Textron Cessna 172R - Page 195

WEIGHT
&
BALANCE
AND
INSTALLED
EQUIPMENT
DATA
CESSNA
AIRCRAFT COMPANY
SINGLE
ENGINE
DIVISION
Cessna
A
Textron
Company
MODEL
SERIAL
&
REGISTRATION
WEIGHT
17281021
1
N24730
(ibsj
ARM
MOMENT
172R
(in)
(lb-in)
(calculated)
STANDARD
EMPTY
WEIGHT
lf
642.0
39.853
65,439
INSTALLED
EQUIPMENT
Net
Change
from
Standard
Aircraft
Altimeter,
Sensitive,
InHg
Audio
Panel,
Bendix/King,
KMA
28
Engine,
Textron
Lycoming,
IO-360-L2A
Gyros,
Attitude,
Directional
&
Turn
Coordinator
NAV/COM
#1,
Bendix/King,
KX
155A
Propeller,
McCauley,
1C235/LFA7570
Transponder,
Bendix/King,
Mode
C,
KT
76C
Vacuum
Pump,
Dual,
Engine
Driven
Wheel
Fairings
GPS,
Bendix/King,
KLN
94
NAV/COM
#2,
Bendix/King,
KX
155A
16.5
4.8
6.6
Circuit
Autopilot,
Bendix
King,
Dual-Axis,
KAP
140
Directional
Gyro
Exchange
Pilot
Control
Wheel
Exchange
GPS/NAV
Selector
0.2
19.7
0.5
0.2
0.2
The
weight
and
balance data
shown
in
this
report
are
computed
on
the
basis
of
Federal
Aviation
Administration
approved
procedures
for
establishing
fleet
weight
averages.
[Far
21
.327(f)(2))
46.100
15.000
17.400
16.500
91.200
14.000
26.000
16.500
761
72
115
1797
7
5
3
Weighed:
02/26/01
Printed:
10/31/01
This Us!
contains
all Installed
optional
oquipment
and
avionics.
All
weights
and
amts
are
the
Installed
difference
from
a
standard
equipped
aircraft
For
a
detailed
list
of aircraft
equipment
weight
and
batanco
data
please
refer
to
the
comprehensive
equipment
list
In
the
pitots
operating
handbook.
BASIC
EMPTY
WEIGHT
1,690.7
40.338
68,199
USEFUL
LOAD
766.3
MAXIMUM
RAMP
WEIGHT
2,457.0
'
MAXIMUM
TAKE-OFF
WEIGHT
2,450.0
Revised
23
Fab.
1989
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