Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 4
Nov 30/06
5J12
91-34-20
P319
P318
D
2
1
FG1A22BL
TO CB8
A
C
FG1A22WT
B
FG3A22BL
FG3A22WT
G
JB8
GS
GS
P319
P318
D
2
1
FG2A22N
GB3-A
A
C
FG3A22N
B
FG1A22
FG4A22
G
JB8
GB3-B
2
1
101902-SHT 12-H
106096 A
101902-SHEET 12-U
S/N’S 2842218 THRU 2842244 BEFORE COMPLIANCE WITH SB1162
STANDBY
ATTITUDE
INDICATOR
STANDBY
BATTERY
STANDBY
ATTITUDE
INDICATOR
STBY ATT
INDICATOR
STBY ATT
INDICATOR
MAIN
BUS
MAIN
BUS
S/N’S 2842245 AND UP;
AND S/N’S 2842218 THRU 2842244 WITH KIT NO. 767-419 INSTALLED PER SB 1162
Standby Attitude Indicator
Figure 4
Eff
ectivity
with Avidyne Entegra

Piper PA-28-161 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-161 Warrior II
Engine	Lycoming O-320-D3G
Horsepower	160 hp
Seating Capacity	4
Wingspan	35 ft (10.7 m)
Length	24 ft 0 in
Maximum Speed	127 knots
Cruise Speed	122 knots
Maximum Takeoff Weight	2, 325 lb (1, 055 kg)
Fuel Capacity	48 US gallons (182 L)