Piper TOMAHAWK User Manual

REPORT: VB-2126 ISSUED: JANUARY 20, 1978
vi-l
REVISED: MAY 2, 2012
PILOT’S OPERATING HANDBOOK LOG OF REVISIONS (cONT)
Revision FAA Approval
Number and Revised Description of Revision Signature and
Code Pages Date
Rev. 13 7-5, Revised para. 7.9.
761 658 7-6
(PR890428) 7-14 Revised fig. 7-13 callouts.
(cont) 7-16 Revised serial numbers.
8-1 Revised para. 8.1
8-2 Revised paras. 8.1 and 8.3.
8-3 Revised para. 8.3. D. H. Trompler
May 15, 1989
Date
Rev. 14 ii Updated copyright.
(PR120502) vi-l Added Rev. 14 to L of R.
4-23 Revised Para. 4.35.
Wayne E. Gaulzetti
May 2, 2012

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