Piper TOMAHAWK User Manual

PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: JUNE 30, 1981 6-25
PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: JUNE 30, 1981 6-25
(I)
Autopilots
(Optional Equipment)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
Inst\.
(Pounds)
Aft Datum (Lb-In.)
(m)
Radio Equipment
(Optional Equipment)
Item
Mark if
Weight
Arm On.)
Moment
No.
Item
Instl.
(Pounds)
Aft Datum
(Lb-In. )
171
King Avionics Inst.
a.
Piper Dwg. 09181-2
13.5
78.6
1061
b.
Piper Dwg. 09349-2 or
09217-3 or 09603-2 or 09604-3
or 09747-2
11.7
81.4
952
173
King Avionics Instl.
Piper Dwg. 09217-2 or 09604-2
10.5
83.8
880
175
King Avionics Instl.
(With Glideslope)
Piper Dwg. 09349-3 or 09603-3
or 09747-3
13.5
76.0
1026

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