Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 6
Nov 30/06
1E22
6-00-00
3. Access And Inspection Provisions
CAUTION: BEFORE ENTERING THE AFT SECTION OF THE FUSELAGE, BE SURE THE
AIRPLANE IS SUPPORTED AT THE TAIL SKID.
The access and inspection provisions for the airplane are shown in Figure 3. The component to be
serviced or inspected through each opening is identified in the illustration. All access plates and panels
are secured by either metal fasteners or screws. To enter the aft section of the fuselage, open the
baggage compartment door and remove the rear trim panel.
Access Plates and Panels
Figure 3

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)