Cessna SkyHawk SP 172S NAV III 2005 Pilot Operating Handbook page 196

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4GHT
$SALANCE AND INSTALLED EQUIPMENT DATA
cEsSNA AIRCRAFT COMPANY
i.
SINGLE ENGINE DMSION
• •
. eel
A...-c:c
.'
MODEL
SERIAL &REGISTRATION
WEIGHT
ARM
MOMEN
1729
17289992
I
N2330F
(Ibs)
(In)
(Ib-ln)
(calaJlab!d)
STANDARD EMPTY WEIGHT
1,683.2
40.719
67.n·
INSTALLED EQUIPMENT
Net
ChBnge
StBntJsnj
AJrcmft
BAGGAGENET
0.0
0.000
0
FUEL SAMPUNG,CUP
0.0
0.000
0
PILOT'S CHECKLIST
0.0
0.000
0
POH AND FAA APPROVED AIRPLANE FUGHT MANUAL
0.0
0.000
0
TOW BAR. NOSE GEAR (STOWED)
0.0
0.000
0
AIRSPEED INDICATOR
0.0
0.000
-0
ALTIMETER WITH 20 FT MARKING. DUAL WINDOW. 20000 FT
0.0
0.000
0
ATTITUDE INDICATOR
0.0
0.000
(j.
COMPONENTS REQUIRED FOR FRONT SEAT INFLATABLE
0.3
45.300
14
DUAL AXIS AUTOPILOT
19.7
91.200
'l,797
EMERGENCY LOCATOR TRANSMITTER INSTL
0.0
0.000
ENGINE, LYCOMING
0,0
'O.QPO
..
'D
PROPELLER ASSY. MCCAULEY. FIXED PITCH, 1A170E1JHA7660
0.0
0.000
STC SA01700LA FRONT SEAT INFLATABLE RESTRAINT SYSTEM
3.8
45.300
in
VlNYULEATHER SEATS
t
.".1/6111
J:w4
0.0
0.000
0
. . n ..................................
"'PI""'''
...
IL'U""
.fL'
-
..
-,
({oro"
......
.
'
-
-,
OJ) ,
0
_.
..
0.0
.,
.-
--
o .
AFT AVIONICS COOLING FAN
1.1
109.500
120
AVIONICS COOUNG FAN
,:., .. :."0.5
p:,
'.
':.:.
-': I.2.4OO
6'
BLIND TURN COORDINATOR
1.. 0
,"; 14.3:
F4
REMOVED FOR NAVlII
0;'
-34.4
. - ....: 48.7
.
.
..1.675
GDC-74 AIR DATA COMPUTER (ADC) . '
.......
_.
, 1.7
'
..
,'/
' 202
GDL-69A XM WEATHER DATAlINK RECEIVER
"
··.. 4 .0
.
·47.000
188
GDU-1040 MFD DISPLAY
8.4
16.260
104
GDU-1040PDF DISPLAY
6.4
16.260
104
2.2
11.450
25
.GJA.63#1 COM/NAVlGPS COMPUTER
5.2
113.400
590
5.2
':',:,.:113.400
S90
GMA-1347 AUDIO PANEL
1.5
14.000
'.
21
GMlJ.44 MAGNETOMETER
0.3
52.650
0(:
16
GRSon ATTITUDE HEADING REFERENCE SYSTEM (AHRS)
2.5
.'
118.750
:.'
297
GTX-33 TRANSPONDER
3.1
....
" 114.000
'
.
353
MFDFAN
0.1
13.870
1
NAV
1\1
ANTENNA WIRING
3.5
44.000
154
NAV III AVIONICS WIRING
25.7
!
55.000
1,414
PFD FAN ,
0.1
13.660
1
1llIs list c:ont8Ins aD Installed
BASIC EMPTY WEIGHT
1,757.4
I
41.617
opIionaJ
oquIpmont
and 8Vionlcs. All
weIgtIts and
arms
lW
the Installed
dIffer8nc:e
fnlma stBndlUd oquIppod
USEFUL LOAD
' I
jn:raft.
For
a
detaBed list of
aircraft
800.6
"quIpment
and balance
MAXIMUM RAMP WBGHT
2,558.0
In
the plIol:& cperaIIng
I
..
;:;:
'
.
MAXIMUM TAKE-QFF WEIGHT
2,550.0
I
.'.
:.
73,137
RBvls8d 27 Aug.

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