Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
SECTION 6 - WEIGHT AND BALANCE
SECTION 9
SUPPLEMENT 1
Factory installed optional equipment is included in the licensed weight
and balance data in Section 6 of the basic Pilot's Operating Handbook.
SECTION 7 - DESCRIPTION AND OPERATION
No change.
ISSUED: AUGUST 13, 1982
REPORT: VB-1180
3 of 4, 9-5

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)