requirement O
5 O
. O

2 O
. O

2 O
. O

3 O
) O
; O
Note O
: O
The O
assumptions O
above O
provide O
a O
clear O
simplification O
to O
the O
calculations O
. O

The O
fact O
that O
they O
are O
used O
here O
does O
not O
mean O
that O
they O
can O
always O
be O
used O
. O

It O
is O
the O
responsibility O
of O
the O
designer O
to O
make O
the O
appropriate O
assumptions O
and O
to O
agree O
them O
with O
the O
Agency O
. O

Based O
on O
the O
above O
assumptions O
the O
following O
equilibrium O
equations O
are O
set O
. O

The O
basis O
system O
of O
equations O
include O
4 O
equations O
with O
the O
following O
unknowns O
: O
L O
: O
wing B-parameter
Lift I-parameter
( O
including O
fuselage B-system
) O
CL O
: O
wing B-parameter
lift I-parameter
coefficient I-parameter
LHT O
: O
HT B-parameter
lift I-parameter
XAC O
f O
+ O
w O
: O
aerodynamic B-parameter
centre I-parameter
w O
+ O
f O
( O
wing B-system
+ O
fuselage B-system
; O
see O
sec O
. O

6 O
. O

1 O
. O

3 O
and O
6 O
. O

1 O
. O

5 O
) O
Equilibrium O
of O
moments B-parameter
( O
f O
. O

6 O
. O

1 O
. O

2 O
. O

1 O
) O
Equilibrium O
of O
forces B-parameter
( O
f O
. O

6 O
. O

1 O
. O

2 O
. O

2 O
) O
wing B-system
pitching B-parameter
moment I-parameter
( O
f O
. O

6 O
. O

1 O
. O

2 O
. O

3 O
) O
( O
for O
wing B-system
) O
wing B-parameter
lift I-parameter
coefficient I-parameter
( O
f O
. O

6 O
. O

1 O
. O

2 O
. O

4 O
) O
Aerodynamic B-parameter
centre I-parameter
The O
aerodynamic B-parameter
centre I-parameter
is O
a O
characteristic O
of O
the O
wing B-system
and O
it O
is O
defined O
as O
the O
point O
about O
which O
the O
pitch B-parameter
moment I-parameter
does O
not O
change O
with O
changes O
of O
the O
angle B-parameter
of I-parameter
attack I-parameter
throughout O
the O
linear O
range O
of O
the O
lift O
curve O
. O

According O
to O
the O
aerodynamic B-parameter
centre I-parameter
can O
be O
estimated O
by O
adding O
a O
correction B-parameter
factor I-parameter
( O
shift O
) O
to O
the O
quarter O
chord O
point O
of O
the O
mean B-parameter
aerodynamic I-parameter
chord I-parameter
. O

The O
correction O
factor O
is O
a O
function O
of O
the O
maximum O
thickness O
of O
the O
profile O
which O
in O
this O
wing B-system
is O
16 O
% O
of O
the O
chord O
. O

For O
a O
tapered O
wing B-system
, O

the O
mean B-parameter
aerodynamic I-parameter
chord I-parameter
corresponds O
to O
the O
mean O
chord O
and O
it O
is O
( O
see O
) O
. O

For O
this O
wing O
the O
correction O
factor O
is O
0 O
. O

012 O
( O
from O
Fig O
. O

2 O
at O
16 O
% O
thickness O
) O
, O

so O
the O
mean O
aerodynamic O
centre O
of O
the O
wing B-system
without O
fuselage B-system
is O
( O
f O
. O

6 O
. O

1 O
. O

3 O
. O

1 O
) O
Pitching B-parameter
moment I-parameter
of O
the O
wing B-system
The O
pitching B-parameter
moment I-parameter
of O
the O
profile O
from O
two O
dimensional O
wind O
tunnel O
test O
data O
does O
not O
represent O
the O
moment O
of O
a O
three O
dimensional O
with O
the O
profile O
. O

The O
pitching B-parameter
moment I-parameter
of O
the O
whole O
wing B-system
is O
calculated O
according O
to O
DATCOM O
method O
1 O
( O
formula O
4 O
. O

1 O
. O

4 O
. O

1 O
. O

a O
) O
. O

( O
formula O
4 O
. O

1 O
. O

4 O
. O

1 O
. O

a O
) O
( O
f O
. O

6 O
. O

1 O
. O

4 O
. O

1 O
) O
With O
quarter O
chord O
sweep B-parameter
angle I-parameter
of O
the O
wing B-system
. O

Influence O
of O
the O
fuselage B-system
The O
fuselage B-system
is O
assumed O
to O
provide O
negligible O
lift B-parameter
. O

On O
the O
other O
hand O
, O

its O
influence O
on O
the O
aeroplane B-asset
equilibrium O
is O
accounted O
for O
as O
a O
contribution O
to O
the O
pitching B-parameter
moment I-parameter
. O

In O
particular O
the O
following O
formula O
( O
taken O
from O
ref O
) O
provides O
the O
shift O
of O
the O
aerodynamic B-parameter
centre I-parameter
of O
the O
wing B-system
due O
to O
fuselage B-system
pitching B-parameter
moment I-parameter
. O

( O
f O
. O

6 O
. O

1 O
. O

5 O
. O

1 O
) O
With O
and O
as O
input O
to O
the O
diagram O
in O
yielding O
and O
a O
correction O
factor O
of O
1 O
. O

05 O
due O
to O
low O
- O
wing O
configuration O
. O

The O
shift O
of O
aerodynamic B-parameter
centre I-parameter
, O

due O
to O
the O
fuselage B-system
, O

is O
calculated O
as O
: O
( O
f O
. O

6 O
. O

1 O
. O

5 O
. O

2 O
) O
Forces B-parameter
and O
moments B-parameter
acting O
on O
the O
wings B-system
In O
previous O
chapter O
the O
Lift B-parameter
and O
the O
lift B-parameter
coefficient O
have O
been O
determined O
. O

Having O
those O
as O
inputs O
, O

the O
drag B-parameter
and O
angle B-parameter
of I-parameter
attack I-parameter
are O
calculated O
. O

Total B-parameter
wing I-parameter
drag I-parameter
coefficient I-parameter
( O
FIG O
. O

X2 O
. O

1 O
of O
) O
( O
f O
. O

6 O
. O

2 O
. O

1 O
) O
Drag B-parameter
force I-parameter
on O
the O
wings B-system
( O
FIG O
. O

X2 O
. O

1 O
of O
) O
( O
f O
. O

6 O
. O

2 O
. O

2 O
) O
The O
angle B-parameter
of I-parameter
attack I-parameter
( O
using O
as O
reference O
instead O
of O
) O
for O
each O
load B-module
case I-module
is O
calculated O
using O
the O
following O
formula O
: O
( O
FIG O
. O

X2 O
. O

1 O
of O
) O
( O
f O
. O

6 O
. O

2 O
. O

3 O
) O
Where O
: O
lift B-parameter
curve I-parameter
slope I-parameter
( O
FIG O
. O

X2 O
. O

1 O
of O
) O
( O
f O
. O

6 O
. O

2 O
. O

4 O
) O
and O
the O
zero B-parameter
- I-parameter
lift I-parameter
angle I-parameter
of O
the O
wing B-system
is O
taken O
as O
. O

This O
value O
is O
the O
zero B-parameter
- I-parameter
lift I-parameter
angle I-parameter
of O
the O
corresponding O
wing B-system
profile O
, O

taken O
from O
ref O
( O
p O
. O

236 O
) O
. O

The O
results O
of O
this O
chapter O
for O
the O
load B-parameter
cases I-parameter
highlighted O
in O
subchapter O
0 O
are O
presented O
within O
the O
table O
below O
. O

Table O
4 O
– O
Loads B-parameter
on O
the O
aeroplane B-asset
Unsymmetrical O
flight O
conditions O
Note O
: O
These O
load B-parameter
cases I-parameter
will O
not O
be O
calculated O
within O
this O
revision O
of O
the O
example O
document O
. O

Wing B-system
load I-parameter
distribution O
After O
having O
calculated O
the O
total B-parameter
load I-parameter
on O
the O
wing B-system
, O

the O
load B-parameter
distribution I-parameter
is O
calculated O
and O
shown O
in O
the O
following O
sections O
. O

Every O
load B-parameter
is O
assumed O
to O
act O
on O
the O
span O
wise O
centre O
of O
each O
station O
. O

Figure O
4 O
– O
Location O
of O
wing B-system
stations O
Wing B-system
lift I-parameter
distribution I-parameter
The O
wing B-system
lift I-parameter
distribution I-parameter
is O
calculated O
here O
. O

The O
lift B-parameter
contribution I-parameter
of O
the O
fuselage B-system
is O
assumed O
to O
be O
zero O
( O
this O
means O
that O
the O
load B-parameter
which O
would O
act O
in O
correspondence O
of O
the O
fuselage B-system
, O

is O
shifted O
externally O
to O
the O
wing B-system
) O
leading O
to O
more O
conservative O
results O
on O
the O
wing B-system
loads B-parameter
since O
they O
provide O
higher O
bending O
. O

Note O
: O
Alternatively O
, O

the O
applicant O
would O
have O
to O
determine O
the O
reduction O
in O
wing B-parameter
lift I-parameter
distribution I-parameter
at O
the O
location O
of O
the O
fuselage B-system
and O
demonstrate O
the O
validity O
of O
the O
approach O
. O

Figure O
5 O
– O
Effect O
of O
the O
fuselage B-system
, O

areas O
A O
( O
total O
lift O
calculated O
at O
the O
end O
of O
this O
chapter O
) O
and O
B O
( O
total O
lift O
according O
to O
Schrenk O
) O
are O
of O
equal O
size O
This O
approach O
is O
based O
on O
the O
approximation O
described O
by O
Schrenk O
and O
requires O
adjustments O
: O
moving O
the O
apex O
of O
the O
elliptical O
distribution O
from O
the O
fuselage B-system
centre O
towards O
the O
wing B-system
root O
increasing O
lift O
of O
wetted O
wing O
sections O
to O
compensate O
for O
zero I-parameter
lift I-parameter
of O
fuselage B-system
wing B-system
section O
The O
formula O
for O
wing B-parameter
lift I-parameter
distribution I-parameter
is O
derived O
from O
Schrenk O
and O
is O
altered O
to O
assume O
zero B-parameter
lift I-parameter
at O
the O
wing B-system
section I-system
within O
the O
fuselage B-system
as O
shown O
below O
. O

The O
formula O
gives O
the O
value O
of O
the O
lift B-parameter
for O
span O
unit O
. O

“ O
i O
” O
identifies O
the O
individual O
station O
. O

Figure O
6 O
– O
lift B-parameter
distribution I-parameter
with O
zero B-parameter
lift I-parameter
at O
fuselage B-system
wing B-system
section O
( O
) O
( O
f O
. O

6 O
. O

4 O
. O

1 O
. O

1 O
) O
Now O
the O
lift B-parameter
of O
the O
wing B-system
section O
within O
the O
fuselage B-system
is O
redistributed O
across O
the O
wetted O
wing B-system
area I-parameter
to O
achieve O
conservative O
results O
. O

The O
lift B-parameter
distribution I-parameter
calculated O
above O
is O
adjusted O
by O
multiplication O
of O
a O
correction O
factor O
derived O
from O
comparison O
between O
total B-parameter
lift I-parameter
of O
the O
whole O
wing B-system
including O
the O
fuselage B-system
section O
and O
the O
wetted O
wing B-system
only O
. O

Figure O
7 O
– O
Fuselage B-system
wing B-system
section O
lift O
redistributed O
across O
wetted O
wing B-system
stations O
or O
( O
f O
. O

6 O
. O

4 O
. O

1 O
. O

2 O
) O
The O
lift B-parameter
distribution I-parameter
corresponding O
to O
the O
formula O
above O
, O

gives O
a O
value O
of O
lift B-parameter
at O
wing B-module
tip I-module
which O
is O
higher O
than O
zero O
and O
therefore O
does O
not O
fully O
reproduce O
the O
actual O
loading O
( O
the O
winglift B-parameter
is O
normally O
zero O
at O
the O
tip B-module
) O
. O

Nevertheless O
this O
assumption O
does O
not O
give O
significant O
changes O
and O
yields O
conservative O
results O
. O

The O
local O
angle B-parameter
of I-parameter
attack I-parameter
for O
the O
station O
I O
, O

as O
a O
result O
of O
this O
corrected O
Schrenk O
distribution O
, O

is O
given O
by O
the O
following O
formula O
: O
( O
from O
f O
. O

6 O
. O

2 O
. O

3 O
and O
f O
. O

6 O
. O

1 O
. O

2 O
. O

4 O
) O
( O
f O
. O

6 O
. O

4 O
. O

1 O
. O

3 O
) O
Note O
: O
FAA O
AC O
23 O
- O
19A O
, O

paragraph O
23 O
. O

301 O
, O

contains O
other O
acceptable O
methods O
. O

Figure O
9 O
– O
Span O
wise O
lift B-parameter
distribution I-parameter
Wing B-parameter
drag I-parameter
distribution O
Since O
the O
effect O
of O
the O
drag B-parameter
is O
negligible O
, O

when O
compared O
to O
the O
effect O
of O
the O
lift B-parameter
, O

the O
span O
wise O
drag B-parameter
distribution O
has O
been O
assumed O
constant O
throughout O
wing B-parameter
span I-parameter
. O

This O
is O
a O
conservative O
assumption O
. O

The O
drag B-parameter
loading O
per O
metre O
of O
span O
: O
( O
f O
. O

6 O
. O

4 O
. O

2 O
. O

1 O
) O
Wing B-system
and O
fuel B-parameter
mass I-parameter
distribution O
The O
local O
masses B-parameter
are O
calculated O
for O
each O
wing B-system
station O
to O
account O
for O
the O
mass B-parameter
of O
the O
structure O
of O
the O
wing B-system
including O
the O
systems O
and O
control O
surfaces O
( O
control B-system
systems I-system
, O

and O
other O
equipment O
) O
. O

It O
is O
assumed O
that O
the O
wing B-system
has O
a O
linear O
distribution O
proportional O
to O
the O
chord O
. O

At O
each O
station O
the O
point O
of O
application O
of O
the O
mass B-parameter
is O
45 O
% O
of O
the O
chord O
. O

Figure O
10 O
– O
Wing B-parameter
mass I-parameter
distribution O
Figure O
11 O
– O
Fuel B-parameter
distribution I-parameter
A O
constant O
fuel B-parameter
distribution I-parameter
( O
at O
a O
point O
of O
application O
of O
20 O
% O
of O
the O
chord O
) O
is O
assumed O
throughout O
the O
fuel B-component
tank I-component
span O
. O

Table O
5 O
– O
Mass B-parameter
distribution O
with O
full O
fuel O
Wing B-system
torsion I-parameter
distribution O
At O
each O
station O
, O

the O
wing B-parameter
lift I-parameter
is O
assumed O
to O
be O
acting O
at O
the O
local O
centre B-parameter
of I-parameter
pressure I-parameter
, O

which O
is O
calculated O
using O
the O
formula O
: O
( O
from O
eq O
. O

9 O
. O

17 O
. O

( O
d O
) O
) O
( O
f O
. O

6 O
. O

4 O
. O

4 O
. O

1 O
) O
Where O
, O

ci O
is O
the O
chord O
at O
each O
station O
, O

cm0 O
_ O
w O
_ O
i O
is O
the O
pitching B-parameter
moment I-parameter
around O
the O
aerodynamic B-parameter
centre I-parameter
of O
the O
wing B-system
section O
( O
it O
is O
- O
0 O
. O

0436 O
across O
the O
wing B-system
from O
chapter O
6 O
. O

1 O
. O

4 O
) O
, O

CL O
_ O
i O
is O
the O
local O
lift B-parameter
coefficient I-parameter
and O
comes O
from O
the O
corrected O
Schrenk O
distribution O
( O
) O
in O
6 O
. O

1 O
. O

5 O
. O

Therefore O
centre B-parameter
of I-parameter
pressure I-parameter
location O
is O
dependent O
on O
the O
local O
angle B-parameter
of I-parameter
attack I-parameter
. O

Each O
station O
’ O
s O
lift B-parameter
force I-parameter
acts O
on O
its O
centre B-parameter
of I-parameter
pressure I-parameter
and O
imposes O
torsion B-parameter
around O
the O
wing B-system
elastic O
axis O
which O
for O
this O
aeroplane B-asset
is O
located O
approximately O
at O
a O
constant O
chord O
percentage O
of O
30 O
% O
( O
see O
design O
data O
- O
the O
main O
spar O
is O
approximately O
at O
25 O
% O
of O
the O
chord O
) O
throughout O
the O
entire O
wing B-system
span O
with O
local O
positions O
as O
local O
shear B-parameter
centres I-parameter
at O
the O
stations O
. O

Note O
: O
the O
location O
of O
the O
elastic B-parameter
axis I-parameter
for O
this O
wing B-system
has O
been O
assumed O
at O
30 O
% O
. O

It O
is O
responsibility O
of O
the O
applicant O
to O
determine O
and O
justify O
the O
location O
of O
the O
elastic B-parameter
axis I-parameter
. O

Incremental O
torsion B-parameter
load I-parameter
on O
structure O
at O
each O
station O
with O
respect O
to O
local O
wing B-system
shear B-parameter
centre I-parameter
including O
contribution O
of O
fuel O
and O
wing B-system
structure O
inertia I-parameter
forces I-parameter
: O
( O
f O
. O

. O

2 O
) O
Torsion B-parameter
at O
each O
station O
i O
( O
with O
respect O
to O
shear B-parameter
centre I-parameter
) O
is O
: O
( O
f O
. O

6 O
. O

4 O
. O

4 O
. O

3 O
) O
Distribution O
of O
internal B-parameter
loads I-parameter
The O
components O
of O
the O
internal B-parameter
loads I-parameter
on O
the O
wing B-system
structure O
are O
calculated O
in O
different O
steps O
for O
each O
station O
. O

The O
flight B-parameter
load I-parameter
factor O
n O
is O
assumed O
to O
act O
in O
parallel O
to O
the O
direction O
of O
the O
lift B-parameter
force I-parameter
instead O
of O
the O
direction O
of O
the O
normal B-parameter
force I-parameter
( O
As O
required O
by O
5 O
. O

2 O
. O

1 O
. O

1 O
of O
ref O
. O

) O
. O

The O
difference O
is O
assumed O
negligible O
. O

The O
incremental O
shear B-parameter
load O
parallel O
to O
lift B-parameter
force I-parameter
vector O
at O
station O
i O
is O
taking O
into O
account O
also O
the O
inertia B-parameter
unloading I-parameter
of O
the O
wing B-system
( O
f O
. O

6 O
. O

4 O
. O

5 O
. O

1 O
) O
Incremental O
shear B-parameter
load O
parallel O
to O
drag B-parameter
force I-parameter
vector O
at O
station O
i O
: O
( O
f O
. O

6 O
. O

4 O
. O

5 O
. O

2 O
) O
With O
representing O
the O
width O
of O
the O
station O
i O
. O

The O
summation O
of O
incremental O
shear B-parameter
loads I-parameter
throughout O
the O
stations O
to O
obtain O
the O
absolute O
shear B-parameter
loads I-parameter
at O
station O
i O
is O
presented O
below O
. O

Shear O
load O
parallel O
to O
lift O
force O
vector O
( O
f O
. O

. O

3 O
) O
Shear O
load O
parallel O
to O
drag O
force O
vector O
( O
f O
. O

6 O
. O

4 O
. O

5 O
. O

4 O
) O
The O
components O
of O
the O
loads B-parameter
along O
the O
normal O
and O
tangential O
directions O
are O
derived O
by O
using O
the O
following O
formulas O
and O
figure O
: O
Figure O
12 O
– O
Forces B-parameter
components O
on O
the O
wing B-system
( O
The O
tangential B-parameter
force I-parameter
is O
oriented O
opposite O
to O
the O
x O
axis O
and O
is O
therefore O
positive O
when O
directed O
towards O
the O
front O
of O
the O
aeroplane B-asset
. O

) O
Resulting B-parameter
force I-parameter
angle I-parameter
( O
f O
. O

6 O
. O

4 O
. O

5 O
. O

5 O
) O
Shear B-parameter
loads I-parameter
along O
the O
directions O
of O
: O
resulting B-parameter
force I-parameter
( O
f O
. O

6 O
. O

4 O
. O

5 O
. O

6 O
) O
tangential B-parameter
force I-parameter
( O
f O
. O

6 O
. O

4 O
. O

5 O
. O

7 O
) O
normal B-parameter
force I-parameter
( O
f O
. O

6 O
. O

4 O
. O

5 O
. O

8 O
) O
With O
the O
local O
angle B-parameter
of I-parameter
attack I-parameter
for O
the O
station O
i O
as O
a O
result O
of O
the O
corrected O
Schrenk O
distribution O
given O
by O
the O
following O
formula O
: O
( O
from O
f O
. O

6 O
. O

4 O
. O

1 O
. O

4 O
) O
Summation O
of O
shear B-parameter
loads I-parameter
to O
obtain O
the O
bending B-parameter
moments I-parameter
at O
each O
station O
and O
using O
the O
increased O
lever O
arm O
( O
instead O
of O
) O
at O
the O
wing B-module
tip I-module
station O
results O
in O
slightly O
more O
conservative O
values O
. O

Bending B-parameter
moment I-parameter
along O
normal O
direction O
( O
f O
. O

6 O
. O

4 O
. O

5 O
. O

9 O
) O
Bending B-parameter
moment I-parameter
along O
tangential O
direction O
( O
f O
. O

6 O
. O

4 O
. O

5 O
. O

10 O
) O
The O
results O
are O
presented O
within O
the O
graphs O
and O
tables O
below O
. O

Compliance O
statements O
Compliance O
statements O
are O
shown O
below O
: O

{ O
" O
extra O
" O
: O
{ O
} O
, O

" O
name O
" O
: O
" O
design O
_ O
10500 O
_ O
9217b3d721c84b45bbee35caefa8d4d3 O
_ O
s O
" O
, O

" O
parameters O
" O
: O
[ O
{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2617 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
307 O
. O

9088076275723 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2617 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
429 O
. O

07552569221474 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
210 O
. O

11323893431475 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2620 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
281 O
. O

86163209688016 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2620 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2620 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2621 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
378 O
. O

5754928834796 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2621 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2621 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2622 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
466 O
. O

41054329636114 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2622 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2622 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2623 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
389 O
. O

28965280986336 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2623 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2623 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2624 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
70 O
. O

2471793093779 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2624 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2624 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2625 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
407 O
. O

3703675241871 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2625 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
BODY B-system
_ O
ROT B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
BOTTOM B-module
_ I-module
CONNECTOR I-module
_ O
ROTATION B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Z B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Bend B-module
_ O
1 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
180 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Bend B-module
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Bend B-module
_ O
2 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
90 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Bend B-module
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Bend B-module
_ O
3 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
270 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Bend B-module
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Bend B-module
_ O
4 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
180 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Bend B-module
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Bend B-module
_ O
5 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
270 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Bend B-module
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Bend B-module
_ O
6 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
90 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Bend B-module
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Bend B-module
_ O
7 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
180 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Bend B-module
_ O
7 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Bend B-module
_ O
8 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
180 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Bend B-module
_ O
8 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
ANGHORZCONN O
" O
, O

" O
value O
" O
: O
" O
90 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoCaseRotation B-parameter
" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Rotation B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoMass B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
property O
" O
: O
" O
WEIGHT B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
ControlChannelAuto B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
9 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
10 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
11 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
12 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
13 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
14 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
AUTOPILOT B-parameter
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
AUTOPILOT B-parameter
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
58 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
BATTERY B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
BATTERY B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
6 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT B-parameter
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
5 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT B-parameter
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
94 O
. O

15 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
5 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
FLOOR B-parameter
_ I-parameter
HEIGHT I-parameter
" O
, O

" O
value O
" O
: O
" O
19 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-parameter
_ I-parameter
HEIGHT I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
floor B-parameter
_ I-parameter
height I-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
7 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
54 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
7 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
HORZ B-parameter
_ I-parameter
DIAMETER I-parameter
" O
, O

" O
value O
" O
: O
" O
372 O
. O

9 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
HORZ B-parameter
_ I-parameter
DIAMETER I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
horz O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
LENGTH B-parameter
" O
, O

" O
value O
" O
: O
" O
189 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FUSE O
_ O
CYL B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
3 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
114 O
. O

3 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
3 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
90 O
. O

15 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
, O

" O
value O
" O
: O
" O
114 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
vert O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
6 O
_ O
DISP O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
111 O
. O

8 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
6 O
_ O
DISP O
_ O
WIDTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FixedRotationArm B-component
_ O
293 O
_ O
1 O
_ O
ROT B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
FixedRotationArm B-component
_ O
293 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
END B-parameter
_ I-parameter
ROT I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FixedRotationArm B-component
_ O
293 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
50 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
FixedRotationArm B-component
_ O
293 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FixedRotationArm B-component
_ O
294 O
_ O
1 O
_ O
ROT B-parameter
" O
, O

" O
value O
" O
: O
" O
180 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
FixedRotationArm B-component
_ O
294 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
END B-parameter
_ I-parameter
ROT I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FixedRotationArm B-component
_ O
294 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
50 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
FixedRotationArm B-component
_ O
294 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
1 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
2 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
1 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
2 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
7 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
8 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
10 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
11 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
12 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
13 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
7 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
11 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
13 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
9 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
14 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
8 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
9 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
10 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
12 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
14 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
1 O
_ O
ROT2 B-parameter
" O
, O

" O
value O
" O
: O
" O
90 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
END B-parameter
_ I-parameter
ROT I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
2 O
_ O
ROT2 B-parameter
" O
, O

" O
value O
" O
: O
" O
270 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
END B-parameter
_ I-parameter
ROT I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
341 O
. O

38350998761973 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
1 O
_ O
ROT2 B-parameter
" O
, O

" O
value O
" O
: O
" O
270 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
END B-parameter
_ I-parameter
ROT I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
2 O
_ O
ROT2 B-parameter
" O
, O

" O
value O
" O
: O
" O
90 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
END B-parameter
_ I-parameter
ROT I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
50 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
] O
, O

" O
components O
" O
: O
[ O
{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
2617 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube B-component
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube B-component
" O
} O
, O

{ O
" O
component O
_ O
instance O
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: O
" O
Flange B-module
_ O
847 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
9 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
UAV B-module
_ I-module
Fuselage I-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
capsule B-module
_ I-module
fuselage I-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Para O
_ O
Hub B-module
_ O
6 O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394od O
_ O
para O
_ O
hub B-module
_ O
6 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
AT4125KV540 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
10 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
MN4014KV400 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
11 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
MN4014KV400 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
12 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE4213XF O
_ O
360 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
13 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE4213XF O
_ O
360 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
14 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE3520XF O
_ O
400 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
MN4014KV400 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
MN4014KV400 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE4213XF O
_ O
360 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE4213XF O
_ O
360 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE3520XF O
_ O
400 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
U7 O
_ O
V2 O
. O

0KV490 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
AntigravityMN5006KV450 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
9 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
U7 O
_ O
V2 O
. O

0KV490 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Orient B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
20x10E O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
10 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
16x8E O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
11 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
16x8E O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
12 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
17x10WE O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
13 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
17x10WE O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
14 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
15x4W O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
16x8E O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
16x8E O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
17x10WE O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
17x10WE O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
15x4W O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
7 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
16x12E O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
8 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
17x8 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
9 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
16x12E O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube B-component
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube B-component
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube B-component
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube B-component
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube B-component
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube B-component
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube B-component
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube B-component
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
RpmTemp B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Autopilot B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Current B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Voltage B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
GPS B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Variometer B-parameter
" O
} O
] O
, O

" O
connections O
" O
: O
[ O
{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2617 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
8 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
9 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
10 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2620 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2620 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2621 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2621 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2622 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2622 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2623 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2623 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2624 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2624 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2625 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
9 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
14 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
12 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
13 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
10 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
11 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2620 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2624 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2623 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ I-module
5 I-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2624 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2623 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
8 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2620 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
FixedRotationArm B-component
_ O
293 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
FixedRotationArm B-component
_ O
294 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2621 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2621 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
FixedRotationArm B-component
_ O
293 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
FixedRotationArm B-component
_ O
294 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
8 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
10 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
13 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
10 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
8 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
11 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
14 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
9 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
9 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
12 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector3 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector1 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
5 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
6 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2622 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2625 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2617 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2622 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Case2HubConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
10 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
10 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
11 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
11 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
12 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
12 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
13 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
13 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
14 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
14 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
8 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
9 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
9 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Orient B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
ORIENTCONN B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Orient B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2617 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
8 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
9 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
10 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2620 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2620 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2621 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2621 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2622 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2622 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2623 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2623 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2624 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2624 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2625 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
9 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
14 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
12 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
13 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
10 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
11 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1663 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2620 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2624 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2623 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2624 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2623 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2620 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
8 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
FixedRotationArm B-component
_ O
293 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
FixedRotationArm B-component
_ O
294 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2619 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Branch B-module
_ O
280 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2621 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2621 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2618 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
FixedRotationArm B-component
_ O
293 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
8 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
FixedRotationArm B-component
_ O
294 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
13 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
10 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
10 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
11 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
8 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
14 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
846 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
9 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
847 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
12 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
9 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector3 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector1 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
5 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2622 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
6 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2625 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2617 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2622 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Case2HubConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
10 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
10 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
11 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
11 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
12 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
12 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
13 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
13 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
14 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
14 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
8 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
9 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
9 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Orient B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Orient B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
ORIENTCONN B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
835 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
836 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
] O
} O

Title O
14 O
— O
Aeronautics O
and O
Space O
Chapter O
I O
— O
Federal O
Aviation B-asset
Administration O
, O

Department O
of O
Transportation O
Subchapter O
C O
— O
Aircraft B-asset
Part O
23 O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
§ O
23 O
. O

1457 O
Cockpit B-module
voice I-module
recorders I-module
. O

§ O
23 O
. O

1459 O
Flight B-module
data I-module
recorders I-module
. O

§ O
23 O
. O

1529 O
Instructions O
for O
continued O
airworthiness O
. O

Subpart O
A O
General O
§ O
23 O
. O

2000 O
Applicability O
and O
definitions O
. O

§ O
23 O
. O

2005 O
Certification O
of O
normal O
category O
airplanes B-asset
. O

§ O
23 O
. O

2010 O
Accepted O
means O
of O
compliance O
. O

Subpart O
B O
Flight O
Performance O
§ O
23 O
. O

2100 O
Weight B-parameter
and O
center B-parameter
of I-parameter
gravity I-parameter
. O

§ O
23 O
. O

2105 O
Performance O
data O
. O

§ O
23 O
. O

2110 O
Stall B-parameter
speed I-parameter
. O

§ O
23 O
. O

2115 O
Takeoff O
performance O
. O

§ O
23 O
. O

2120 O
Climb O
requirements O
. O

§ O
23 O
. O

2125 O
Climb O
information O
. O

§ O
23 O
. O

2130 O
Landing O
. O

Flight O
Characteristics O
§ O
23 O
. O

2135 O
Controllability O
. O

§ O
23 O
. O

2140 O
Trim O
. O

§ O
23 O
. O

2145 O
Stability B-parameter
. O

§ O
23 O
. O

2150 O
Stall B-parameter
characteristics I-parameter
, O

stall B-parameter
warning I-parameter
, O

and O
spins B-parameter
. O

§ O
23 O
. O

2155 O
Ground O
and O
water O
handling O
characteristics O
. O

§ O
23 O
. O

2160 O
Vibration B-parameter
, O

buffeting B-parameter
, O

and O
high B-parameter
- I-parameter
speed I-parameter
characteristics O
. O

§ O
23 O
. O

2165 O
Performance O
and O
flight O
characteristics O
requirements O
for O
flight O
in O
icing O
conditions O
. O

Subpart O
C O
Structures O
§ O
23 O
. O

2200 O
Structural O
design O
envelope O
. O

§ O
23 O
. O

2205 O
Interaction O
of O
systems O
and O
structures O
. O

Structural B-parameter
Loads I-parameter
§ O
23 O
. O

2210 O
Structural B-parameter
design I-parameter
loads I-parameter
. O

§ O
23 O
. O

2215 O
Flight B-parameter
load I-parameter
conditions O
. O

§ O
23 O
. O

2220 O
Ground O
and O
water O
load O
conditions O
. O

§ O
23 O
. O

2225 O
Component O
loading O
conditions O
. O

This O
content O
is O
from O
the O
eCFR O
and O
is O
authoritative O
but O
unofficial O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
Part O
23 O
( O
June O
27 O
, O

2024 O
) O
14 O
CFR O
Part O
23 O
( O
June O
27 O
, O

2024 O
) O
( O
enhanced O
display O
) O
page O
1 O
of O
31 O
§ O
23 O
. O

2230 O
Limit O
and O
ultimate B-parameter
loads I-parameter
. O

Structural O
Performance O
§ O
23 O
. O

2235 O
Structural B-parameter
strength I-parameter
. O

§ O
23 O
. O

2240 O
Structural B-parameter
durability I-parameter
. O

§ O
23 O
. O

2245 O
Aeroelasticity B-parameter
. O

Design O
§ O
23 O
. O

2250 O
Design O
and O
construction O
principles O
. O

§ O
23 O
. O

2255 O
Protection O
of O
structure O
. O

§ O
23 O
. O

2260 O
Materials O
and O
processes O
. O

§ O
23 O
. O

2265 O
Special O
factors O
of O
safety O
. O

Structural O
Occupant O
Protection O
§ O
23 O
. O

2270 O
Emergency O
conditions O
. O

Subpart O
D O
Design O
and O
Construction O
§ O
23 O
. O

2300 O
Flight B-system
control I-system
systems I-system
. O

§ O
23 O
. O

2305 O
Landing B-system
gear I-system
systems I-system
. O

§ O
23 O
. O

2310 O
Buoyancy O
for O
seaplanes O
and O
amphibians O
. O

Occupant O
System O
Design O
Protection O
§ O
23 O
. O

2315 O
Means O
of O
egress O
and O
emergency O
exits O
. O

§ O
23 O
. O

2320 O
Occupant O
physical O
environment O
. O

Fire O
and O
High O
Energy O
Protection O
§ O
23 O
. O

2325 O
Fire O
protection O
. O

§ O
23 O
. O

2330 O
Fire O
protection O
in O
designated O
fire O
zones O
and O
adjacent O
areas O
. O

§ O
23 O
. O

2335 O
Lightning O
protection O
. O

Subpart O
E O
Powerplant B-system
§ O
23 O
. O

2400 O
Powerplant B-system
installation O
. O

§ O
23 O
. O

2405 O
Automatic B-parameter
power I-parameter
or O
thrust B-system
control I-system
systems I-system
. O

§ O
23 O
. O

2410 O
Powerplant B-system
installation O
hazard O
assessment O
. O

§ O
23 O
. O

2415 O
Powerplant B-system
ice O
protection O
. O

§ O
23 O
. O

2420 O
Reversing B-system
systems I-system
. O

§ O
23 O
. O

2425 O
Powerplant B-system
operational O
characteristics O
. O

§ O
23 O
. O

2430 O
Fuel B-system
systems I-system
. O

§ O
23 O
. O

2435 O
Powerplant B-system
induction O
and O
exhaust B-system
systems I-system
. O

§ O
23 O
. O

2440 O
Powerplant B-system
fire O
protection O
. O

Subpart O
F O
Equipment O
§ O
23 O
. O

2500 O
Airplane B-system
level I-system
systems I-system
requirements O
. O

§ O
23 O
. O

2505 O
Function O
and O
installation O
. O

§ O
23 O
. O

2510 O
Equipment O
, O

systems O
, O

and O
installations O
. O

§ O
23 O
. O

2515 O
Electrical B-system
and I-system
electronic I-system
system I-system
lightning O
protection O
. O

§ O
23 O
. O

2520 O
High O
- O
intensity O
Radiated O
Fields O
( O
HIRF O
) O
protection O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
Part O
23 O
( O
June O
27 O
, O

2024 O
) O
14 O
CFR O
Part O
23 O
( O
June O
27 O
, O

2024 O
) O
( O
enhanced O
display O
) O
page O
2 O
of O
31 O
Appendix O
A O
to O
Part O
23 O
Instructions O
for O
Continued O
Airworthiness O
§ O
23 O
. O

2525 O
System O
power O
generation O
, O

storage O
, O

and O
distribution O
. O

§ O
23 O
. O

2530 O
External O
and O
cockpit O
lighting O
. O

§ O
23 O
. O

2535 O
Safety B-system
equipment I-system
. O

§ O
23 O
. O

2540 O
Flight O
in O
icing O
conditions O
. O

§ O
23 O
. O

2545 O
Pressurized B-system
systems I-system
elements O
. O

§ O
23 O
. O

2550 O
Equipment O
containing O
high B-component
- I-component
energy I-component
rotors I-component
. O

Subpart O
G O
Flightcrew O
Interface O
and O
Other O
Information O
§ O
23 O
. O

2600 O
Flightcrew O
interface O
. O

§ O
23 O
. O

2605 O
Installation O
and O
operation O
. O

§ O
23 O
. O

2610 O
Instrument O
markings O
, O

control O
markings O
, O

and O
placards O
. O

§ O
23 O
. O

2615 O
Flight O
, O

navigation O
, O

and O
powerplant B-module
instruments I-module
. O

§ O
23 O
. O

2620 O
Airplane B-asset
flight O
manual O
. O

PART O
23 O
— O
AIRWORTHINESS O
STANDARDS O
: O
NORMAL O
CATEGORY O
AIRPLANES B-asset
Authority O
: O
49 O
U O
. O

S O
. O

C O
. O

106 O
( O
f O
) O
, O

106 O
( O
g O
) O
, O

40113 O
, O

44701 O
- O
44702 O
, O

44704 O
, O

Pub O
. O

L O
. O

113 O
- O
53 O
, O

127 O
Stat O
. O

584 O
( O
49 O
U O
. O

S O
. O

C O
. O

44704 O
) O
note O
. O

Source O
: O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

unless O
otherwise O
noted O
. O

§ O
23 O
. O

1457 O
Cockpit B-module
voice I-module
recorders I-module
. O

( O
a O
) O
Each O
cockpit B-system
voice I-system
recorder I-system
required O
by O
the O
operating O
rules O
of O
this O
chapter O
must O
be O
approved O
and O
must O
be O
installed O
so O
that O
it O
will O
record O
the O
following O
: O
( O
1 O
) O
Voice O
communications O
transmitted O
from O
or O
received O
in O
the O
airplane B-asset
by O
radio B-module
. O

( O
2 O
) O
Voice O
communications O
of O
flightcrew O
members O
on O
the O
flight B-module
deck I-module
. O

( O
3 O
) O
Voice O
communications O
of O
flightcrew O
members O
on O
the O
flight B-module
deck I-module
, O

using O
the O
airplane B-asset
' O
s O
interphone B-system
system I-system
. O

( O
4 O
) O
Voice O
or O
audio O
signals O
identifying O
navigation O
or O
approach O
aids O
introduced O
into O
a O
headset B-module
or O
speaker B-module
. O

( O
5 O
) O
Voice O
communications O
of O
flightcrew O
members O
using O
the O
passenger B-system
loudspeaker I-system
system I-system
, O

if O
there O
is O
such O
a O
system O
and O
if O
the O
fourth O
channel O
is O
available O
in O
accordance O
with O
the O
requirements O
of O
paragraph O
( O
c O
) O
( O
4 O
) O
( O
ii O
) O
of O
this O
section O
. O

( O
6 O
) O
If O
datalink B-module
communication I-module
equipment I-module
is O
installed O
, O

all O
datalink O
communications O
, O

using O
an O
approved O
data O
message O
set O
. O

Datalink O
messages O
must O
be O
recorded O
as O
the O
output O
signal O
from O
the O
communications B-module
unit I-module
that O
translates O
the O
signal O
into O
usable O
data O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
Part O
23 O
( O
June O
27 O
, O

2024 O
) O
14 O
CFR O
23 O
. O

1457 O
( O
a O
) O
( O
6 O
) O
( O
enhanced O
display O
) O
page O
3 O
of O
31 O
( O
b O
) O
The O
recording O
requirements O
of O
paragraph O
( O
a O
) O
( O
2 O
) O
of O
this O
section O
must O
be O
met O
by O
installing O
a O
cockpit B-module
￾ O
mounted O
area B-module
microphone I-module
, O

located O
in O
the O
best O
position O
for O
recording O
voice O
communications O
originating O
at O
the O
first O
and O
second O
pilot O
stations O
and O
voice O
communications O
of O
other O
crewmembers O
on O
the O
flight B-module
deck I-module
when O
directed O
to O
those O
stations O
. O

The O
microphone B-module
must O
be O
so O
located O
and O
, O

if O
necessary O
, O

the O
preamplifiers B-component
and O
filters B-component
of O
the O
recorder O
must O
be O
so O
adjusted O
or O
supplemented O
, O

so O
that O
the O
intelligibility O
of O
the O
recorded O
communications O
is O
as O
high O
as O
practicable O
when O
recorded O
under O
flight B-module
cockpit I-module
noise O
conditions O
and O
played O
back O
. O

Repeated O
aural O
or O
visual O
playback O
of O
the O
record O
may O
be O
used O
in O
evaluating O
intelligibility O
. O

( O
c O
) O
Each O
cockpit B-system
voice I-system
recorder I-system
must O
be O
installed O
so O
that O
the O
part O
of O
the O
communication O
or O
audio O
signals O
specified O
in O
paragraph O
( O
a O
) O
of O
this O
section O
obtained O
from O
each O
of O
the O
following O
sources O
is O
recorded O
on O
a O
separate O
channel O
: O
( O
1 O
) O
For O
the O
first O
channel O
, O

from O
each O
boom B-component
, O

mask B-component
, O

or O
handheld B-component
microphone I-component
, O

headset B-module
, O

or O
speaker B-module
used O
at O
the O
first O
pilot O
station O
. O

( O
2 O
) O
For O
the O
second O
channel O
from O
each O
boom B-component
, O

mask B-component
, O

or O
handheld B-component
microphone I-component
, O

headset B-module
, O

or O
speaker B-module
used O
at O
the O
second O
pilot O
station O
. O

( O
3 O
) O
For O
the O
third O
channel O
— O
from O
the O
cockpit B-module
- I-module
mounted I-module
area I-module
microphone I-module
. O

( O
4 O
) O
For O
the O
fourth O
channel O
from O
: O
( O
i O
) O
Each O
boom B-component
, O

mask B-component
, O

or O
handheld B-component
microphone I-component
, O

headset B-module
, O

or O
speaker B-module
used O
at O
the O
station O
for O
the O
third O
and O
fourth O
crewmembers O
. O

( O
ii O
) O
If O
the O
stations O
specified O
in O
paragraph O
( O
c O
) O
( O
4 O
) O
( O
i O
) O
of O
this O
section O
are O
not O
required O
or O
if O
the O
signal O
at O
such O
a O
station O
is O
picked O
up O
by O
another O
channel O
, O

each O
microphone B-module
on O
the O
flight B-module
deck I-module
that O
is O
used O
with O
the O
passenger B-system
loudspeaker I-system
system I-system
, O

if O
its O
signals O
are O
not O
picked O
up O
by O
another O
channel O
. O

( O
5 O
) O
And O
that O
as O
far O
as O
is O
practicable O
all O
sounds O
received O
by O
the O
microphone B-module
listed O
in O
paragraphs O
( O
c O
) O
( O
1 O
) O
, O

( O
2 O
) O
, O

and O
( O
4 O
) O
of O
this O
section O
must O
be O
recorded O
without O
interruption O
irrespective O
of O
the O
position O
of O
the O
interphone B-component
- I-component
transmitter I-component
key I-component
switch I-component
. O

The O
design O
shall O
ensure O
that O
sidetone O
for O
the O
flightcrew O
is O
produced O
only O
when O
the O
interphone B-component
, O

public B-system
address I-system
system I-system
, O

or O
radio B-component
transmitters I-component
are O
in O
use O
. O

( O
d O
) O
Each O
cockpit B-system
voice I-system
recorder I-system
must O
be O
installed O
so O
that O
: O
( O
1 O
) O
( O
i O
) O
It O
receives O
its O
electrical B-parameter
power I-parameter
from O
the O
bus B-component
that O
provides O
the O
maximum O
reliability O
for O
operation O
of O
the O
cockpit B-system
voice I-system
recorder I-system
without O
jeopardizing O
service O
to O
essential O
or O
emergency O
loads B-parameter
. O

( O
ii O
) O
It O
remains O
powered O
for O
as O
long O
as O
possible O
without O
jeopardizing O
emergency O
operation O
of O
the O
airplane B-asset
. O

( O
2 O
) O
There O
is O
an O
automatic O
means O
to O
simultaneously O
stop O
the O
recorder B-module
and O
prevent O
each O
erasure O
feature O
from O
functioning O
, O

within O
10 O
minutes O
after O
crash O
impact O
. O

( O
3 O
) O
There O
is O
an O
aural O
or O
visual O
means O
for O
preflight O
checking O
of O
the O
recorder O
for O
proper O
operation O
. O

( O
4 O
) O
Any O
single O
electrical O
failure O
external O
to O
the O
recorder O
does O
not O
disable O
both O
the O
cockpit B-system
voice I-system
recorder I-system
and O
the O
flight B-module
data I-module
recorder I-module
. O

( O
5 O
) O
It O
has O
an O
independent B-module
power I-module
source I-module
— O
( O
i O
) O
That O
provides O
10 O
± O
1 O
minutes O
of O
electrical B-parameter
power I-parameter
to O
operate O
both O
the O
cockpit B-system
voice I-system
recorder I-system
and O
cockpit B-module
- I-module
mounted I-module
area I-module
microphone I-module
; O
14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

1457 O
( O
b O
) O
14 O
CFR O
23 O
. O

1457 O
( O
d O
) O
( O
5 O
) O
( O
i O
) O
( O
enhanced O
display O
) O
page O
4 O
of O
31 O
§ O
23 O
. O

1459 O
Flight B-module
data I-module
recorders I-module
. O

( O
ii O
) O
That O
is O
located O
as O
close O
as O
practicable O
to O
the O
cockpit B-system
voice I-system
recorder I-system
; O
and O
( O
iii O
) O
To O
which O
the O
cockpit B-system
voice I-system
recorder I-system
and O
cockpit B-module
- I-module
mounted I-module
area I-module
microphone I-module
are O
switched O
automatically O
in O
the O
event O
that O
all O
other O
power O
to O
the O
cockpit B-system
voice I-system
recorder I-system
is O
interrupted O
either O
by O
normal O
shutdown O
or O
by O
any O
other O
loss O
of O
power O
to O
the O
electrical B-module
power I-module
bus I-module
. O

( O
6 O
) O
It O
is O
in O
a O
separate O
container O
from O
the O
flight B-module
data I-module
recorder I-module
when O
both O
are O
required O
. O

If O
used O
to O
comply O
with O
only O
the O
cockpit B-system
voice I-system
recorder I-system
requirements O
, O

a O
combination O
unit O
may O
be O
installed O
. O

( O
e O
) O
The O
recorder B-module
container I-module
must O
be O
located O
and O
mounted O
to O
minimize O
the O
probability O
of O
rupture O
of O
the O
container O
as O
a O
result O
of O
crash O
impact O
and O
consequent O
heat O
damage O
to O
the O
recorder B-module
from O
fire O
. O

( O
1 O
) O
Except O
as O
provided O
in O
paragraph O
( O
e O
) O
( O
2 O
) O
of O
this O
section O
, O

the O
recorder B-module
container I-module
must O
be O
located O
as O
far O
aft O
as O
practicable O
, O

but O
need O
not O
be O
outside O
of O
the O
pressurized B-module
compartment I-module
, O

and O
may O
not O
be O
located O
where O
aft O
- O
mounted O
engines B-system
may O
crush O
the O
container O
during O
impact O
. O

( O
2 O
) O
If O
two O
separate O
combination B-module
digital I-module
flight I-module
data I-module
recorder I-module
and O
cockpit B-system
voice I-system
recorder I-system
units O
are O
installed O
instead O
of O
one O
cockpit B-system
voice I-system
recorder I-system
and O
one O
digital B-module
flight I-module
data I-module
recorder I-module
, O

the O
combination O
unit O
that O
is O
installed O
to O
comply O
with O
the O
cockpit B-system
voice I-system
recorder I-system
requirements O
may O
be O
located O
near O
the O
cockpit B-module
. O

( O
f O
) O
If O
the O
cockpit B-system
voice I-system
recorder I-system
has O
a O
bulk B-module
erasure I-module
device I-module
, O

the O
installation O
must O
be O
designed O
to O
minimize O
the O
probability O
of O
inadvertent O
operation O
and O
actuation O
of O
the O
device O
during O
crash O
impact O
. O

( O
g O
) O
Each O
recorder B-module
container I-module
must O
— O
( O
1 O
) O
Be O
either O
bright O
orange O
or O
bright O
yellow O
; O
( O
2 O
) O
Have O
reflective B-component
tape I-component
affixed O
to O
its O
external O
surface O
to O
facilitate O
its O
location O
under O
water O
; O
and O
( O
3 O
) O
Have O
an O
underwater B-component
locating I-component
device I-component
, O

when O
required O
by O
the O
operating O
rules O
of O
this O
chapter O
, O

on O
or O
adjacent O
to O
the O
container O
, O

which O
is O
secured O
in O
such O
manner O
that O
they O
are O
not O
likely O
to O
be O
separated O
during O
crash O
impact O
. O

( O
a O
) O
Each O
flight B-module
recorder I-module
required O
by O
the O
operating O
rules O
of O
this O
chapter O
must O
be O
installed O
so O
that O
— O
( O
1 O
) O
It O
is O
supplied O
with O
airspeed B-parameter
, O

altitude B-parameter
, O

and O
directional O
data O
obtained O
from O
sources O
that O
meet O
the O
aircraft B-asset
level O
system O
requirements O
and O
the O
functionality O
specified O
in O
§ O
23 O
. O

2500 O
; O
( O
2 O
) O
The O
vertical B-component
acceleration I-component
sensor I-component
is O
rigidly O
attached O
, O

and O
located O
longitudinally O
either O
within O
the O
approved O
center B-parameter
of I-parameter
gravity I-parameter
limits O
of O
the O
airplane B-asset
, O

or O
at O
a O
distance O
forward O
or O
aft O
of O
these O
limits O
that O
does O
not O
exceed O
25 O
percent O
of O
the O
airplane B-parameter
' I-parameter
s I-parameter
mean I-parameter
aerodynamic I-parameter
chord I-parameter
; O
( O
3 O
) O
( O
i O
) O
It O
receives O
its O
electrical B-parameter
power I-parameter
from O
the O
bus O
that O
provides O
the O
maximum O
reliability O
for O
operation O
of O
the O
flight B-module
data I-module
recorder I-module
without O
jeopardizing O
service O
to O
essential O
or O
emergency B-parameter
loads I-parameter
; O
( O
ii O
) O
It O
remains O
powered O
for O
as O
long O
as O
possible O
without O
jeopardizing O
emergency O
operation O
of O
the O
airplane B-asset
; O
( O
4 O
) O
There O
is O
an O
aural O
or O
visual O
means O
for O
preflight O
checking O
of O
the O
recorder O
for O
proper O
recording O
of O
data O
in O
the O
storage O
medium O
; O
14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

1457 O
( O
d O
) O
( O
5 O
) O
( O
ii O
) O
14 O
CFR O
23 O
. O

1459 O
( O
a O
) O
( O
4 O
) O
( O
enhanced O
display O
) O
page O
5 O
of O
31 O
§ O
23 O
. O

1529 O
Instructions O
for O
continued O
airworthiness O
. O

The O
applicant O
must O
prepare O
Instructions O
for O
Continued O
Airworthiness O
, O

in O
accordance O
with O
appendix O
A O
of O
this O
part O
, O

that O
are O
acceptable O
to O
the O
Administrator O
. O

The O
instructions O
may O
be O
incomplete O
at O
type O
certification O
if O
a O
program O
exists O
to O
ensure O
their O
completion O
prior O
to O
delivery O
of O
the O
first O
airplane B-asset
or O
issuance O
of O
a O
standard O
certificate O
of O
airworthiness O
, O

whichever O
occurs O
later O
. O

Subpart O
A O
— O
General O
§ O
23 O
. O

2000 O
Applicability O
and O
definitions O
. O

( O
5 O
) O
Except O
for O
recorders B-module
powered O
solely O
by O
the O
engine O
- O
driven O
electrical B-system
generator I-system
system I-system
, O

there O
is O
an O
automatic O
means O
to O
simultaneously O
stop O
a O
recorder B-module
that O
has O
a O
data O
erasure O
feature O
and O
prevent O
each O
erasure O
feature O
from O
functioning O
, O

within O
10 O
minutes O
after O
crash O
impact O
; O
( O
6 O
) O
Any O
single O
electrical O
failure O
external O
to O
the O
recorder B-module
does O
not O
disable O
both O
the O
cockpit B-system
voice I-system
recorder I-system
and O
the O
flight B-module
data I-module
recorder I-module
; O
and O
( O
7 O
) O
It O
is O
in O
a O
separate B-component
container I-component
from O
the O
cockpit B-system
voice I-system
recorder I-system
when O
both O
are O
required O
. O

If O
used O
to O
comply O
with O
only O
the O
flight B-module
data I-module
recorder I-module
requirements O
, O

a O
combination O
unit O
may O
be O
installed O
. O

If O
a O
combination O
unit O
is O
installed O
as O
a O
cockpit B-system
voice I-system
recorder I-system
to O
comply O
with O
§ O
23 O
. O

1457 O
( O
e O
) O
( O
2 O
) O
, O

a O
combination B-component
unit I-component
must O
be O
used O
to O
comply O
with O
this O
flight B-module
data I-module
recorder I-module
requirement O
. O

( O
b O
) O
Each O
non O
- O
ejectable O
record B-component
container I-component
must O
be O
located O
and O
mounted O
so O
as O
to O
minimize O
the O
probability O
of O
container B-component
rupture O
resulting O
from O
crash O
impact O
and O
subsequent O
damage O
to O
the O
record O
from O
fire O
. O

In O
meeting O
this O
requirement O
, O

the O
record B-component
container I-component
must O
be O
located O
as O
far O
aft O
as O
practicable O
, O

but O
need O
not O
be O
aft O
of O
the O
pressurized O
compartment O
, O

and O
may O
not O
be O
where O
aft B-system
- I-system
mounted I-system
engines I-system
may O
crush O
the O
container O
upon O
impact O
. O

( O
c O
) O
A O
correlation O
must O
be O
established O
between O
the O
flight B-module
recorder I-module
readings O
of O
airspeed B-parameter
, O

altitude B-parameter
, O

and O
heading B-parameter
and O
the O
corresponding B-parameter
readings I-parameter
( O
taking O
into O
account O
correction O
factors O
) O
of O
the O
first O
pilot O
' O
s O
instruments O
. O

The O
correlation O
must O
cover O
the O
airspeed B-parameter
range O
over O
which O
the O
airplane B-asset
is O
to O
be O
operated O
, O

the O
range O
of O
altitude B-parameter
to O
which O
the O
airplane B-asset
is O
limited O
, O

and O
360 O
degrees O
of O
heading O
. O

Correlation O
may O
be O
established O
on O
the O
ground O
as O
appropriate O
. O

( O
d O
) O
Each O
recorder B-module
container I-module
must O
— O
( O
1 O
) O
Be O
either O
bright O
orange O
or O
bright O
yellow O
; O
( O
2 O
) O
Have O
reflective B-component
tape I-component
affixed O
to O
its O
external O
surface O
to O
facilitate O
its O
location O
under O
water O
; O
and O
( O
3 O
) O
Have O
an O
underwater O
locating O
device O
, O

when O
required O
by O
the O
operating O
rules O
of O
this O
chapter O
, O

on O
or O
adjacent O
to O
the O
container B-component
, O

which O
is O
secured O
in O
such O
a O
manner O
that O
they O
are O
not O
likely O
to O
be O
separated O
during O
crash O
impact O
. O

( O
e O
) O
Any O
novel O
or O
unique O
design O
or O
operational O
characteristics O
of O
the O
aircraft B-asset
shall O
be O
evaluated O
to O
determine O
if O
any O
dedicated O
parameters O
must O
be O
recorded O
on O
flight B-module
recorders I-module
in O
addition O
to O
or O
in O
place O
of O
existing O
requirements O
. O

( O
a O
) O
This O
part O
prescribes O
airworthiness O
standards O
for O
the O
issuance O
of O
type O
certificates O
, O

and O
changes O
to O
those O
certificates O
, O

for O
airplanes O
in O
the O
normal O
category O
. O

( O
b O
) O
For O
the O
purposes O
of O
this O
part O
, O

the O
following O
definition O
applies O
: O
14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

1459 O
( O
a O
) O
( O
5 O
) O
14 O
CFR O
23 O
. O

2000 O
( O
b O
) O
( O
enhanced O
display O
) O
page O
6 O
of O
31 O
§ O
23 O
. O

2005 O
Certification O
of O
normal O
category O
airplanes B-asset
. O

§ O
23 O
. O

2010 O
Accepted O
means O
of O
compliance O
. O

Subpart O
B O
— O
Flight O
PERFORMANCE O
§ O
23 O
. O

2100 O
Weight B-parameter
and O
center B-parameter
of I-parameter
gravity I-parameter
. O

Continued O
safe O
flight O
and O
landing O
means O
an O
airplane B-asset
is O
capable O
of O
continued O
controlled O
flight O
and O
landing O
, O

possibly O
using O
emergency O
procedures O
, O

without O
requiring O
exceptional O
pilot O
skill O
or O
strength O
. O

Upon O
landing O
, O

some O
airplane B-asset
damage O
may O
occur O
as O
a O
result O
of O
a O
failure O
condition O
. O

( O
a O
) O
Certification O
in O
the O
normal O
category O
applies O
to O
airplanes B-asset
with O
a O
passenger O
- O
seating O
configuration O
of O
19 O
or O
less O
and O
a O
maximum O
certificated O
takeoff B-parameter
weight I-parameter
of O
19 O
, O

000 O
pounds B-measurement
or O
less O
. O

( O
b O
) O
Airplane O
certification O
levels O
are O
: O
( O
1 O
) O
Level O
1 O
— O
for O
airplanes B-asset
with O
a O
maximum B-parameter
seating I-parameter
configuration I-parameter
of O
0 O
to O
1 O
passengers O
. O

( O
2 O
) O
Level O
2 O
— O
for O
airplanes B-asset
with O
a O
maximum B-parameter
seating I-parameter
configuration I-parameter
of O
2 O
to O
6 O
passengers O
. O

( O
3 O
) O
Level O
3 O
— O
for O
airplanes B-asset
with O
a O
maximum B-parameter
seating I-parameter
configuration I-parameter
of O
7 O
to O
9 O
passengers O
. O

( O
4 O
) O
Level O
4 O
— O
for O
airplanes B-asset
with O
a O
maximum B-parameter
seating I-parameter
configuration I-parameter
of O
10 O
to O
19 O
passengers O
. O

( O
c O
) O
Airplane B-asset
performance O
levels O
are O
: O
( O
1 O
) O
Low O
speed B-parameter
— O
for O
airplanes B-asset
with O
a O
VNO O
and O
VMO O
≤ O
250 O
Knots B-measurement
Calibrated B-parameter
Airspeed I-parameter
( O
KCAS O
) O
and O
a O
MMO O
≤ O
0 O
. O

6 O
. O

( O
2 O
) O
High O
speed B-parameter
— O
for O
airplanes B-asset
with O
a O
VNO O
or O
VMO O
> O
250 O
KCAS O
or O
a O
MMO O
> O
0 O
. O

6 O
. O

( O
d O
) O
Airplanes B-asset
not O
certified O
for O
aerobatics O
may O
be O
used O
to O
perform O
any O
maneuver O
incident O
to O
normal O
flying O
, O

including O
— O
( O
1 O
) O
Stalls O
( O
except O
whip O
stalls O
) O
; O
and O
( O
2 O
) O
Lazy O
eights O
, O

chandelles O
, O

and O
steep O
turns O
, O

in O
which O
the O
angle O
of O
bank O
is O
not O
more O
than O
60 O
degrees B-measurement
. O

( O
e O
) O
Airplanes B-asset
certified O
for O
aerobatics O
may O
be O
used O
to O
perform O
maneuvers O
without O
limitations O
, O

other O
than O
those O
limitations O
established O
under O
subpart O
G O
of O
this O
part O
. O

( O
a O
) O
An O
applicant O
must O
comply O
with O
this O
part O
using O
a O
means O
of O
compliance O
, O

which O
may O
include O
consensus O
standards O
, O

accepted O
by O
the O
Administrator O
. O

( O
b O
) O
An O
applicant O
requesting O
acceptance O
of O
a O
means O
of O
compliance O
must O
provide O
the O
means O
of O
compliance O
to O
the O
FAA O
in O
a O
form O
and O
manner O
acceptable O
to O
the O
Administrator O
. O

( O
a O
) O
The O
applicant O
must O
determine O
limits O
for O
weights B-parameter
and O
centers B-parameter
of I-parameter
gravity I-parameter
that O
provide O
for O
the O
safe O
operation O
of O
the O
airplane O
. O

( O
b O
) O
The O
applicant O
must O
comply O
with O
each O
requirement O
of O
this O
subpart O
at O
critical O
combinations O
of O
weight B-parameter
and O
center B-parameter
of I-parameter
gravity I-parameter
within O
the O
airplane B-asset
' O
s O
range O
of O
loading O
conditions O
using O
tolerances O
acceptable O
to O
the O
Administrator O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2000 O
“ O
Continued O
safe O
flight O
and O
landing O
” O
14 O
CFR O
23 O
. O

2100 O
( O
b O
) O
( O
enhanced O
display O
) O
page O
7 O
of O
31 O
§ O
23 O
. O

2105 O
Performance O
data O
. O

§ O
23 O
. O

2110 O
Stall B-parameter
speed I-parameter
. O

The O
applicant O
must O
determine O
the O
airplane B-asset
stall B-parameter
speed I-parameter
or O
the O
minimum O
steady B-parameter
flight I-parameter
speed I-parameter
for O
each O
flight O
configuration O
used O
in O
normal O
operations O
, O

including O
takeoff O
, O

climb O
, O

cruise O
, O

descent O
, O

approach O
, O

and O
landing O
. O

The O
stall B-parameter
speed I-parameter
or O
minimum O
steady B-parameter
flight I-parameter
speed I-parameter
determination O
must O
account O
for O
the O
most O
adverse O
conditions O
for O
each O
flight O
configuration O
with O
power O
set O
at O
— O
§ O
23 O
. O

2115 O
Takeoff O
performance O
. O

( O
c O
) O
The O
condition O
of O
the O
airplane B-asset
at O
the O
time O
of O
determining O
its O
empty B-parameter
weight I-parameter
and O
center B-parameter
of I-parameter
gravity I-parameter
must O
be O
well O
defined O
and O
easily O
repeatable O
. O

( O
a O
) O
Unless O
otherwise O
prescribed O
, O

an O
airplane B-asset
must O
meet O
the O
performance O
requirements O
of O
this O
subpart O
in O
— O
( O
1 O
) O
Still O
air O
and O
standard O
atmospheric O
conditions O
at O
sea O
level O
for O
all O
airplanes B-asset
; O
and O
( O
2 O
) O
Ambient O
atmospheric O
conditions O
within O
the O
operating O
envelope O
for O
levels O
1 O
and O
2 O
high O
- O
speed O
and O
levels O
3 O
and O
4 O
airplanes B-asset
. O

( O
b O
) O
Unless O
otherwise O
prescribed O
, O

the O
applicant O
must O
develop O
the O
performance O
data O
required O
by O
this O
subpart O
for O
the O
following O
conditions O
: O
( O
1 O
) O
Airport B-asset
altitudes B-parameter
from O
sea O
level O
to O
10 O
, O

000 O
feet B-measurement
( O
3 O
, O

048 O
meters B-measurement
) O
; O
and O
( O
2 O
) O
Temperatures B-parameter
above O
and O
below O
standard O
day O
temperature B-parameter
that O
are O
within O
the O
range O
of O
operating O
limitations O
, O

if O
those O
temperatures B-parameter
could O
have O
a O
negative O
effect O
on O
performance O
. O

( O
c O
) O
The O
procedures O
used O
for O
determining O
takeoff O
and O
landing B-parameter
distances I-parameter
must O
be O
executable O
consistently O
by O
pilots O
of O
average O
skill O
in O
atmospheric O
conditions O
expected O
to O
be O
encountered O
in O
service O
. O

( O
d O
) O
Performance O
data O
determined O
in O
accordance O
with O
paragraph O
( O
b O
) O
of O
this O
section O
must O
account O
for O
losses O
due O
to O
atmospheric O
conditions O
, O

cooling O
needs O
, O

and O
other O
demands O
on O
power O
sources O
. O

( O
a O
) O
Idle O
or O
zero O
thrust O
for O
propulsion B-system
systems I-system
that O
are O
used O
primarily O
for O
thrust O
; O
and O
( O
b O
) O
A O
nominal O
thrust O
for O
propulsion B-system
systems I-system
that O
are O
used O
for O
thrust B-parameter
, O

flight B-system
control I-system
, O

and O
/ O
or O
high B-system
- I-system
lift I-system
systems I-system
. O

( O
a O
) O
The O
applicant O
must O
determine O
airplane O
takeoff O
performance O
accounting O
for O
— O
( O
1 O
) O
Stall B-parameter
speed I-parameter
safety B-parameter
margins I-parameter
; O
( O
2 O
) O
Minimum B-parameter
control I-parameter
speeds I-parameter
; O
and O
( O
3 O
) O
Climb B-parameter
gradients I-parameter
. O

( O
b O
) O
For O
single B-parameter
engine I-parameter
airplanes B-asset
and O
levels O
1 O
, O

2 O
, O

and O
3 O
low O
- O
speed O
multiengine O
airplanes B-asset
, O

takeoff O
performance O
includes O
the O
determination O
of O
ground B-parameter
roll I-parameter
and O
initial B-parameter
climb I-parameter
distance I-parameter
to O
50 O
feet B-measurement
( O
15 O
meters B-measurement
) O
above O
the O
takeoff O
surface O
. O

( O
c O
) O
For O
levels O
1 O
, O

2 O
, O

and O
3 O
high O
- O
speed O
multiengine O
airplanes B-asset
, O

and O
level O
4 O
multiengine O
airplanes B-asset
, O

takeoff O
performance O
includes O
a O
determination O
of O
the O
following O
distances O
after O
a O
sudden O
critical O
loss O
of O
thrust O
— O
( O
1 O
) O
An O
aborted O
takeoff O
at O
critical B-parameter
speed I-parameter
; O
( O
2 O
) O
Ground O
roll O
and O
initial O
climb O
to O
35 O
feet B-measurement
( O
11 O
meters B-measurement
) O
above O
the O
takeoff O
surface O
; O
and O
14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2100 O
( O
c O
) O
14 O
CFR O
23 O
. O

2115 O
( O
c O
) O
( O
2 O
) O
( O
enhanced O
display O
) O
page O
8 O
of O
31 O
[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
§ O
23 O
. O

2120 O
Climb O
requirements O
. O

The O
design O
must O
comply O
with O
the O
following O
minimum O
climb O
performance O
out O
of O
ground O
effect O
: O
[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
§ O
23 O
. O

2125 O
Climb O
information O
. O

( O
3 O
) O
Net O
takeoff O
flight O
path O
. O

( O
a O
) O
With O
all O
engines B-system
operating O
and O
in O
the O
initial O
climb O
configuration O
( O
s O
) O
— O
( O
1 O
) O
For O
levels O
1 O
and O
2 O
low O
- O
speed O
airplanes O
, O

a O
climb O
gradient O
of O
8 O
. O

3 O
percent O
for O
landplanes B-asset
and O
6 O
. O

7 O
percent O
for O
seaplanes B-asset
and O
amphibians B-asset
; O
and O
( O
2 O
) O
For O
levels O
1 O
and O
2 O
high O
- O
speed O
airplanes B-asset
, O

all O
level O
3 O
airplanes B-asset
, O

and O
level O
4 O
single O
- O
engines O
a O
climb O
gradient O
after O
takeoff O
of O
4 O
percent O
. O

( O
b O
) O
After O
a O
critical O
loss O
of O
thrust O
on O
multiengine O
airplanes B-asset
— O
( O
1 O
) O
For O
levels O
1 O
and O
2 O
low O
- O
speed O
airplanes B-asset
that O
do O
not O
meet O
single O
- O
engine O
crashworthiness O
requirements O
, O

a O
climb O
gradient O
of O
1 O
. O

5 O
percent O
at O
a O
pressure B-parameter
altitude I-parameter
of O
5 O
, O

000 O
feet B-measurement
( O
1 O
, O

524 O
meters B-measurement
) O
in O
the O
cruise O
configuration O
( O
s O
) O
; O
( O
2 O
) O
For O
levels O
1 O
and O
2 O
high O
- O
speed O
airplanes B-asset
, O

and O
level O
3 O
low O
- O
speed O
airplanes B-asset
, O

a O
1 O
percent O
climb O
gradient O
at O
400 O
feet B-measurement
( O
122 O
meters B-measurement
) O
above O
the O
takeoff O
surface O
with O
the O
landing B-system
gear I-system
retracted O
and O
flaps O
in O
the O
takeoff O
configuration O
( O
s O
) O
; O
and O
( O
3 O
) O
For O
level O
3 O
high O
- O
speed O
airplanes B-asset
and O
all O
level O
4 O
airplanes B-asset
, O

a O
2 O
percent O
climb O
gradient O
at O
400 O
feet B-measurement
( O
122 O
meters B-measurement
) O
above O
the O
takeoff O
surface O
with O
the O
landing B-system
gear I-system
retracted O
and O
flaps O
in O
the O
approach O
configuration O
( O
s O
) O
. O

( O
c O
) O
For O
a O
balked O
landing O
, O

a O
climb O
gradient O
of O
3 O
percent O
without O
creating O
undue O
pilot O
workload O
with O
the O
landing B-system
gear I-system
extended O
and O
flaps O
in O
the O
landing O
configuration O
( O
s O
) O
. O

( O
a O
) O
The O
applicant O
must O
determine O
climb O
performance O
at O
each O
weight B-parameter
, O

altitude B-parameter
, O

and O
ambient B-parameter
temperature I-parameter
within O
the O
operating O
limitations O
— O
( O
1 O
) O
For O
all O
single O
- O
engine O
airplanes B-asset
; O
( O
2 O
) O
For O
levels O
1 O
and O
2 O
high O
- O
speed O
multiengine O
airplanes B-asset
and O
level O
3 O
multiengine O
airplanes B-asset
, O

following O
a O
critical O
loss O
of O
thrust B-parameter
on O
takeoff O
in O
the O
initial O
climb O
configuration O
; O
and O
( O
3 O
) O
For O
all O
multiengine O
airplanes B-asset
, O

during O
the O
enroute O
phase O
of O
flight O
with O
all O
engines B-system
operating O
and O
after O
a O
critical O
loss O
of O
thrust B-parameter
in O
the O
cruise O
configuration O
. O

( O
b O
) O
The O
applicant O
must O
determine O
the O
glide O
performance O
for O
single O
- O
engine O
airplanes B-asset
after O
a O
complete O
loss O
of O
thrust B-parameter
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2115 O
( O
c O
) O
( O
3 O
) O
14 O
CFR O
23 O
. O

2125 O
( O
b O
) O
( O
enhanced O
display O
) O
page O
9 O
of O
31 O
§ O
23 O
. O

2130 O
Landing O
. O

The O
applicant O
must O
determine O
the O
following O
, O

for O
standard O
temperatures B-parameter
at O
critical O
combinations O
of O
weight B-parameter
and O
altitude B-parameter
within O
the O
operational O
limits O
: O
FLIGHT O
CHARACTERISTICS O
§ O
23 O
. O

2135 O
Controllability O
. O

§ O
23 O
. O

2140 O
Trim O
. O

( O
a O
) O
The O
distance B-parameter
, O

starting O
from O
a O
height O
of O
50 O
feet B-measurement
( O
15 O
meters B-measurement
) O
above O
the O
landing O
surface O
, O

required O
to O
land O
and O
come O
to O
a O
stop O
. O

( O
b O
) O
The O
approach O
and O
landing B-parameter
speeds I-parameter
, O

configurations O
, O

and O
procedures O
, O

which O
allow O
a O
pilot O
of O
average O
skill O
to O
land O
within O
the O
published O
landing B-parameter
distance I-parameter
consistently O
and O
without O
causing O
damage O
or O
injury O
, O

and O
which O
allow O
for O
a O
safe O
transition O
to O
the O
balked O
landing O
conditions O
of O
this O
part O
accounting O
for O
: O
( O
1 O
) O
Stall B-parameter
speed I-parameter
safety B-parameter
margin I-parameter
; O
and O
( O
2 O
) O
Minimum B-parameter
control I-parameter
speeds I-parameter
. O

( O
a O
) O
The O
airplane B-asset
must O
be O
controllable O
and O
maneuverable O
, O

without O
requiring O
exceptional O
piloting O
skill O
, O

alertness O
, O

or O
strength O
, O

within O
the O
operating O
envelope O
— O
( O
1 O
) O
At O
all O
loading O
conditions O
for O
which O
certification O
is O
requested O
; O
( O
2 O
) O
During O
all O
phases O
of O
flight O
; O
( O
3 O
) O
With O
likely O
reversible O
flight O
control O
or O
propulsion O
system O
failure O
; O
and O
( O
4 O
) O
During O
configuration O
changes O
. O

( O
b O
) O
The O
airplane B-asset
must O
be O
able O
to O
complete O
a O
landing O
without O
causing O
substantial O
damage O
or O
serious O
injury O
using O
the O
steepest O
approved O
approach O
gradient O
procedures O
and O
providing O
a O
reasonable O
margin B-parameter
below O
Vref O
or O
above O
approach O
angle B-parameter
of I-parameter
attack I-parameter
. O

( O
c O
) O
VMC O
is O
the O
calibrated O
airspeed B-parameter
at O
which O
, O

following O
the O
sudden O
critical O
loss O
of O
thrust B-parameter
, O

it O
is O
possible O
to O
maintain O
control O
of O
the O
airplane B-asset
. O

For O
multiengine O
airplanes B-asset
, O

the O
applicant O
must O
determine O
VMC O
, O

if O
applicable O
, O

for O
the O
most O
critical O
configurations O
used O
in O
takeoff O
and O
landing O
operations O
. O

( O
d O
) O
If O
the O
applicant O
requests O
certification O
of O
an O
airplane B-asset
for O
aerobatics O
, O

the O
applicant O
must O
demonstrate O
those O
aerobatic O
maneuvers O
for O
which O
certification O
is O
requested O
and O
determine O
entry O
speeds B-parameter
. O

( O
a O
) O
The O
airplane B-asset
must O
maintain B-parameter
lateral I-parameter
and O
directional B-parameter
trim I-parameter
without O
further O
force O
upon O
, O

or O
movement O
of O
, O

the O
primary B-control
flight I-control
controls I-control
or O
corresponding B-control
trim I-control
controls I-control
by O
the O
pilot O
, O

or O
the O
flight B-system
control I-system
system I-system
, O

under O
the O
following O
conditions O
: O
( O
1 O
) O
For O
levels O
1 O
, O

2 O
, O

and O
3 O
airplanes B-asset
in O
cruise O
. O

( O
2 O
) O
For O
level O
4 O
airplanes B-asset
in O
normal O
operations O
. O

( O
b O
) O
The O
airplane B-asset
must O
maintain O
longitudinal O
trim O
without O
further O
force O
upon O
, O

or O
movement O
of O
, O

the O
primary B-control
flight I-control
controls I-control
or O
corresponding B-control
trim I-control
controls I-control
by O
the O
pilot O
, O

or O
the O
flight B-system
control I-system
system I-system
, O

under O
the O
following O
conditions O
: O
14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2130 O
14 O
CFR O
23 O
. O

2140 O
( O
b O
) O
( O
enhanced O
display O
) O
page O
10 O
of O
31 O
§ O
23 O
. O

2145 O
Stability O
. O

§ O
23 O
. O

2150 O
Stall O
characteristics O
, O

stall O
warning O
, O

and O
spins O
. O

§ O
23 O
. O

2155 O
Ground O
and O
water O
handling O
characteristics O
. O

For O
airplanes B-asset
intended O
for O
operation O
on O
land O
or O
water O
, O

the O
airplane B-asset
must O
have O
controllable O
longitudinal O
and O
directional O
handling O
characteristics O
during O
taxi O
, O

takeoff O
, O

and O
landing O
operations O
. O

§ O
23 O
. O

2160 O
Vibration O
, O

buffeting O
, O

and O
high O
- O
speed O
characteristics O
. O

( O
1 O
) O
Climb O
. O

( O
2 O
) O
Level O
flight O
. O

( O
3 O
) O
Descent O
. O

( O
4 O
) O
Approach O
. O

( O
c O
) O
Residual O
control O
forces O
must O
not O
fatigue O
or O
distract O
the O
pilot O
during O
normal O
operations O
of O
the O
airplane O
and O
likely O
abnormal O
or O
emergency O
operations O
, O

including O
a O
critical O
loss O
of O
thrust O
on O
multiengine O
airplanes O
. O

( O
a O
) O
Airplanes B-asset
not O
certified O
for O
aerobatics O
must O
— O
( O
1 O
) O
Have O
static B-parameter
longitudinal I-parameter
, O

lateral O
, O

and O
directional B-parameter
stability I-parameter
in O
normal O
operations O
; O
( O
2 O
) O
Have O
dynamic B-parameter
short I-parameter
period I-parameter
and O
Dutch B-parameter
roll I-parameter
stability I-parameter
in O
normal O
operations O
; O
and O
( O
3 O
) O
Provide O
stable O
control O
force O
feedback O
throughout O
the O
operating O
envelope O
. O

( O
b O
) O
No O
airplane B-asset
may O
exhibit O
any O
divergent B-parameter
longitudinal I-parameter
stability I-parameter
characteristic O
so O
unstable O
as O
to O
increase O
the O
pilot O
' O
s O
workload O
or O
otherwise O
endanger O
the O
airplane B-asset
and O
its O
occupants O
. O

( O
a O
) O
The O
airplane B-asset
must O
have O
controllable O
stall O
characteristics O
in O
straight O
flight O
, O

turning O
flight O
, O

and O
accelerated O
turning O
flight O
with O
a O
clear O
and O
distinctive O
stall O
warning O
that O
provides O
sufficient O
margin O
to O
prevent O
inadvertent O
stalling O
. O

( O
b O
) O
Single O
- O
engine O
airplanes B-asset
, O

not O
certified O
for O
aerobatics O
, O

must O
not O
have O
a O
tendency O
to O
inadvertently O
depart O
controlled O
flight O
. O

( O
c O
) O
Levels O
1 O
and O
2 O
multiengine O
airplanes B-asset
, O

not O
certified O
for O
aerobatics O
, O

must O
not O
have O
a O
tendency O
to O
inadvertently O
depart O
controlled O
flight O
from O
thrust B-parameter
asymmetry O
after O
a O
critical O
loss O
of O
thrust B-parameter
. O

( O
d O
) O
Airplanes B-asset
certified O
for O
aerobatics O
that O
include O
spins O
must O
have O
controllable O
stall O
characteristics O
and O
the O
ability O
to O
recover O
within O
one O
and O
one O
- O
half O
additional O
turns O
after O
initiation O
of O
the O
first O
control O
action O
from O
any O
point O
in O
a O
spin O
, O

not O
exceeding O
six O
turns O
or O
any O
greater O
number O
of O
turns O
for O
which O
certification O
is O
requested O
, O

while O
remaining O
within O
the O
operating O
limitations O
of O
the O
airplane B-asset
. O

( O
e O
) O
Spin O
characteristics O
in O
airplanes B-asset
certified O
for O
aerobatics O
that O
includes O
spins O
must O
recover O
without O
exceeding O
limitations O
and O
may O
not O
result O
in O
unrecoverable O
spins O
— O
( O
1 O
) O
With O
any O
typical O
use O
of O
the O
flight O
or O
engine B-control
power I-control
controls I-control
; O
or O
( O
2 O
) O
Due O
to O
pilot O
disorientation O
or O
incapacitation O
. O

( O
a O
) O
Vibration O
and O
buffeting O
, O

for O
operations O
up O
to O
VD O
/ O
MD O
, O

must O
not O
interfere O
with O
the O
control O
of O
the O
airplane B-asset
or O
cause O
excessive O
fatigue O
to O
the O
flightcrew O
. O

Stall O
warning O
buffet O
within O
these O
limits O
is O
allowable O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2140 O
( O
b O
) O
( O
1 O
) O
14 O
CFR O
23 O
. O

2160 O
( O
a O
) O
( O
enhanced O
display O
) O
page O
11 O
of O
31 O
§ O
23 O
. O

2165 O
Performance O
and O
flight O
characteristics O
requirements O
for O
flight O
in O
icing O
conditions O
. O

[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
Subpart O
C O
— O
Structures O
§ O
23 O
. O

2200 O
Structural B-parameter
design I-parameter
envelope I-parameter
. O

The O
applicant O
must O
determine O
the O
structural B-parameter
design I-parameter
envelope I-parameter
, O

which O
describes O
the O
range O
and O
limits O
of O
airplane B-asset
design O
and O
operational O
parameters O
for O
which O
the O
applicant O
will O
show O
compliance O
with O
the O
requirements O
of O
this O
subpart O
. O

The O
applicant O
must O
account O
for O
all O
airplane B-asset
design O
and O
operational O
parameters O
that O
affect O
structural B-parameter
loads I-parameter
, O

strength O
, O

durability O
, O

and O
aeroelasticity O
, O

including O
: O
( O
b O
) O
For O
high O
- O
speed O
airplanes B-asset
and O
all O
airplanes B-asset
with O
a O
maximum B-parameter
operating I-parameter
altitude I-parameter
greater O
than O
25 O
, O

000 O
feet B-measurement
( O
7 O
, O

620 O
meters B-measurement
) O
pressure B-parameter
altitude I-parameter
, O

there O
must O
be O
no O
perceptible O
buffeting O
in O
cruise O
configuration O
at O
1g O
and O
at O
any O
speed B-parameter
up O
to O
VMO O
/ O
MMO O
, O

except O
stall O
buffeting O
. O

( O
c O
) O
For O
high O
- O
speed O
airplanes B-asset
, O

the O
applicant O
must O
determine O
the O
positive O
maneuvering B-parameter
load I-parameter
factors I-parameter
at O
which O
the O
onset O
of O
perceptible O
buffet O
occurs O
in O
the O
cruise O
configuration O
within O
the O
operational B-parameter
envelope I-parameter
. O

Likely O
inadvertent O
excursions O
beyond O
this O
boundary O
must O
not O
result O
in O
structural O
damage O
. O

( O
d O
) O
High O
- O
speed O
airplanes B-asset
must O
have O
recovery O
characteristics O
that O
do O
not O
result O
in O
structural O
damage O
or O
loss O
of O
control O
, O

beginning O
at O
any O
likely O
speed B-parameter
up O
to O
VMO O
/ O
MMO O
, O

following O
— O
( O
1 O
) O
An O
inadvertent O
speed B-parameter
increase O
; O
and O
( O
2 O
) O
A O
high O
- O
speed O
trim O
upset O
for O
airplanes B-asset
where O
dynamic B-parameter
pressure I-parameter
can O
impair O
the O
longitudinal B-system
trim I-system
system I-system
operation O
. O

( O
a O
) O
An O
applicant O
who O
requests O
certification O
for O
flight O
in O
icing O
conditions O
defined O
in O
part O
1 O
of O
appendix O
C O
to O
part O
25 O
of O
this O
chapter O
, O

or O
an O
applicant O
who O
requests O
certification O
for O
flight O
in O
these O
icing O
conditions O
and O
any O
additional O
atmospheric O
icing O
conditions O
, O

must O
show O
the O
following O
in O
the O
icing O
conditions O
for O
which O
certification O
is O
requested O
under O
normal O
operation O
of O
the O
ice B-system
protection I-system
system I-system
( O
s O
) O
: O
( O
1 O
) O
Compliance O
with O
each O
requirement O
of O
this O
subpart O
, O

except O
those O
applicable O
to O
spins O
and O
any O
that O
must O
be O
demonstrated O
at O
speeds B-parameter
in O
excess O
of O
— O
( O
i O
) O
250 O
KCAS O
; O
( O
ii O
) O
VMO O
/ O
MMO O
or O
VNE O
; O
or O
( O
iii O
) O
A O
speed B-parameter
at O
which O
the O
applicant O
demonstrates O
the O
airframe B-system
will O
be O
free O
of O
ice O
accretion O
. O

( O
2 O
) O
The O
means O
by O
which O
stall O
warning O
is O
provided O
to O
the O
pilot O
for O
flight O
in O
icing O
conditions O
and O
non O
- O
icing O
conditions O
is O
the O
same O
. O

( O
b O
) O
If O
an O
applicant O
requests O
certification O
for O
flight O
in O
icing O
conditions O
, O

the O
applicant O
must O
provide O
a O
means O
to O
detect O
any O
icing O
conditions O
for O
which O
certification O
is O
not O
requested O
and O
show O
the O
airplane O
' O
s O
ability O
to O
avoid O
or O
exit O
those O
conditions O
. O

( O
c O
) O
The O
applicant O
must O
develop O
an O
operating O
limitation O
to O
prohibit O
intentional O
flight O
, O

including O
takeoff O
and O
landing O
, O

into O
icing O
conditions O
for O
which O
the O
airplane O
is O
not O
certified O
to O
operate O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2160 O
( O
b O
) O
14 O
CFR O
23 O
. O

2200 O
( O
enhanced O
display O
) O
page O
12 O
of O
31 O
[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
§ O
23 O
. O

2205 O
Interaction O
of O
systems O
and O
structures O
. O

For O
airplanes B-asset
equipped O
with O
systems O
that O
modify O
structural O
performance O
, O

alleviate O
the O
impact O
of O
this O
subpart O
' O
s O
requirements O
, O

or O
provide O
a O
means O
of O
compliance O
with O
this O
subpart O
, O

the O
applicant O
must O
account O
for O
the O
influence O
and O
failure O
of O
these O
systems O
when O
showing O
compliance O
with O
the O
requirements O
of O
this O
subpart O
. O

STRUCTURAL B-parameter
LOADS I-parameter
§ O
23 O
. O

2210 O
Structural B-parameter
design I-parameter
loads I-parameter
. O

§ O
23 O
. O

2215 O
Flight B-parameter
load I-parameter
conditions O
. O

The O
applicant O
must O
determine O
the O
structural B-parameter
design I-parameter
loads I-parameter
resulting O
from O
the O
following O
flight O
conditions O
: O
( O
a O
) O
Structural O
design B-parameter
airspeeds I-parameter
, O

landing B-parameter
descent I-parameter
speeds I-parameter
, O

and O
any O
other O
airspeed B-parameter
limitation O
at O
which O
the O
applicant O
must O
show O
compliance O
to O
the O
requirements O
of O
this O
subpart O
. O

The O
structural B-parameter
design I-parameter
airspeeds I-parameter
must O
— O
( O
1 O
) O
Be O
sufficiently O
greater O
than O
the O
stalling B-parameter
speed I-parameter
of O
the O
airplane B-asset
to O
safeguard O
against O
loss O
of O
control O
in O
turbulent O
air O
; O
and O
( O
2 O
) O
Provide O
sufficient O
margin O
for O
the O
establishment O
of O
practical O
operational B-parameter
limiting I-parameter
airspeeds I-parameter
. O

( O
b O
) O
Design O
maneuvering B-parameter
load I-parameter
factors I-parameter
not O
less O
than O
those O
, O

which O
service O
history O
shows O
, O

may O
occur O
within O
the O
structural B-parameter
design I-parameter
envelope I-parameter
. O

( O
c O
) O
Inertial O
properties O
including O
weight B-parameter
, O

center B-parameter
of I-parameter
gravity I-parameter
, O

and O
mass B-parameter
moments I-parameter
of I-parameter
inertia I-parameter
, O

accounting O
for O
— O
( O
1 O
) O
Each O
critical B-parameter
weight I-parameter
from O
the O
airplane B-asset
empty B-parameter
weight I-parameter
to O
the O
maximum B-parameter
weight I-parameter
; O
and O
( O
2 O
) O
The O
weight B-parameter
and O
distribution O
of O
occupants O
, O

payload O
, O

and O
fuel O
. O

( O
d O
) O
Characteristics O
of O
airplane B-asset
control B-system
systems I-system
, O

including O
range O
of O
motion O
and O
tolerances O
for O
control O
surfaces O
, O

high O
- O
lift O
devices O
, O

or O
other O
moveable O
surfaces O
. O

( O
e O
) O
Each O
critical B-parameter
altitude I-parameter
up O
to O
the O
maximum B-parameter
altitude I-parameter
. O

( O
a O
) O
The O
applicant O
must O
: O
( O
1 O
) O
Determine O
the O
applicable O
structural B-parameter
design I-parameter
loads I-parameter
resulting O
from O
likely O
externally O
or O
internally O
applied O
pressures B-parameter
, O

forces B-parameter
, O

or O
moments B-parameter
that O
may O
occur O
in O
flight O
, O

ground O
and O
water O
operations O
, O

ground O
and O
water O
handling O
, O

and O
while O
the O
airplane B-asset
is O
parked O
or O
moored O
. O

( O
2 O
) O
Determine O
the O
loads B-parameter
required O
by O
paragraph O
( O
a O
) O
( O
1 O
) O
of O
this O
section O
at O
all O
critical O
combinations O
of O
parameters O
, O

on O
and O
within O
the O
boundaries O
of O
the O
structural B-parameter
design I-parameter
envelope I-parameter
. O

( O
b O
) O
The O
magnitude O
and O
distribution O
of O
the O
applicable O
structural B-parameter
design I-parameter
loads I-parameter
required O
by O
this O
section O
must O
be O
based O
on O
physical O
principles O
. O

( O
a O
) O
Atmospheric O
gusts O
where O
the O
magnitude O
and O
gradient O
of O
these O
gusts O
are O
based O
on O
measured O
gust O
statistics O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2200 O
( O
a O
) O
14 O
CFR O
23 O
. O

2215 O
( O
a O
) O
( O
enhanced O
display O
) O
page O
13 O
of O
31 O
§ O
23 O
. O

2220 O
Ground O
and O
water O
load O
conditions O
. O

The O
applicant O
must O
determine O
the O
structural B-parameter
design I-parameter
loads I-parameter
resulting O
from O
taxi O
, O

takeoff O
, O

landing O
, O

and O
handling O
conditions O
on O
the O
applicable O
surface O
in O
normal O
and O
adverse B-parameter
attitudes I-parameter
and O
configurations O
. O

§ O
23 O
. O

2225 O
Component O
loading O
conditions O
. O

The O
applicant O
must O
determine O
the O
structural B-parameter
design I-parameter
loads I-parameter
acting O
on O
: O
§ O
23 O
. O

2230 O
Limit O
and O
ultimate B-parameter
loads I-parameter
. O

The O
applicant O
must O
determine O
— O
STRUCTURAL O
PERFORMANCE O
( O
b O
) O
Symmetric O
and O
asymmetric O
maneuvers O
. O

( O
c O
) O
Asymmetric O
thrust B-parameter
resulting O
from O
the O
failure O
of O
a O
powerplant O
unit O
. O

( O
a O
) O
Each O
engine B-module
mount I-module
and O
its O
supporting O
structure O
such O
that O
both O
are O
designed O
to O
withstand O
loads O
resulting O
from O
— O
( O
1 O
) O
Powerplant B-module
operation I-module
combined O
with O
flight B-parameter
gust I-parameter
and O
maneuver B-parameter
loads I-parameter
; O
and O
( O
2 O
) O
For O
non O
- O
reciprocating O
powerplants B-module
, O

sudden O
powerplant B-module
stoppage O
. O

( O
b O
) O
Each O
flight O
control O
and O
high O
- O
lift O
surface O
, O

their O
associated O
system O
and O
supporting O
structure O
resulting O
from O
— O
( O
1 O
) O
The O
inertia O
of O
each O
surface O
and O
mass O
balance O
attachment O
; O
( O
2 O
) O
Flight O
gusts O
and O
maneuvers O
; O
( O
3 O
) O
Pilot O
or O
automated B-system
system I-system
inputs O
; O
( O
4 O
) O
System O
induced O
conditions O
, O

including O
jamming O
and O
friction O
; O
and O
( O
5 O
) O
Taxi O
, O

takeoff O
, O

and O
landing O
operations O
on O
the O
applicable O
surface O
, O

including O
downwind O
taxi O
and O
gusts O
occurring O
on O
the O
applicable O
surface O
. O

( O
c O
) O
A O
pressurized O
cabin O
resulting O
from O
the O
pressurization O
differential O
— O
( O
1 O
) O
From O
zero O
up O
to O
the O
maximum O
relief O
pressure O
combined O
with O
gust O
and O
maneuver B-parameter
loads I-parameter
; O
( O
2 O
) O
From O
zero O
up O
to O
the O
maximum O
relief O
pressure O
combined O
with O
ground B-parameter
and I-parameter
water I-parameter
loads I-parameter
if O
the O
airplane B-asset
may O
land O
with O
the O
cabin O
pressurized O
; O
and O
( O
3 O
) O
At O
the O
maximum B-parameter
relief I-parameter
pressure I-parameter
multiplied O
by O
1 O
. O

33 O
, O

omitting O
all O
other O
loads O
. O

( O
a O
) O
The O
limit B-parameter
loads I-parameter
, O

which O
are O
equal O
to O
the O
structural B-parameter
design I-parameter
loads I-parameter
unless O
otherwise O
specified O
elsewhere O
in O
this O
part O
; O
and O
( O
b O
) O
The O
ultimate B-parameter
loads I-parameter
, O

which O
are O
equal O
to O
the O
limit B-parameter
loads I-parameter
multiplied O
by O
a O
1 O
. O

5 O
factor O
of O
safety O
unless O
otherwise O
specified O
elsewhere O
in O
this O
part O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2215 O
( O
b O
) O
14 O
CFR O
23 O
. O

2230 O
( O
b O
) O
( O
enhanced O
display O
) O
page O
14 O
of O
31 O
§ O
23 O
. O

2235 O
Structural B-parameter
strength I-parameter
. O

The O
structure O
must O
support O
: O
§ O
23 O
. O

2240 O
Structural B-parameter
durability I-parameter
. O

§ O
23 O
. O

2245 O
Aeroelasticity B-parameter
. O

DESIGN O
§ O
23 O
. O

2250 O
Design O
and O
construction O
principles O
. O

( O
a O
) O
Limit B-parameter
loads I-parameter
without O
— O
( O
1 O
) O
Interference O
with O
the O
safe O
operation O
of O
the O
airplane B-asset
; O
and O
( O
2 O
) O
Detrimental O
permanent O
deformation O
. O

( O
b O
) O
Ultimate B-parameter
loads I-parameter
. O

( O
a O
) O
The O
applicant O
must O
develop O
and O
implement O
inspections O
or O
other O
procedures O
to O
prevent O
structural O
failures O
due O
to O
foreseeable O
causes O
of O
strength O
degradation O
, O

which O
could O
result O
in O
serious O
or O
fatal O
injuries O
, O

or O
extended O
periods O
of O
operation O
with O
reduced O
safety O
margins O
. O

Each O
of O
the O
inspections O
or O
other O
procedures O
developed O
under O
this O
section O
must O
be O
included O
in O
the O
Airworthiness O
Limitations O
Section O
of O
the O
Instructions O
for O
Continued O
Airworthiness O
required O
by O
§ O
23 O
. O

1529 O
. O

( O
b O
) O
For O
Level O
4 O
airplanes B-asset
, O

the O
procedures O
developed O
for O
compliance O
with O
paragraph O
( O
a O
) O
of O
this O
section O
must O
be O
capable O
of O
detecting O
structural O
damage O
before O
the O
damage O
could O
result O
in O
structural O
failure O
. O

( O
c O
) O
For O
pressurized O
airplanes B-asset
: O
( O
1 O
) O
The O
airplane B-asset
must O
be O
capable O
of O
continued O
safe O
flight O
and O
landing O
following O
a O
sudden O
release O
of O
cabin B-parameter
pressure I-parameter
, O

including O
sudden O
releases O
caused O
by O
door O
and O
window O
failures O
. O

( O
2 O
) O
For O
airplanes B-asset
with O
maximum B-parameter
operating I-parameter
altitude I-parameter
greater O
than O
41 O
, O

000 O
feet B-measurement
, O

the O
procedures O
developed O
for O
compliance O
with O
paragraph O
( O
a O
) O
of O
this O
section O
must O
be O
capable O
of O
detecting O
damage O
to O
the O
pressurized O
cabin O
structure O
before O
the O
damage O
could O
result O
in O
rapid O
decompression O
that O
would O
result O
in O
serious O
or O
fatal O
injuries O
. O

( O
d O
) O
The O
airplane B-asset
must O
be O
designed O
to O
minimize O
hazards O
to O
the O
airplane B-asset
due O
to O
structural O
damage O
caused O
by O
high O
- O
energy O
fragments O
from O
an O
uncontained O
engine B-system
or O
rotating O
machinery O
failure O
. O

( O
a O
) O
The O
airplane B-asset
must O
be O
free O
from O
flutter O
, O

control O
reversal O
, O

and O
divergence O
— O
( O
1 O
) O
At O
all O
speeds B-parameter
within O
and O
sufficiently O
beyond O
the O
structural B-parameter
design I-parameter
envelope I-parameter
; O
( O
2 O
) O
For O
any O
configuration O
and O
condition O
of O
operation O
; O
( O
3 O
) O
Accounting O
for O
critical B-parameter
degrees I-parameter
of I-parameter
freedom I-parameter
; O
and O
( O
4 O
) O
Accounting O
for O
any O
critical O
failures O
or O
malfunctions O
. O

( O
b O
) O
The O
applicant O
must O
establish O
tolerances O
for O
all O
quantities O
that O
affect O
flutter B-parameter
. O

( O
a O
) O
The O
applicant O
must O
design O
each O
part O
, O

article O
, O

and O
assembly O
for O
the O
expected O
operating O
conditions O
of O
the O
airplane O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2235 O
14 O
CFR O
23 O
. O

2250 O
( O
a O
) O
( O
enhanced O
display O
) O
page O
15 O
of O
31 O
§ O
23 O
. O

2255 O
Protection O
of O
structure O
. O

[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
§ O
23 O
. O

2260 O
Materials O
and O
processes O
. O

( O
b O
) O
Design O
data O
must O
adequately O
define O
the O
part O
, O

article O
, O

or O
assembly O
configuration O
, O

its O
design O
features O
, O

and O
any O
materials O
and O
processes O
used O
. O

( O
c O
) O
The O
applicant O
must O
determine O
the O
suitability O
of O
each O
design O
detail O
and O
part O
having O
an O
important O
bearing O
on O
safety O
in O
operations O
. O

( O
d O
) O
The O
control B-system
system I-system
must O
be O
free O
from O
jamming O
, O

excessive O
friction O
, O

and O
excessive O
deflection O
when O
the O
airplane O
is O
subjected O
to O
expected O
limit B-parameter
airloads I-parameter
. O

( O
e O
) O
Doors O
, O

canopies O
, O

and O
exits O
must O
be O
protected O
against O
inadvertent O
opening O
in O
flight O
, O

unless O
shown O
to O
create O
no O
hazard O
when O
opened O
in O
flight O
. O

( O
a O
) O
The O
applicant O
must O
protect O
each O
part O
of O
the O
airplane B-asset
, O

including O
small O
parts O
such O
as O
fasteners B-component
, O

against O
deterioration O
or O
loss O
of O
strength O
due O
to O
any O
cause O
likely O
to O
occur O
in O
the O
expected O
operational O
environment O
. O

( O
b O
) O
Each O
part O
of O
the O
airplane O
must O
have O
adequate O
provisions O
for O
ventilation O
and O
drainage O
. O

( O
c O
) O
For O
each O
part O
that O
requires O
maintenance O
, O

preventive O
maintenance O
, O

or O
servicing O
, O

the O
applicant O
must O
incorporate O
a O
means O
into O
the O
airplane B-asset
design O
to O
allow O
such O
actions O
to O
be O
accomplished O
. O

( O
a O
) O
The O
applicant O
must O
determine O
the O
suitability O
and O
durability O
of O
materials O
used O
for O
parts O
, O

articles O
, O

and O
assemblies O
, O

accounting O
for O
the O
effects O
of O
likely O
environmental O
conditions O
expected O
in O
service O
, O

the O
failure O
of O
which O
could O
prevent O
continued O
safe O
flight O
and O
landing O
. O

( O
b O
) O
The O
methods O
and O
processes O
of O
fabrication O
and O
assembly O
used O
must O
produce O
consistently O
sound O
structures O
. O

If O
a O
fabrication O
process O
requires O
close O
control O
to O
reach O
this O
objective O
, O

the O
applicant O
must O
perform O
the O
process O
under O
an O
approved O
process O
specification O
. O

( O
c O
) O
Except O
as O
provided O
in O
paragraphs O
( O
f O
) O
and O
( O
g O
) O
of O
this O
section O
, O

the O
applicant O
must O
select O
design O
values O
that O
ensure O
material O
strength O
with O
probabilities O
that O
account O
for O
the O
criticality O
of O
the O
structural O
element O
. O

Design O
values O
must O
account O
for O
the O
probability O
of O
structural O
failure O
due O
to O
material O
variability O
. O

( O
d O
) O
If O
material O
strength O
properties O
are O
required O
, O

a O
determination O
of O
those O
properties O
must O
be O
based O
on O
sufficient O
tests O
of O
material O
meeting O
specifications O
to O
establish O
design O
values O
on O
a O
statistical O
basis O
. O

( O
e O
) O
If O
thermal O
effects O
are O
significant O
on O
a O
critical O
component O
or O
structure O
under O
normal O
operating O
conditions O
, O

the O
applicant O
must O
determine O
those O
effects O
on O
allowable O
stresses O
used O
for O
design O
. O

( O
f O
) O
Design O
values O
, O

greater O
than O
the O
minimums O
specified O
by O
this O
section O
, O

may O
be O
used O
, O

where O
only O
guaranteed O
minimum O
values O
are O
normally O
allowed O
, O

if O
a O
specimen O
of O
each O
individual O
item O
is O
tested O
before O
use O
to O
determine O
that O
the O
actual O
strength B-parameter
properties I-parameter
of O
that O
particular O
item O
will O
equal O
or O
exceed O
those O
used O
in O
the O
design O
. O

( O
g O
) O
An O
applicant O
may O
use O
other O
material O
design O
values O
if O
approved O
by O
the O
Administrator O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes O
14 O
CFR O
23 O
. O

2250 O
( O
b O
) O
14 O
CFR O
23 O
. O

2260 O
( O
g O
) O
( O
enhanced O
display O
) O
page O
16 O
of O
31 O
§ O
23 O
. O

2265 O
Special O
factors O
of O
safety O
. O

STRUCTURAL O
OCCUPANT O
PROTECTION O
§ O
23 O
. O

2270 O
Emergency O
conditions O
. O

( O
a O
) O
The O
applicant O
must O
determine O
a O
special O
factor B-parameter
of I-parameter
safety I-parameter
for O
each O
critical O
design O
value O
for O
each O
part O
, O

article O
, O

or O
assembly O
for O
which O
that O
critical O
design O
value O
is O
uncertain O
, O

and O
for O
each O
part O
, O

article O
, O

or O
assembly O
that O
is O
— O
( O
1 O
) O
Likely O
to O
deteriorate O
in O
service O
before O
normal O
replacement O
; O
or O
( O
2 O
) O
Subject O
to O
appreciable O
variability O
because O
of O
uncertainties O
in O
manufacturing O
processes O
or O
inspection O
methods O
. O

( O
b O
) O
The O
applicant O
must O
determine O
a O
special O
factor O
of O
safety O
using O
quality O
controls O
and O
specifications O
that O
account O
for O
each O
— O
( O
1 O
) O
Type O
of O
application O
; O
( O
2 O
) O
Inspection O
method O
; O
( O
3 O
) O
Structural O
test O
requirement O
; O
( O
4 O
) O
Sampling O
percentage O
; O
and O
( O
5 O
) O
Process O
and O
material O
control O
. O

( O
c O
) O
The O
applicant O
must O
multiply O
the O
highest O
pertinent O
special O
factor O
of O
safety O
in O
the O
design O
for O
each O
part O
of O
the O
structure O
by O
each O
limit O
and O
ultimate B-parameter
load I-parameter
, O

or O
ultimate O
load O
only O
, O

if O
there O
is O
no O
corresponding O
limit O
load O
, O

such O
as O
occurs O
with O
emergency O
condition O
loading O
. O

( O
a O
) O
The O
airplane B-asset
, O

even O
when O
damaged O
in O
an O
emergency O
landing O
, O

must O
protect O
each O
occupant O
against O
injury O
that O
would O
preclude O
egress O
when O
— O
( O
1 O
) O
Properly O
using O
safety O
equipment O
and O
features O
provided O
for O
in O
the O
design O
; O
( O
2 O
) O
The O
occupant O
experiences O
ultimate B-parameter
static I-parameter
inertia I-parameter
loads I-parameter
likely O
to O
occur O
in O
an O
emergency O
landing O
; O
and O
( O
3 O
) O
Items O
of O
mass O
, O

including O
engines B-system
or O
auxiliary B-module
power I-module
units I-module
( O
APUs O
) O
, O

within O
or O
aft O
of O
the O
cabin B-system
, O

that O
could O
injure O
an O
occupant O
, O

experience O
ultimate B-parameter
static I-parameter
inertia I-parameter
loads I-parameter
likely O
to O
occur O
in O
an O
emergency O
landing O
. O

( O
b O
) O
The O
emergency O
landing O
conditions O
specified O
in O
paragraph O
( O
a O
) O
( O
1 O
) O
and O
( O
a O
) O
( O
2 O
) O
of O
this O
section O
, O

must O
— O
( O
1 O
) O
Include O
dynamic O
conditions O
that O
are O
likely O
to O
occur O
in O
an O
emergency O
landing O
; O
and O
( O
2 O
) O
Not O
generate O
loads B-parameter
experienced O
by O
the O
occupants O
, O

which O
exceed O
established O
human O
injury O
criteria O
for O
human O
tolerance O
due O
to O
restraint O
or O
contact O
with O
objects O
in O
the O
airplane O
. O

( O
c O
) O
The O
airplane O
must O
provide O
protection O
for O
all O
occupants O
, O

accounting O
for O
likely O
flight O
, O

ground O
, O

and O
emergency O
landing O
conditions O
. O

( O
d O
) O
Each O
occupant B-system
protection I-system
system I-system
must O
perform O
its O
intended O
function O
and O
not O
create O
a O
hazard O
that O
could O
cause O
a O
secondary O
injury O
to O
an O
occupant O
. O

The O
occupant B-system
protection I-system
system I-system
must O
not O
prevent O
occupant O
egress O
or O
interfere O
with O
the O
operation O
of O
the O
airplane B-asset
when O
not O
in O
use O
. O

( O
e O
) O
Each O
baggage B-system
and O
cargo B-system
compartment O
must O
— O
14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2265 O
14 O
CFR O
23 O
. O

2270 O
( O
e O
) O
( O
enhanced O
display O
) O
page O
17 O
of O
31 O
Subpart O
D O
— O
Design O
and O
Construction O
§ O
23 O
. O

2300 O
Flight B-system
control I-system
systems I-system
. O

§ O
23 O
. O

2305 O
Landing B-system
gear I-system
systems I-system
. O

§ O
23 O
. O

2310 O
Buoyancy O
for O
seaplanes B-asset
and O
amphibians O
. O

Airplanes B-asset
intended O
for O
operations O
on O
water O
, O

must O
— O
( O
1 O
) O
Be O
designed O
for O
its O
maximum B-parameter
weight I-parameter
of O
contents O
and O
for O
the O
critical B-parameter
load I-parameter
distributions O
at O
the O
maximum B-parameter
load I-parameter
factors I-parameter
corresponding O
to O
the O
flight O
and O
ground B-parameter
load I-parameter
conditions O
determined O
under O
this O
part O
; O
( O
2 O
) O
Have O
a O
means O
to O
prevent O
the O
contents O
of O
the O
compartment O
from O
becoming O
a O
hazard O
by O
impacting O
occupants O
or O
shifting O
; O
and O
( O
3 O
) O
Protect O
any O
controls B-system
, O

wiring O
, O

lines O
, O

equipment O
, O

or O
accessories O
whose O
damage O
or O
failure O
would O
affect O
safe O
operations O
. O

( O
a O
) O
The O
applicant O
must O
design O
airplane B-asset
flight B-system
control I-system
systems I-system
to O
: O
( O
1 O
) O
Operate O
easily O
, O

smoothly O
, O

and O
positively O
enough O
to O
allow O
proper O
performance O
of O
their O
functions O
. O

( O
2 O
) O
Protect O
against O
likely O
hazards O
. O

( O
b O
) O
The O
applicant O
must O
design O
trim B-system
systems I-system
, O

if O
installed O
, O

to O
: O
( O
1 O
) O
Protect O
against O
inadvertent O
, O

incorrect O
, O

or O
abrupt O
trim O
operation O
. O

( O
2 O
) O
Provide O
a O
means O
to O
indicate O
— O
( O
i O
) O
The O
direction O
of O
trim O
control O
movement O
relative O
to O
airplane B-asset
motion O
; O
( O
ii O
) O
The O
trim B-parameter
position I-parameter
with O
respect O
to O
the O
trim B-parameter
range I-parameter
; O
( O
iii O
) O
The O
neutral O
position O
for O
lateral O
and O
directional B-parameter
trim I-parameter
; O
and O
( O
iv O
) O
The O
range O
for O
takeoff O
for O
all O
applicant O
requested O
center B-parameter
of I-parameter
gravity I-parameter
ranges O
and O
configurations O
. O

( O
a O
) O
The O
landing B-system
gear I-system
must O
be O
designed O
to O
— O
( O
1 O
) O
Provide O
stable O
support O
and O
control O
to O
the O
airplane O
during O
surface O
operation O
; O
and O
( O
2 O
) O
Account O
for O
likely O
system O
failures O
and O
likely O
operation O
environments O
( O
including O
anticipated O
limitation O
exceedances O
and O
emergency O
procedures O
) O
. O

( O
b O
) O
All O
airplanes B-asset
must O
have O
a O
reliable O
means O
of O
stopping O
the O
airplane B-asset
with O
sufficient O
kinetic O
energy O
absorption O
to O
account O
for O
landing O
. O

Airplanes B-asset
that O
are O
required O
to O
demonstrate O
aborted O
takeoff O
capability O
must O
account O
for O
this O
additional O
kinetic O
energy O
. O

( O
c O
) O
For O
airplanes B-asset
that O
have O
a O
system O
that O
actuates O
the O
landing B-system
gear I-system
, O

there O
is O
— O
( O
1 O
) O
A O
positive O
means O
to O
keep O
the O
landing B-system
gear I-system
in O
the O
landing O
position O
; O
and O
( O
2 O
) O
An O
alternative O
means O
available O
to O
bring O
the O
landing O
gear O
in O
the O
landing O
position O
when O
a O
non O
- O
deployed O
system O
position O
would O
be O
a O
hazard O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2270 O
( O
e O
) O
( O
1 O
) O
14 O
CFR O
23 O
. O

2310 O
( O
enhanced O
display O
) O
page O
18 O
of O
31 O
OCCUPANT O
SYSTEM O
DESIGN O
PROTECTION O
§ O
23 O
. O

2315 O
Means O
of O
egress O
and O
emergency O
exits O
. O

[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
§ O
23 O
. O

2320 O
Occupant O
physical O
environment O
. O

FIRE O
AND O
HIGH O
ENERGY O
PROTECTION O
( O
a O
) O
Provide O
buoyancy O
of O
80 O
percent O
in O
excess O
of O
the O
buoyancy O
required O
to O
support O
the O
maximum B-parameter
weight I-parameter
of O
the O
airplane B-asset
in O
fresh O
water O
; O
and O
( O
b O
) O
Have O
sufficient O
margin O
so O
the O
airplane B-asset
will O
stay O
afloat O
at O
rest O
in O
calm O
water O
without O
capsizing O
in O
case O
of O
a O
likely O
float O
or O
hull O
flooding O
. O

( O
a O
) O
With O
the O
cabin O
configured O
for O
takeoff O
or O
landing O
, O

the O
airplane B-asset
is O
designed O
to O
: O
( O
1 O
) O
Facilitate O
rapid O
and O
safe O
evacuation O
of O
the O
airplane B-asset
in O
conditions O
likely O
to O
occur O
following O
an O
emergency O
landing O
, O

excluding O
ditching O
for O
level O
1 O
, O

level O
2 O
, O

and O
single O
- O
engine O
level O
3 O
airplanes B-asset
. O

( O
2 O
) O
Have O
means O
of O
egress O
( O
openings O
, O

exits O
, O

or O
emergency O
exits O
) O
, O

that O
can O
be O
readily O
located O
and O
opened O
from O
the O
inside O
and O
outside O
. O

The O
means O
of O
opening O
must O
be O
simple O
and O
obvious O
and O
marked O
inside O
and O
outside O
the O
airplane O
. O

( O
3 O
) O
Have O
easy O
access O
to O
emergency O
exits O
when O
present O
. O

( O
b O
) O
Airplanes B-asset
approved O
for O
aerobatics O
must O
have O
a O
means O
to O
egress O
the O
airplane B-asset
in O
flight O
. O

( O
a O
) O
The O
applicant O
must O
design O
the O
airplane B-asset
to O
— O
( O
1 O
) O
Allow O
clear O
communication O
between O
the O
flightcrew O
and O
passengers O
; O
( O
2 O
) O
Protect O
the O
pilot O
and O
flight O
controls O
from O
propellers B-system
; O
and O
( O
3 O
) O
Protect O
the O
occupants O
from O
serious O
injury O
due O
to O
damage O
to O
windshields B-component
, O

windows B-component
, O

and O
canopies B-component
. O

( O
b O
) O
For O
level O
4 O
airplanes B-asset
, O

each O
windshield B-component
and O
its O
supporting B-component
structure I-component
directly O
in O
front O
of O
the O
pilot O
must O
withstand O
, O

without O
penetration O
, O

the O
impact O
equivalent O
to O
a O
two O
- O
pound O
bird O
when O
the O
velocity O
of O
the O
airplane B-asset
is O
equal O
to O
the O
airplane B-asset
' O
s O
maximum B-parameter
approach I-parameter
flap I-parameter
speed I-parameter
. O

( O
c O
) O
The O
airplane B-asset
must O
provide O
each O
occupant O
with O
air O
at O
a O
breathable O
pressure O
, O

free O
of O
hazardous O
concentrations O
of O
gases O
, O

vapors O
, O

and O
smoke O
during O
normal O
operations O
and O
likely O
failures O
. O

( O
d O
) O
If O
a O
pressurization B-system
system I-system
is O
installed O
in O
the O
airplane B-asset
, O

it O
must O
be O
designed O
to O
protect O
against O
— O
( O
1 O
) O
Decompression O
to O
an O
unsafe O
level O
; O
and O
( O
2 O
) O
Excessive O
differential O
pressure O
. O

( O
e O
) O
If O
an O
oxygen B-system
system I-system
is O
installed O
in O
the O
airplane B-asset
, O

it O
must O
— O
( O
1 O
) O
Effectively O
provide O
oxygen O
to O
each O
user O
to O
prevent O
the O
effects O
of O
hypoxia O
; O
and O
( O
2 O
) O
Be O
free O
from O
hazards O
in O
itself O
, O

in O
its O
method O
of O
operation O
, O

and O
its O
effect O
upon O
other O
components O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2310 O
( O
a O
) O
14 O
CFR O
23 O
. O

2320 O
( O
e O
) O
( O
2 O
) O
( O
enhanced O
display O
) O
page O
19 O
of O
31 O
§ O
23 O
. O

2325 O
Fire O
protection O
. O

§ O
23 O
. O

2330 O
Fire O
protection O
in O
designated O
fire O
zones O
and O
adjacent O
areas O
. O

( O
a O
) O
The O
following O
materials O
must O
be O
self O
- O
extinguishing O
— O
( O
1 O
) O
Insulation O
on O
electrical B-component
wire I-component
and O
electrical B-component
cable I-component
; O
( O
2 O
) O
For O
levels O
1 O
, O

2 O
, O

and O
3 O
airplanes B-asset
, O

materials O
in O
the O
baggage B-system
and O
cargo B-system
compartments O
inaccessible O
in O
flight O
; O
and O
( O
3 O
) O
For O
level O
4 O
airplanes B-asset
, O

materials O
in O
the O
cockpit B-module
, O

cabin B-system
, O

baggage B-system
, O

and O
cargo B-system
compartments O
. O

( O
b O
) O
The O
following O
materials O
must O
be O
flame O
resistant O
— O
( O
1 O
) O
For O
levels O
1 O
, O

2 O
and O
3 O
airplanes B-asset
, O

materials O
in O
each O
compartment O
accessible O
in O
flight O
; O
and O
( O
2 O
) O
Any O
equipment O
associated O
with O
any O
electrical B-component
cable I-component
installation O
and O
that O
would O
overheat O
in O
the O
event O
of O
circuit O
overload O
or O
fault O
. O

( O
c O
) O
Thermal O
/ O
acoustic O
materials O
in O
the O
fuselage B-system
, O

if O
installed O
, O

must O
not O
be O
a O
flame O
propagation O
hazard O
. O

( O
d O
) O
Sources O
of O
heat O
within O
each O
baggage B-system
and O
cargo B-system
compartment O
that O
are O
capable O
of O
igniting O
adjacent O
objects O
must O
be O
shielded O
and O
insulated O
to O
prevent O
such O
ignition O
. O

( O
e O
) O
For O
level O
4 O
airplanes B-asset
, O

each O
baggage B-system
and O
cargo B-system
compartment O
must O
— O
( O
1 O
) O
Be O
located O
where O
a O
fire O
would O
be O
visible O
to O
the O
pilots O
, O

or O
equipped O
with O
a O
fire B-system
detection I-system
system I-system
and O
warning B-system
system I-system
; O
and O
( O
2 O
) O
Be O
accessible O
for O
the O
manual O
extinguishing O
of O
a O
fire O
, O

have O
a O
built O
- O
in O
fire B-system
extinguishing I-system
system I-system
, O

or O
be O
constructed O
and O
sealed O
to O
contain O
any O
fire O
within O
the O
compartment O
. O

( O
f O
) O
There O
must O
be O
a O
means O
to O
extinguish O
any O
fire O
in O
the O
cabin B-system
such O
that O
— O
( O
1 O
) O
The O
pilot O
, O

while O
seated O
, O

can O
easily O
access O
the O
fire O
extinguishing O
means O
; O
and O
( O
2 O
) O
For O
levels O
3 O
and O
4 O
airplanes B-asset
, O

passengers O
have O
a O
fire O
extinguishing O
means O
available O
within O
the O
passenger O
compartment O
. O

( O
g O
) O
Each O
area O
where O
flammable O
fluids O
or O
vapors O
might O
escape O
by O
leakage O
of O
a O
fluid B-system
system I-system
must O
— O
( O
1 O
) O
Be O
defined O
; O
and O
( O
2 O
) O
Have O
a O
means O
to O
minimize O
the O
probability O
of O
fluid O
and O
vapor O
ignition O
, O

and O
the O
resultant O
hazard O
, O

if O
ignition O
occurs O
. O

( O
h O
) O
Combustion B-module
heater I-module
installations I-module
must O
be O
protected O
from O
uncontained O
fire O
. O

( O
a O
) O
Flight B-control
controls I-control
, O

engine B-module
mounts I-module
, O

and O
other O
flight O
structures O
within O
or O
adjacent O
to O
designated O
fire O
zones O
must O
be O
capable O
of O
withstanding O
the O
effects O
of O
a O
fire O
. O

( O
b O
) O
Engines B-system
in O
a O
designated O
fire O
zone O
must O
remain O
attached O
to O
the O
airplane B-asset
in O
the O
event O
of O
a O
fire O
. O

( O
c O
) O
In O
designated O
fire O
zones O
, O

terminals O
, O

equipment O
, O

and O
electrical O
cables O
used O
during O
emergency O
procedures O
must O
be O
fire O
- O
resistant O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2325 O
14 O
CFR O
23 O
. O

2330 O
( O
c O
) O
( O
enhanced O
display O
) O
page O
20 O
of O
31 O
§ O
23 O
. O

2335 O
Lightning O
protection O
. O

The O
airplane B-asset
must O
be O
protected O
against O
catastrophic O
effects O
from O
lightning O
. O

Subpart O
E O
— O
Powerplant B-system
§ O
23 O
. O

2400 O
Powerplant B-system
installation O
. O

[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
§ O
23 O
. O

2405 O
Automatic O
power O
or O
thrust B-system
control I-system
systems I-system
. O

( O
a O
) O
For O
the O
purpose O
of O
this O
subpart O
, O

the O
airplane B-asset
powerplant B-module
installation I-module
must O
include O
each O
component O
necessary O
for O
propulsion O
, O

which O
affects O
propulsion O
safety O
, O

or O
provides O
auxiliary O
power O
to O
the O
airplane B-asset
. O

( O
b O
) O
Each O
airplane B-asset
engine B-system
and O
propeller B-system
must O
be O
type O
certificated O
, O

except O
for O
engines B-system
and O
propellers B-system
installed O
on O
level O
1 O
low O
- O
speed O
airplanes B-asset
, O

which O
may O
be O
approved O
under O
the O
airplane B-asset
type O
certificate O
in O
accordance O
with O
a O
standard O
accepted O
by O
the O
Administrator O
that O
contains O
airworthiness O
criteria O
the O
Administrator O
has O
found O
appropriate O
and O
applicable O
to O
the O
specific O
design O
and O
intended O
use O
of O
the O
engine B-system
or O
propeller B-system
and O
provides O
a O
level O
of O
safety O
acceptable O
to O
the O
Administrator O
. O

( O
c O
) O
The O
applicant O
must O
construct O
and O
arrange O
each O
powerplant B-module
installation I-module
to O
account O
for O
— O
( O
1 O
) O
Likely O
operating O
conditions O
, O

including O
foreign O
object O
threats O
; O
( O
2 O
) O
Sufficient O
clearance O
of O
moving O
parts O
to O
other O
airplane O
parts O
and O
their O
surroundings O
; O
( O
3 O
) O
Likely O
hazards O
in O
operation O
including O
hazards O
to O
ground O
personnel O
; O
and O
( O
4 O
) O
Vibration O
and O
fatigue O
. O

( O
d O
) O
Hazardous O
accumulations O
of O
fluids O
, O

vapors O
, O

or O
gases O
must O
be O
isolated O
from O
the O
airplane O
and O
personnel O
compartments O
, O

and O
be O
safely O
contained O
or O
discharged O
. O

( O
e O
) O
Powerplant B-component
components I-component
must O
comply O
with O
their O
component O
limitations O
and O
installation O
instructions O
or O
be O
shown O
not O
to O
create O
a O
hazard O
. O

( O
a O
) O
An O
automatic O
power O
or O
thrust B-system
control I-system
system I-system
intended O
for O
in O
- O
flight O
use O
must O
be O
designed O
so O
no O
unsafe O
condition O
will O
result O
during O
normal O
operation O
of O
the O
system O
. O

( O
b O
) O
Any O
single O
failure O
or O
likely O
combination O
of O
failures O
of O
an O
automatic O
power O
or O
thrust B-system
control I-system
system I-system
must O
not O
prevent O
continued O
safe O
flight O
and O
landing O
of O
the O
airplane B-asset
. O

( O
c O
) O
Inadvertent O
operation O
of O
an O
automatic O
power O
or O
thrust B-system
control I-system
system I-system
by O
the O
flightcrew O
must O
be O
prevented O
, O

or O
if O
not O
prevented O
, O

must O
not O
result O
in O
an O
unsafe O
condition O
. O

( O
d O
) O
Unless O
the O
failure O
of O
an O
automatic O
power O
or O
thrust B-system
control I-system
system I-system
is O
extremely O
remote O
, O

the O
system O
must O
— O
( O
1 O
) O
Provide O
a O
means O
for O
the O
flightcrew O
to O
verify O
the O
system O
is O
in O
an O
operating O
condition O
; O
( O
2 O
) O
Provide O
a O
means O
for O
the O
flightcrew O
to O
override O
the O
automatic O
function O
; O
and O
( O
3 O
) O
Prevent O
inadvertent O
deactivation O
of O
the O
system O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2335 O
14 O
CFR O
23 O
. O

2405 O
( O
d O
) O
( O
3 O
) O
( O
enhanced O
display O
) O
page O
21 O
of O
31 O
§ O
23 O
. O

2410 O
Powerplant B-module
installation I-module
hazard O
assessment O
. O

The O
applicant O
must O
assess O
each O
powerplant B-module
separately O
and O
in O
relation O
to O
other O
airplane B-system
systems I-system
and O
installations O
to O
show O
that O
any O
hazard O
resulting O
from O
the O
likely O
failure O
of O
any O
powerplant B-module
system O
, O

component O
, O

or O
accessory O
will O
not O
— O
§ O
23 O
. O

2415 O
Powerplant B-system
ice O
protection O
. O

§ O
23 O
. O

2420 O
Reversing B-system
systems I-system
. O

Each O
reversing B-system
system I-system
must O
be O
designed O
so O
that O
— O
§ O
23 O
. O

2425 O
Powerplant B-system
operational O
characteristics O
. O

§ O
23 O
. O

2430 O
Fuel B-system
systems I-system
. O

( O
a O
) O
Prevent O
continued O
safe O
flight O
and O
landing O
or O
, O

if O
continued O
safe O
flight O
and O
landing O
cannot O
be O
ensured O
, O

the O
hazard O
has O
been O
minimized O
; O
( O
b O
) O
Cause O
serious O
injury O
that O
may O
be O
avoided O
; O
and O
( O
c O
) O
Require O
immediate O
action O
by O
any O
crewmember O
for O
continued O
operation O
of O
any O
remaining O
powerplant B-module
system O
. O

( O
a O
) O
The O
airplane B-asset
design O
, O

including O
the O
induction O
and O
inlet B-system
system I-system
, O

must O
prevent O
foreseeable O
accumulation O
of O
ice O
or O
snow O
that O
adversely O
affects O
powerplant B-module
operation O
. O

( O
b O
) O
The O
powerplant B-module
installation I-module
design O
must O
prevent O
any O
accumulation O
of O
ice O
or O
snow O
that O
adversely O
affects O
powerplant B-module
operation O
, O

in O
those O
icing O
conditions O
for O
which O
certification O
is O
requested O
. O

( O
a O
) O
No O
unsafe O
condition O
will O
result O
during O
normal O
operation O
of O
the O
system O
; O
and O
( O
b O
) O
The O
airplane B-asset
is O
capable O
of O
continued O
safe O
flight O
and O
landing O
after O
any O
single O
failure O
, O

likely O
combination O
of O
failures O
, O

or O
malfunction O
of O
the O
reversing B-system
system I-system
. O

( O
a O
) O
The O
installed O
powerplant B-module
must O
operate O
without O
any O
hazardous O
characteristics O
during O
normal O
and O
emergency O
operation O
within O
the O
range O
of O
operating O
limitations O
for O
the O
airplane B-asset
and O
the O
engine B-system
. O

( O
b O
) O
The O
pilot O
must O
have O
the O
capability O
to O
stop O
the O
powerplant B-module
in O
flight O
and O
restart O
the O
powerplant B-module
within O
an O
established O
operational O
envelope O
. O

( O
a O
) O
Each O
fuel B-system
system I-system
must O
— O
( O
1 O
) O
Be O
designed O
and O
arranged O
to O
provide O
independence O
between O
multiple O
fuel O
storage O
and O
supply B-system
systems I-system
so O
that O
failure O
of O
any O
one O
component O
in O
one O
system O
will O
not O
result O
in O
loss O
of O
fuel O
storage O
or O
supply O
of O
another O
system O
; O
( O
2 O
) O
Be O
designed O
and O
arranged O
to O
prevent O
ignition O
of O
the O
fuel O
within O
the O
system O
by O
direct O
lightning O
strikes O
or O
swept O
lightning O
strokes O
to O
areas O
where O
such O
occurrences O
are O
highly O
probable O
, O

or O
by O
corona O
or O
streamering O
at O
fuel O
vent O
outlets O
; O
( O
3 O
) O
Provide O
the O
fuel O
necessary O
to O
ensure O
each O
powerplant B-module
and O
auxiliary B-module
power I-module
unit I-module
functions O
properly O
in O
all O
likely O
operating O
conditions O
; O
14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2410 O
14 O
CFR O
23 O
. O

2430 O
( O
a O
) O
( O
3 O
) O
( O
enhanced O
display O
) O
page O
22 O
of O
31 O
§ O
23 O
. O

2435 O
Powerplant B-system
induction O
and O
exhaust B-system
systems I-system
. O

§ O
23 O
. O

2440 O
Powerplant B-system
fire O
protection O
. O

( O
4 O
) O
Provide O
the O
flightcrew O
with O
a O
means O
to O
determine O
the O
total O
useable O
fuel O
available O
and O
provide O
uninterrupted O
supply O
of O
that O
fuel O
when O
the O
system O
is O
correctly O
operated O
, O

accounting O
for O
likely O
fuel O
fluctuations O
; O
( O
5 O
) O
Provide O
a O
means O
to O
safely O
remove O
or O
isolate O
the O
fuel O
stored O
in O
the O
system O
from O
the O
airplane B-asset
; O
( O
6 O
) O
Be O
designed O
to O
retain O
fuel O
under O
all O
likely O
operating O
conditions O
and O
minimize O
hazards O
to O
the O
occupants O
during O
any O
survivable O
emergency O
landing O
. O

For O
level O
4 O
airplanes B-asset
, O

failure O
due O
to O
overload O
of O
the O
landing B-system
system I-system
must O
be O
taken O
into O
account O
; O
and O
( O
7 O
) O
Prevent O
hazardous O
contamination O
of O
the O
fuel O
supplied O
to O
each O
powerplant B-module
and O
auxiliary B-module
power I-module
unit I-module
. O

( O
b O
) O
Each O
fuel B-system
storage I-system
system I-system
must O
— O
( O
1 O
) O
Withstand O
the O
loads O
under O
likely O
operating O
conditions O
without O
failure O
; O
( O
2 O
) O
Be O
isolated O
from O
personnel O
compartments O
and O
protected O
from O
hazards O
due O
to O
unintended O
temperature O
influences O
; O
( O
3 O
) O
Be O
designed O
to O
prevent O
significant O
loss O
of O
stored O
fuel O
from O
any O
vent B-system
system I-system
due O
to O
fuel O
transfer O
between O
fuel O
storage O
or O
supply B-system
systems I-system
, O

or O
under O
likely O
operating O
conditions O
; O
( O
4 O
) O
Provide O
fuel O
for O
at O
least O
one O
- O
half O
hour O
of O
operation O
at O
maximum B-parameter
continuous I-parameter
power I-parameter
or O
thrust B-parameter
; O
and O
( O
5 O
) O
Be O
capable O
of O
jettisoning O
fuel O
safely O
if O
required O
for O
landing O
. O

( O
c O
) O
Each O
fuel O
storage O
refilling O
or O
recharging B-system
system I-system
must O
be O
designed O
to O
— O
( O
1 O
) O
Prevent O
improper O
refilling O
or O
recharging O
; O
( O
2 O
) O
Prevent O
contamination O
of O
the O
fuel O
stored O
during O
likely O
operating O
conditions O
; O
and O
( O
3 O
) O
Prevent O
the O
occurrence O
of O
any O
hazard O
to O
the O
airplane B-asset
or O
to O
persons O
during O
refilling O
or O
recharging O
. O

( O
a O
) O
The O
air B-system
induction I-system
system I-system
for O
each O
powerplant B-module
or O
auxiliary B-module
power I-module
unit I-module
and O
their O
accessories O
must O
— O
( O
1 O
) O
Supply O
the O
air O
required O
by O
that O
powerplant B-module
or O
auxiliary B-module
power I-module
unit I-module
and O
its O
accessories O
under O
likely O
operating O
conditions O
; O
( O
2 O
) O
Be O
designed O
to O
prevent O
likely O
hazards O
in O
the O
event O
of O
fire O
or O
backfire O
; O
( O
3 O
) O
Minimize O
the O
ingestion O
of O
foreign O
matter O
; O
and O
( O
4 O
) O
Provide O
an O
alternate B-component
intake I-component
if O
blockage O
of O
the O
primary B-component
intake I-component
is O
likely O
. O

( O
b O
) O
The O
exhaust B-system
system I-system
, O

including O
exhaust B-component
heat I-component
exchangers I-component
for O
each O
powerplant B-module
or O
auxiliary B-module
power I-module
unit I-module
, O

must O
— O
( O
1 O
) O
Provide O
a O
means O
to O
safely O
discharge O
potential O
harmful O
material O
; O
and O
( O
2 O
) O
Be O
designed O
to O
prevent O
likely O
hazards O
from O
heat O
, O

corrosion O
, O

or O
blockage O
. O

( O
a O
) O
A O
powerplant B-module
, O

auxiliary B-module
power I-module
unit I-module
, O

or O
combustion B-component
heater I-component
that O
includes O
a O
flammable O
fluid O
and O
an O
ignition O
source O
for O
that O
fluid O
must O
be O
installed O
in O
a O
designated O
fire O
zone O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2430 O
( O
a O
) O
( O
4 O
) O
14 O
CFR O
23 O
. O

2440 O
( O
a O
) O
( O
enhanced O
display O
) O
page O
23 O
of O
31 O
[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
Subpart O
F O
— O
Equipment O
§ O
23 O
. O

2500 O
Airplane B-asset
level B-system
systems I-system
requirements O
. O

This O
section O
applies O
generally O
to O
installed O
equipment O
and O
systems O
unless O
a O
section O
of O
this O
part O
imposes O
requirements O
for O
a O
specific O
piece O
of O
equipment O
, O

system O
, O

or O
systems O
. O

( O
b O
) O
Each O
designated O
fire O
zone O
must O
provide O
a O
means O
to O
isolate O
and O
mitigate O
hazards O
to O
the O
airplane B-asset
in O
the O
event O
of O
fire O
or O
overheat O
within O
the O
zone O
. O

( O
c O
) O
Each O
component O
, O

line O
, O

fitting O
, O

and O
control O
subject O
to O
fire O
conditions O
must O
— O
( O
1 O
) O
Be O
designed O
and O
located O
to O
prevent O
hazards O
resulting O
from O
a O
fire O
, O

including O
any O
located O
adjacent O
to O
a O
designated O
fire O
zone O
that O
may O
be O
affected O
by O
fire O
within O
that O
zone O
; O
( O
2 O
) O
Be O
fire O
- O
resistant O
if O
carrying O
flammable O
fluid O
, O

gas O
or O
air O
, O

or O
is O
required O
to O
operate O
in O
the O
event O
of O
a O
fire O
; O
and O
( O
3 O
) O
Be O
fireproof B-component
or O
enclosed O
by O
a O
fire B-component
proof I-component
shield I-component
if O
storing O
concentrated O
flammable O
fluids O
. O

( O
d O
) O
The O
applicant O
must O
provide O
a O
means O
to O
prevent O
hazardous O
quantities O
of O
flammable O
fluids O
from O
flowing O
into O
, O

within O
or O
through O
each O
designated O
fire O
zone O
. O

This O
means O
must O
— O
( O
1 O
) O
Not O
restrict O
flow O
or O
limit O
operation O
of O
any O
remaining O
powerplant B-module
or O
auxiliary B-module
power I-module
unit I-module
, O

or O
equipment O
necessary O
for O
safety O
; O
( O
2 O
) O
Prevent O
inadvertent O
operation O
; O
and O
( O
3 O
) O
Be O
located O
outside O
the O
fire O
zone O
unless O
an O
equal O
degree O
of O
safety O
is O
provided O
with O
a O
means O
inside O
the O
fire O
zone O
. O

( O
e O
) O
A O
means O
to O
ensure O
the O
prompt O
detection O
of O
fire O
must O
be O
provided O
for O
each O
designated O
fire O
zone O
— O
( O
1 O
) O
On O
a O
multiengine O
airplane B-asset
where O
detection O
will O
mitigate O
likely O
hazards O
to O
the O
airplane B-asset
; O
or O
( O
2 O
) O
That O
contains O
a O
fire B-component
extinguisher I-component
. O

( O
f O
) O
A O
means O
to O
extinguish O
fire O
within O
a O
fire O
zone O
, O

except O
a O
combustion B-component
heater I-component
fire O
zone O
, O

must O
be O
provided O
for O
— O
( O
1 O
) O
Any O
fire O
zone O
located O
outside O
the O
pilot O
' O
s O
view O
; O
( O
2 O
) O
Any O
fire O
zone O
embedded O
within O
the O
fuselage B-system
, O

which O
must O
also O
include O
a O
redundant O
means O
to O
extinguish O
fire O
; O
and O
( O
3 O
) O
Any O
fire O
zone O
on O
a O
level O
4 O
airplane B-asset
. O

( O
a O
) O
The O
equipment O
and O
systems O
required O
for O
an O
airplane B-asset
to O
operate O
safely O
in O
the O
kinds O
of O
operations O
for O
which O
certification O
is O
requested O
( O
Day O
VFR O
, O

Night O
VFR O
, O

IFR O
) O
must O
be O
designed O
and O
installed O
to O
— O
( O
1 O
) O
Meet O
the O
level O
of O
safety O
applicable O
to O
the O
certification O
and O
performance O
level O
of O
the O
airplane B-asset
; O
and O
( O
2 O
) O
Perform O
their O
intended O
function O
throughout O
the O
operating O
and O
environmental O
limits O
for O
which O
the O
airplane B-asset
is O
certificated O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2440 O
( O
b O
) O
14 O
CFR O
23 O
. O

2500 O
( O
a O
) O
( O
2 O
) O
( O
enhanced O
display O
) O
page O
24 O
of O
31 O
[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
§ O
23 O
. O

2505 O
Function O
and O
installation O
. O

When O
installed O
, O

each O
item O
of O
equipment O
must O
function O
as O
intended O
. O

§ O
23 O
. O

2510 O
Equipment O
, O

systems O
, O

and O
installations O
. O

For O
any O
airplane B-system
system I-system
or O
equipment O
whose O
failure O
or O
abnormal O
operation O
has O
not O
been O
specifically O
addressed O
by O
another O
requirement O
in O
this O
part O
, O

the O
applicant O
must O
design O
and O
install O
each O
system O
and O
equipment O
, O

such O
that O
there O
is O
a O
logical O
and O
acceptable O
inverse O
relationship O
between O
the O
average O
probability O
and O
the O
severity O
of O
failure O
conditions O
to O
the O
extent O
that O
: O
§ O
23 O
. O

2515 O
Electrical O
and O
electronic B-system
system I-system
lightning O
protection O
. O

An O
airplane B-asset
approved O
for O
IFR O
operations O
must O
meet O
the O
following O
requirements O
, O

unless O
an O
applicant O
shows O
that O
exposure O
to O
lightning O
is O
unlikely O
: O
§ O
23 O
. O

2520 O
High O
- O
intensity O
Radiated O
Fields O
( O
HIRF O
) O
protection O
. O

( O
b O
) O
The O
systems O
and O
equipment O
not O
covered O
by O
paragraph O
( O
a O
) O
of O
this O
section O
— O
considered O
separately O
and O
in O
relation O
to O
other O
systems O
— O
must O
be O
designed O
and O
installed O
so O
their O
operation O
does O
not O
have O
an O
adverse O
effect O
on O
the O
airplane B-asset
or O
its O
occupants O
. O

( O
a O
) O
Each O
catastrophic O
failure O
condition O
is O
extremely O
improbable O
; O
( O
b O
) O
Each O
hazardous O
failure O
condition O
is O
extremely O
remote O
; O
and O
( O
c O
) O
Each O
major O
failure O
condition O
is O
remote O
. O

( O
a O
) O
Each O
electrical O
or O
electronic B-system
system I-system
that O
performs O
a O
function O
, O

the O
failure O
of O
which O
would O
prevent O
the O
continued O
safe O
flight O
and O
landing O
of O
the O
airplane B-asset
, O

must O
be O
designed O
and O
installed O
such O
that O
— O
( O
1 O
) O
The O
function O
at O
the O
airplane B-asset
level O
is O
not O
adversely O
affected O
during O
and O
after O
the O
time O
the O
airplane B-asset
is O
exposed O
to O
lightning O
; O
and O
( O
2 O
) O
The O
system O
recovers O
normal O
operation O
of O
that O
function O
in O
a O
timely O
manner O
after O
the O
airplane B-asset
is O
exposed O
to O
lightning O
unless O
the O
system O
' O
s O
recovery O
conflicts O
with O
other O
operational O
or O
functional O
requirements O
of O
the O
system O
. O

( O
b O
) O
Each O
electrical O
and O
electronic B-system
system I-system
that O
performs O
a O
function O
, O

the O
failure O
of O
which O
would O
significantly O
reduce O
the O
capability O
of O
the O
airplane B-asset
or O
the O
ability O
of O
the O
flightcrew O
to O
respond O
to O
an O
adverse O
operating O
condition O
, O

must O
be O
designed O
and O
installed O
such O
that O
the O
system O
recovers O
normal O
operation O
of O
that O
function O
in O
a O
timely O
manner O
after O
the O
airplane B-asset
is O
exposed O
to O
lightning O
. O

( O
a O
) O
Each O
electrical O
and O
electronic B-system
system I-system
that O
performs O
a O
function O
, O

the O
failure O
of O
which O
would O
prevent O
the O
continued O
safe O
flight O
and O
landing O
of O
the O
airplane B-asset
, O

must O
be O
designed O
and O
installed O
such O
that O
— O
( O
1 O
) O
The O
function O
at O
the O
airplane B-asset
level O
is O
not O
adversely O
affected O
during O
and O
after O
the O
time O
the O
airplane B-asset
is O
exposed O
to O
the O
HIRF O
environment O
; O
and O
14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2500 O
( O
b O
) O
14 O
CFR O
23 O
. O

2520 O
( O
a O
) O
( O
1 O
) O
( O
enhanced O
display O
) O
page O
25 O
of O
31 O
[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
§ O
23 O
. O

2525 O
System O
power O
generation O
, O

storage O
, O

and O
distribution O
. O

The O
power O
generation O
, O

storage O
, O

and O
distribution O
for O
any O
system O
must O
be O
designed O
and O
installed O
to O
— O
§ O
23 O
. O

2530 O
External O
and O
cockpit O
lighting O
. O

§ O
23 O
. O

2535 O
Safety O
equipment O
. O

Safety O
and O
survival O
equipment O
, O

required O
by O
the O
operating O
rules O
of O
this O
chapter O
, O

must O
be O
reliable O
, O

readily O
accessible O
, O

easily O
identifiable O
, O

and O
clearly O
marked O
to O
identify O
its O
method O
of O
operation O
. O

( O
2 O
) O
The O
system O
recovers O
normal O
operation O
of O
that O
function O
in O
a O
timely O
manner O
after O
the O
airplane B-asset
is O
exposed O
to O
the O
HIRF O
environment O
, O

unless O
the O
system O
' O
s O
recovery O
conflicts O
with O
other O
operational O
or O
functional O
requirements O
of O
the O
system O
. O

( O
b O
) O
For O
airplanes B-asset
approved O
for O
IFR O
operations O
, O

each O
electrical O
and O
electronic B-system
system I-system
that O
performs O
a O
function O
, O

the O
failure O
of O
which O
would O
significantly O
reduce O
the O
capability O
of O
the O
airplane B-asset
or O
the O
ability O
of O
the O
flightcrew O
to O
respond O
to O
an O
adverse O
operating O
condition O
, O

must O
be O
designed O
and O
installed O
such O
that O
the O
system O
recovers O
normal O
operation O
of O
that O
function O
in O
a O
timely O
manner O
after O
the O
airplane B-asset
is O
exposed O
to O
the O
HIRF O
environment O
. O

( O
a O
) O
Supply O
the O
power O
required O
for O
operation O
of O
connected O
loads O
during O
all O
intended O
operating O
conditions O
; O
( O
b O
) O
Ensure O
no O
single O
failure O
or O
malfunction O
of O
any O
one O
power O
supply O
, O

distribution O
system O
, O

or O
other O
utilization O
system O
will O
prevent O
the O
system O
from O
supplying O
the O
essential B-parameter
loads I-parameter
required O
for O
continued O
safe O
flight O
and O
landing O
; O
and O
( O
c O
) O
Have O
enough O
capacity O
, O

if O
the O
primary O
source O
fails O
, O

to O
supply O
essential O
loads O
, O

including O
non O
- O
continuous O
essential O
loads O
for O
the O
time O
needed O
to O
complete O
the O
function O
required O
for O
continued O
safe O
flight O
and O
landing O
. O

( O
a O
) O
The O
applicant O
must O
design O
and O
install O
all O
lights O
to O
minimize O
any O
adverse O
effects O
on O
the O
performance O
of O
flightcrew O
duties O
. O

( O
b O
) O
Any O
position O
and O
anti B-component
- I-component
collision I-component
lights I-component
, O

if O
required O
by O
part O
91 O
of O
this O
chapter O
, O

must O
have O
the O
intensities O
, O

flash O
rate O
, O

colors O
, O

fields O
of O
coverage O
, O

and O
other O
characteristics O
to O
provide O
sufficient O
time O
for O
another O
aircraft B-asset
to O
avoid O
a O
collision O
. O

( O
c O
) O
Any O
position B-component
lights I-component
, O

if O
required O
by O
part O
91 O
of O
this O
chapter O
, O

must O
include O
a O
red B-component
light I-component
on O
the O
left O
side O
of O
the O
airplane B-asset
, O

a O
green B-component
light I-component
on O
the O
right O
side O
of O
the O
airplane B-asset
, O

spaced O
laterally O
as O
far O
apart O
as O
practicable O
, O

and O
a O
white B-component
light I-component
facing O
aft O
, O

located O
on O
an O
aft O
portion O
of O
the O
airplane B-asset
or O
on O
the O
wing B-component
tips I-component
. O

( O
d O
) O
Any O
taxi O
and O
landing B-component
lights I-component
must O
be O
designed O
and O
installed O
so O
they O
provide O
sufficient O
light O
for O
night O
operations O
. O

( O
e O
) O
For O
seaplanes B-asset
or O
amphibian B-asset
airplanes I-asset
, O

riding B-component
lights I-component
must O
provide O
a O
white O
light O
visible O
in O
clear O
atmospheric O
conditions O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2520 O
( O
a O
) O
( O
2 O
) O
14 O
CFR O
23 O
. O

2535 O
( O
enhanced O
display O
) O
page O
26 O
of O
31 O
§ O
23 O
. O

2540 O
Flight O
in O
icing O
conditions O
. O

An O
applicant O
who O
requests O
certification O
for O
flight O
in O
icing O
conditions O
defined O
in O
part O
1 O
of O
appendix O
C O
to O
part O
25 O
of O
this O
chapter O
, O

or O
an O
applicant O
who O
requests O
certification O
for O
flight O
in O
these O
icing O
conditions O
and O
any O
additional O
atmospheric O
icing O
conditions O
, O

must O
show O
the O
following O
in O
the O
icing O
conditions O
for O
which O
certification O
is O
requested O
: O
§ O
23 O
. O

2545 O
Pressurized B-system
systems I-system
elements O
. O

Pressurized B-system
systems I-system
must O
withstand O
appropriate O
proof O
and O
burst O
pressures O
. O

§ O
23 O
. O

2550 O
Equipment O
containing O
high B-component
- I-component
energy I-component
rotors I-component
. O

Equipment O
containing O
high B-component
- I-component
energy I-component
rotors I-component
must O
be O
designed O
or O
installed O
to O
protect O
the O
occupants O
and O
airplane B-asset
from O
uncontained O
fragments O
. O

Subpart O
G O
— O
Flightcrew O
Interface O
and O
Other O
Information O
§ O
23 O
. O

2600 O
Flightcrew O
interface O
. O

[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
§ O
23 O
. O

2605 O
Installation O
and O
operation O
. O

( O
a O
) O
The O
ice B-system
protection I-system
system I-system
provides O
for O
safe O
operation O
. O

( O
b O
) O
The O
airplane B-asset
design O
must O
provide O
protection O
from O
stalling O
when O
the O
autopilot O
is O
operating O
. O

( O
a O
) O
The O
pilot B-module
compartment I-module
, O

its O
equipment O
, O

and O
its O
arrangement O
to O
include O
pilot O
view O
, O

must O
allow O
each O
pilot O
to O
perform O
his O
or O
her O
duties O
, O

including O
taxi O
, O

takeoff O
, O

climb O
, O

cruise O
, O

descent O
, O

approach O
, O

landing O
, O

and O
perform O
any O
maneuvers O
within O
the O
operating O
envelope O
of O
the O
airplane B-asset
, O

without O
excessive O
concentration O
, O

skill O
, O

alertness O
, O

or O
fatigue O
. O

( O
b O
) O
The O
applicant O
must O
install O
flight O
, O

navigation O
, O

surveillance O
, O

and O
powerplant B-control
controls I-control
and O
displays B-module
so O
flightcrew O
members O
can O
monitor O
and O
perform O
defined O
tasks O
associated O
with O
the O
intended O
functions O
of O
systems O
and O
equipment O
. O

The O
system O
and O
equipment O
design O
must O
minimize O
flightcrew O
errors O
, O

which O
could O
result O
in O
additional O
hazards O
. O

( O
c O
) O
For O
level O
4 O
airplanes B-asset
, O

the O
flightcrew O
interface O
design O
must O
allow O
for O
continued O
safe O
flight O
and O
landing O
after O
the O
loss O
of O
vision O
through O
any O
one O
of O
the O
windshield B-component
panels I-component
. O

( O
a O
) O
Each O
item O
of O
installed O
equipment O
related O
to O
the O
flightcrew O
interface O
must O
be O
labelled O
, O

if O
applicable O
, O

as O
to O
it O
identification O
, O

function O
, O

or O
operating O
limitations O
, O

or O
any O
combination O
of O
these O
factors O
. O

( O
b O
) O
There O
must O
be O
a O
discernible O
means O
of O
providing O
system O
operating O
parameters O
required O
to O
operate O
the O
airplane B-asset
, O

including O
warnings O
, O

cautions O
, O

and O
normal O
indications O
to O
the O
responsible O
crewmember O
. O

( O
c O
) O
Information O
concerning O
an O
unsafe O
system O
operating O
condition O
must O
be O
provided O
in O
a O
timely O
manner O
to O
the O
crewmember O
responsible O
for O
taking O
corrective O
action O
. O

The O
information O
must O
be O
clear O
enough O
to O
avoid O
likely O
crewmember O
errors O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2540 O
14 O
CFR O
23 O
. O

2605 O
( O
c O
) O
( O
enhanced O
display O
) O
page O
27 O
of O
31 O
§ O
23 O
. O

2610 O
Instrument B-component
markings I-component
, O

control B-component
markings I-component
, O

and O
placards B-component
. O

§ O
23 O
. O

2615 O
Flight O
, O

navigation O
, O

and O
powerplant B-module
instruments I-module
. O

§ O
23 O
. O

2620 O
Airplane B-asset
flight O
manual O
. O

The O
applicant O
must O
provide O
an O
Airplane B-asset
Flight O
Manual O
that O
must O
be O
delivered O
with O
each O
airplane B-asset
. O

( O
a O
) O
Each O
airplane B-asset
must O
display O
in O
a O
conspicuous O
manner O
any O
placard O
and O
instrument O
marking O
necessary O
for O
operation O
. O

( O
b O
) O
The O
design O
must O
clearly O
indicate O
the O
function O
of O
each O
cockpit B-control
control I-control
, O

other O
than O
primary O
flight B-control
controls I-control
. O

( O
c O
) O
The O
applicant O
must O
include O
instrument O
marking O
and O
placard O
information O
in O
the O
Airplane O
Flight O
Manual O
. O

( O
a O
) O
Installed O
systems O
must O
provide O
the O
flightcrew O
member O
who O
sets O
or O
monitors O
parameters O
for O
the O
flight O
, O

navigation O
, O

and O
powerplant B-module
, O

the O
information O
necessary O
to O
do O
so O
during O
each O
phase O
of O
flight O
. O

This O
information O
must O
— O
( O
1 O
) O
Be O
presented O
in O
a O
manner O
that O
the O
crewmember O
can O
monitor O
the O
parameter O
and O
determine O
trends O
, O

as O
needed O
, O

to O
operate O
the O
airplane B-asset
; O
and O
( O
2 O
) O
Include O
limitations O
, O

unless O
the O
limitation O
cannot O
be O
exceeded O
in O
all O
intended O
operations O
. O

( O
b O
) O
Indication B-system
systems I-system
that O
integrate O
the O
display O
of O
flight O
or O
powerplant B-module
parameters O
to O
operate O
the O
airplane B-asset
or O
are O
required O
by O
the O
operating O
rules O
of O
this O
chapter O
must O
— O
( O
1 O
) O
Not O
inhibit O
the O
primary O
display O
of O
flight O
or O
powerplant B-module
parameters O
needed O
by O
any O
flightcrew O
member O
in O
any O
normal O
mode O
of O
operation O
; O
and O
( O
2 O
) O
In O
combination O
with O
other O
systems O
, O

be O
designed O
and O
installed O
so O
information O
essential O
for O
continued O
safe O
flight O
and O
landing O
will O
be O
available O
to O
the O
flightcrew O
in O
a O
timely O
manner O
after O
any O
single O
failure O
or O
probable O
combination O
of O
failures O
. O

( O
a O
) O
The O
Airplane B-asset
Flight O
Manual O
must O
contain O
the O
following O
information O
— O
( O
1 O
) O
Airplane B-asset
operating O
limitations O
; O
( O
2 O
) O
Airplane B-asset
operating O
procedures O
; O
( O
3 O
) O
Performance O
information O
; O
( O
4 O
) O
Loading O
information O
; O
and O
( O
5 O
) O
Other O
information O
that O
is O
necessary O
for O
safe O
operation O
because O
of O
design O
, O

operating O
, O

or O
handling O
characteristics O
. O

( O
b O
) O
The O
following O
sections O
of O
the O
Airplane B-asset
Flight O
Manual O
must O
be O
approved O
by O
the O
FAA O
in O
a O
manner O
specified O
by O
the O
Administrator O
— O
( O
1 O
) O
For O
low O
- O
speed O
, O

level O
1 O
and O
2 O
airplanes B-asset
, O

those O
portions O
of O
the O
Airplane B-asset
Flight O
Manual O
containing O
the O
information O
specified O
in O
paragraph O
( O
a O
) O
( O
1 O
) O
of O
this O
section O
; O
and O
( O
2 O
) O
For O
high O
- O
speed O
level O
1 O
and O
2 O
airplanes B-asset
and O
all O
level O
3 O
and O
4 O
airplanes B-asset
, O

those O
portions O
of O
the O
Airplane B-asset
Flight O
Manual O
containing O
the O
information O
specified O
in O
paragraphs O
( O
a O
) O
( O
1 O
) O
thru O
( O
a O
) O
( O
4 O
) O
of O
this O
section O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2610 O
14 O
CFR O
23 O
. O

2620 O
( O
b O
) O
( O
2 O
) O
( O
enhanced O
display O
) O
page O
28 O
of O
31 O
[ O
Doc O
. O

No O
. O

FAA O
- O
2015 O
- O
1621 O
, O

Amdt O
. O

23 O
- O
64 O
, O

81 O
FR O
96689 O
, O

Dec O
. O

30 O
, O

2016 O
, O

as O
amended O
by O
Doc O
. O

No O
. O

FAA O
- O
2022 O
- O
1355 O
, O

Amdt O
. O

23 O
- O
65 O
, O

87 O
FR O
75710 O
, O

Dec O
. O

9 O
, O

2022 O
] O
Appendix O
A O
to O
Part O
23 O
— O
Instructions O
for O
Continued O
Airworthiness O
A23 O
. O

1 O
General O
A23 O
. O

2 O
Format O
A23 O
. O

3 O
Content O
The O
contents O
of O
the O
manual O
or O
manuals O
must O
be O
prepared O
in O
the O
English O
language O
. O

The O
Instructions O
for O
Continued O
Airworthiness O
must O
contain O
the O
following O
manuals O
or O
sections O
and O
information O
: O
( O
a O
) O
This O
appendix O
specifies O
requirements O
for O
the O
preparation O
of O
Instructions O
for O
Continued O
Airworthiness O
as O
required O
by O
this O
part O
. O

( O
b O
) O
The O
Instructions O
for O
Continued O
Airworthiness O
for O
each O
airplane B-asset
must O
include O
the O
Instructions O
for O
Continued O
Airworthiness O
for O
each O
engine B-system
and O
propeller B-system
( O
hereinafter O
designated O
“ O
products O
” O
) O
, O

for O
each O
appliance O
required O
by O
this O
chapter O
, O

and O
any O
required O
information O
relating O
to O
the O
interface O
of O
those O
appliances O
and O
products O
with O
the O
airplane B-asset
. O

If O
Instructions O
for O
Continued O
Airworthiness O
are O
not O
supplied O
by O
the O
manufacturer O
of O
an O
appliance O
or O
product O
installed O
in O
the O
airplane B-asset
, O

the O
Instructions O
for O
Continued O
Airworthiness O
for O
the O
airplane B-asset
must O
include O
the O
information O
essential O
to O
the O
continued O
airworthiness O
of O
the O
airplane B-asset
. O

( O
c O
) O
The O
applicant O
must O
submit O
to O
the O
FAA O
a O
program O
to O
show O
how O
changes O
to O
the O
Instructions O
for O
Continued O
Airworthiness O
made O
by O
the O
applicant O
or O
by O
the O
manufacturers O
of O
products O
and O
appliances O
installed O
in O
the O
airplane B-asset
will O
be O
distributed O
. O

( O
a O
) O
The O
Instructions O
for O
Continued O
Airworthiness O
must O
be O
in O
the O
form O
of O
a O
manual O
or O
manuals O
as O
appropriate O
for O
the O
quantity O
of O
data O
to O
be O
provided O
. O

( O
b O
) O
The O
format O
of O
the O
manual O
or O
manuals O
must O
provide O
for O
a O
practical O
arrangement O
. O

( O
a O
) O
Airplane B-asset
maintenance O
manual O
or O
section O
. O

( O
1 O
) O
Introduction O
information O
that O
includes O
an O
explanation O
of O
the O
airplane B-asset
' I-asset
s O
features O
and O
data O
to O
the O
extent O
necessary O
for O
maintenance O
or O
preventive O
maintenance O
. O

( O
2 O
) O
A O
description O
of O
the O
airplane B-asset
and O
its O
systems O
and O
installations O
including O
its O
engines B-system
, O

propellers B-system
, O

and O
appliances O
. O

( O
3 O
) O
Basic O
control O
and O
operation O
information O
describing O
how O
the O
airplane B-asset
components O
and O
systems O
are O
controlled O
and O
how O
they O
operate O
, O

including O
any O
special O
procedures O
and O
limitations O
that O
apply O
. O

( O
4 O
) O
Servicing O
information O
that O
covers O
details O
regarding O
servicing O
points O
, O

capacities O
of O
tanks O
, O

reservoirs O
, O

types O
of O
fluids O
to O
be O
used O
, O

pressures O
applicable O
to O
the O
various O
systems O
, O

location O
of O
access B-component
panels I-component
for O
inspection O
and O
servicing O
, O

locations O
of O
lubrication O
points O
, O

lubricants O
to O
be O
used O
, O

equipment O
required O
for O
servicing O
, O

tow O
instructions O
and O
limitations O
, O

mooring O
, O

jacking O
, O

and O
leveling O
information O
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2620 O
( O
b O
) O
( O
2 O
) O
14 O
CFR O
23 O
. O

2620 O
( O
b O
) O
( O
2 O
) O
( O
enhanced O
display O
) O
page O
29 O
of O
31 O
A23 O
. O

4 O
Airworthiness O
limitations O
section O
. O

The O
Instructions O
for O
Continued O
Airworthiness O
must O
contain O
a O
section O
titled O
Airworthiness O
Limitations O
that O
is O
segregated O
and O
clearly O
distinguishable O
from O
the O
rest O
of O
the O
document O
. O

This O
section O
must O
set O
forth O
each O
mandatory O
replacement O
time O
, O

structural O
inspection O
interval O
, O

and O
related O
structural O
inspection O
procedure O
required O
for O
type O
certification O
. O

If O
the O
Instructions O
for O
Continued O
Airworthiness O
consist O
of O
multiple O
documents O
, O

the O
section O
required O
by O
this O
paragraph O
must O
be O
included O
in O
the O
principal O
manual O
. O

This O
section O
must O
contain O
a O
legible O
statement O
in O
a O
( O
b O
) O
Maintenance O
Instructions O
. O

( O
1 O
) O
Scheduling O
information O
for O
each O
part O
of O
the O
airplane B-asset
and O
its O
engines B-system
, O

auxiliary B-module
power I-module
units I-module
, O

propellers B-system
, O

accessories B-component
, O

instruments B-component
, O

and O
equipment O
that O
provides O
the O
recommended O
periods O
at O
which O
they O
should O
be O
cleaned O
, O

inspected O
, O

adjusted O
, O

tested O
, O

and O
lubricated O
, O

and O
the O
degree O
of O
inspection O
, O

the O
applicable O
wear O
tolerances O
, O

and O
work O
recommended O
at O
these O
periods O
. O

However O
, O

the O
applicant O
may O
refer O
to O
an O
accessory O
, O

instrument O
, O

or O
equipment O
manufacturer O
as O
the O
source O
of O
this O
information O
if O
the O
applicant O
shows O
that O
the O
item O
has O
an O
exceptionally O
high O
degree O
of O
complexity O
requiring O
specialized O
maintenance O
techniques O
, O

test O
equipment O
, O

or O
expertise O
. O

The O
recommended O
overhaul O
periods O
and O
necessary O
cross O
reference O
to O
the O
Airworthiness O
Limitations O
section O
of O
the O
manual O
must O
also O
be O
included O
. O

In O
addition O
, O

the O
applicant O
must O
include O
an O
inspection O
program O
that O
includes O
the O
frequency O
and O
extent O
of O
the O
inspections O
necessary O
to O
provide O
for O
the O
continued O
airworthiness O
of O
the O
airplane B-asset
. O

( O
2 O
) O
Troubleshooting O
information O
describing O
probable O
malfunctions O
, O

how O
to O
recognize O
those O
malfunctions O
, O

and O
the O
remedial O
action O
for O
those O
malfunctions O
. O

( O
3 O
) O
Information O
describing O
the O
order O
and O
method O
of O
removing O
and O
replacing O
products O
and O
parts O
with O
any O
necessary O
precautions O
to O
be O
taken O
. O

( O
4 O
) O
Other O
general O
procedural O
instructions O
including O
procedures O
for O
system O
testing O
during O
ground O
running O
, O

symmetry B-parameter
checks O
, O

weighing O
and O
determining O
the O
center B-parameter
of I-parameter
gravity I-parameter
, O

lifting O
and O
shoring O
, O

and O
storage O
limitations O
. O

( O
c O
) O
Diagrams O
of O
structural O
access O
plates O
and O
information O
needed O
to O
gain O
access O
for O
inspections O
when O
access O
plates O
are O
not O
provided O
. O

( O
d O
) O
Details O
for O
the O
application O
of O
special O
inspection O
techniques O
including O
radiographic O
and O
ultrasonic O
testing O
where O
such O
processes O
are O
specified O
by O
the O
applicant O
. O

( O
e O
) O
Information O
needed O
to O
apply O
protective O
treatments O
to O
the O
structure O
after O
inspection O
. O

( O
f O
) O
All O
data O
relative O
to O
structural O
fasteners O
such O
as O
identification O
, O

discard O
recommendations O
, O

and O
torque B-parameter
values I-parameter
. O

( O
g O
) O
A O
list O
of O
special O
tools O
needed O
. O

( O
h O
) O
In O
addition O
, O

for O
level O
4 O
airplanes B-asset
, O

the O
following O
information O
must O
be O
furnished O
— O
( O
1 O
) O
Electrical B-parameter
loads I-parameter
applicable O
to O
the O
various O
systems O
; O
( O
2 O
) O
Methods O
of O
balancing B-parameter
control I-parameter
surfaces I-parameter
; O
( O
3 O
) O
Identification O
of O
primary O
and O
secondary O
structures O
; O
and O
( O
4 O
) O
Special O
repair O
methods O
applicable O
to O
the O
airplane B-asset
. O

14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2620 O
( O
b O
) O
( O
2 O
) O
14 O
CFR O
23 O
. O

2620 O
( O
b O
) O
( O
2 O
) O
( O
enhanced O
display O
) O
page O
30 O
of O
31 O
prominent O
location O
that O
reads O
“ O
The O
Airworthiness O
Limitations O
section O
is O
FAA O
approved O
and O
specifies O
maintenance O
required O
under O
§ O
§ O
43 O
. O

16 O
and O
91 O
. O

403 O
of O
Title O
14 O
of O
the O
Code O
of O
Federal O
Regulations O
unless O
an O
alternative O
program O
has O
been O
FAA O
approved O
. O

” O
14 O
CFR O
Part O
23 O
( O
up O
to O
date O
as O
of O
6 O
/ O
27 O
/ O
2024 O
) O
Airworthiness O
Standards O
: O
Normal O
Category O
Airplanes B-asset
14 O
CFR O
23 O
. O

2620 O
( O
b O
) O
( O
2 O
) O
14 O
CFR O
23 O
. O

2620 O
( O
b O
) O
( O
2 O
) O
( O
enhanced O
display O
) O
page O
31 O
of O
31 O

{ O
" O
extra O
" O
: O
{ O
} O
, O

" O
name O
" O
: O
" O
design O
_ O
1015 O
_ O
eec0fb333ea04024a8bf80feaea9414c O
_ O
s O
" O
, O

" O
parameters O
" O
: O
[ O
{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
455 O
. O

0848750871123 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
266 O
. O

17505374981715 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
321 O
. O

048542145391 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
BODY B-system
_ O
ROT B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
30 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
BOTTOM B-module
_ I-module
CONNECTOR I-module
_ O
ROTATION B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Z B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoCaseRotation B-parameter
" O
, O

" O
value O
" O
: O
" O
330 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Rotation B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoMass B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
property O
" O
: O
" O
WEIGHT B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
ControlChannelAuto B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
AUTOPILOT O
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
AUTOPILOT O
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
51 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
BATTERY B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
BATTERY B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
6 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT B-parameter
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
5 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT B-parameter
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
87 O
. O

65 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
5 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
FLOOR B-parameter
_ I-parameter
HEIGHT I-parameter
" O
, O

" O
value O
" O
: O
" O
8 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-parameter
_ I-parameter
HEIGHT I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
floor B-parameter
_ I-parameter
height I-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
7 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
47 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
7 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
HORZ B-parameter
_ I-parameter
DIAMETER I-parameter
" O
, O

" O
value O
" O
: O
" O
353 O
. O

4 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
HORZ B-parameter
_ I-parameter
DIAMETER I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
horz O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-parameter
_ I-parameter
LENGTH I-parameter
" O
, O

" O
value O
" O
: O
" O
137 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FUSE O
_ O
CYL O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
3 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
107 O
. O

8 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
3 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
83 O
. O

65 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
, O

" O
value O
" O
: O
" O
51 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
vert O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
6 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
105 O
. O

3 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
6 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
1 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
2 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
1 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
2 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop B-parameter
_ I-parameter
type I-parameter
" O
} O
] O
} O
] O
, O

" O
components O
" O
: O
[ O
{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
BatteryController B-control
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
BatteryController B-control
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Battery B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
TurnigyGraphene3000mAh4S75C O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Cargo B-system
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
type O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
CargoCase B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
UAV O
_ O
Fuselage B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
capsule O
_ O
fuselage B-system
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Para O
_ O
Hub O
_ O
6 O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394od O
_ O
para O
_ O
hub O
_ O
6 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE600XF O
_ O
530 O
_ O
G3 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE600XF O
_ O
530 O
_ O
G3 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
MN4012KV480 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
AT4130KV300 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
AT4130KV300 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
MN4012KV480 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Orient B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
16x7 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
16x7 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
17x7E O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
14x14 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
14x14 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
17x7E O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
RpmTemp B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Autopilot O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Current B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Voltage B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
GPS B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Variometer B-parameter
" O
} O
] O
, O

" O
connections O
" O
: O
[ O
{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector1 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector3 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Case2HubConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
6 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
5 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Orient B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
ORIENTCONN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Orient B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
491 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
263 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
264 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector1 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector3 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Case2HubConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
6 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
821 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
5 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
820 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
819 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Orient B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Orient B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
ORIENTCONN O
" O
} O
] O
} O

WEIGHT B-parameter
AND O
BALANCE B-parameter
REPORT O
( O
Example O
document O
for O
LSA O
applicants O
– O
v1 O
of O
08 O
. O

03 O
. O

16 O
) O
Introduction O
This O
document O
defines O
the O
weight B-parameter
and I-parameter
balance I-parameter
envelope I-parameter
of O
the O
ABCD O
aircraft B-asset
according O
to O
the O
applicable O
certification O
specification O
CS O
- O
LSA O
. O

The O
requirements O
are O
referenced O
in O
the O
compliance O
checklist O
of O
the O
certification O
programme O
ABCD O
- O
CP O
- O
00 O
. O

The O
permissible O
centre B-parameter
of I-parameter
gravity I-parameter
range I-parameter
is O
dictated O
by O
the O
aerodynamic O
design O
requirements O
for O
the O
airplane O
. O

Then O
the O
centre B-parameter
of I-parameter
gravity I-parameter
locations I-parameter
corresponding O
to O
the O
critical B-parameter
weights I-parameter
are O
calculated O
. O

All O
units O
used O
are O
metric O
( O
SI O
units O
) O
except O
for O
airspeeds B-parameter
( O
CAS O
) O
given O
in O
knots O
if O
not O
stated O
otherwise O
. O

Note O
: O
The O
values O
defined O
within O
this O
document O
should O
be O
used O
for O
the O
placards O
, O

markings O
, O

aeroplane O
flight O
manual O
( O
limitations O
) O
, O

load O
calculations O
and O
need O
to O
be O
verified O
by O
testing O
. O

References O
List O
of O
Abbreviations O
CG O
centre B-parameter
of I-parameter
gravity I-parameter
MAC O
mean O
aerodynamic O
chord O
from O
design O
description O
( O
) O
g O
gravity B-parameter
acceleration I-parameter
equals O
9 O
. O

81 O
m I-measurement
/ I-measurement
s2 I-measurement
[ O
m B-measurement
/ I-measurement
s2 I-measurement
] O
maximum O
level B-parameter
flying I-parameter
speed I-parameter
with O
maximum O
continuous B-parameter
power I-parameter
[ O
kts B-measurement
] O
aeroplane O
empty B-parameter
weight I-parameter
[ O
kg B-measurement
] O
aeroplane O
basic B-parameter
empty I-parameter
weight I-parameter
including O
unusable B-parameter
fuel I-parameter
[ O
kg B-measurement
] O
aeroplane O
maximum O
take B-parameter
- I-parameter
off I-parameter
weight I-parameter
[ O
kg B-measurement
] O
aeroplane O
minimum O
flying B-parameter
weight I-parameter
[ O
kg B-measurement
] O
aeroplane O
minimum O
flying B-parameter
weight I-parameter
with O
full O
fuel O
[ O
kg B-measurement
] O
minimum O
useful B-parameter
load I-parameter
[ O
kg B-measurement
] O
aeroplane O
maximum O
zero O
wing B-system
fuel B-parameter
weight I-parameter
[ O
kg B-measurement
] O
WE O
maximum O
empty B-parameter
weight I-parameter
[ O
kg B-measurement
] O
Requirements O
This O
document O
covers O
the O
following O
certification O
specifications O
requirements O
: O
Table O
1 O
– O
Requirements O
Reference O
for O
centre B-parameter
of I-parameter
gravity I-parameter
values I-parameter
Datum O
plane O
: O
leading O
edge O
at O
wing O
mean O
aerodynamic O
chord O
Mass O
items O
The O
single O
weight O
items O
with O
their O
corresponding O
centre B-parameter
of I-parameter
gravity I-parameter
locations I-parameter
are O
listed O
below O
. O

The O
data O
contained O
herein O
is O
used O
to O
establish O
aeroplane B-asset
loading O
limits O
: O
Table O
2 O
– O
Mass B-parameter
items O
( O
Note O
: O
In O
this O
document O
the O
weight B-parameter
of O
the O
empty O
aircraft B-asset
is O
assumed O
to O
be O
determined O
through O
direct O
weighing O
. O

Such O
information O
might O
be O
needed O
during O
early O
phases O
of O
the O
design O
, O

when O
no O
prototype O
is O
available O
. O

In O
this O
case O
the O
weight B-parameter
of O
the O
empty O
aircraft B-asset
should O
be O
determined O
through O
estimation O
. O

It O
is O
important O
in O
this O
case O
to O
have O
a O
breakdown O
of O
the O
main O
items O
in O
terms O
of O
weight B-parameter
and O
locations O
, O

so O
that O
the O
weight B-parameter
can O
be O
kept O
under O
control O
and O
avoid O
situations O
where O
the O
assumed O
envelope O
cannot O
be O
achieved O
. O

) O
Aircraft B-asset
weights B-parameter
The O
following O
design B-parameter
weights I-parameter
have O
been O
identified O
since O
: O
either O
they O
are O
clearly O
required O
by O
the O
CS O
- O
LSA O
requirements O
, O

or O
they O
impose O
critical O
loads O
or O
flight O
characteristics O
. O

Basic B-parameter
empty I-parameter
weight I-parameter
WBEW O
The O
basic B-parameter
empty I-parameter
weight I-parameter
needs O
to O
be O
determined O
to O
identify O
its O
centre B-parameter
of I-parameter
gravity I-parameter
according O
to O
requirement O
4 O
. O

2 O
. O

3 O
as O
empty O
CG O
. O

All O
load O
conditions O
determined O
within O
this O
document O
are O
based O
on O
the O
basic O
empty O
weight B-parameter
of O
the O
aircraft B-asset
. O

It O
includes O
empty O
weight B-parameter
of O
the O
aircraft B-asset
and O
the O
unusable O
amount O
of O
fuel O
. O

Basic O
empty O
weight B-parameter
has O
been O
determined O
to O
WBEW O
= O
366 O
kg B-measurement
. O

Note O
: O
The O
basic B-parameter
empty I-parameter
weight I-parameter
must O
include O
all O
equipment O
for O
the O
operation O
intended O
including O
optional O
avionics O
packages O
– O
for O
example O
. O

Basic B-parameter
empty I-parameter
weight I-parameter
( O
366 O
kg B-measurement
) O
vs O
maximum O
empty B-parameter
weight I-parameter
WMEW O
( O
400kg O
) O
According O
to O
4 O
. O

2 O
. O

1 O
of O
, O

the O
minimum O
useful B-parameter
load I-parameter
should O
be O
200kg O
consisting O
of O
172Kg O
= O
both O
seats B-system
occupied O
with O
persons O
of O
86kg O
each O
( O
4 O
. O

2 O
. O

1 O
. O

1 O
) O
28kg O
= O
fuel O
for O
1 O
hour B-measurement
flight O
at O
as O
determined O
by O
( O
4 O
. O

2 O
. O

1 O
. O

2 O
) O
According O
to O
3 O
. O

1 O
. O

2 O
the O
maximum O
empty B-parameter
weight I-parameter
of O
the O
aeroplane B-asset
shall O
be O
equal O
to O
: O
. O

The O
aeroplane B-asset
complies O
with O
its O
Basic B-parameter
empty I-parameter
weight I-parameter
including O
unusable O
fuel O
: O
. O

Minimum O
flying B-parameter
weight I-parameter
Wmin O
( O
421kg O
) O
The O
minimum O
flying B-parameter
weight I-parameter
needs O
to O
be O
determined O
by O
requirement O
4 O
. O

2 O
. O

2 O
and O
is O
a O
design B-parameter
load I-parameter
case O
leading O
to O
highest O
load O
factors O
during O
gust O
penetration O
. O

It O
assumes O
only O
a O
pilot O
of O
weight B-parameter
of O
55 O
kg B-measurement
. O

Minimum O
full B-parameter
fuel I-parameter
flying I-parameter
weight I-parameter
WminFF O
( O
495kg O
) O
The O
minimum O
flying B-parameter
weight I-parameter
with O
full O
fuel O
is O
a O
design B-parameter
load I-parameter
case O
imposing O
highest O
load B-parameter
factors I-parameter
on O
the O
fuel B-component
tank I-component
. O

This O
is O
critical O
for O
the O
fuel B-component
tank I-component
design O
and O
it O
can O
be O
critical O
also O
for O
the O
wing B-system
structure O
since O
in O
this O
scenario O
the O
highest O
inertia B-parameter
load I-parameter
on O
the O
fuel B-component
tank I-component
introduces O
torsion O
about O
the O
shear O
centre O
in O
the O
same O
direction O
of O
the O
wing B-system
aerodynamic B-parameter
load I-parameter
of O
the O
wing B-system
( O
the O
CG O
of O
the O
fuel O
is O
forward O
to O
the O
shear B-parameter
centre I-parameter
which O
is O
forward O
to O
the O
wing B-system
centre B-parameter
of I-parameter
pressure I-parameter
) O
. O

Maximum O
zero B-parameter
wing I-parameter
fuel I-parameter
weight I-parameter
WZWF O
( O
600kg O
) O
The O
maximum O
zero B-parameter
wing I-parameter
fuel I-parameter
weight I-parameter
needs O
to O
be O
determined O
by O
requirement O
5 O
. O

2 O
. O

1 O
. O

3 O
and O
is O
a O
design B-parameter
load I-parameter
case O
for O
the O
wing B-system
loads B-parameter
due O
to O
lowest O
inertia O
discharge O
of O
the O
wing B-system
structure O
. O

In O
this O
aeroplane B-asset
this O
weight B-parameter
equals O
the O
Maximum O
Take B-parameter
- I-parameter
off I-parameter
weight I-parameter
. O

Maximum O
take B-parameter
- I-parameter
off I-parameter
weight I-parameter
WMTOW O
( O
600kg O
) O
The O
total O
aircraft B-asset
weight B-parameter
must O
not O
exceed O
600kg O
regardless O
whether O
the O
aircraft B-asset
is O
on O
ground O
or O
in O
flight O
. O

The O
gross O
weight B-parameter
of O
the O
aeroplane B-asset
shall O
not O
exceed O
WMTOW O
= O
600kg O
. O

The O
maximum O
landing B-parameter
weight I-parameter
equals O
the O
maximum O
take B-parameter
- I-parameter
off I-parameter
weight I-parameter
. O

Loading O
cases O
The O
following O
loading O
conditions O
have O
been O
established O
to O
identify O
the O
critical O
cases O
. O

Table O
3 O
– O
Loading O
cases O
for O
standard O
configuration O
Centre B-parameter
of I-parameter
gravity I-parameter
location I-parameter
The O
maximum O
permissible O
centre B-parameter
of I-parameter
gravity I-parameter
locations I-parameter
are O
defined O
within O
this O
chapter O
. O

Flight O
limits O
The O
maximum O
permissible O
centre B-parameter
of I-parameter
gravity I-parameter
range I-parameter
during O
flight O
with O
respect O
to O
datum O
plane O
is O
most O
forward O
0 O
. O

25m O
( O
required O
by O
4 O
. O

2 O
. O

3 O
) O
most O
rearward O
0 O
. O

39m O
( O
required O
by O
4 O
. O

2 O
. O

3 O
) O
Limitations O
on O
ground O
The O
most O
rearward O
centre B-parameter
of I-parameter
gravity I-parameter
with O
the O
plane O
on O
ground O
must O
not O
exceed O
( O
with O
respect O
to O
datum O
plane O
) O
0 O
. O

46m O
to O
prevent O
the O
aircraft B-asset
from O
flipping O
on O
the O
tail O
although O
not O
more O
than O
0 O
. O

41m O
might O
be O
reached O
with O
the O
most O
critical O
loading O
configuration O
. O

Centre B-parameter
of I-parameter
gravity I-parameter
envelope I-parameter
The O
following O
table O
of O
load B-parameter
cases I-parameter
defines O
the O
limits O
for O
the O
certified O
envelope O
of O
centre B-parameter
of I-parameter
gravity I-parameter
locations I-parameter
and O
the O
position O
of O
load B-parameter
cases I-parameter
of O
6 O
. O

7 O
within O
the O
envelope O
. O

Table O
4 O
– O
Load O
cases O
on O
centre O
of O
gravity O
envelope O
for O
standard O
configuration O
The O
centre B-parameter
of I-parameter
gravity I-parameter
envelope I-parameter
covers O
all O
valid O
loading O
cases O
. O

Figure O
1 O
– O
Centre B-parameter
of I-parameter
gravity I-parameter
envelope I-parameter
for O
standard O
configuration O
Expanded O
centre B-parameter
of I-parameter
gravity I-parameter
envelope I-parameter
for O
certification O
To O
cover O
alterations O
to O
the O
aeroplane B-asset
where O
need O
might O
arise O
or O
after O
certification O
the O
aeroplane B-asset
will O
be O
tested O
and O
certified O
against O
an O
extended O
envelope O
. O

Additional O
weights B-parameter
will O
be O
added O
during O
testing O
at O
their O
corresponding O
locations O
to O
establish O
the O
desired O
loading O
cases O
. O

Table O
5 O
– O
Weights B-parameter
required O
to O
achieve O
expanded O
envelope O
for O
certification O
The O
expanded O
centre B-parameter
of I-parameter
gravity I-parameter
envelope I-parameter
is O
defined O
by O
the O
load B-parameter
cases I-parameter
below O
using O
ballast B-parameter
weights I-parameter
at O
their O
corresponding O
locations O
. O

Table O
6 O
– O
Load B-parameter
cases I-parameter
on O
expanded O
centre B-parameter
of I-parameter
gravity I-parameter
envelope I-parameter
for O
certification O
Note O
: O
The O
values O
above O
are O
preliminary O
assumptions O
. O

Ballast O
weights B-parameter
need O
to O
be O
checked O
to O
be O
in O
accordance O
with O
airframe B-parameter
strength I-parameter
limitations O
and O
their O
impact O
on O
the O
flight O
characteristics O
in O
terms O
of O
inertia O
before O
test O
flights O
. O

This O
might O
require O
narrowing O
the O
centre B-parameter
of I-parameter
gravity I-parameter
envelope I-parameter
. O

Figure O
2 O
– O
Expanded O
centre B-parameter
of I-parameter
gravity I-parameter
envelope I-parameter
for O
certification O
Compliance O
statements O
Compliance O
statements O
are O
shown O
below O
: O

{ O
" O
extra O
" O
: O
{ O
} O
, O

" O
name O
" O
: O
" O
design O
_ O
10007 O
_ O
34a9ce88002a45de81845813212ebd27 O
_ O
s O
" O
, O

" O
parameters O
" O
: O
[ O
{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
495 O
. O

5496724719351 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
491 O
. O

17236250723363 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
228 O
. O

4569996357744 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
BODY B-system
_ O
ROT B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
30 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
BOTTOM B-module
_ I-module
CONNECTOR I-module
_ O
ROTATION B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Z B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoCaseRotation B-parameter
" O
, O

" O
value O
" O
: O
" O
330 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Rotation B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoMass B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
property O
" O
: O
" O
WEIGHT B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
ControlChannelAuto B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
AUTOPILOT O
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
4 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
AUTOPILOT O
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
47 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
BATTERY B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
4 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
BATTERY B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
6 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT O
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
4 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
5 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT O
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
83 O
. O

15 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
5 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
FLOOR B-parameter
_ I-parameter
HEIGHT I-parameter
" O
, O

" O
value O
" O
: O
" O
8 O
. O

75 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-parameter
_ I-parameter
HEIGHT I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
floor B-parameter
_ I-parameter
height I-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
4 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
7 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
43 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
7 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
HORZ B-parameter
_ I-parameter
DIAMETER I-parameter
" O
, O

" O
value O
" O
: O
" O
339 O
. O

9 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
HORZ B-parameter
_ I-parameter
DIAMETER I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
horz O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
LENGTH B-parameter
" O
, O

" O
value O
" O
: O
" O
84 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FUSE O
_ O
CYL O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
4 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
3 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
103 O
. O

3 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
3 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
4 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
79 O
. O

15 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
, O

" O
value O
" O
: O
" O
52 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
vert O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
4 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
6 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
100 O
. O

8 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
6 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
1 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
2 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
1 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
2 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
] O
} O
] O
, O

" O
components O
" O
: O
[ O
{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
BatteryController B-control
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
BatteryController B-control
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Battery B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
TurnigyGraphene1300mAh4S75C O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Cargo B-system
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
type O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
CargoCase B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
UAV O
_ O
Fuselage B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
capsule O
_ O
fuselage B-system
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Para O
_ O
Hub O
_ O
6 O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394od O
_ O
para O
_ O
hub O
_ O
6 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor O
_ O
U7 O
_ O
V2 O
. O

0KV490 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
U7 O
_ O
V2 O
. O

0KV490 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
MN4010KV370 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
AT4130KV300 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
AT4130KV300 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
MN4010KV370 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Orient B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
17x10E O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
17x10E O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
15x5 O
_ O
5MR O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
14x14N O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
14x14N O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
15x5 O
_ O
5MR O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
RpmTemp B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Autopilot O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Current O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Voltage B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
GPS B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Variometer B-parameter
" O
} O
] O
, O

" O
connections O
" O
: O
[ O
{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector3 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector1 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
5 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
6 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Case2HubConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Orient B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
ORIENTCONN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Orient B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
33 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
15 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
16 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector3 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector1 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
5 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
43 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
42 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
6 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
41 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Case2HubConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Orient B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Orient B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
ORIENTCONN O
" O
} O
] O
} O

ELECTRICAL B-system
SYSTEM I-system
DESCRIPTION O
AND O
ELECTRICAL B-parameter
LOAD I-parameter
ANALYSIS O
( O
Example O
document O
for O
LSA O
applicants O
– O
v1 O
of O
17 O
. O

02 O
. O

16 O
) O
Introduction O
This O
document O
describes O
the O
electrical B-system
system I-system
and O
provides O
the O
electrical B-parameter
load I-parameter
analysis O
( O
ELA O
) O
of O
the O
ABCD O
aircraft B-asset
and O
demonstrates O
compliance O
to O
the O
requirements O
as O
defined O
in O
the O
certification O
basis O
and O
in O
the O
certification O
programme O
( O
Ref O
. O

1 O
) O
. O

This O
ELA O
is O
based O
on O
ASTM O
std O
. O

F2490 O
- O
05 O
. O

( O
Note O
: O
This O
ASTM O
standard O
is O
not O
required O
by O
the O
CS O
- O
LSA O
, O

although O
it O
gives O
good O
guidelines O
to O
prepare O
that O
document O
) O
. O

The O
aim O
of O
ELA O
is O
to O
demonstrate O
that O
the O
capacity O
of O
the O
electrical B-system
system I-system
of O
the O
ABCD O
Airplane B-asset
is O
sufficient O
to O
support O
the O
expected O
electrical B-parameter
loads I-parameter
in O
all O
foreseeable O
conditions O
. O

To O
do O
this O
, O

all O
the O
electrical B-parameter
loads I-parameter
( O
average O
and O
maximum O
) O
are O
taken O
into O
account O
. O

The O
analysis O
accounts O
for O
operations O
in O
normal O
, O

abnormal O
and O
emergency O
conditions O
. O

This O
document O
should O
be O
maintained O
throughout O
the O
lifetime O
of O
the O
aircraft B-asset
type O
and O
updated O
in O
case O
of O
changes O
to O
the O
electrical B-system
system I-system
. O

References O
Certification O
Programme O
ABCD O
- O
CP O
- O
00 O
FAA O
Advisory O
Curricular O
, O

AC43 O
. O

13 O
ASTM O
F2490 O
- O
05 O
Abbreviations O
used O
in O
this O
document O
AC B-parameter
– O
Alternating B-parameter
Current I-parameter
Ah B-measurement
– O
Ampere B-parameter
- I-parameter
hour I-parameter
CB B-component
– O
Circuit B-component
Breaker I-component
COM B-component
– O
Communications B-component
Equipment I-component
( I-component
Radio I-component
) I-component
DC B-parameter
– O
Direct B-parameter
Current I-parameter
EFIS B-system
– O
Electronic B-system
Flight I-system
Information I-system
System I-system
ELA O
– O
Electrical B-parameter
Load I-parameter
Analysis O
GPS O
– O
Equipment B-system
using I-system
Global I-system
Positioning I-system
System I-system
NAV O
– O
Navigation B-component
equipment I-component
RPM B-measurement
– O
Revolutions O
per O
minute B-measurement
VHF O
– O
Very O
High O
Frequency O
( O
in O
this O
case O
, O

VHF O
COM O
equipment O
) O
List O
of O
requirements O
( O
NOTE O
: O
at O
the O
time O
of O
issue O
of O
this O
template O
, O

the O
CS O
- O
LSA O
amdt O
1 O
is O
in O
place O
which O
includes O
the O
ASTM O
F2245 O
- O
12d O
. O

If O
later O
amendments O
of O
the O
CS O
- O
LSA O
or O
ASTM O
are O
in O
place O
, O

they O
should O
be O
considered O
. O

The O
structure O
of O
the O
document O
remains O
the O
same O
, O

but O
the O
requirements O
defined O
in O
the O
certification O
basis O
agreed O
with O
the O
Agency O
shall O
be O
considered O
) O
. O

Electrical B-system
System I-system
General O
Description O
The O
primary O
DC B-parameter
electrical I-parameter
source I-parameter
is O
an O
alternator B-module
with O
14V O
DC B-parameter
output O
, O

rated O
at O
40 O
Amperes B-measurement
at O
2500 O
RPM B-measurement
of O
propeller B-parameter
speed I-parameter
. O

During O
normal O
conditions O
it O
recharges O
the O
battery B-module
. O

The O
alternator B-module
starts O
to O
provide O
voltage B-parameter
output I-parameter
above O
1200 O
RPM B-measurement
. O

The O
alternator B-module
and O
the O
battery B-module
are O
connected O
to O
the O
electrical B-component
bus I-component
in O
order O
to O
energize O
the O
electrical B-system
system I-system
. O

Secondary O
DC B-component
power I-component
is O
provided O
by O
a O
lead O
type O
battery B-module
which O
provides O
the O
energy O
necessary O
for O
feeding O
the O
essential O
electrical B-parameter
loads I-parameter
in O
the O
event O
of O
the O
alternator B-module
failure O
. O

The O
battery B-module
also O
provides O
electrical O
energy O
for O
engine O
start O
. O

For O
ground O
starting O
an O
external B-module
power I-module
socket I-module
is O
provided O
. O

Each O
electrical B-component
supply I-component
is O
connected O
to O
a O
circuit B-component
breaker I-component
. O

All O
the O
electric B-component
cables I-component
installed O
to O
the O
instrument B-system
panel I-system
comply O
with O
the O
MIL O
- O
C O
- O
27500 O
standards O
. O

( O
NOTE O
: O
For O
LSA O
aircraft O
, O

automotive O
industry O
cables O
, O

e O
. O

g O
. O

wiring O
conforms O
SAE O
AS O
22759 O
/ O
186 O
standards O
are O
also O
acceptable O
. O

Cable O
sizing O
also O
could O
be O
classified O
by O
AWG O
numbers O
. O

) O
Some O
aircraft B-system
systems I-system
( O
e O
. O

g O
. O

avionics O
) O
have O
a O
separate O
master B-control
switch I-control
. O

The O
architecture O
of O
the O
Electrical B-system
system I-system
, O

sizing O
of O
cables O
and O
fuses O
is O
shown O
in O
Figure O
1 O
. O

For O
sizing O
of O
cables O
and O
fuses O
of O
the O
avionics B-system
subsystem I-system
see O
Table O
1 O
. O

These O
have O
been O
sized O
according O
to O
[ O
2 O
] O
. O

Figure O
1 O
– O
Electrical O
power O
schematic O
diagram O
Table O
1 O
– O
Avionics B-component
subsystem I-component
cables I-component
and O
CB O
/ O
Fuses O
sizing O
Load O
Analysis O
Electrical B-component
power I-component
sources I-component
Following O
table O
contains O
a O
summary O
about O
all O
the O
electrical B-component
power I-component
sources I-component
. O

Table O
2 O
– O
Electrical B-component
power I-component
sources I-component
Analysis O
The O
list O
of O
the O
electrical B-parameter
consumptions I-parameter
can O
be O
found O
in O
the O
table O
below O
. O

The O
electrical B-parameter
current I-parameter
rates I-parameter
below O
are O
taken O
from O
the O
corresponding O
data O
sheets O
. O

Table O
3 O
– O
Load O
analysis O
The O
maximum O
electrical B-parameter
power I-parameter
needed O
for O
all O
the O
equipment O
is O
20 O
. O

1 O
Amperes B-measurement
and O
is O
below O
the O
continuous O
rating O
of O
the O
alternator B-module
. O

In O
case O
of O
generator O
failure O
, O

the O
instruments O
could O
run O
on O
battery B-module
. O

To O
provide O
backup B-component
power I-component
for O
at O
least O
30 O
minutes B-measurement
, O

the O
required O
minimum O
battery B-parameter
capacity I-parameter
is O
10 O
. O

05 O
Ah B-measurement
. O

The O
battery B-parameter
capacity I-parameter
is O
15 O
Ah B-measurement
, O

considering O
the O
aging O
of O
the O
battery B-module
. O

Emergency O
conditions O
assessment O
The O
capacity O
of O
the O
15 O
Ah B-measurement
battery B-module
is O
assumed O
conservatively O
75 O
% O
of O
the O
full O
capacity O
iaw O
. O

paragraph O
6 O
. O

5 O
. O

8 O
. O

1 O
of O
ASTM O
F2490 O
- O
05 O
[ O
3 O
] O
. O

75 O
% O
of O
the O
15Ah O
capacity O
is O
11 O
. O

25 O
Ah B-measurement
. O

It O
means O
675 O
A B-measurement
- I-measurement
min I-measurement
( O
Ampere B-measurement
- I-measurement
minutes I-measurement
. O

) O
With O
20 O
. O

1 O
A B-measurement
electric O
demand O
, O

( O
675 O
/ O
20 O
. O

1 O
= O
33 O
. O

58 O
) O
it O
means O
33 O
. O

58 O
minutes B-measurement
continuous O
operation O
( O
which O
is O
above O
30 O
minutes B-measurement
) O
without O
load O
shed O
. O

The O
calculation O
above O
is O
conservative O
since O
the O
flap B-component
motor I-component
and O
the O
electrical B-component
fuel I-component
pump I-component
are O
not O
operated O
continuously O
, O

therefore O
the O
real O
capacity O
could O
be O
a O
bit O
longer O
. O

NOTE O
: O
Not O
all O
the O
equipment O
loads O
should O
be O
calculated O
for O
the O
emergency O
conditions O
assessment O
. O

Compliance O
Statements O
Compliance O
statements O
are O
shown O
below O
: O

{ O
" O
extra O
" O
: O
{ O
} O
, O

" O
name O
" O
: O
" O
design O
_ O
10269 O
_ O
827464835bf0466791434cdddd1a9c09 O
_ O
s O
" O
, O

" O
parameters O
" O
: O
[ O
{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
473 O
. O

7242484080575 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
BODY B-system
_ O
ROT B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
BOTTOM B-module
_ I-module
CONNECTOR I-module
_ O
ROTATION B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Z B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoCaseRotation B-parameter
" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Rotation B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoMass B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
property O
" O
: O
" O
WEIGHT B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
ControlChannelAuto B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
AUTOPILOT O
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
AUTOPILOT O
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
46 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
BATTERY B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
BATTERY B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
6 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT B-parameter
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
5 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT B-parameter
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
82 O
. O

65 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
5 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
FLOOR B-parameter
_ I-parameter
HEIGHT I-parameter
" O
, O

" O
value O
" O
: O
" O
8 O
. O

75 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-parameter
_ I-parameter
HEIGHT I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
floor B-parameter
_ I-parameter
height I-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
7 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
42 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
7 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
HORZ B-parameter
_ I-parameter
DIAMETER I-parameter
" O
, O

" O
value O
" O
: O
" O
338 O
. O

4 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
HORZ B-parameter
_ I-parameter
DIAMETER I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
horz O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
LENGTH B-parameter
" O
, O

" O
value O
" O
: O
" O
95 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FUSE O
_ O
CYL O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
3 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
102 O
. O

8 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
3 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
78 O
. O

65 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
, O

" O
value O
" O
: O
" O
52 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
vert O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
6 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
Y O
_ O
OFFSET B-parameter
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, O

" O
value O
" O
: O
" O
100 O
. O

3 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
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: O
" O
FLOOR B-module
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CONNECTOR I-module
_ O
6 O
_ O
DISP B-parameter
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WIDTH I-parameter
" O
} O
] O
, O

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optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
1 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
2 O
_ O
CLOCK B-parameter
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ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
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ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
3 O
_ O
CLOCK B-parameter
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ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
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" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
4 O
_ O
CLOCK B-parameter
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ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
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" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
5 O
_ O
CLOCK B-parameter
_ I-parameter
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" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
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" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
6 O
_ O
CLOCK B-parameter
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" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
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" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
] O
} O
] O
, O

" O
components O
" O
: O
[ O
{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
BatteryController B-control
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
BatteryController B-control
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Battery B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
TurnigyGraphene1600mAh4S75CSquare O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Cargo B-system
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
type O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
CargoCase B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
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" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
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_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
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, O

" O
component O
_ O
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" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
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" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
UAV O
_ O
Fuselage B-system
" O
, O

" O
component O
_ O
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" O
: O
" O
capsule O
_ O
fuselage B-system
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Para O
_ O
Hub O
_ O
6 O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394od O
_ O
para O
_ O
hub O
_ O
6 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE700XF O
_ O
295 O
_ O
G3 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE700XF O
_ O
295 O
_ O
G3 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE700XF O
_ O
295 O
_ O
G3 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE700XF O
_ O
295 O
_ O
G3 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE700XF O
_ O
295 O
_ O
G3 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE700XF O
_ O
295 O
_ O
G3 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Orient B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
13x4 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
13x4 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
13x4 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
13x4 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
13x4 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
13x4 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
RpmTemp B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Autopilot O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Current B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Voltage B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
GPS B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Variometer B-parameter
" O
} O
] O
, O

" O
connections O
" O
: O
[ O
{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector3 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector1 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
6 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
5 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Case2HubConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Orient B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
ORIENTCONN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Orient B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
887 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
489 O
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector3 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector1 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
6 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
5 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
1423 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Case2HubConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Orient B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Orient B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
ORIENTCONN O
" O
} O
] O
} O

FLIGHT B-asset
TEST O
PROGRAMME O
( O
Example O
document O
for O
LSA O
applicants O
– O
v1 O
of O
17 O
. O

02 O
. O

16 O
) O
0 O
. O

Introduction O
This O
document O
shows O
the O
programme O
of O
flights B-asset
for O
certification O
of O
the O
aircraft B-asset
ABCD O
. O

The O
table O
of O
section O
0 O
contains O
the O
purposed O
test O
sequence O
with O
an O
overview O
of O
the O
main O
test O
points O
and O
certification O
conditions O
. O

This O
document O
demonstrates O
compliance O
to O
the O
requirements O
as O
defined O
in O
the O
certification O
basis O
and O
in O
the O
certification O
programme O
( O
Ref O
. O

1 O
) O
. O

This O
documents O
does O
not O
give O
full O
details O
of O
each O
test O
points O
. O

These O
details O
can O
be O
found O
in O
the O
individual O
Flight O
Test O
Plans O
and O
Flight O
Test O
Orders O
. O

Table O
of O
contents O
0 O
. O

Introduction O
2 O
1 O
. O

Scope O
5 O
2 O
. O

References O
5 O
3 O
. O

Weight O
and O
Balance O
data O
and O
limits O
for O
flight O
test O
phases O
5 O
4 O
. O

Flight O
test O
methods O
8 O
5 O
. O

Configuration O
of O
the O
prototype O
9 O
6 O
. O

Flight O
test O
team O
composition O
9 O
7 O
. O

Facilities O
10 O
8 O
. O

Test O
instrumentation O
and O
configuration O
13 O
a O
. O

Test O
instrumentation O
13 O
b O
. O

Test O
aircraft O
configuration O
13 O
9 O
. O

Test O
airspace O
13 O
10 O
. O

Timeline O
of O
the O
flight O
test O
14 O
a O
. O

The O
planned O
steps O
of O
the O
flight O
tests O
are O
the O
following O
: O
14 O
b O
. O

Preconditions O
of O
flight O
tests O
15 O
c O
. O

Schedule O
of O
flights O
15 O
11 O
. O

Flight O
test O
orders O
21 O
Appendix O
1 O
– O
Organisational O
aspects O
22 O
Appendix O
2 O
– O
Flight O
Conditions O
and O
Permit O
to O
Fly O
39 O
Appendix O
3 O
– O
Best O
Practices O
39 O
1 O
. O

Scope O
This O
Flight O
Test O
Program O
is O
intended O
as O
a O
plan O
of O
the O
essential O
activities O
required O
to O
validate O
the O
flight O
characteristics O
and O
the O
performances O
of O
the O
aircraft B-asset
model O
ABCD O
. O

The O
aim O
of O
that O
test O
program O
is O
to O
demonstrate O
compliance O
with O
CS O
- O
LSA O
in O
particular O
paragraphs O
from O
ASTM O
F2245 O
- O
12d O
. O

NOTE O
: O
This O
template O
has O
been O
created O
with O
the O
assumption O
that O
the O
applicant O
is O
not O
a O
DOA O
holder O
thus O
also O
aspects O
related O
organization O
and O
safety O
of O
the O
flight O
are O
addressed O
. O

In O
case O
of O
a O
DOA O
holder O
these O
latter O
aspects O
are O
normally O
defined O
in O
DOA O
procedures O
) O
2 O
. O

References O
[ O
1 O
] O
Certification O
Programme O
ABCD O
- O
CP O
- O
00 O
[ O
2 O
] O
ABCD O
- O
CCL O
Compliance O
Check O
- O
list O
( O
Means O
of O
Compliance O
list O
) O
[ O
3 O
] O
ABCD O
- O
GD O
- O
00 O
General O
Description O
Document O
[ O
4 O
] O
ABCD O
- O
WB O
- O
08 O
- O
00 O
Weight B-parameter
and O
Balance B-parameter
Report O
[ O
5 O
] O
ABCD O
- O
FL O
- O
00 O
Flight B-parameter
Load I-parameter
Calculations O
[ O
6 O
] O
AFM O
( O
POH O
) O
[ O
7 O
] O
Flight O
conditions O
documents O
3 O
. O

Weight B-parameter
and O
Balance B-parameter
data O
and O
limits O
for O
flight O
test O
phases O
Subparagraph O
4 O
. O

1 O
. O

2 O
of O
ASTM O
F2245 O
- O
12d O
requires O
the O
following O
tolerances O
of O
weight B-parameter
and O
CG O
: O
Datum O
plane O
: O
a O
plane O
through O
the O
leading B-location
edge I-location
of O
the O
wing B-system
at O
mean O
aerodynamic O
chord O
, O

perpendicular O
to O
the O
longitudinal O
axis O
of O
the O
aircraft B-asset
. O

See O
[ O
3 O
] O
. O

NOTE O
: O
Datum O
planes O
could O
be O
different O
( O
plane O
of O
the O
firewall B-component
, O

at O
the O
propeller B-system
cone O
, O

etc O
. O

) O
The O
CG O
values O
may O
be O
shown O
also O
in O
MAC O
% O
. O

( O
There O
is O
no O
regulation O
for O
it O
, O

it O
depends O
on O
practical O
issues O
. O

) O
Because O
of O
datum O
plane O
is O
at O
the O
wing B-system
leading B-location
edge I-location
at O
the O
mean O
aerodynamic O
chord O
, O

the O
CG O
limit O
values O
in O
centimetres O
could O
be O
calculated O
to O
MAC O
% O
values O
easily O
. O

The O
MAC O
is O
1 O
, O

40 O
m B-measurement
, O

therefore O
the O
forward O
limit O
can O
be O
calculated O
with O
interpolation O
; O
the O
forward O
limit O
is O
17 O
. O

86 O
% O
MAC O
, O

the O
aft O
limit O
is O
27 O
. O

86 O
% O
MAC O
. O

The O
aircraft B-asset
’ O
s O
centre B-parameter
of I-parameter
gravity I-parameter
envelope I-parameter
is O
shown O
on O
the O
next O
page O
: O
Calculated O
Weight B-parameter
and O
CG B-parameter
values O
in O
different O
conditions O
: O
Minimum B-parameter
flying I-parameter
weight I-parameter
( O
and O
CG B-parameter
position I-parameter
) O
( O
minimal O
useful O
pilot O
+ O
fuel O
+ O
consumable O
material B-parameter
load I-parameter
) O
: O
469 O
kg B-measurement
. O

See O
limitations O
in O
the O
table O
below O
. O

Aircraft B-asset
’ O
s O
MTOW O
with O
maximum O
seat O
load O
( O
pilot O
+ O
pax O
) O
with O
maximum O
allowed O
fuel B-parameter
load I-parameter
and O
max O
. O

baggage B-parameter
compartment I-parameter
load I-parameter
: O
600 O
kg B-measurement
. O

The O
forward O
and O
aft O
centre B-parameter
of I-parameter
gravity I-parameter
limit I-parameter
will O
be O
aft O
of O
datum O
plane O
. O

The O
following O
table O
will O
describe O
the O
weight B-parameter
and O
balance O
limitations O
iaw O
. O

ASTM O
F2245 O
4 O
. O

1 O
. O

2 O
: O
NOTE O
: O
Standard O
values O
from O
ASTM O
F2245 O
4 O
. O

1 O
. O

2 O
are O
highlighted O
. O

Actual O
aircraft B-parameter
weight I-parameter
and O
balance O
is O
determined O
and O
noted O
in O
each O
test O
order O
prior O
flight O
using O
a O
scale O
. O

Weight B-parameter
correction O
for O
fuel O
and O
occupant B-parameter
loading I-parameter
might O
be O
applied O
. O

See O
[ O
3 O
] O
Calculated O
speeds B-parameter
of O
the O
designed O
flight B-parameter
envelope I-parameter
: O
NOTE O
: O
the O
speeds B-parameter
are O
example O
speeds O
, O

the O
VA O
and O
VNE O
are O
calculated O
according O
to O
ASTM O
F2245 O
- O
12d O
. O

The O
flight B-parameter
envelope I-parameter
is O
shown O
below O
; O
it O
shows O
the O
different O
limitations O
in O
different O
test O
phases O
. O

See O
paragraph O
11 O
. O

The O
designed O
airspeeds B-parameter
are O
calibrated O
airspeeds B-parameter
( O
CAS O
) O
, O

however O
, O

all O
the O
limitations O
and O
indications O
to O
the O
pilot O
are O
indicated O
airspeeds B-parameter
( O
IAS O
) O
4 O
. O

Flight O
test O
methods O
Flight O
test O
methods O
are O
detailed O
in O
the O
test O
order O
. O

Guidelines O
are O
shown O
in O
: O
– O
FAA O
AC O
23 O
- O
8C O
– O
Flight O
Test O
Guide O
for O
Certification O
of O
Part O
23 O
Airplanes B-asset
– O
FAA O
AC O
23 O
- O
15A O
– O
Small O
Airplane B-asset
Certification O
Compliance O
Program O
– O
FAA O
AC O
90 O
- O
89A O
– O
Amateur O
- O
built O
Aircraft B-asset
And O
Ultralight O
Flight O
Testing O
Handbook O
– O
C O
. O

Edward O
Lan O
and O
Jan O
Roskam O
: O
Airplane B-asset
Aerodynamics O
and O
Performance O
, O

Roskam O
Aviation O
Co O
. O

– O
Russel O
M O
. O

Herrington O
et O
al O
: O
Flight O
Test O
Engineering O
Handbook O
, O

Air O
Force O
Technical O
Report O
no O
. O

6273 O
, O

NTIS O
No O
. O

AD O
636 O
. O

392 O
National O
Technical O
Information O
Service O
, O

Springfield O
, O

VA O
. O

– O
NATIONAL O
ADVISORY O
COMMITTEE O
FOR O
AERONAUTICS O
( O
TECHNICAL O
NOTE O
2098 O
) O
– O
The O
Effects O
Of O
Stability O
Of O
Spin O
- O
recovery O
Tail O
Parachutes O
On O
The O
Behavior O
Of O
Airplanes B-asset
In O
Gliding O
Flight O
And O
In O
Spins O
. O

By O
Stanley O
H O
. O

Scher O
and O
John O
W O
. O

Draper O
, O

Langley O
Aeronautical O
Laboratory O
, O

Langley O
Air O
Force O
Base O
, O

Va O
. O

– O
NASA O
Technical O
Memorandum O
80237 O
– O
A O
Spin O
- O
Recovery O
Parachute O
System O
for O
Light O
General O
- O
Aviation O
Airplanes B-asset
by O
Charles O
F O
. O

Bradshaw O
, O

Langley O
Research O
Center O
, O

Hampton O
, O

Virginia O
– O
CS O
- O
23 O
Book O
2 O
, O

Flight O
Test O
Guide O
– O
USNTPS O
- O
FTM O
- O
No O
. O

103 O
U O
. O

S O
. O

NAVAL O
TEST O
PILOT O
SCHOOL O
– O
FLIGHT O
TEST O
MANUAL O
– O
FIXED O
WING O
STABILITY O
AND O
CONTROL O
, O

Theory O
and O
Flight O
Test O
Techniques O
. O

Naval O
Air O
Warfare O
Center O
Aircraft O
Division O
, O

Patuxent O
River O
, O

MD O
January O
1997 O
– O
Ralph O
D O
. O

Kimberlin O
: O
Flight O
Testing O
of O
Fixed O
- O
Wing O
Aircraft B-asset
, O

AIAA O
Education O
series O
, O

2003 O
5 O
. O

Configuration O
of O
the O
prototype O
The O
configuration O
of O
the O
prototype O
is O
schematically O
described O
in O
the O
table O
below O
. O

Test O
configuration O
table O
: O
NOTE O
: O
AoA O
and O
slip O
- O
flags O
may O
be O
attached O
to O
the O
swivel O
- O
head O
pitot B-component
tube I-component
Details O
of O
how O
the O
Configuration O
management O
will O
take O
place O
are O
described O
in O
the O
appendix O
. O

( O
NOTE O
: O
configuration O
management O
procedures O
normally O
are O
not O
the O
part O
of O
the O
Flight O
Test O
Program O
. O

) O
NOTE O
: O
The O
prototype O
, O

and O
its O
configuration O
is O
under O
the O
responsibility O
of O
the O
Design O
Organization O
iaw O
. O

21 O
. O

A O
. O

33 O
. O

6 O
. O

Flight O
test O
team O
composition O
Classification O
of O
Flight O
Test O
Pilots O
and O
Engineers O
as O
well O
as O
mechanics O
involved O
in O
flight O
test O
campaign O
. O

Notes O
: O
( O
1 O
) O
Experience O
: O
1600 O
flight O
hours B-measurement
on O
CS O
- O
23 O
aircrafts B-asset
, O

400 O
hours B-measurement
as O
instructor O
and O
150 O
during O
flight O
testing O
, O

aerobatic O
rating O
( O
2 O
) O
Experience O
: O
600 O
flight O
hours B-measurement
( O
3 O
) O
Experience O
: O
800 O
flight O
hours B-measurement
( O
4 O
) O
Leading O
Flight O
Test O
Engineer O
( O
5 O
) O
Chief O
of O
CS O
( O
6 O
) O
Mechanic O
All O
the O
members O
of O
Flight O
Test O
Team O
have O
received O
special O
egress O
training O
iaw O
. O

FAA O
Order O
8900 O
, O

Volume O
3 O
, O

Chapter O
4 O
, O

“ O
Flight O
crew O
General O
Emergency O
Training O
Curriculum O
Segments O
” O
Records O
of O
all O
the O
training O
can O
be O
found O
in O
… O
NOTE O
: O
( O
put O
the O
reference O
here O
for O
the O
personal O
file O
; O
e O
. O

g O
. O

Training O
records O
are O
stored O
in O
computer O
files O
as O
well O
as O
in O
“ O
hard O
copy O
” O
. O

A O
summary O
document O
about O
the O
trainings O
can O
be O
found O
on O
the O
company O
’ O
s O
local O
network O
. O

) O
Responsibilities O
of O
personnel O
can O
be O
also O
described O
here O
. O

Details O
of O
available O
maintenance O
personnel O
( O
staff O
number O
, O

list O
of O
certifying O
staff O
) O
also O
can O
be O
described O
in O
present O
paragraph O
. O

7 O
. O

Facilities O
The O
airport O
for O
test O
flights O
and O
test O
airspace O
are O
described O
here O
. O

NOTE O
: O
The O
information O
may O
be O
found O
in O
AIP O
, O

or O
in O
data O
provided O
by O
airport O
operator O
. O

Local O
Airfield O
( O
Home O
Base O
) O
Runways O
: O
Other O
airfield O
Other O
airfield O
is O
used O
as O
an O
alternate O
airport O
during O
flight O
tests O
. O

Runways O
: O
Hangar O
In O
this O
paragraph O
, O

the O
following O
points O
will O
be O
defined O
: O
– O
General O
description O
– O
Layout O
– O
Protection O
of O
the O
test O
aircraft B-asset
Rescue O
and O
safety O
equipment O
This O
point O
will O
contain O
all O
the O
required O
safety O
equipment O
. O

– O
Description O
the O
location O
of O
fire O
extinguishers O
, O

first O
aid O
kits O
, O

or O
other O
rescue O
and O
safety O
equipment O
. O

– O
Ground O
personnel O
protection O
( O
visors O
, O

helmets O
, O

headphones O
) O
– O
Description O
of O
fire O
station O
and O
ambulance O
station O
’ O
s O
notification O
procedures O
( O
about O
the O
test O
flights O
) O
. O

– O
Classification O
the O
responsible O
search O
and O
rescue O
service O
. O

– O
Permanently O
installed O
safety O
equipment O
( O
on O
- O
board O
) O
( O
seat O
belt O
, O

ELT O
, O

pilot O
parachute O
, O

crash O
axe O
, O

etc O
. O

) O
– O
Specific O
safety O
provisions O
for O
the O
prototype O
( O
jettisonable O
canopy O
, O

parachutes O
) O
– O
Special O
safety O
equipment O
( O
life O
vests O
, O

survival O
kit O
, O

oxygen O
bottle O
, O

etc O
. O

) O
– O
Operation O
rules O
for O
a O
chase O
plane B-asset
Emergency O
response O
plan O
Aims O
of O
Emergency O
Response O
Plan O
( O
ERP O
) O
: O
– O
highlight O
the O
policies O
and O
procedures O
to O
be O
implemented O
in O
case O
of O
a O
crisis O
, O

– O
offer O
advice O
to O
the O
members O
of O
the O
crisis O
management O
team O
in O
carrying O
out O
their O
responsibilities O
, O

– O
communicate O
relevant O
information O
to O
employees O
of O
the O
organization O
and O
members O
of O
the O
public O
. O

NOTE O
: O
The O
ERP O
might O
be O
designed O
as O
a O
separate O
document O
or O
part O
of O
the O
test O
program O
, O

according O
to O
the O
decision O
of O
the O
applicant O
. O

As O
opposed O
to O
other O
manuals O
of O
the O
company O
, O

the O
ERP O
manual O
is O
designed O
to O
cover O
crisis O
situations O
which O
cannot O
specifically O
or O
precisely O
be O
defined O
. O

An O
organizational O
framework O
of O
the O
actions O
and O
policies O
required O
to O
be O
implemented O
is O
presented O
. O

However O
, O

it O
is O
unlikely O
that O
an O
actual O
emergency O
situation O
will O
adapt O
to O
a O
precise O
framework O
. O

Adaptability O
and O
flexibility O
should O
therefore O
be O
demonstrated O
in O
the O
handling O
of O
such O
events O
. O

The O
following O
events O
may O
result O
in O
a O
crisis O
situation O
and O
activate O
the O
Emergency O
Response O
Plan O
: O
– O
Aviation B-asset
accident O
/ O
Serious O
incident O
– O
Disaster O
in O
the O
premises O
: O
Fire O
, O

explosion O
, O

pollution O
, O

flood O
– O
Loss O
of O
the O
working O
resource O
: O
workshop O
, O

offices O
, O

hangar O
, O

aircraft B-asset
– O
Impacts O
of O
a O
disaster O
within O
the O
vicinity O
of O
the O
establishment O
– O
Climatic O
event O
: O
snow O
, O

storm O
, O

flood O
, O

lightning O
– O
Natural O
disaster O
: O
earthquake O
, O

volcanic O
eruption O
– O
Food O
poisoning O
, O

epidemic O
– O
Death O
at O
the O
workplace O
– O
Multiple O
victims O
connected O
to O
a O
disaster O
, O

illness O
or O
contagion O
– O
Accident O
to O
the O
public O
transportation O
of O
the O
personnel O
– O
Social O
movements O
: O
strike O
, O

blocking O
of O
the O
accesses O
– O
Internal O
or O
external O
threat O
: O
Attack O
, O

bomb O
alert O
, O

sabotage O
, O

terrorism O
, O

– O
Loss O
of O
energy O
: O
electricity O
, O

gas O
– O
Loss O
of O
communication O
means O
: O
internet O
, O

landlines O
or O
mobile O
telephones O
– O
Major O
media O
event O
– O
Accident O
during O
missions O
: O
business O
trip O
, O

abroad O
. O

Proposed O
parts O
of O
ERP O
: O
1 O
. O

Definitions O
( O
use O
ICAO O
Annex O
13 O
, O

Chapter O
1 O
for O
reference O
) O
2 O
. O

Organizing O
emergency O
responses O
( O
checklists O
, O

list O
of O
managers O
to O
notify O
, O

etc O
. O

) O
3 O
. O

Emergency O
call O
action O
4 O
. O

Crisis O
management O
; O
roles O
of O
crisis O
management O
5 O
. O

Rules O
of O
internal O
and O
external O
communication O
6 O
. O

Egress O
training O
schedule O
and O
rules O
8 O
. O

Test O
instrumentation O
and O
configuration O
a O
. O

Test O
instrumentation O
See O
the O
table O
below O
; O
this O
table O
will O
summarize O
the O
configurations O
during O
the O
flight O
test O
campaign O
. O

NOTE O
: O
“ O
I0 O
– O
instrumentation O
” O
is O
the O
basic O
applied O
instrumentation O
for O
the O
flight O
test O
campaign O
. O

In O
the O
column O
“ O
priority O
” O
there O
is O
a O
priority O
index O
for O
each O
equipment O
. O

The O
meaning O
: O
lower O
numbers O
- O
higher O
priority O
- O
“ O
must O
have O
” O
equipment O
. O

NOTE O
: O
if O
the O
aircraft B-asset
is O
designed O
with O
“ O
glass O
- O
cockpit O
” O
, O

and O
the O
system O
has O
the O
capability O
to O
log O
to O
an O
SD O
card O
, O

it O
can O
be O
acceptable O
for O
use O
as O
long O
as O
its O
suitability O
is O
assessed O
. O

b O
. O

Test O
aircraft O
configuration O
Test O
aircraft B-asset
configuration O
is O
like O
the O
production O
aircraft B-asset
; O
exceptions O
are O
noted O
in O
chapter O
7 O
. O

9 O
. O

Test O
airspace O
Flight O
tests O
will O
be O
executed O
in O
a O
separated O
airspace O
10 O
NM O
from O
ZZZZ O
airport O
. O

The O
area O
is O
unpopulated O
, O

the O
next O
inhabited O
area O
is O
XXX O
, O

in O
the O
direction O
of O
N O
/ O
S O
/ O
W O
/ O
E O
in O
a O
distance O
of O
YY O
NM O
. O

( O
Or O
defined O
by O
the O
responsible O
ATS O
unit O
. O

) O
Temporary O
airspace O
limitations O
might O
be O
requested O
from O
the O
national O
aeronautical O
navigation O
company O
, O

and O
issued O
in O
NOTAMs O
. O

10 O
. O

Timeline O
of O
the O
flight O
test O
a O
. O

The O
planned O
steps O
of O
the O
flight O
tests O
are O
the O
following O
: O
NOTE O
: O
the O
phases O
are O
the O
following O
: O
 O
Phase1 O
: O
first O
flights O
; O
preliminary O
performances O
, O

handling O
qualities O
, O

If O
necessary O
, O

a O
“ O
Phase O
1b O
” O
also O
could O
be O
added O
between O
Phase O
1 O
and O
2 O
. O

This O
phase O
has O
the O
same O
limitations O
as O
“ O
Phase O
1 O
” O
, O

except O
the O
wider O
CG O
range O
. O

 O
Phase2 O
: O
performances O
in O
various O
flight O
phases O
 O
Phase3 O
: O
assessing O
the O
limitations O
, O

extend O
the O
flight B-parameter
envelope I-parameter
to O
its O
limits O
. O

Between O
each O
steps O
, O

there O
are O
breakpoints O
; O
each O
breakpoints O
will O
include O
an O
assessment O
about O
the O
continuation O
of O
the O
program O
. O

If O
the O
airplane B-asset
fails O
any O
of O
the O
pass O
/ O
fail O
criteria O
; O
the O
part O
of O
the O
test O
program O
should O
be O
repeated O
. O

For O
each O
part O
of O
the O
flight O
test O
campaign O
, O

different O
flight O
conditions O
may O
be O
applicable O
. O

An O
example O
for O
that O
is O
shown O
below O
: O
Phase O
1 O
: O
Limitations O
( O
design O
value O
are O
shown O
in O
brackets O
for O
comparison O
) O
– O
Never O
exceed O
speed B-parameter
VNE O
: O
130 O
kts B-measurement
( O
160 O
kts B-measurement
) O
– O
Manoeuvring O
speed B-parameter
VA O
: O
90 O
kts B-measurement
( O
100 O
kts B-measurement
) O
– O
VNO O
: O
110 O
kts B-measurement
( O
120 O
kts B-measurement
) O
– O
Crosswind O
component O
limit O
: O
5 O
kts B-measurement
– O
Max O
. O

manoeuvring O
load B-parameter
factors O
: O
+ O
1 O
. O

5 O
/ O
– O
1 O
( O
+ O
4 O
/ O
– O
2 O
) O
– O
Max O
. O

operating O
altitude B-parameter
: O
5000 O
feet B-measurement
( O
13000 O
feet B-measurement
) O
– O
MTOM O
: O
520 O
kg B-measurement
( O
600 O
kg B-measurement
) O
– O
Flight B-parameter
centre I-parameter
of I-parameter
gravity I-parameter
limits O
: O
29 O
. O

7 O
– O
34 O
. O

9 O
centimetres B-measurement
aft O
of O
datum O
( O
24 O
– O
39 O
cm B-measurement
aft O
of O
datum O
) O
– O
Air O
crew O
: O
1 O
pilot O
( O
1 O
+ O
1 O
) O
– O
Airspace O
: O
10 O
NM O
radius O
of O
ZZZZ O
airfield O
, O

avoiding O
inhabited O
areas O
Phase O
1b O
: O
Limitations O
( O
design O
value O
are O
shown O
in O
brackets O
for O
comparison O
) O
– O
Never O
exceed O
speed B-parameter
VNE O
: O
130 O
kts B-measurement
( O
160 O
kts B-measurement
) O
– O
Manoeuvring B-parameter
speed I-parameter
VA O
: O
90 O
kts B-measurement
( O
100 O
kts B-measurement
) O
– O
VNO O
: O
110 O
kts B-measurement
( O
120 O
kts B-measurement
) O
– O
Crosswind O
component O
limit O
: O
5 O
kts B-measurement
( O
15 O
kts B-measurement
) O
– O
Max O
. O

manoeuvring O
load B-parameter
factors O
: O
+ O
2 O
/ O
– O
1 O
( O
+ O
4 O
/ O
– O
2 O
) O
– O
Max O
. O

operating O
altitude B-parameter
: O
5000 O
feet B-measurement
( O
13000 O
feet B-measurement
) O
– O
MTOM O
: O
520 O
kg B-measurement
( O
600 O
kg B-measurement
) O
– O
Flight B-parameter
centre I-parameter
of I-parameter
gravity I-parameter
limits O
: O
24 O
– O
39 O
centimetres B-measurement
aft O
of O
datum O
– O
Air O
crew O
: O
1 O
pilot O
( O
1 O
+ O
1 O
) O
– O
Airspace O
: O
10 O
NM O
radius O
of O
ZZZZ O
airfield O
, O

avoiding O
inhabited O
areas O
Phase O
2 O
: O
Limitations O
( O
design O
value O
are O
shown O
in O
brackets O
for O
comparison O
) O
– O
Never O
exceed O
speed B-parameter
VNE O
: O
145 O
kts B-measurement
( O
160 O
kts B-measurement
) O
– O
Manoeuvring B-parameter
speed I-parameter
VA O
: O
100 O
kts B-measurement
– O
VNO O
: O
120 O
kts B-measurement
– O
Crosswind O
component O
limit O
: O
5 O
kts B-measurement
( O
15 O
kts B-measurement
) O
– O
Max O
. O

manoeuvring O
load B-parameter
factors O
: O
+ O
2 O
/ O
– O
1 O
. O

5 O
( O
+ O
4 O
/ O
– O
2 O
) O
– O
Max O
. O

operating O
altitude B-parameter
: O
8000 O
feet B-measurement
( O
13000 O
feet B-measurement
) O
– O
MTOM O
: O
600 O
kg B-measurement
– O
Flight B-parameter
centre I-parameter
of I-parameter
gravity I-parameter
limits O
: O
24 O
– O
39 O
centimetres B-measurement
aft O
of O
datum O
( O
different O
value O
can O
be O
used O
, O

see O
flight O
test O
order O
) O
– O
Air O
crew O
: O
1 O
pilot O
+ O
1engineer O
( O
if O
needed O
) O
– O
Airspace O
: O
10 O
NM O
radius O
of O
ZZZZ O
airfield O
, O

avoiding O
inhabited O
areas O
Phase O
3 O
Limitations O
( O
design O
value O
are O
shown O
in O
brackets O
for O
comparison O
) O
– O
Never O
exceed O
speed B-parameter
VNE O
: O
160 O
kts B-measurement
– O
Manoeuvring B-parameter
speed I-parameter
VA O
: O
100 O
kts B-measurement
– O
VNO O
: O
120 O
kts B-measurement
– O
Crosswind O
component O
limit O
: O
15 O
kts B-measurement
– O
Max O
. O

manoeuvring B-parameter
load I-parameter
factors O
: O
+ O
4 O
/ O
2 O
– O
Max O
. O

operating O
altitude B-parameter
: O
13000 O
feet B-measurement
– O
MTOM O
: O
600 O
kg B-measurement
– O
Flight B-parameter
centre I-parameter
of I-parameter
gravity I-parameter
limits O
: O
24 O
– O
39 O
centimetres O
aft O
of O
datum B-parameter
– O
Air B-component
crew I-component
: O
1 O
pilot O
+ O
1 O
engineer O
( O
if O
needed O
) O
– O
Airspace O
: O
10 O
NM O
radius O
of O
ZZZZ O
airfield O
, O

avoiding O
inhabited O
areas O
b O
. O

Preconditions O
of O
flight O
tests O
Flight O
tests O
can O
be O
conducted O
, O

when O
: O
– O
static O
tests O
of O
wing B-system
, O

fuselage B-system
, O

empennages B-component
are O
done O
( O
within O
the O
initial O
limited O
flight B-parameter
envelope I-parameter
, O

it O
may O
acceptable O
that O
some O
static O
tests O
are O
not O
completed O
. O

A O
proposal O
, O

supported O
by O
an O
engineering O
rationale O
, O

should O
be O
agreed O
with O
the O
Agency O
. O

Supporting O
analysis O
, O

similarity O
with O
previously O
approved O
design O
, O

simplicity O
of O
the O
design O
can O
be O
used O
to O
support O
the O
rationale O
. O

Service O
experience O
is O
not O
normally O
, O

alone O
, O

a O
valid O
argument O
) O
– O
Control B-control
system I-control
static O
and O
operation O
tests O
are O
done O
; O
– O
An O
analysis O
at O
least O
of O
the O
Landing B-system
gear I-system
strength O
and O
absorption O
capability O
– O
Flutter O
analysis O
supported O
by O
GVT O
( O
a O
preliminary O
analysis O
can O
be O
acceptable O
within O
the O
limited O
envelope O
, O

but O
before O
full O
opening O
of O
the O
envelope O
, O

the O
full O
analysis O
shall O
be O
agreed O
by O
the O
agency O
) O
; O
– O
Before O
first O
flight O
, O

a O
maintenance O
check O
must O
be O
carried O
out O
. O

After O
engine B-system
ground O
run O
, O

all O
the O
operational O
fluids O
( O
fuel O
, O

oil O
, O

coolant O
) O
must O
be O
drained O
, O

and O
inspected O
for O
contamination O
, O

particles O
, O

etc O
. O

– O
Ground O
tests O
of O
the O
powerplant B-system
systems I-system
are O
completed O
; O
– O
Ground O
tests O
of O
the O
avionic B-system
systems I-system
are O
completed O
; O
– O
Test O
aircraft O
configuration O
properly O
documented O
; O
( O
the O
above O
set O
of O
tests O
/ O
analyses O
can O
vary O
significantly O
from O
project O
to O
project O
. O

A O
proposal O
shall O
be O
agreed O
in O
advance O
with O
the O
Agency O
. O

For O
this O
reason O
it O
is O
important O
that O
this O
document O
is O
drafted O
in O
a O
fairly O
early O
phase O
of O
the O
project O
) O
. O

c O
. O

Schedule O
of O
flights O
N O
/ O
A O
– O
the O
test O
point O
is O
not O
directly O
performed O
for O
certification O
( O
development O
flight O
) O
( O
for O
example O
: O
Flights O
aimed O
to O
go O
through O
a O
stepped O
approach O
to O
the O
compliance O
test O
point O
are O
also O
considered O
development O
flight O
: O
stalls O
at O
mid O
CG O
, O

ceiling O
flights O
, O

general O
flight O
characteristics O
, O

etc O
. O

) O
Some O
paragraph O
from O
the O
requirements O
are O
not O
covered O
with O
particular O
flight O
tasks O
, O

these O
parameters O
will O
be O
observed O
throughout O
the O
complete O
flight O
test O
program O
. O

Observations O
and O
reports O
are O
reported O
into O
a O
document O
named O
“ O
Qualitative O
pilot O
statements O
” O
( O
example O
: O
assessment O
of O
the O
cockpit O
accessibility O
and O
visibility O
) O
. O

11 O
. O

Flight O
test O
orders O
Normally O
, O

the O
test O
plan O
must O
contain O
the O
flight O
test O
orders O
( O
for O
each O
flight O
) O
, O

each O
flight O
test O
order O
must O
contain O
the O
flight O
test O
cards O
( O
for O
each O
test O
points O
) O
. O

Each O
test O
order O
will O
contain O
the O
following O
parts O
: O
– O
Sequence O
of O
planning O
of O
flights O
– O
If O
the O
flights O
are O
certification O
flights O
, O

a O
reference O
to O
the O
applicable O
requirements O
– O
Method O
of O
test O
flight O
– O
Weight B-parameter
and O
balance O
settings O
– O
Required O
weather O
conditions O
( O
and O
log O
for O
the O
actual O
) O
– O
Required O
facilities O
and O
airspace O
– O
Designated O
crew O
( O
pilot O
, O

engineer O
) O
– O
Communication O
rules O
( O
frequencies O
) O
– O
Aircraft B-asset
configuration O
and O
instrumentation O
– O
Specific O
limitations O
for O
the O
flights O
– O
Emergency O
procedures O
, O

risk O
mitigation O
– O
Test O
points O
, O

limits O
, O

and O
assessments O
– O
Flight O
profile O
– O
Test O
cards O
for O
each O
flight O
For O
a O
test O
card O
example O
; O
see O
part O
14 O
of O
Appendix O
. O

For O
risk O
mitigation O
example O
, O

see O
part O
10 O
. O

of O
the O
Appendix O
. O

Appendix O
1 O
– O
Organisational O
aspects O
This O
appendix O
is O
intended O
to O
provide O
guidance O
for O
applicants O
without O
a O
Flight O
Test O
Organization O
( O
and O
a O
DOA O
) O
. O

In O
fact O
, O

the O
aspects O
treated O
here O
are O
normally O
treated O
in O
the O
FTOM O
. O

In O
case O
a O
Flight O
test O
organization O
is O
not O
in O
place O
, O

the O
content O
of O
this O
appendix O
can O
be O
used O
to O
complement O
the O
flight O
test O
program O
. O

This O
appendix O
can O
be O
seen O
as O
a O
“ O
small O
” O
FTOM O
. O

1 O
. O

Special O
tools O
and O
equipment O
– O
Data O
source O
summary O
The O
table O
shown O
below O
list O
all O
special O
/ O
measurement O
equipment O
typically O
used O
and O
its O
purpose O
. O

All O
measurement O
equipment O
shall O
be O
calibrated O
( O
see O
21 O
. O

A O
. O

33 O
2 O
. O

) O
. O

( O
1 O
) O
Picture O
could O
be O
inserted O
there O
( O
2 O
) O
Picture O
, O

or O
engineering O
drawing O
could O
be O
inserted O
there O
2 O
. O

Airfield O
assessment O
It O
is O
recommended O
, O

that O
for O
the O
first O
flights O
the O
airport O
must O
be O
obstacle O
- O
free O
. O

Aspects O
like O
obstacles O
and O
suitability O
of O
the O
areas O
for O
emergency O
landing O
( O
Congested O
areas O
, O

lakes O
, O

uncultivated O
lands O
, O

pits O
, O

etc O
. O

) O
shall O
be O
assessed O
and O
noted O
on O
a O
VFR O
chart O
( O
or O
even O
a O
google O
map O
picture O
! O
! O
) O
. O

An O
example O
below O
. O

3 O
. O

Requirement O
of O
Flight O
Test O
Team O
Below O
2000 O
kg B-measurement
of O
MTOW O
, O

there O
is O
no O
specific O
requirement O
in O
qualifications O
and O
/ O
or O
flight B-parameter
hours I-parameter
. O

Although O
, O

the O
applicant O
should O
establish O
its O
rules O
about O
selection O
of O
crewmembers O
. O

E O
. O

g O
. O

Flight B-parameter
hours I-parameter
, O

previous O
experience O
, O

aerobatic O
rating O
( O
iaw O
. O

FCL O
. O

800 O
) O
, O

etc O
. O

4 O
. O

Phases O
of O
the O
flight O
tests O
This O
section O
defines O
how O
the O
Flight O
Test O
Campaign O
phases O
are O
organized O
and O
the O
general O
criteria O
for O
the O
opening O
of O
the O
envelope O
. O

Since O
, O

these O
aspects O
have O
been O
already O
addressed O
in O
the O
core O
part O
of O
the O
document O
, O

they O
will O
not O
be O
treated O
in O
this O
appendix O
. O

5 O
. O

Strategy O
for O
extension O
of O
the O
flight B-parameter
envelope I-parameter
The O
extension O
of O
the O
envelope O
will O
be O
done O
step O
by O
step O
. O

– O
Familiarization O
: O
In O
this O
phase O
the O
flight O
test O
crew O
familiarizes O
themselves O
with O
the O
aircraft O
, O

its O
controls O
, O

and O
the O
evacuation O
procedures O
– O
Ground O
tests O
: O
In O
this O
phase O
, O

necessary O
ground O
tests O
before O
the O
first O
flight O
will O
be O
performed O
( O
wing B-system
static O
test O
, O

control B-system
system I-system
test O
, O

etc O
. O

) O
– O
First O
flight O
: O
The O
demonstration O
of O
the O
aircraft B-asset
is O
capable O
for O
flight O
– O
Stability O
, O

handling O
. O

First O
with O
limited O
CG O
range O
, O

and O
limited O
weight B-parameter
– O
Extending O
the O
stability O
and O
handling O
tests O
to O
the O
whole O
CG O
range O
– O
Performances O
( O
take O
- O
off O
, O

landing O
, O

go O
- O
around O
, O

climbing O
, O

gliding O
characteristics O
) O
– O
Extending O
the O
flight B-parameter
envelope I-parameter
( O
flutter O
assessment O
, O

stalls O
, O

spins O
, O

flights O
around O
– O
and O
beyond O
- O
VNE O
) O
6 O
. O

Briefing O
rules O
A O
flight O
test O
order O
will O
be O
filled O
for O
each O
flight O
. O

This O
order O
contains O
data O
about O
: O
– O
the O
flight O
test O
team O
– O
their O
medical O
fitness O
for O
the O
particular O
task O
– O
the O
predefined O
sequence O
of O
tasks O
( O
and O
referring O
flight O
test O
cards O
) O
– O
the O
flight O
profile O
– O
weight O
and O
balance O
information O
– O
limitations O
applicable O
to O
that O
flight O
– O
emergency O
procedures O
– O
aircraft O
’ O
s O
status O
and O
maintenance O
release O
for O
the O
test O
– O
test O
points O
and O
test O
methods O
, O

assessment O
methods O
( O
See O
the O
Cooper O
- O
Harper O
handling O
scale O
for O
reference O
) O
After O
filling O
the O
flight O
test O
order O
, O

a O
daily O
briefing O
will O
be O
commenced O
. O

It O
will O
cover O
: O
– O
the O
points O
of O
the O
flight O
test O
order O
– O
establishing O
the O
flight O
test O
cards O
– O
the O
meteorological O
situation O
– O
the O
proposed O
actions O
in O
an O
emergency O
– O
check O
- O
up O
of O
necessary O
documents O
( O
aircraft O
, O

personnel O
) O
7 O
. O

Handling O
qualities O
assessment O
example O
Figure O
1 O
– O
Cooper O
- O
Harper O
handling O
scale O
Example O
: O
Ground O
stability O
and O
control O
tests O
to O
see O
compliance O
against O
4 O
. O

7 O
. O

1 O
and O
4 O
. O

7 O
. O

2 O
of O
ASTM O
F2245 O
. O

The O
aim O
of O
the O
test O
: O
evaluate O
the O
aircraft O
’ O
s O
controllability O
on O
ground O
and O
show O
, O

that O
the O
pilot O
is O
able O
to O
maintain O
the O
direction O
of O
taxiing O
. O

The O
pilot O
should O
assess O
these O
questions O
on O
the O
left O
side O
of O
the O
diagram O
: O
– O
Is O
it O
controllable O
? O
Is O
the O
pilot O
able O
to O
maintain O
the O
centreline O
of O
the O
runway O
? O
If O
yes O
, O

move O
to O
the O
next O
question O
; O
– O
Is O
adequate O
performance O
attainable O
with O
a O
tolerable O
pilot O
workload O
? O
Does O
the O
aircraft B-asset
run O
in O
the O
direction O
, O

are O
there O
any O
tendency O
to O
steer O
left O
or O
right O
? O
Does O
the O
pilot O
need O
to O
correct O
the O
movements O
? O
If O
the O
aircraft B-asset
could O
maintain O
the O
direction O
, O

move O
to O
the O
next O
; O
– O
Is O
it O
satisfactory O
without O
improvement O
? O
If O
yes O
, O

see O
, O

how O
many O
pilot O
compensations O
is O
needed O
to O
maintain O
the O
centreline O
. O

Scale O
it O
between O
1 O
– O
3 O
8 O
. O

Workload O
assessment O
( O
if O
necessary O
) O
Normally O
, O

workload O
assessment O
is O
not O
a O
part O
of O
the O
certification O
of O
a O
Light O
Sport O
Airplane B-asset
. O

Although O
, O

when O
the O
applicant O
intends O
to O
use O
special O
conditions O
( O
e O
. O

g O
. O

Night O
VFR O
) O
or O
intends O
to O
use O
special O
equipment O
, O

the O
pilot O
workload O
should O
be O
assessed O
. O

Assessment O
methods O
: O
There O
are O
many O
workload O
assessment O
techniques O
, O

a O
few O
example O
is O
shown O
. O

A O
. O

NASA O
Task O
Load O
Index O
( O
TLX O
) O
: O
http O
: O
/ O
/ O
humansystems O
. O

arc O
. O

nasa O
. O

gov O
/ O
groups O
/ O
tlx O
/ O
B O
. O

Bedford O
rating O
scale O
: O
See O
para O
0 O
for O
“ O
best O
practices O
” O
C O
. O

Heart O
- O
rate O
variability O
examination O
; O
see O
articles O
and O
papers O
about O
it O
: O
[ O
1 O
] O
M O
. O

H O
. O

Asyali O
, O

Discrimination O
Power O
of O
Long O
- O
Term O
Heart O
Rate O
Variability O
Measures O
, O

Proceedings O
of O
the O
25th O
Annual O
International O
Conference O
of O
the O
IEEE O
Engineering O
in O
Medicine O
and O
Biology O
Society O
, O

pp O
. O

200 O
– O
203 O
, O

Cancún O
, O

México O
, O

September O
17 O
– O
21 O
, O

2003 O
. O

[ O
2 O
] O
Bansevicius O
D O
, O

Westgaard O
RH O
, O

Jensen O
C O
, O

Mental O
Stress O
of O
Long O
Duration O
: O
EMG O
Activity O
, O

Perceived O
Tension O
, O

Fatigue O
, O

and O
Pain O
Development O
in O
Pain O
- O
Free O
Subjects O
, O

Medline O
, O

Headache O
, O

Volume O
37 O
, O

Issue O
8 O
, O

pp O
. O

499 O
– O
510 O
, O

1997 O
. O

[ O
3 O
] O
L O
. O

Izsó O
, O

Developing O
Evaluation O
Methodologies O
for O
Human O
- O
Computer O
Interaction O
( O
INTERFACE O
) O
, O

Delft O
University O
Press O
, O

2001 O
. O

NOTE O
: O
for O
method O
“ O
C O
” O
, O

proper O
crew O
( O
aviation O
psychologist O
) O
and O
equipment O
( O
ECG O
) O
is O
essential O
. O

9 O
. O

Post O
flight O
data O
processing O
This O
section O
should O
define O
how O
the O
data O
are O
post O
processed O
. O

For O
examples O
: O
– O
Airspeed B-parameter
correction O
method O
( O
for O
errors O
) O
– O
Engine B-parameter
power I-parameter
corrections O
to O
ISA O
( O
for O
performance O
calculations O
– O
air B-parameter
temperature I-parameter
affects O
density O
what O
affects O
power B-parameter
– O
a O
brief O
method O
how O
to O
do O
it O
) O
– O
Temperature B-parameter
and O
altitude B-parameter
graph O
( O
for O
density O
altitude B-parameter
and O
ISA O
calculations O
) O
10 O
. O

Safety O
management O
/ O
risk O
assessment O
This O
section O
should O
explain O
how O
the O
safety O
of O
the O
flight O
is O
managed O
. O

In O
this O
case O
, O

the O
Appendices O
C O
and O
D O
of O
FAA O
Order O
4040 O
. O

26B O
have O
been O
followed O
. O

Further O
information O
on O
Risk O
Management O
can O
also O
be O
found O
in O
various O
sources O
, O

for O
example O
, O

in O
the O
EHEST O
SMS O
Toolkit O
. O

Identify O
a O
person O
responsible O
of O
the O
safety O
: O
it O
is O
advised O
to O
identify O
a O
“ O
safety O
manager O
” O
, O

that O
will O
be O
responsible O
over O
the O
“ O
safe O
” O
execution O
of O
the O
whole O
flight O
test O
campaign O
through O
the O
proper O
implementation O
of O
the O
established O
procedures O
. O

Identify O
the O
test O
technique O
involved O
: O
Generally O
, O

the O
risk O
associated O
with O
a O
specific O
flight O
test O
, O

is O
dependent O
, O

among O
others O
, O

on O
the O
specific O
flying O
test O
techniques O
. O

However O
, O

there O
may O
be O
risks O
associated O
with O
flying O
a O
test O
airplane B-asset
that O
result O
strictly O
from O
the O
airplane B-asset
’ O
s O
configuration O
or O
the O
environment O
into O
which O
it O
is O
flown O
and O
these O
sources O
of O
risk O
must O
also O
be O
considered O
. O

Identify O
the O
hazard O
( O
s O
) O
associated O
with O
the O
test O
technique O
: O
Ask O
“ O
What O
adverse O
events O
might O
happen O
when O
accomplishing O
this O
test O
technique O
? O
” O
Note O
that O
one O
test O
technique O
may O
have O
several O
hazards O
and O
each O
should O
be O
addressed O
( O
e O
. O

g O
. O

, O

another O
hazard O
with O
this O
test O
technique O
would O
be O
engine B-system
failure O
caused O
by O
inlet O
distortion O
, O

or O
fuel O
starvation O
, O

or O
the O
aircraft B-asset
may O
enter O
into O
spin O
during O
a O
stall O
characteristic O
test O
) O
. O

List O
the O
cause O
of O
each O
hazard O
: O
Ask O
“ O
Why O
might O
the O
hazard O
happen O
? O
” O
List O
the O
effect O
of O
each O
hazard O
: O
Ask O
“ O
What O
will O
be O
the O
effect O
? O
” O
These O
should O
be O
related O
to O
either O
injury O
/ O
loss O
of O
life O
or O
damage O
to O
aircraft B-asset
/ O
property O
. O

Perform O
a O
subjective O
risk O
assessment O
by O
: O
( O
1 O
) O
Estimating O
the O
probability O
of O
each O
hazard O
occurring O
. O

Defined O
as O
improbable O
, O

remote O
, O

occasional O
, O

probable O
, O

or O
frequent O
. O

( O
2 O
) O
Estimating O
the O
severity O
of O
each O
hazard O
, O

if O
it O
occurs O
. O

Defined O
as O
no O
safety O
effect O
, O

minor O
, O

major O
, O

hazardous O
, O

or O
catastrophic O
. O

( O
3 O
) O
Defining O
the O
risk O
of O
each O
hazard O
as O
a O
combination O
of O
the O
probability O
and O
severity O
. O

Defined O
as O
low O
, O

medium O
, O

high O
, O

or O
avoid O
. O

Describe O
the O
steps O
for O
Mitigation O
of O
causes O
for O
each O
hazard O
: O
Develop O
controls O
that O
mitigate O
all O
risks O
to O
an O
acceptable O
level O
. O

Mitigations O
are O
actions O
to O
minimize O
, O

understand O
, O

prepare O
or O
respond O
to O
causes O
of O
the O
hazards O
. O

They O
can O
be O
in O
the O
form O
of O
actions O
from O
the O
flight O
test O
crew O
or O
information O
developed O
by O
the O
design O
engineers O
( O
e O
. O

g O
. O

, O

lab O
testing O
, O

simulator O
evaluations O
) O
. O

Mitigations O
will O
reduce O
either O
the O
probability O
of O
the O
event O
, O

or O
the O
severity O
of O
the O
effect O
, O

or O
both O
. O

Mitigations O
should O
be O
detailed O
and O
specific O
in O
nature O
. O

Describe O
any O
Emergency O
Procedures O
to O
accomplish O
if O
the O
hazard O
occurs O
, O

despite O
mitigation O
steps O
. O

Document O
and O
verify O
the O
risk O
assessment O
: O
The O
risk O
level O
after O
mitigation O
shall O
be O
highlighted O
and O
classified O
iaw O
. O

the O
table O
below O
and O
it O
shall O
be O
independently O
verified O
. O

Table O
app O
. O

1 O
– O
Summary O
table O
for O
risk O
assessment O
Example O
: O
Stall O
characteristics O
test O
iaw O
. O

ASTM O
F2245 O
- O
12d O
4 O
. O

5 O
. O

7 O
. O

Because O
the O
envelope O
is O
not O
yet O
fully O
opened O
, O

and O
the O
flight O
characteristics O
are O
still O
not O
completely O
determined O
, O

the O
aircraft B-asset
could O
enter O
into O
spin O
and O
could O
not O
be O
able O
to O
recover O
. O

The O
effect O
of O
the O
risk O
could O
be O
fatal O
. O

The O
severity O
is O
class O
“ O
A O
” O
, O

which O
means O
“ O
Destruction O
of O
equipment O
, O

Fatalities O
” O
. O

The O
probability O
of O
that O
effect O
is O
very O
low O
, O

because O
the O
aircraft B-asset
’ O
s O
behaviour O
can O
be O
modelled O
, O

and O
if O
the O
spin O
occurs O
, O

the O
autorotation O
could O
be O
stopped O
with O
proper O
pilot O
technique O
( O
reducing O
power O
, O

using O
rudder O
in O
opposite O
direction O
, O

and O
pushing O
the O
elevator O
to O
decrease O
AoA O
) O
. O

Although O
, O

the O
probability O
is O
low O
, O

the O
only O
action O
is O
that O
the O
pilot O
abandons O
the O
aircraft B-asset
. O

If O
the O
pilot O
cannot O
bail O
out O
before O
a O
certain O
altitude B-parameter
, O

he O
/ O
she O
would O
not O
have O
enough O
time O
to O
jump O
out O
and O
open O
the O
parachute O
. O

So O
it O
’ O
s O
improbable O
, O

but O
may O
occur O
, O

it O
’ O
s O
classification O
is O
“ O
3 O
” O
according O
to O
Table O
app O
. O

3 O
. O

The O
overall O
risk O
classification O
is O
3A O
. O

The O
colour O
of O
the O
3A O
risk O
is O
red O
, O

what O
means O
unacceptable O
. O

( O
See O
Table O
app O
. O

4 O
) O
Because O
the O
kind O
of O
risk O
is O
unacceptable O
, O

it O
must O
be O
mitigated O
. O

– O
The O
stall O
test O
would O
be O
performed O
at O
a O
minimal O
safe O
altitude B-parameter
( O
to O
get O
enough O
time O
to O
bailout O
, O

if O
the O
spin O
is O
unrecoverable O
) O
for O
example O
at O
least O
at O
6000 O
feet B-measurement
( O
1800 O
m B-measurement
) O
above O
ground O
level O
– O
To O
make O
the O
bailout O
easier O
, O

a O
canopy O
or O
door B-system
jettison I-system
system I-system
may O
be O
installed O
. O

– O
Ultimately O
also O
the O
aeroplane B-asset
can O
be O
modified O
, O

adding O
a O
test O
spin O
- O
chute O
or O
a O
BRS O
( O
for O
such O
flights O
the O
crew O
must O
anyway O
wear O
parachutes O
) O
. O

– O
Emergency O
procedures O
shall O
be O
established O
, O

e O
. O

g O
. O

in O
this O
case O
, O

if O
recovery O
attempts O
are O
unsuccessful O
until O
a O
certain O
altitude B-parameter
( O
e O
. O

g O
. O

1500 O
feet B-measurement
AGL O
) O
, O

the O
aircraft B-asset
must O
be O
abandoned O
. O

After O
the O
risk O
management O
, O

the O
situation O
is O
the O
following O
: O
– O
The O
aircraft B-asset
still O
could O
enter O
into O
an O
inadvertent O
and O
unrecoverable O
spin O
. O

The O
possibility O
remains O
3 O
– O
The O
risk O
for O
the O
flight O
crew O
is O
lower O
, O

because O
they O
have O
chance O
to O
save O
their O
lives O
( O
wearing O
parachutes O
, O

abandoning O
the O
aircraft O
is O
easier O
with O
the O
jettisonable O
canopy O
) O
, O

therefore O
the O
only O
outcome O
of O
a O
spin O
accident O
would O
be O
the O
loss O
of O
the O
aircraft B-asset
( O
the O
flights O
were O
planned O
in O
uninhabited O
areas O
– O
see O
point O
11 O
– O
therefore O
the O
only O
endangered O
people O
are O
the O
crew O
on O
board O
) O
. O

The O
severity O
will O
be O
D O
( O
loss O
of O
the O
aircraft O
, O

injuries O
during O
bailout O
– O
applying O
emergency O
procedures O
) O
– O
The O
overall O
risk O
decreases O
to O
3D O
, O

which O
is O
yellow O
- O
coloured O
. O

It O
will O
be O
acceptable O
after O
the O
review O
of O
the O
operations O
Table O
app O
. O

2 O
– O
Example O
of O
use O
of O
risk O
mitigation O
table O
Table O
app O
. O

3 O
– O
Risk O
classification O
table O
Legend O
of O
risk O
( O
and O
colouring O
) O
: O
Table O
app O
. O

4 O
– O
Acceptability O
of O
risks O
In O
the O
probability O
table O
, O

you O
can O
assign O
a O
value O
from O
1 O
to O
5 O
to O
the O
probability O
of O
each O
hazard O
. O

Table O
app O
. O

5 O
– O
Probability O
Severities O
could O
be O
classified O
in O
the O
table O
below O
: O
Table O
app O
. O

6 O
– O
Severity O
classification O
11 O
. O

Configuration O
management O
The O
prototype O
will O
have O
to O
be O
released O
with O
a O
statement O
of O
conformity O
to O
the O
design O
configuration O
identified O
by O
the O
design O
organisation O
. O

The O
conformity O
statement O
will O
be O
( O
normally O
) O
provided O
by O
the O
Production O
Organisation O
. O

After O
this O
step O
, O

the O
airplane B-asset
will O
be O
fully O
managed O
by O
the O
Design O
Organization O
. O

The O
Maintenance O
and O
calibration O
of O
the O
equipment O
will O
be O
performed O
by O
Maintenance O
personnel O
identified O
and O
accepted O
by O
the O
design O
organisation O
. O

The O
Design O
organization O
is O
responsible O
to O
maintain O
a O
current O
list O
of O
scheduled O
maintenance O
tasks O
and O
calibration O
planning O
for O
each O
test B-component
equipment I-component
and O
to O
arrange O
for O
timely O
performance O
of O
those O
tasks O
. O

Each O
modification O
in O
the O
aircraft B-asset
configuration O
shall O
be O
assessed O
against O
: O
– O
The O
safety O
of O
the O
flights O
– O
The O
validity O
of O
the O
approved O
flight O
conditions O
; O
– O
The O
already O
executed O
Flight O
tests O
( O
example O
: O
installation O
of O
vertical B-component
fin I-component
might O
give O
results O
which O
cannot O
be O
compared O
with O
already O
executed O
flights O
) O
; O
– O
The O
already O
executed O
certification O
activities O
( O
example O
: O
reduction O
of O
the O
size O
a O
control O
surface O
might O
invalid O
the O
flutter O
analysis O
) O
Each O
modification O
in O
the O
aircraft B-asset
configuration O
shall O
be O
logged O
into O
the O
technical O
log O
, O

and O
each O
test O
card O
must O
be O
signed O
by O
the O
personnel O
. O

An O
example O
for O
the O
flight O
test O
card O
layout O
can O
be O
found O
in O
the O
paragraph O
14 O
of O
this O
appendix O
. O

At O
the O
moment O
of O
issuing O
of O
this O
document O
, O

the O
prototype O
aircraft O
is O
conforming O
to O
the O
type O
design O
and O
the O
equipment O
corresponds O
to O
the O
designated O
equipment O
list O
items O
, O

except O
: O
– O
A O
spare O
set O
of O
backup B-module
instrumentation I-module
for O
the O
EFIS B-system
– O
Separate O
transponder B-module
instead O
of O
the O
remote O
- O
controlled O
one O
– O
The O
baggage B-module
compartment I-module
is O
modified O
to O
accommodate O
the O
specific O
test B-module
instrumentation I-module
. O

( O
Installed O
instrument O
racks O
, O

removed O
carpets O
, O

etc O
) O
12 O
. O

Maintenance O
procedures O
( O
arrangements O
with O
maintenance O
organizations O
) O
Throughout O
the O
whole O
flight O
test O
campaign O
the O
aircraft B-asset
’ O
s O
maintenance O
tasks O
will O
be O
performed O
in O
accordance O
with O
the O
provisional O
version O
of O
the O
AMM O
( O
iaw O
. O

CS O
- O
LSA O
. O

30 O
– O
ASTM O
F2483 O
- O
12 O
) O
. O

Additional O
inspections O
will O
be O
carried O
out O
according O
to O
the O
flight O
test O
pilot O
’ O
s O
observations O
and O
remarks O
noted O
into O
each O
flight O
report O
. O

Any O
maintenance O
task O
on O
the O
prototype O
will O
be O
performed O
by O
qualified O
personnel O
, O

holding O
a O
proper O
authorization O
. O

Certifying O
Staff O
member O
must O
held O
a O
Part O
- O
66 O
( O
Annex O
III O
. O

Of O
1321 O
/ O
2014 O
EC O
) O
licence O
. O

The O
aircraft B-asset
’ O
s O
technical O
log O
will O
be O
kept O
and O
updated O
as O
soon O
as O
any O
kind O
of O
maintenance O
are O
carried O
out O
. O

Modifications O
in O
configuration O
will O
be O
recorded O
the O
regarding O
section O
of O
the O
following O
flight O
test O
order O
, O

and O
the O
responsible O
person O
for O
the O
design O
must O
declare O
the O
aircraft B-asset
is O
airworthy O
before O
each O
flight O
during O
the O
pre O
- O
flight O
briefing O
by O
signing O
the O
appropriate O
field O
on O
a O
given O
Flight O
Test O
Order O
. O

The O
maintenance O
staff O
preparing O
the O
aircraft B-asset
for O
test O
is O
responsible O
to O
check O
the O
calibration B-parameter
status I-parameter
of O
each O
installed O
test O
equipment O
/ O
test O
instrumentation O
and O
record O
the O
respective O
calibration B-parameter
expiry I-parameter
date I-parameter
in O
the O
referring O
technical O
log O
. O

The O
earliest O
expiry B-parameter
date I-parameter
of O
all O
installed O
test B-component
equipment I-component
shall O
be O
referred O
to O
in O
the O
aircraft B-asset
’ O
s O
conformity O
statement O
( O
“ O
Calibration O
status O
of O
all O
FTE O
/ O
FTI O
has O
been O
checked O
and O
will O
not O
expire O
before O
[ O
date O
] O
” O
) O
. O

13 O
. O

Technical O
log O
example O
14 O
. O

Example O
for O
flight O
test O
card O
preparation O
This O
card O
should O
be O
designed O
in O
a O
DIN O
A5 O
size O
, O

to O
get O
it O
fit O
to O
the O
knee O
block O
. O

The O
test O
point O
in O
this O
example O
, O

the O
para O
. O

4 O
. O

5 O
. O

3 O
. O

1 O
“ O
Directional B-parameter
and O
Lateral B-control
Control I-control
” O
from O
ASTM O
F2245 O
- O
12d O
4 O
. O

5 O
. O

3 O
. O

1 O
. O

Requirement O
: O
4 O
. O

5 O
. O

3 O
. O

1 O
It O
must O
be O
possible O
to O
reverse O
a O
steady O
30 O
° B-measurement
banked O
coordinated O
turn O
through O
an O
angle O
of O
60 O
° B-measurement
, O

from O
both O
directions O
: O
( O
1 O
) O
within O
5 O
s B-measurement
from O
initiation O
of O
roll O
reversal O
, O

with O
the O
airplane B-asset
trimmed O
as O
closely O
as O
possible O
to O
1 O
. O

3 O
VS1 O
, O

flaps O
in O
the O
take O
- O
off O
position O
, O

and O
maximum B-parameter
take I-parameter
- I-parameter
off I-parameter
power I-parameter
; O
and O
( O
2 O
) O
within O
4 O
s B-measurement
from O
initiation O
of O
roll O
reversal O
, O

with O
the O
airplane B-asset
trimmed O
as O
closely O
as O
possible O
to O
1 O
. O

3 O
VSO O
, O

flaps B-module
fully O
extended O
, O

and O
engine B-system
at O
idle O
. O

One O
flight O
will O
be O
performed O
, O

with O
two O
tests O
for O
each O
points O
. O

The O
aircraft B-asset
’ O
s O
stall B-parameter
speeds I-parameter
are O
the O
following O
: O
Instrumentation O
and O
configuration O
: O
see O
# O
15 O
of O
flight O
test O
sequence O
. O

CG O
setting O
: O
controllability O
must O
be O
examined O
at O
forward O
CG O
position O
, O

therefore O
the O
CG O
will O
be O
at O
FWD O
end O
. O

Configuration O
: O
a O
stopwatch B-component
must O
be O
on O
board O
to O
measure O
reversal B-parameter
time I-parameter
, O

in O
this O
case O
I3 O
was O
used O
. O

Instrumentation O
: O
Conventional O
instrumentation O
, O

the O
pitot O
- O
boom O
is O
not O
necessary O
due O
to O
the O
low O
airspeeds B-parameter
VMAX O
90 O
– O
100 O
knots B-measurement
, O

and O
the O
flight O
envelope O
has O
been O
already O
opened O
until O
130 O
knots B-measurement
. O

Limitations O
: O
as O
per O
“ O
Phase O
1b O
” O
. O

See O
para O
11 O
. O

a O
. O

For O
risk O
assessment O
, O

follow O
the O
method O
from O
para O
. O

10 O
from O
Appendix O
. O

Flight O
profile O
: O
The O
altitude B-parameter
was O
shown O
in O
QFE O
. O

The O
airfield O
’ O
s O
elevation O
is O
310 O
feet B-measurement
( O
see O
para O
. O

8 O
“ O
Facilities O
” O
) O
Estimated O
time O
of O
test O
task O
: O
30 O
minutes B-measurement
. O

Description O
: O
– O
In O
the O
first O
two O
minutes B-measurement
, O

until O
500 O
feet B-measurement
there O
is O
a O
climb O
with O
small O
gradient O
, O

and O
performing O
the O
after O
take O
- O
off O
checklist O
. O

– O
Climbing O
to O
4000 O
feet B-measurement
will O
last O
around O
6 O
minutes B-measurement
( O
estimated O
) O
– O
Between O
8 O
– O
12 O
minutes B-measurement
from O
take O
- O
off O
, O

steps O
6 O
– O
13 O
can O
be O
performed O
( O
estimated O
) O
– O
Between O
12 O
– O
15 O
minutes B-measurement
from O
take O
- O
off O
, O

steps O
14 O
– O
22 O
can O
be O
performed O
( O
estimated O
) O
– O
In O
the O
remaining O
time O
: O
descent O
with O
avg O
. O

250 O
feet B-measurement
/ I-measurement
min I-measurement
and O
perform O
normal O
landing O
. O

The O
test O
cards O
can O
be O
used O
to O
prepare O
the O
flight O
test O
order O
. O

The O
test O
order O
will O
define O
the O
sequence O
of O
test O
points O
. O

After O
the O
flight O
, O

the O
filled O
test O
cards O
can O
be O
used O
for O
establishing O
the O
test O
report O
. O

NOTE O
: O
The O
level O
of O
explication O
should O
be O
as O
detailed O
as O
practical O
. O

An O
example O
is O
shown O
here O
, O

NOTE O
: O
This O
task O
is O
planned O
as O
an O
individual O
flight O
. O

However O
, O

the O
applicant O
may O
choose O
to O
combine O
flights O
. O

( O
If O
fuel O
allows O
it O
. O

) O
For O
example O
, O

the O
task O
nr O
. O

13 O
– O
14 O
– O
15 O
from O
the O
test O
timeline O
( O
see O
para O
. O

c O
) O
may O
be O
combined O
. O

In O
this O
case O
, O

all O
the O
instrumentation O
for O
the O
other O
tasks O
should O
be O
installed O
to O
the O
aircraft B-asset
. O

Task O
nr O
. O

13 O
and O
13 O
/ O
A O
could O
be O
interchanged O
, O

because O
these O
flights O
can O
be O
performed O
with O
the O
same O
way O
, O

although O
the O
CG O
position O
is O
not O
the O
same O
. O

IMPORTANT O
: O
each O
test O
point O
from O
the O
test O
order O
must O
have O
separate O
test O
card O
, O

to O
avoid O
confusion O
. O

Appendix O
2 O
– O
Flight O
Conditions O
and O
Permit O
to O
Fly O
A O
valid O
Permit O
to O
Fly O
shall O
be O
held O
in O
accordance O
with O
Subpart O
P O
of O
EU O
748 O
/ O
2012 O
Application O
for O
associated O
Flight O
Conditions O
( O
shall O
be O
submitted O
to O
EASA O
) O
. O

The O
application O
for O
Permit O
to O
Fly O
shall O
be O
submitted O
to O
the O
Competent O
Authority O
after O
the O
Flight O
Conditions O
are O
approved O
by O
EASA O
. O

See O
: O
http O
: O
/ O
/ O
easa O
. O

europa O
. O

eu O
/ O
easa O
- O
and O
- O
you O
/ O
aviation O
- O
domain O
/ O
aircraft O
- O
products O
/ O
permit O
- O
fly O
http O
: O
/ O
/ O
easa O
. O

europa O
. O

eu O
/ O
document O
- O
library O
/ O
application O
- O
forms O
/ O
focert00037 O
Application O
form O
direct O
link O
: O
http O
: O
/ O
/ O
easa O
. O

europa O
. O

eu O
/ O
system O
/ O
files O
/ O
dfu O
/ O
FO O
. O

CERT O
_ O
. O

00037 O
- O
002 O
% O
20Application O
% O
20for O
% O
20AFC O
% O
20for O
% O
20a O
% O
20permit O
% O
20to O
% O
20fly O
. O

docx O
Application O
should O
include O
the O
Flight O
Test O
Program O
, O

the O
proposed O
flight O
conditions O
, O

and O
a O
declaration O
that O
the O
aircraft B-asset
is O
capable O
for O
safe O
flight O
under O
the O
restrictions O
iaw O
. O

21 O
. O

A O
. O

708 O
( O
b O
) O
. O

Appendix O
3 O
– O
Best O
Practices O
 O
Flight O
Test O
Safety O
Committee O
: O
http O
: O
/ O
/ O
flighttestsafety O
. O

org O
/ O
best O
- O
practices O
: O
NOTE O
: O
The O
Flight O
Test O
Safety O
Committee O
( O
FTSC O
) O
is O
an O
international O
non O
- O
profit O
organization O
formed O
jointly O
in O
November O
1994 O
by O
members O
of O
the O
Society O
of O
Experimental O
Test O
Pilots O
( O
SETP O
) O
, O

the O
Society O
of O
Flight O
Test O
Engineers O
( O
SFTE O
) O
and O
the O
American O
Institute O
of O
Aeronautics O
and O
Astronautics O
( O
AIAA O
) O
. O

 O
FAA O
Order O
4040 O
. O

26B O
( O
as O
amended O
) O
Aircraft B-asset
Certification O
Service O
Flight O
Test O
Risk O
Management O
Program O
: O
http O
: O
/ O
/ O
www O
. O

faa O
. O

gov O
/ O
documentLibrary O
/ O
media O
/ O
Order O
/ O
4040 O
. O

26B O
. O

pdf O
 O
Peter O
W O
. O

Merlin O
, O

Gregg O
A O
. O

Bendrick O
, O

and O
Dwight O
A O
. O

Holland O
: O
Breaking O
the O
Mishap O
Chain O
( O
NASA O
eBook O
) O
http O
: O
/ O
/ O
www O
. O

nasa O
. O

gov O
/ O
connect O
/ O
ebooks O
/ O
break O
_ O
mishap O
_ O
chain O
_ O
detail O
. O

html O
NOTE O
: O
This O
linked O
eBook O
contains O
a O
collection O
of O
case O
studies O
of O
mishaps O
involving O
experimental O
aircraft B-asset
, O

aerospace B-asset
vehicles O
, O

and O
spacecraft O
in O
which O
human O
factors O
played O
a O
significant O
role O
. O

In O
all O
cases O
the O
engineers O
involved O
, O

the O
leaders O
and O
managers O
, O

and O
the O
operators O
( O
i O
. O

e O
. O

, O

pilots O
and O
astronauts O
) O
were O
supremely O
qualified O
and O
by O
all O
accounts O
superior O
performers O
. O

Such O
accidents O
and O
incidents O
rarely O
resulted O
from O
a O
single O
cause O
but O
were O
the O
outcome O
of O
a O
chain O
of O
events O
in O
which O
altering O
at O
least O
one O
element O
might O
have O
prevented O
disaster O
. O

As O
such O
, O

this O
work O
is O
most O
certainly O
not O
an O
anthology O
of O
blame O
. O

It O
is O
offered O
as O
a O
learning O
tool O
so O
that O
future O
organizations O
, O

programs O
, O

and O
projects O
may O
not O
be O
destined O
to O
repeat O
the O
mistakes O
of O
the O
past O
. O

These O
lessons O
were O
learned O
at O
high O
material O
and O
personal O
costs O
and O
should O
not O
be O
lost O
to O
the O
pages O
of O
history O
. O

 O
Bedford O
Workload O
Scale O
( O
FAA O
) O
: O
http O
: O
/ O
/ O
www O
. O

hf O
. O

faa O
. O

gov O
/ O
workbenchtools O
/ O
default O
. O

aspx O
? O
rPage O
= O
Tooldetails O
& O
subCatId O
= O
11 O
& O
toolID O
= O
316 O
 O
Bedford O
Workload O
Scale O
( O
eurocontrol O
) O
: O
https O
: O
/ O
/ O
www O
. O

eurocontrol O
. O

int O
/ O
ehp O
/ O
? O
q O
= O
node O
/ O
1643 O

{ O
" O
extra O
" O
: O
{ O
} O
, O

" O
name O
" O
: O
" O
design O
_ O
10567 O
_ O
3f7f9a3614c449e6b049c26bc57d2e7b O
_ O
s O
" O
, O

" O
parameters O
" O
: O
[ O
{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2922 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
438 O
. O

71318291081235 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2922 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
499 O
. O

4780709630923 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
255 O
. O

74047020283285 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2925 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
261 O
. O

757967013828 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2925 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2925 O
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2926 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
143 O
. O

62670586329142 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Arm B-system
_ O
2926 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
BODY B-system
_ O
ROT B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
BOTTOM O
_ O
CONNECTOR O
_ O
ROTATION O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Z B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Bend B-module
_ O
1 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
180 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Bend B-module
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Bend B-module
_ O
2 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
180 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Bend B-module
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
ANGHORZCONN O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoCaseRotation B-parameter
" O
, O

" O
value O
" O
: O
" O
360 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Rotation B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
CargoMass B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
property O
" O
: O
" O
WEIGHT B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
ControlChannelAuto B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
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" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
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, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
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: O
" O
CONTROL B-parameter
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CHANNEL I-parameter
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} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
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: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
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, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
CONTROL B-parameter
_ I-parameter
CHANNEL I-parameter
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} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
component O
_ O
property O
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: O
" O
CONTROL B-parameter
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CHANNEL I-parameter
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} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Motor B-system
_ O
8 O
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, O

" O
component O
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CONTROL B-parameter
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] O
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, O

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parameter O
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name O
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: O
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FUSELAGE B-system
_ O
AUTOPILOT O
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X O
_ O
OFFSET B-parameter
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, O

" O
value O
" O
: O
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0 O
. O

0 O
" O
, O

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component O
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: O
[ O
{ O
" O
component O
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: O
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_ O
1 O
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, O

" O
component O
_ O
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: O
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FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP B-parameter
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LENGTH I-parameter
" O
} O
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optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
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, O

{ O
" O
parameter O
_ O
name O
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: O
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FUSELAGE B-system
_ O
AUTOPILOT O
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Y O
_ O
OFFSET B-parameter
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, O

" O
value O
" O
: O
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59 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
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: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
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Fuselage B-system
_ O
1 O
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, O

" O
component O
_ O
property O
" O
: O
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FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
4 O
_ O
DISP B-parameter
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WIDTH I-parameter
" O
} O
] O
, O

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optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
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, O

{ O
" O
parameter O
_ O
name O
" O
: O
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FUSELAGE B-system
_ O
BATTERY B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

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optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
BATTERY B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
6 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
1 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

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optimization O
" O
: O
" O
fuselage B-system
_ O
battery B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT B-parameter
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
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_ O
5 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

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optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
CURRENT B-parameter
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
95 O
. O

65 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
5 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

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optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
FLOOR B-parameter
_ I-parameter
HEIGHT I-parameter
" O
, O

" O
value O
" O
: O
" O
12 O
. O

75 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-parameter
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" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
floor B-parameter
_ I-parameter
height I-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
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_ O
7 O
_ O
DISP B-parameter
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" O
} O
] O
, O

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optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
GPS B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
55 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
7 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

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optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
HORZ B-parameter
_ I-parameter
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" O
, O

" O
value O
" O
: O
" O
377 O
. O

4 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
HORZ B-parameter
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" O
} O
] O
, O

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optimization O
" O
: O
" O
fuselage B-system
_ O
horz O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
LENGTH B-parameter
" O
, O

" O
value O
" O
: O
" O
145 O
. O

0 O
" O
, O

" O
component O
_ O
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" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FUSE O
_ O
CYL O
_ O
LENGTH B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
length B-parameter
" O
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, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
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_ O
3 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
RPM B-measurement
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
115 O
. O

8 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
3 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VARIO B-module
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
91 O
. O

65 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
8 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
, O

" O
value O
" O
: O
" O
76 O
. O

5 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
VERT B-parameter
_ I-parameter
DIAMETER I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
vert O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
X O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
6 O
_ O
DISP B-parameter
_ I-parameter
LENGTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
x O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
FUSELAGE B-system
_ O
VOLTAGE B-parameter
_ O
Y O
_ O
OFFSET B-parameter
" O
, O

" O
value O
" O
: O
" O
113 O
. O

3 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
FLOOR B-module
_ I-module
CONNECTOR I-module
_ O
6 O
_ O
DISP B-parameter
_ I-parameter
WIDTH I-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
fuselage B-system
_ O
sensor B-module
_ O
y O
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
Flange B-module
_ O
955 O
_ O
1 O
_ O
CLOCK B-parameter
_ I-parameter
ANGLE I-parameter
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Flange B-module
_ O
955 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
SIDE B-parameter
_ I-parameter
ANGLE I-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller O
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
7 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
NegPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
- O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
7 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropDir B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
8 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Direction B-parameter
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
PosPropType B-parameter
" O
, O

" O
value O
" O
: O
" O
1 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
, O

{ O
" O
component O
_ O
name O
" O
: O
" O
Propeller B-system
_ O
8 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Prop O
_ O
type O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
941 O
_ O
1 O
_ O
ROT2 O
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
941 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
END O
_ O
ROT O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
941 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
260 O
. O

8078766905325 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
941 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
942 O
_ O
1 O
_ O
ROT2 O
" O
, O

" O
value O
" O
: O
" O
0 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
942 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
END O
_ O
ROT O
" O
} O
] O
} O
, O

{ O
" O
parameter O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
942 O
_ O
Length B-parameter
" O
, O

" O
value O
" O
: O
" O
50 O
. O

0 O
" O
, O

" O
component O
_ O
properties O
" O
: O
[ O
{ O
" O
component O
_ O
name O
" O
: O
" O
RotatedArm B-component
_ O
942 O
_ O
1 O
" O
, O

" O
component O
_ O
property O
" O
: O
" O
Length B-parameter
" O
} O
] O
, O

" O
optimization O
" O
: O
" O
arm B-system
_ O
length B-parameter
" O
} O
] O
, O

" O
components O
" O
: O
[ O
{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
2922 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
2925 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
2925 O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Arm B-system
_ O
2926 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
BatteryController B-control
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
BatteryController B-control
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Battery B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
TurnigyGraphene5000mAh6S75C O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Bend B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Para O
_ O
Hub O
_ O
2 O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394od O
_ O
para O
_ O
hub O
_ O
2 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Bend B-module
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Para O
_ O
Hub O
_ O
2 O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394od O
_ O
para O
_ O
hub O
_ O
2 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Cargo B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Cargo B-system
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
type O
" O
: O
" O
CargoCase B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
CargoCase B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Cross O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Para O
_ O
Hub O
_ O
4 O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394od O
_ O
para O
_ O
hub O
_ O
4 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Cross O
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Para O
_ O
Hub O
_ O
4 O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394od O
_ O
para O
_ O
hub O
_ O
4 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
7 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Flange B-module
_ O
955 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Flange B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394 O
_ O
para O
_ O
flange B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
UAV O
_ O
Fuselage B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
capsule O
_ O
fuselage B-system
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Para O
_ O
Hub O
_ O
4 O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394od O
_ O
para O
_ O
hub O
_ O
4 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor B-system
_ O
MN4014KV400 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE5215XF O
_ O
435 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE5215XF O
_ O
435 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE700XF O
_ O
455 O
_ O
G3 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
t O
_ O
motor O
_ O
MN3520KV400 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE5215XF O
_ O
435 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE5215XF O
_ O
435 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Motor B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
kde O
_ O
direct O
_ O
KDE700XF O
_ O
455 O
_ O
G3 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Orient B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Orient B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
17x8N O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
15x5 O
_ O
5MR O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
15x5 O
_ O
5MR O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
15x11 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
17x8N O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
15x5 O
_ O
5MR O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
7 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
15x5 O
_ O
5MR O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Propeller B-system
_ O
8 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Propeller B-system
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
apc O
_ O
propellers B-system
_ O
15x11 O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
RotatedArm B-component
_ O
941 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
RotatedArm B-component
_ O
942 O
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Tube O
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
0394OD O
_ O
para O
_ O
tube O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
RpmTemp B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Autopilot O
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Current B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Voltage B-parameter
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
GPS B-module
" O
} O
, O

{ O
" O
component O
_ O
instance O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
component O
_ O
type O
" O
: O
" O
Sensor B-module
" O
, O

" O
component O
_ O
choice O
" O
: O
" O
Variometer B-parameter
" O
} O
] O
, O

" O
connections O
" O
: O
[ O
{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2922 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
955 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2925 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2925 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2926 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
942 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2922 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
955 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector3 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
FloorConnector1 B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2925 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Bottom B-system
_ I-system
Connector I-system
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Case2HubConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2926 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2925 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
941 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Prop B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Propeller B-system
_ O
8 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MOTOR B-component
_ I-component
CONNECTOR I-component
_ O
CS O
_ O
IN O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Orient B-module
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
ORIENTCONN O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Orient B-component
_ I-component
Connector I-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
941 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
942 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
955 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SideConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2922 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2925 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
3 O
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2925 O
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2926 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
EndConnection B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
MotorPower B-module
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
BatteryController B-control
_ O
1865 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BatteryPower B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Battery B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
PowerBus B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
RotatedArm B-component
_ O
942 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2922 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Bend B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Cargo B-system
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
CargoCase B-module
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
CargoConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
4 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2923 O
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
2 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Arm B-system
_ O
2924 O
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
BaseConnection B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Cross B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
Side B-component
_ I-component
Connector I-component
_ O
1 O
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
2 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
3 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
4 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
5 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
7 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
6 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
8 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
7 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Motor B-system
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Base B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Flange B-module
_ O
955 O
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
TopConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
3 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector5 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
4 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector6 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
MainHub B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
Top B-component
_ I-component
Connector I-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
BottomConnector B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
2 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector4 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
5 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector7 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
6 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O

" O
to O
_ O
ci O
" O
: O
" O
Fuselage B-system
_ O
1 O
" O
, O

" O
to O
_ O
conn O
" O
: O
" O
FloorConnector8 B-component
" O
} O
, O

{ O
" O
from O
_ O
ci O
" O
: O
" O
Sensor B-module
_ O
1 O
" O
, O

" O
from O
_ O
conn O
" O
: O
" O
SensorConnector B-component
" O
, O