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Piper PA-28-161 User Manual

Piper PA-28-161
257 pages
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SECTION
1
GENERAL
Maximum
Takeoff
Weight
Maximum
Landing Weight
Maximum
Zero
Fuel Weight
REPORT:
VB-1180
1-10
PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR
II
Maximum
weight
approved
for the start
of
the
takeoff
run.
Maximum
weight
approved
for
the landing
touchdown.
Maximum
weight exclusive
of
usable fuel
ISSUED:
AUGUST
13, 1982

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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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