Piper PA-28-161 User Manual

SECTION 4
NORMAL PROCEDURES
PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
4.3 AIRSPEEDS FOR SAFE OPERATIONS
The following airspeeds are those which are significant to the operation
of the airplane. These figures are for standard airplanes flown at gross weight
under standard conditions at sea level.
Performance for a specific airplane may vary from published figures
depending upon the equipment installed: the condition of the engine. air-
plane and equipment: atmospheric conditions and piloting technique.
(a)
Best Rate of Climb Speed
(b) Best Angle of Climb Speed
(c) Turbulent Air Operating Speed (See Subsection 2.3)
(d) Maximum Flap Speed
(e) Landing Final Approach Speed (Flaps 40°)
(f) Maximum Demonstrated Crosswind Velocity
79 KIAS
63 KIAS
Ill KJAS
103 KIAS
63 KIAS
!7 KTS
REPORT: VB-1180
4-2
ISSUED: AUGUST 13, 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)