Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
TAKEOFF
NORMAL
SECTION 4
NORMAL PROCEDURES
Flaps ........................................................ set
Tab ......................................................... set
Accelerate to
45 to 55 KIAS
Control wheel .................................... back pressure to
rotate to climb attitude
0°FLAPSTAKEOFFPERFORMANCE
Flaps ........................................................ UP
Accelerate to 40-52 KIAS (depending on weight)
Control wheel
.................................... back pressure to
rotate to climb attitude
Accelerate to and maintain
44 to 57 KIAS (depending on weight) until
obstacle clearance
is achieved and climb out at 79 KIAS.
~o FLAPS TAKEOFF PERFORMANCE
Flaps .......................................... 25° (second notch)
Accelerate to
40-52 KIAS (depending on weight)
Control wheel
.................................... back pressure to
rotate to climb attitude
Accelerate to and maintain 44 to
57 KIAS (depending on weight) until
obstacle clearance
is achieved and climb out at 79 KIAS.
Flaps ............................................... retract slowly
SOFT FIELD, OBSTACLE CLEARANCE
Flaps .......................................... 25° (second notch)
Accelerate and lift off nose gear as soon as possible. Lift off
at lowest
possible airspeed. Accelerate
just above ground to 52 KIAS to climb past
obstacle height. Continue climbing while accelerating to best rate
of climb
speed,
79 KIAS.
Flaps ............................................... retract slowly
ISSUED: AUGUST 13, 1982
REPORT: VB-1180
4-9

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)