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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
2
PILOT'S
OPERATING
HANDBOOK
AND
FAA
APPROVED
AIRPLANE
FLIGHT
MANUAL
SUPPLEMENT
NO.2
FOR
AIR
CONDITIONING
INSTALLATION
This supplement must be attached to the Pilot's Operating
Handbook
and
FAA
Approved Airplane Flight Manual when the Air Conditioning
System
is
installed in accordance with Piper Drawing No. 99575-4.
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-=~=)~a~t~~-~=~~~~*-·------------
WARD
EVANS
D.O.A. NO. SO-I
PIPER
AIRCRAFT
CORPORATION
VERO
BEACH,
FLORIDA
DATE
OF
APPROV
AL
____
~A:..;:;U;_;:G"-'U"-'S;..;;T~I3~19=8=2---
ISSUED:
AUGUST
13, 1982
REPORT:
VB-1180
1
of
4,
9-7

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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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