Piper WARRIOR III PA-28-161 User Manual

WARRIOR III
pA-28-161
pIlOt’s
OpeRAtIng
hAndbOOk
And
fAA AppROved
AIRplAne flIght mAnuAl
FAA APPROVED IN NORMAL AND UTILITY CATEGORIES BASED ON CAR 3.
THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO
THE PILOT BY CAR 3 AND CONSTITUTES THE APPROVED AIRPLANE FLIGHT
MANUAL AND MUST BE CARRIED IN THE AIRPLANE AT ALL TIMES.
AIRPLANE AIRPLANE
SERIAL NO. ______________________ REGIST. NO. ___________________
PA-28-161
REPORT: VB-1565 FAA APPROVED BY:
WILLIAM R. MOREU
D.O.A. NO. SO-1
DATE OF APPROVAL: PIPER AIRCRAFT CORPORATION
JULY 1, 1994 VERO BEACH, FLORIDA

Piper WARRIOR III PA-28-161 Specifications

General

Manufacturer	Piper Aircraft
Engine	Lycoming O-320-D3G
Horsepower	160 hp
Seating Capacity	4
Model	PA-28-161
Type	Single-engine, low-wing aircraft
Service Ceiling	11, 000 feet
Maximum Takeoff Weight	2, 440 pounds
Wingspan	35 ft
Fuel Capacity	48 US gal (180 L)
Length	24 ft
Height	7 ft 3 in