Piper TOMAHAWK User Manual

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)

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