Piper TOMAHAWK User Manual

PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: JANUARY 15, 1981 6-19
PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: JANUARY 15, 1981 6-19
(f)
Miscellaneous
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item Instl.
(Pounds)
Aft Datum
(Lb-In.)
77 A
Seat Belts
(2) and Shoulder Harness (2) ea.
Piper Dwg. 77767-2 and 3
TSO-C-22F
2.0
95.0
190
79 A
Ash Tray, Grand Rapids Metal Craft
2A-21560
0.5
86.6
43
81
A
Pilot's Operating Handbook
2.6
83 A
Flow Strips
Inboard
Outboard
(g)
Engine and Engine Accessories
(Optional Equipment)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
Instl.
(Pounds)
Aft
Datum
(Lb-In.)
87 C
Engine, Lycoming Model 0-235-L2A
(with Bendix Magnetos)
Piper Dwg. 77650-3
Cert. Basis -
Lyc. TC E223
252.0*
24.3
6124
*Dry basic engine

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