Piper TOMAHAWK User Manual

SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK
SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK
CPoI"
(k)
Instruments
~~
(Optional Equipment) (cont)
~~
0
"
Item
Mark if Weight
Arm (In.)
Moment
~
N
No. Item
Instl.
(Pounds)
Aft Datum
(Lb-ln.)
~
N
CPoI
147
Outside Air Temp. Gauge,
Piper Dwg. 99479-0,-2
or -3
0.2
75.1
15
149 Clock, CA 7613
Piper Dwg. 77970
0.4
62.5
25
151 Hour Meter, Hobbs
M-15006-15, Datcon 773,
Piper Dwg. 77946-2
0.3 61.3
19
"
153 Vacuum Gauge,
~-
<00
UMA 3-200-1
_00
Piper Dwg. 77970-5
0.1 62.0
7
oo~
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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