Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 8
Nov 30/06
3E8
32-20-00
(10) Ensure that the steering rods fit between the steering horn and the rudder pedals without any
load on the steering rods. Adjust rod ends to obtain this no load setting. Connect the steering
rods to the steering horn.
NO
TE: Check that the rod ends have sufficient thread engagement, by use of the check holes
in the rods.
(11) Check that the rudder pedal stops are adjusted in accordance with instructions given in
Rudder Control Cables - Rigging and Adjustment, 27-20-00.
(12) Adjust the shimmy dampener by turning the nose wheel against its stops and adjusting the rod
end of the dampener for adequate travel to both directions. (Maintain a minimum of
one-quarter in thread engagement.
(13) Remove the airplane from jacks.

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)