Piper TOMAHAWK User Manual

PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE
PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE
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Instruments
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(Optional Equipment)
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Item
Mark if
Weight Arm (In.)
Moment
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No.
Item Instl.
(Pounds) Aft Datum
(Lb-In.)
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135 C
Airspeed Indicator, (True Airspeed)
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Piper Dwg. 61906-2
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Cert. Basis - TSO C2b 0.6
61.9
37
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137 C
Altimeter, Piper
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PS50008- 3- 2
1.0
61.0
61
\0....:1
0000
.,...
139
Attitude Gyro,
Piper Dwg. 77970-5
Cert. Basis - TSO C4c
2.2 59.5
131
141
Directional Gyro,
Piper Dwg. 77970-5 •
Cert. Basis - TSO C5c 2.6
59.8
156
143
Vertical Speed Indicator,
"
Piper Dwg. 77970-3 or -4 or-5
l'!!I
Cert. Basis - TSO C8c 1.0
66.0 66
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0
Turn and Slip Indicator,
"
145
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Piper Dwg. 77970-4 or -5
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Cert. Basis - TSO C3b
2.6 59.8
156
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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