Piper TOMAHAWK User Manual

PITOT-STATIC SYSTEM
Figure 7-15
PIPER AIRCRAFT CORPORATION SECTION 7 PA-38-112, TOMAHAWK DESCRIPTION & OPERATION ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: APRIL 30, 1981 7-17
PITOT-STATIC SYSTEM
Figure 7-15
PIPER AIRCRAFT CORPORATION SECTION 7 PA-38-112, TOMAHAWK DESCRIPTION & OPERATION ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: APRIL 30, 1981 7-17

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