Piper TOMAHAWK User Manual

SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-18 REVISED: NOVEMBER 2, 1981
SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-18 REVISED: NOVEMBER 2, 1981
(e)
Instruments (cont)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
Instl.
(Pounds)
Aft .Datum
( Lb-In.)
65
A
Engine Cluster,
*
Piper Dwg. 77913-2 or -7
0.6
62.5
38
67
A
Fuel Gauges (Left and Right)
Piper Dwg. 77985-2 and -3
0.4
63.5
26
69
Outside Air
Temp. Gauge
Piper Dwg. 99479-2 or -3
0.2
75.1
15
* Ammeter, Oil Temp., Oil Pressure, Fuel Pressure

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