Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 7
Nov 30/064H17
57-50-00
3. Flaps (Refer to Figure 1.)
CAUTION: CONTROL SURFACE SKINS MUST BE REPLACED IF THEY SUSTAIN DAMAGE OR
EXHIBIT CRACKS.
A. Removal
(1) Extend the flaps to their fullest degree and remove the bolt and bushing from the rod end
bearing.
(2) Remove the nuts, washers, bushing and hinge bolts that hold the flap to the wing assembly.
(3) Pull the flap straight back off the wing.
B. Installation
(1) Replace the wing flap by placing the flap onto its proper position and inserting the hinge bolts,
bushings, washers and nuts.
(2) With the flap control in the full flap position, place the bushing on the outboard side of the rod
end bearing and insert and tighten the bolt.
(3) Operate the flap several times to be certain it is operating freely. (Refer to Flap Controls,
Rigging and Adjustment, 27-50-00.)

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)