Piper TOMAHAWK User Manual

SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 15, 1981 6-17a
SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 15, 1981 6-17a
(d) Electrical Equipment
Item
Mark if Weight
Arm (In.)
Moment
No.
Item
Instl.
(Pounds)
Aft
Datum
(Lb-In.)
41 A
Battery
12Y, 25 A.H.,
Rebat Model S-25
21.9
42.6
933
43 A
Y oltage Regulator,
Wico Electric No. X 18150
or Lamar FY R 3024
0.9
48.0
44
45 A
Overvoltage Relay,
Wico Electric No. X 16799
0.5
48.2
24
47 A
Stall Warning Device,
Safe Flight I nstrument Corp.
C52207-4
0.2
48.5
10
49 A
Stall Warning
Horn,
Piper Dwg. 77976-2
Safeflight 53534-1
0.2 48.5
10
51
Instrument Lights Instl. (Supplemental)
Piper Dwg. 77534-2
0.6
64.5
39
53
Emergency Light Instl.
Piper Dwg. 77535-2
0.6
56.7
34

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