Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 1
Nov 30/06
1C17
5-10-00
TIME LIMITS
1. Refer to 4-00-00 for the FAA-approved airworthiness limitations section. It sets forth each mandatory
replacement time, structural inspection interval, and related structural inspection procedure required for
type certification.
2. Refer to 5-20-00 for Piper’s recommended Inspection Programs. They include the frequency and extent
of the inspections required for the continued airworthiness of these airplanes.
3. Inspections required by Flight Hour or Calendar Year, if due, are included as part of the Annual / 100
Hour Inspection and/or the Progressive Inspection Event cycles, and are listed individually in 5-30-00.

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)