Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION SECTION 3
PA-28-161, WARRIOR II EMERGENCY PROC'EDt:RES
If upper latch is open ........................................ latch
If side latch is open .......................... pull on arm rest while
moving latch handle to
latched position.
If both latches arc open ............................. latch side latch
then top latch
ENGINE ROUGHNESS
Carburetor heat .............................................. ON
If roughne~s continues after one min:
Carburetor heat. .. : ......................................... OFF
Mixture .......................................... adjust for max.
smoothness
Electric fuel pump ........................................... ON
Fuel sdl'Ctor ......................................... switch tanks
Engin~ gauges .............................................. check
Magneto switch .......................................... L then R
then BOTH
If operation is satisfactory on either one. continue on that magneto at
n:duccd power and full RICH mixture to first airport.
Prepare for power off landing.
CARBURETOR ICING
Carburetor heat .......•...................................... ON
Mixture .......................................... adjust for max.
ISSUED: AUGUST 13, 1981
smoothness
REPORT: VB-1180
3-7

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)