Piper TOMAHAWK User Manual

PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 15,1981 REPORT: 2126
6-17b
PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 15,1981 REPORT: 2126
6-17b
(e)
Instruments
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
Instl.
(
Pounds)
Aft Datum (Lb-In. )
57
A
Compass, Airpath C-2200 L48.
Piper Dwg. 77970-2
Cert. Basis -
TSO C7c
0.9 70.5
64
59 B Airspeed
Indicator,
Piper Dwg. 61905-2
Cert. Basis -
TSO C2b
0.6
61.9
37
61
A
Tachometer, Piper Dwg. 77980-2
0.7
61.3
43
62
A
Altimeter
a.
Piper PS50008-10
1.0
61.0
61
b.
United Instr.. Inc. - 5934
PA-I
Piper Dwg. 77970
1.0
61.0
61
63
B
Altimeter,
Piper PS50008-2-2
Cert. Basis -
TSO C lOb
1.0
61.0
61

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