Piper TOMAHAWK User Manual

SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-16 REVISED: JANUARY 15, 1981
SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-16 REVISED: JANUARY 15, 1981
(c)
Landing Gear and Brakes
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
Instl.
(
Pounds) Aft Datum ( Lb-In.)
31
Two Main Wheel Assemblies
25.3 90.0 2277
B
a. Cleveland Aircraft
Prod ucts
Wheel Assy
.• Piper PS50035-17
Cert. Basis -
TSO C26a
9.5
90.0 855
Brake Assy
.• Piper PS50 121-6 and -7
Cert. Basis -
TSO C26a
4.3*
90.0 387
B
b.
5.00-5 4 ply tires. Piper PS501191-1.
with Regular tubes. Piper PS50119-100
Cert. Basis -
TSO C62
11.5
90.0 1035
33
One Nose Wheel Assembly
13.7
33.0 452
B a.
Cleveland
Aircraft Prod ucts
Wheel Assy ..
Piper PS50035-12 or -15
Cert. Basis -
TSO C26a
7.9
33.0
261
B
b.
5.00-5 4 ply tires. Piper PS50019-1. with
Regular tube. Piper PS50019-100
Cert. Basis -
TSO C62
5.8
33.0
191
*Indudes two axles

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