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 6-21
PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: JANUARY 15, 1981 6-21
(i)
Landing Gear and Brakes
(Optional Equipment) (cont)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
Instl. (Pounds)
Aft Datum
(Lb-In.)
104 C
6.00 x 6 Tire Assemblies (Complete)
Piper Dwgs: 77775-3, 61889-2
&
61889-3
14.6*
67.6 987
(j) Electrical Equipment
(Optional Equipment)
Item
Mark if Weight Arm (In.)
Moment
No. Item
Instl. (Pounds)
Aft
Datum
(Lb-In.)
119
Night Lighting
Piper Dwg. 77920-3
(Includes Instrument, Landing, Tail
and Navigation -Strobe lights with
Power Supply and Harnesses)
8.3 81.3
675
*Weight and moment difference between 5.00 x 5 and 6.00 x 6 Tire Assemblies. (Optional 6.00 x 6
Tire Assemblies must include two main wheel assemblies and one nose wheel assembly.)

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