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Piper TOMAHAWK User Manual

Piper TOMAHAWK
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SECTION 6 PIPER AIRCRAFT CORPORATION
WEIGHT AND BALANCE PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
6-8
PA-38-112 Serial Number Registration Number Page Number
Running Basic
Weight Change
Empty Weight
Date
Description of Article
or Modification
Wt. Arm Moment Wt. Moment
(Lb.) (In.) /100 (Lb.) /100
Item No.
Added (+)
Removed (-)
WEIGHT AND BALANCE RECORD (cont)
Figure 6-9 (cont)
SECTION 6 PIPER AIRCRAFT CORPORATION
WEIGHT AND BALANCE PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
6-8
PA-38-112 Serial Number Registration Number Page Number
Running Basic
Weight Change
Empty Weight
Date
Description of Article
or Modification
Wt. Arm Moment Wt. Moment
(Lb.) (In.) /100 (Lb.) /100
Item No.
Added (+)
Removed (-)
WEIGHT AND BALANCE RECORD (cont)
Figure 6-9 (cont)

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Piper TOMAHAWK Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelPA-38 Tomahawk
RoleTrainer aircraft
First flight1977
Number built2, 484
Engine typeLycoming O-235-L2C
Horsepower112 hp (84 kW)
Max takeoff weight1, 670 lb (757 kg)
Wingspan34 ft 0 in (10.36 m)
Height9 ft 0 in
Range500 miles
Rate of Climb720 ft/min

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