Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 1
Nov 30/06
5I3
91-30-30
Pitot Heat
Figure 1 (Sheet 1 of 2)
PITOT HEAT
OFF/INOP
P3A
8
10
7
ANNUNCIATOR PANEL
(REF.)
TO P1-
CONT-7
PITOT
HEAT
L2A 20
1
1
2
2
3
3
4
4
WHT WHT
BLK BLK
WHT WHT
GRN GRN
PITOT SENSOR ASSY.
S/N'S 2842001 THRU 2842007
ONLY
H2B 18
7 1/2 A
9
D19A 20
D19B 20
1
2
1
2
H2D 18
H3A 18
DN20A 20
100W 70W
PTT
H3B 18
H2C 18
H3C 18
DN18A 22
H2E 18
J302
PITOT
HEAD
5
4
OFF
ON
6
PITOT
HEAT
SWITCH
P303
J303
P302
WHT
BLK BLK
WHT WHT
GRN GRN
PITOT SENSOR ASSY.
S/N'S 2842008 AND UP
WHT
TO DN2B22
- ANNUNCIATOR BREAKER
85423 F
104295 F

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)