General
Two-seat light training and utility aircraft.
last update: 4 October 2025
History
Aircraft is predecessor of the PA-38-112 Tomahawk & Tomahawk II (which see). Compared to the Tomahawk it had a 100 hp (74 kW) engine, a conventional low tail and a trailing link landing gear. Only a single prototype was built (N56436, c/n 38-7320001), which first flew in August 1973.
Airframe
wing: Cantilever low-wing monoplane.
fuselage: Light alloy, semi-monocoque structure.
tail: Conventional light alloy cantilever tailplane.
landing gear: Fixed tricycle undercarriage, trailing link on main gear.
No further information is available.
Powerplant
engine: A single 100 hp (74 kW) piston engine, driving a fixed-pitch propeller.
No further information is available.
Systems
No information is available.
Avionics
No information is available.
Accommodation
Two seats, side-by-side, with bubble cabin roof.
No further information is available.
Armament
Not applicable.
Dimensions
No information is available.
Weights & Loads
No information is available.
Performance
No information is available.