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Piper PA 28-181 User Manual

Piper PA 28-181
118 pages
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sEcTtoN 5
PERFORMANCE
PIPER AIRCRAFT
CORPORATION
PA-2&rtr, aRcHEn
ll
REPORT: VFll20
912
;
PA-28-181
KIAS NO INSTRUMENT EBROR
AIRSPEED SYSTEM
CALIBRATION
Fisure 5-3
ISSUED:
JULY
2, 1979

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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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