Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 14
Nov 30/06
3H14
34-20-00
(3) Slaving Control Compensator Check and Adjustment
As in (a) above, place the aircraft in simulated flight conditions: engine running, battery master
ON, alternator ON, all radios ON, and lights – recognition, instrument panel, navigation,
position, and strobe – ON. Power ON the KCS-55A (allow to synchronize). Place the slaving
control in the "Free Gyro" position. Use a brass or other non-magnetic screwdriver to make
adjustments to compensator screws.
(a) Place the aircraft on the North compass rose heading. Rotate the indicator card to North
using the manual slave buttons on the slaving control. With a non-magnetic screwdriver in
the N/S opening on the slaving control, center the slave meter.
(b) Place the aircraft on the East compass rose heading. Rotate the indicator card to East
using the manual slave buttons on the slaving meter. With a non-magnetic screwdriver in
the E/W opening on the slaving control, center the slave meter.
FLUX DETECTOR
SCREW,
WASHER
(3 REQ.)
SCREW, WASHER,
NUT (6 REQ.)
FLUX DETECTOR
HARNESS
FWD
LEFT WING EDGE,
TOP VIEW, LOOKING DOWN
LEFT WING VIEW,
LOOKING INBOARD
BRACKET ASSEMBLY
(REF.)
F. S.
106.628
(REF.)
104737 A
101259 K
W.S.
207.40
(REF.)
Flux Detector Installation
Figure 4
Effectivity
Optional, 2842064 and up

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)