Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION
PA-ls.-161,
WARRIOR II
APPROACH AND LANDING
SECTION 4
NORMAL PROCEDURES
Fuel selector ......................................... proper tank
Seat backs ................................................. erect
Belts/ harness
........................................ fasten/ check
Electric fuel
pump ........................................... ON
Mixture ..................................................... set
Flaps
......................................... set- 103 KIAS max
Air conditioner ............................................. OFF
Trim to 70 KlAS
Final approach speed (flaps 40°) ........................... 63 KlAS
STOPPING ENGINE
Flaps
..................................................... retract
Electric fuel
pump .......................................... OFF
Air conditioner ............................................. OFF
Radios .................................................... OFF
Throttle .................................................. full aft
Mixture
.............................................. idle cut-off
Magnetos
.................................................. OFF
Master switch .............................................. OFF
PARKING
Parking brake ................................................ set
Control wheel .................................... secure with belts
Flaps
..................................................... full up
Wheel
chocks ............................................. in place
Tie downs
................................................. secure
ISSUED: AUGUST 13, 1982
REPORT: VB-1180
4-11

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)