Piper PA-28-161 User Manual

SECTION 3 PIPER AIRCRAFT CORPORATION
EMERGENCY PROCEDURES PA-28-161, WARRIOR II
If roughness persists. prepare for a precautionary landing at pilot's
discretion.
NOTE
Partial carburetor heat may be worse than no
heat at all, since it may melt part of the ice
which will refreeze in the intake system. There-
fore when using carburetor heat always use full
heat~ and. when ice is removed. return the
control to the full cold position.
REPORT: VB-1180
3-16
ISSUED: JULY I, 1982

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)