Piper TOMAHAWK User Manual

PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: MARCH 1, 1979 6-15
PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: MARCH 1, 1979 6-15
(b)
Engine and Engine Accessories (cont)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item Instl.
(Pounds) Aft
Datum
(Lb-In.)
19 A
Air Filter,
Donaldson P 12-0494
0.4
24.5
10
21
A
Gascolator,
Piper Dwg. 77908-4 0.6
39.5
24
23 A
Fuel Quick Drains
(2)
Curtis CCA 1550 0.05
79.3
4
25 A
Oil Filter - Lyc. L W 13215*
(Champion
CH 48110)
Cert. Basis -
TC E223
2.5
40.0
100
27 A
Engine Primer Pump**
Essex K2406-SAE-2
0.4
24.4
10
*With adapter
**Standard
on aircraft with serial nos. 38-79AOOOI and up. Optional on earlier aircraft.

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