Piper TOMAHAWK User Manual

SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-30 REVISED: JUNE 30, 1981
SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-30 REVISED: JUNE 30, 1981
(n)
Miscellaneous
(Optional Equipment)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
Instl.
(Pounds)
Aft
Datum
(Lb-In.)
301
Stainless Steel Control Cables
Piper Dwg. 77825-4. -5
303 Assist Step.
Piper Dwg. 77768-2 and
-3
1.9 (ea.)
112.5
214
305 C
I nertia Safety Belts, 4 point harness
(2) 0.8 Ibs. each,
Piper Dwg. 77824-2
1.6
108.0
173
307
Sun Visors (2)
Piper Dwg. 77757-3 & 77725-2
1.3
71.2
92
309
Tow Bar
Piper Dwg. 77503-2
1.3
105.1
137
311
Vacuum System, Piper Dwg. 77948,
61998-2. 61999-2
3.9*
42.6
166
*Pump, regulator, filter and hoses.

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