Piper TOMAHAWK User Manual

PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 15, 1981 REPORT: 2126 REVISED: JUNE 30, 1981 6-31
PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 15, 1981 REPORT: 2126 REVISED: JUNE 30, 1981 6-31
(n)
Miscellaneous
(Optional Equipment) (cont)
Item
Mark if
Weight
Arm (In.)
Moment
No. Item
Instl.
(Pounds)
Aft Datum
(Lb-In. )
313
Fire Extinguisher Instl.
Piper Dwg. 77803-2 5.3
101.5
538
315
Document Container
Piper Dwg. 77555-2 1.5
117.3
176
317
Static Wicks. set of seven
Piper Dwg. 77886-2
319
Glove
Compartment
Piper Dwg. 61939-2 0.9
57.2
52
321
Engine Breather Tube
Insulation Instl.
Piper Dwg. 77540-2
TOTAL OPTIONAL EQUIPMENT

Piper TOMAHAWK Specifications

General

Manufacturer	Piper Aircraft
Model	PA-38 Tomahawk
Role	Trainer aircraft
First flight	1977
Number built	2, 484
Engine type	Lycoming O-235-L2C
Horsepower	112 hp (84 kW)
Max takeoff weight	1, 670 lb (757 kg)
Wingspan	34 ft 0 in (10.36 m)
Height	9 ft 0 in
Range	500 miles
Rate of Climb	720 ft/min