THK-11
Türk Hava Kurumu · Turkey · first flew 1947 · light aircraft
The THK 11 was a 1940s prototype Turkish monoplane, designed by Stanisław Rogalski and built by Türk Hava Kurumu, the Turkish Aeronautical Association.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, fuselage-mounted |
| F — Fuselage | 8.44 m fuselage |
| T — Tail | Twin fin |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- High-wing twin-boom cantilever cabin monoplane
- Pusher propeller behind the cabin
- Fixed nose-wheel landing gear
A twin-boom pusher with a high wing and a fixed nose-wheel undercarriage, 8.44 m long with a wingspan of 11.8 m.
Specifications
- The THK-11 has a length of 8.44 m (28 ft).
- It has a wingspan of 11.8 m (39 ft).
- Its maximum speed is 201 km/h (125 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It was a high-wing twin-boom cantilever cabin monoplane with a 135 hp de Havilland Gipsy Major engine driving a pusher propeller. It was first flown in 1947.
Variants
Only one THK-11 was built, and it was the prototype of the design.
Where you'll see it
The prototype did not go into production and the project was abandoned.
Related aircraft
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