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Piper PA 28-181 User Manual

Piper PA 28-181
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PIPER AIRCRAFT
CORPORATTON
PA.2&T6I.
ARCHER II
SECTION
5
PERFORMANCE
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ENDURANCE
Figure
5-29
ISSUf,D: JULY 2, 1979
REvISED:
JL'LY s, 1985
REPORT: VB-1120
s25

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Piper PA 28-181 Specifications

General IconGeneral
ManufacturerPiper Aircraft
EngineLycoming O-360-A4M
Horsepower180 hp
Wingspan35 ft 6 in (10.82 m)
Height7 ft 3 in (2.21 m)
Maximum Takeoff Weight2, 550 lb (1, 157 kg)
Seating4
Service Ceiling14, 100 ft
Fuel Capacity50 US gal (190 L)
PropellerFixed Pitch

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