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Piper PA-28-161 User Manual

Piper PA-28-161
257 pages
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PIPER AIRCRAFT CORPORATION SECTION 7
PA·28-161, WARRIOR II DESCRIPTION & OPERATION
ENGIIIl
fUEL
PUMP
HECTRIC
fUEl
PUMP
LEFT
MAIII
lANK
CARBURETOR
fUEl
QUAIIIITY
r.AUGES
FUEL SYSTEM SCHEMATIC
Figure 7-9
ISSUED: AUGUST 13,
1982
RIGHT
MAIN
TAN~
REPORT:
VB-1180
7-9

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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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