Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
In full view of the pilot:
SECTION 2
LIMITATIONS
UTILITY CATEGORY OPERATION ONLY
(I) NO AFT PASSENGERS ALLOWED.
(2) ACROBATIC MANEUVERS ARE LIMITED TO
THE FOLLOWING:
SPINS
PROHIBITED
STEEP TURNS
LAZY EIGHTS
CHANDELLES
In full view qf the pilot:
ENTRY SPEED
Ill KIAS
Ill KIAS
Ill KIAS
WARNING- TURN OFF STROBE LIGHTS WHEN
IN CLOSE PROXIMITY TO GROUND OR DURING
FLIGHT
THROUGH CLOUD, FOG OR HAZE.
Adjacent to fuel filler caps:
FUEL- 100 OR IOOLL AVIATION GRADE
Adjacent to fuel filler caps (serial numbers 28-8316037 and up):
AVGAS ONLY
''
GRADE
100LL
ISSUED: AUGUST 13, 1982
REVISED: JULY 15, 1983
GRADE
100
REPORT: VB-1180
2-9

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)