Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 13
Nov 30/06
5C19
74-10-00
(2) Install rotor shaft assembly (see Figure 11.)
(a) Place magneto frame in T-125 assembly
fixture (flange down).
(b) Position rotor shaft assembly in the magneto
frame.
(c) Insert rotor and frame assembly plug (T-102)
into the T-handle.
(d) Turn T-handle until the bearing cap bottoms in
the frame. Place cap over end of rotorshaft first.
(e) Place T-151 cam and rotor set onto the end
of the rotor shaft and turn T-handle until the
shaft bottoms in magneto frame.
(f) Install bearing clamps and the hold-down
screws.
(g) Torque screws to 20-24 in-lbs.
(3) Install oil seal (see Figure 12.)
(a) Lubricate oil seal with engine oil.
(b) Reverse the magneto on the T-125 assembly
fixture so the flange is facing up.
(c) Insert the oil seal over the rotor shaft.
(d) Press the oil seal flush into the frame using
the oil seal assembly plug (T-103) and the T-
handle screw.
Installing Bearings
Figure 11
Oil Seal Installation
Figure 12

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)