Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
SECTION 9
SUPPLEMENT 4
PILOT'S OPERATING HANDBOOK
AND
FAA
APPROVED AIRPLANE FLIGHT MANUAL
SUPPLEMENT NO. 4
FOR
CENTURY 21 AUTOPILOT INSTALLATION
This supplement must be attached to the Pilot's Operating Handbook
and FAA Approved Airplane Flight Manual when the Century 21 Autopilot
is installed in accordance with STC SA3352SW. 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, pr,ocedures and performance information not
contained in this supplement, consult the basic Pilot's Operating Handbook
and FAA Approved Airplane Flight Manual.
FAA APPROVED ·L)q_.y£ 6~
WARD EVANS
D.O.A. NO. SO-l
PIPER AIRCRAFT CORPORATION
VERO BEACH, FLORIDA
DATE OF. APPROV AL ___ --.!.A~U~G::!.JU~S~T---'1!..:::3.._, ~19~82!:...._ __
ISSUED: AUGUST 13, 1982
REPORT: VB-1180
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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)