Piper PA 28-181 User Manual

SECTION 5
Pf,RFORMANCE
PIPER AIRCRAFT
CORPORÄTION
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BEST ECONOMY MIXTURE
RANGE
Fisure 5-27
REPORT:
VB- 20
*24
ISSUED: JULY
2,
1979
REVISED:
JLILY 5, 1985

Piper PA 28-181 Specifications

General

Manufacturer	Piper Aircraft
Engine	Lycoming O-360-A4M
Horsepower	180 hp
Wingspan	35 ft 6 in (10.82 m)
Height	7 ft 3 in (2.21 m)
Maximum Takeoff Weight	2, 550 lb (1, 157 kg)
Seating	4
Service Ceiling	14, 100 ft
Fuel Capacity	50 US gal (190 L)
Propeller	Fixed Pitch