Piper TOMAHAWK User Manual

SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-22 REVISED: JANUARY 15, 1981
SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-22 REVISED: JANUARY 15, 1981
G)
Electrical Equipment
(Optional Equipment) (cont)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
Instl.
(Pounds)
Aft
Datum
(Lb-In.)
121
Heated Pi tot Head,
Piper Dwg. 77929-4
0.4
79.2
32
123
Cabin Speaker,
Magitran P-5B
0.6
92.3
56
125
Auxiliary Power Receptacle,
Piper Dwg. 77583-2
5.7
88.0
502
127
External Power Cable,
Piper Dwg. 62355-2
4.6
as installed
131
Carburetor Air Temperature
Indicator Instl.
Piper Dwg. 77531-2
2.0
51.4
103

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