Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 3
Nov 30/06
1E19
6-00-00
CHART 1 (Sheet 2 of 2)
LEADING PARTICULARS AND PRINCIPAL DIMENSIONS
MODEL PA-28-161 - WARRIOR III
LANDING GEAR
Type Fixed
Shock Strut Type Combination Air-Oil
Fluid Required (Struts and Brakes) MIL-H-5606
Strut Exposure (under static load
1
):
Nose 3.25 ± .25 in
Main 4.50 ± .50 in.
Wheel Track 10.0 ft.
Wheel Base 6 ft. 8 in.
Nose Wheel Travel
Left 20° ± 1°
Right 20° ± 1°
Wheel:
Nose Cleveland 40-77B, 5.00 x 5, or
McCauley D-30500, 5.00 x 5
Main Cleveland 40-86B, 6.00 x 6
Brake Type Cleveland 30-55
Tires:
Nose 5.00 x 5, 4 ply, Type III
Michelin Air, or
McCreary Airhawk
Main 6.00 x 6, 4 ply, Type III, or
B.F. Goodrich, or
Airtrac
6.00 x 6, 6 ply, Type III
Michelin Air
Tire Pressure:
Nose 30 psi.
Main 24 psi.
NO
TE: (1) Static Load is the empty weight of the airplane plus full fuel and oil.

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)