Piper TOMAHAWK User Manual

Performance for a specific airplane may vary from published figures
depending upon the equipment installed, the condition of the engine,
airplane and equipment, atmospheric conditions and piloting technique.
(a) Best Rate Of Climb Speed 70 KIAS
(b) Best Angle of Climb Speed 61 KIAS
(c) Turbulent Air Operating Speed (See CAUTION
Subsection 2.3) 103 KIAS
(d) Maximum Flap Speed 89 KIAS
(e) Landing Final Approach Speed
Full Flaps, 34° (Outboard Flow Strips Installed) 62 KIAS
Full Flaps, 34° (Outboard and Inboard Flow
Strips Installed) 67 KIAS
(f) Maximum Demonstrated Crosswind Velocity 15 KTS
SECTION 4 PIPER AIRCRAFT CORPORATION
NORMAL PROCEDURES PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
4-2 REVISED: DECEMBER 18, 1978
Performance for a specific airplane may vary from published figures
depending upon the equipment installed, the condition of the engine,
airplane and equipment, atmospheric conditions and piloting technique.
(a) Best Rate Of Climb Speed 70 KIAS
(b) Best Angle of Climb Speed 61 KIAS
(c) Turbulent Air Operating Speed (See CAUTION
Subsection 2.3) 103 KIAS
(d) Maximum Flap Speed 89 KIAS
(e) Landing Final Approach Speed
Full Flaps, 34° (Outboard Flow Strips Installed) 62 KIAS
Full Flaps, 34° (Outboard and Inboard Flow
Strips Installed) 67 KIAS
(f) Maximum Demonstrated Crosswind Velocity 15 KTS
SECTION 4 PIPER AIRCRAFT CORPORATION
NORMAL PROCEDURES PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
4-2 REVISED: DECEMBER 18, 1978

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