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 6-17
PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: JANUARY 15, 1981 6-17
(c)
Landing Gear and Brakes (cont)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
Instl.
(Pounds)
Aft
Datum
(Lb-In.)
35
Two Main Wheel Assemblies
34.2
90.0
3078
A
a. Cleveland Aircraft Products
Wheel Assy., No.
40-590
Cert. Basis - TSO C26a
14.3 ,90.0
1287
Brake Assy., No. 30-53A
Cert. Basis -
TSO C26a 4.9*
90.0
441
A b.
6.00-6 Type III 4 ply Rating Tires
with Regular tubes
Cert. Basis - TSO C62
15.0 90.0
1350
37
One Nose Wheel Assembly
19.3
33.0
637
A a.
Cleveland Aircraft Products
Wheel Assy., Piper PS50035-23
Cert. Basis -
TSO C26a
11.8
33.0
390
A b.
6.00-6 Type
III 4 ply Rating Tire
with Regular tube
Cert. Basis -
TSO C62
7.5
33.0
248
39 A Parking/ Handbrake
Piper Dwg. 77420-2
1.6
56.9
91
*Inc1udes 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