Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
SECTION 9
SUPPLEMENT 3
PILOT'S OPERATING HANDBOOK
AND
FAA APPROVED AIRPLANE FLIGHT MANUAL
SUPPLEMENT NO. 3
FOR
PIPER CONTROL WHEEL CLOCK INSTALLATION
This supplement must be attached to the Pilot's Operating Handbook
and FAA Approved Airplane Flight Manual when the Piper Control Wheel
Clock
is installed in. accordance with Piper Drawing No. 87347-3. The
information contained herein supplements
or supersedes the basic Pilot's
Operating Handbook and FAA Approved Airplane Flight Manual only in
those areas listed herein.
For limitations, procedures and performance
information
not contained in this supplement, consult the basic Pilot's
Operating Handbook and FAA Approved Airplane Flight Manual.
FAAAPPROVED~Lu~\~oh~-~J.~~~f~~~~'------------
WARD EVANS
D.O.A. NO. SO-l
PIPER AIRCRAFT CORPORATION
VERO BEACH, FLORIDA
DATE OF APPROV AL ____ ...:...:A=U'-"G;..;:U;..;:S:....:T_l=3.....:..:19:...::8..:.2 __ _
ISSUED: AUGUST 13, 1982
REPORT: VB-1180
1 of 4, 9-11

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)