Piper PA-39 Twin Comanche C/R User Manual

WEIGHT AND BALANCE
EmptyWeight ...................................................
2
BasicWeight ....................................................
Weight and Balance - Visual Plotter
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i
Summary of Disposable Load
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6
Equipment List
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9
A. Propellers and Propeller Accessories
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9
B. Engine and Engine Accessories - Fuel and Oil Systems
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11
C. Landing Gear
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15
D. Electrical Equipment
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17
E. Interior Equipment
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F. Miscellaneous Equipment
i;
L
G. Radio Equipment
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27

Piper PA-39 Twin Comanche C/R Specifications

General

Manufacturer	Piper Aircraft
Model	PA-39 Twin Comanche C/R
Type	Light twin-engine aircraft
Engines	2
Crew	1
Seating Capacity	4
Max Takeoff Weight	3, 600 lb (1, 633 kg)
Powerplant Output	160 hp each
Capacity	4
Wingspan	36 ft 0 in (10.97 m)
Service Ceiling	20, 000 ft (6, 100 m)
Fuel Capacity	100 US gal (379 L)