Piper TOMAHAWK User Manual

MODEL PA-38-112 TOMAHAWK
Airplane Serial Number _______________________
Registration Number__________________________
Date _______________________________________
AIRPLANE BASIC EMPTY WEIGHT
C.G. Arm
Weight x (Inches Aft = Moment
Item (Lbs ) of Datum) (Lb-In.)
Actual
Standard Empty Weight* Computed
Optional Equipment
Basic Empty Weight
*The standard empty weight includes full oil capacity and 2.0 gallons of
unusable fuel.
AIRPLANE USEFUL LOAD - NORMAL CATEGORY OPERATION
(Gross Weight) - (Basic Empty Weight) = Useful Load
Normal Category: (1670 lbs.) - ( lbs.) = lbs.
Utility Category: (1670 lbs.) - ( lbs.) = lbs.
THIS BASIC EMPTY WEIGHT, C.G. AND USEFUL LOAD ARE
FOR THE AIRPLANE AS LICENSED AT THE FACTORY.
REFER TO APPROPRIATE AIRCRAFT RECORD WHEN
ALTERATIONS HAVE BEEN MADE.
WEIGHT AND BALANCE DATA FORM
Figure 6-7
SECTION 6 PIPER AIRCRAFT CORPORATION
WEIGHT AND BALANCE PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
6-6 REVISED: MAY 10, 1982
MODEL PA-38-112 TOMAHAWK
Airplane Serial Number _______________________
Registration Number__________________________
Date _______________________________________
AIRPLANE BASIC EMPTY WEIGHT
C.G. Arm
Weight x (Inches Aft = Moment
Item (Lbs ) of Datum) (Lb-In.)
Actual
Standard Empty Weight* Computed
Optional Equipment
Basic Empty Weight
*The standard empty weight includes full oil capacity and 2.0 gallons of
unusable fuel.
AIRPLANE USEFUL LOAD - NORMAL CATEGORY OPERATION
(Gross Weight) - (Basic Empty Weight) = Useful Load
Normal Category: (1670 lbs.) - ( lbs.) = lbs.
Utility Category: (1670 lbs.) - ( lbs.) = lbs.
THIS BASIC EMPTY WEIGHT, C.G. AND USEFUL LOAD ARE
FOR THE AIRPLANE AS LICENSED AT THE FACTORY.
REFER TO APPROPRIATE AIRCRAFT RECORD WHEN
ALTERATIONS HAVE BEEN MADE.
WEIGHT AND BALANCE DATA FORM
Figure 6-7
SECTION 6 PIPER AIRCRAFT CORPORATION
WEIGHT AND BALANCE PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
6-6 REVISED: MAY 10, 1982

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