Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION SECTION 3
PA-28-161,
WARRIOR II EMERGENCY PROCEDURES
3.3 EMERGENCY PROCEDURES CHECKLIST
ENGINE FIRE DURING START
Starter ........................................ ·. . . . . . crank engine
Mixture
.............................................. idle cut-off
Throttle
• . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . open
Electric
fuel pump .......................................... OFF
Fuel selector ............................................... OFF
Abandon if fire continues
ENGINE POWER LOSS DURING TAKEOFF
If sufficient runway remains for a normal landing, land straight ahead.
If insufficient runway remains:
Maintain safe airspeed
Make only shallow turn
to avoid obstructions
Flaps
as situation requires
If sufficient altitude has been gained to attempt a restart:
Maintain
safe airspeed
Fuel selector
....................................... switch to tank
containing fuel
Electric fuel pump ...................................... check ON
Mixture ............................................. check RICH
Carburetor heat
.............................................. ON
Primer .................................................... locked
If power
is not regained, proceed with power off landing.
ENGINE POWER LOSS IN FLIGHT
Fuel selector .......•............................... switch to tank
containing fuel
Electric fuel pump ........................................... ON
Mixture .................................................. RICH
Carburetor heat
.............................................. ON
Engine gauges ................................. check for indication
of cause of power
loss
Primer ............................................... check lor. ked
If no fuel pressure is indicated. check tank selector position to be sure it is
on a tank containing fuel.
ISSUED: AUGUST 13, 1982
REPORT: VB-1180
3-3

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)