Aircraft
Publi~~rlons
Piper
Comanchc
250
(Early Modcl)
Section
-
6
Weight
and
Balance
EQUIPMENT
LIST
(Cont.)
4.)
Electrical Equipment:
Generator
Delco Remy
12
Volt
-
35
Ampere
Delco Remy
12
Volt
-
50
Ampere
Battery
12
Volt
-
35
Ampere Hour
Two Landing Lights
GE Model
4509
Rotating Beacon
Whelen No.
WRM-
12
Grimes No.
D7080
or
D7080A-1-12
5.)
Autopilots:
Piper Auto Control (WIO Gyros)
Piper Auto Control
11
(WIO Gyros)
Piper Altimatic (WIO Gyros)
Piper Altimatic I1 (WIO Gyros)
6.)
Miscellaneous Equipment:
Heated Pitot Head
Fire Extinguisher
-
Walter Kidde
Fire Extinguisher
-
MIL-E-5220A
EGT Indicator
Shoulder Harness (Seats
1
&
2)
Shoulder Harness (Seats
3
&
4)
Anti-Static Equipment
Piper Electric Trim
Vertically Adjustable Front Seats
Rudder Balance Weight
Stabilator Modification
Aux Power Receptacle
WIJumper Cable
Oxygen System Installation PAC
25342
Landing Gear Security Kit
Alternate Static Air Source
Stall Warning Indicator
DMCR Approved Airplane Flight Manual
FAA Approved Airplane Flight Manual
Weight
.Arm
(W
(IVi
of
Datum)
18.0 11.5
18.0 11.5
27.0 162.0
1.0
ea.
86.0
2.1 161.0
2.0 161.0
1.0 99.0
5.0 84.8
8.0 84.8
2.0 54.0
.6
ea.
100.0
.6
ea.
133.0
2.0 154.0
4.0 163.0
21.3
ea.
84.8
4.5 272.0
7.0 260.0
7.0 153.3
Moment
(in lb)
207.0
207.0
4374.0
172.0
338.1
322.0
254.3
260.0
587.6
740.2
99.0
424.0
678.4
108.0
120.0
159.6
308.0
652.0
3612.5
1224.0
1820.0
1073.1
6689.8
Neghgible Weight Change
Negligible Weight Change
Negligible Weight Change
Negligible Weight Change
Negligible Weight Change
Copyright:
1993
Page
6-8