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Piper PA 28-181 User Manual

Piper PA 28-181
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SECTION
5
PERFONMANCE
PIPER
AIRCRAFT CORPORATION
PÄ.2&ItI, ARCHER II
a=
ö
CP
o
N
o.
ö
CLIMB
PERFORMANCE
Figure
5-15
REPORT: Vlll20
rlt
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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