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Piper PA-28-161 User Manual

Piper PA-28-161
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PIPER
AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
SECTION 9
SUPPLEMENT 1
PILOT'S OPERATING HANDBOOK
AND
FAA
APPROVED AIRPLANE FLIGHT MANUAL
SUPPLEMENT NO.
1
FOR
PIPER
ELECTRIC PITCH
TRIM
This supplement must be attached to the Pilot's Operating Handbook
and FAA Approved Airplane Flight Manual when the
Piper Electric Pitch
Trim System
is
installed in accordance with Piper Drawing No. 67496-3.
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 per-
formance information not contained in this supplement, consult the basic
Pilot's Operating Handbook and FAA Approved Airplane Flight Manual.
FAAAPPROVED-=LJ=~===-=~~~~---------
WARD EVANS
D.O.A. NO. SO-l
PIPER
AIRCRAFT CORPORATION
VERO
BEACH, FLORIDA
DATEOFAPPROVAL
________
A~U=G=U=ST~I3~1~98~2~----
ISSUED: AUGUST 13, 1982
REPORT:
VB-1180
I
of
4,
9-3

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Piper PA-28-161 Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelPA-28-161 Warrior II
EngineLycoming O-320-D3G
Horsepower160 hp
Seating Capacity4
Wingspan35 ft (10.7 m)
Length24 ft 0 in
Maximum Speed127 knots
Cruise Speed122 knots
Maximum Takeoff Weight2, 325 lb (1, 055 kg)
Fuel Capacity48 US gallons (182 L)

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