Piper TOMAHAWK User Manual

SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-14 REVISED: JANUARY 15, 1981
SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-14 REVISED: JANUARY 15, 1981
(b)
Engine
and Engine Accessories
Item
No.
Item
7 B
Engine, Lycoming Model 0-235-L2C
Piper Dwg. 77650-2
Cert. Basis - Lyc.
TC E223
9 A
Alternator
60 amp,
Prestolite No. AL
Y6421
11
A
Starter, Prestolite
MZ4204
13 A
Fuel Pump, Elec. Aux.,
Bendix Model 478360
15 A
Fuel Pump, Engine Driven,
Lycoming Dwg. 75246 or LW-15472
Cert. Basis - Lyc.
TC E223
17 B
Oil Filter Cooling Shroud,
Piper Dwg. 77672-2
*Dry basic engine
**Included in engine weight
Mark if
Weight
Arm (In.)
Moment
Instl.
(Pounds)
Aft
Datum
(Lb-In.)
248.0*
24.3
6026
13.0**
15.2
198
17.0**
16.5
280
1.8
44.0
79
1.5
36.6
55
1.0
40.5
41

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