Piper PA 28-181 User Manual

PIPER AIRCRAI'T
CORPORATION
PA.28.18T, ARCHER II
SECTION 6
WEIGHT AND BALANCE
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SAMPLE PROBLEM
SAMPLE PROBLEM
Figule 6-17
ISSUED: MAY 29, 1980
REVISED: FEBRUARY 2, 1990
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REPORI: Vl,-1120
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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