Piper TOMAHAWK User Manual

SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-20 REVISED: JANUARY 15, 1981
SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-20 REVISED: JANUARY 15, 1981
(g)
Engine
and Engine Accessories
(Optional Equipment) (cont)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
1:nstl.
(Pounds)
Aft
Datum
(Lh-In.)
89
Engine Primer Pump**
Essex K2406-SAE-2
0.4
24.4
10
90
Oil Cooler Instl.
Piper Dwg. 77896-2
4.0
33.5
134
(h)
Propeller and Propeller Accessories
(Optional Equipment)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
Instl.
(Pounds)
Aft
Datum
(Lh-In.)
(i)
Landing Gear and Brakes
(Optional Equipment)
Item
Mark if Weight Arm (In.) Moment
No. Item
Instl. (Pounds)
Aft
Datum
(Lh-In.)
103
Toe Brakes (Dual),
Piper Dwg. 77825-3
& 77918-3
7.6* 49.4
375
*Right and Left
**Optional
on aircraft with serial nos. 38-78AOOO I through 38-78A0844. All aircraft included the engine primer

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