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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
9.1
GENERAL
SECTION 9
SUPPLEMENTS
SECTION 9
SUPPLEMENTS
This section provides information in the form
of
Supplements which are
necessary for efficient operation of the airplane when equipped with one
or
more
of
the various optional systems
and
equipment
not
provided with the
standard airplane.
All
of
the Supplements provided
by
this section are FAA Approved
and
consecutive!)' numbered as a permanent part
of
this Handbook. The
information contained
in
each Supplement applies only when the related
equipment
is
installed in the airplane.
iSSUED:
AUGUST 13, 1981
REPORT: VB-1180
9-1

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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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