Piper TOMAHAWK User Manual

TOMAHAWK
PILOT’S
OPERATING
HANDBOOK
AND
FAA APPROVED
AIRPLANE FLIGHT MANUAL
AIRPLANE AIRPLANE
SERIAL NO. __________________________ REGIST. NO. ______________________
PA-38-112
REPORT: 2126 FAA APPROVED BY: _____________________________________
WARD EVANS
D.O.A. NO. SO-1
DATE OF APPROVAL: PIPER AIRCRAFT CORPORATION
JANUARY 20,1978 VERO BEACH, FLORIDA
FAA APPROVED IN NORMAL AND UTILITY CATEGORIES BASED ON FAR 23 AND
FAR PART 21, SUBPART J. THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED
TO BE FURNISHED TO THE PILOT BY FAR 23 AND FAR PART 21, SUBPART J AND
CONSTITUTES THE APPROVED AIRPLANE FLIGHT MANUAL AND MUST BE CARRIED IN
THE AIRPLANE AT ALL TIMES.
HANDBOOK PART NO. 761 658

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