Hodek HK-101
Hodek · Czechoslovakia · first flew 1947 · light aircraft
The Hodek HK-101 was a Czechoslovak twin-engined, two-seat light aircraft.
Recognition (WEFT)
| W — Wings | Low-mounted, straight |
|---|---|
| E — Engines | 2 × piston, wing-mounted |
| F — Fuselage | Compact two-seat cabin on a 5.9 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Low-wing monoplane with an engine on each wing
- Two inline engines driving tractor propellers
- Compact two-seat cabin on a 5.9 m fuselage
A very small twin-engined low-wing aircraft with a wingspan of 7.7 m and a length of 5.91 m.
Specifications
- The Hodek HK-101 has a length of 5.91 m (19 ft).
- It has a wingspan of 7.7 m (25 ft).
- Its maximum speed is 350 km/h (217 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
Two prototypes were built in 1947, and the first flew in September 1947. Development was abandoned after the 1948 Czechoslovak coup d'etat.
Variants
Only the two prototypes were built.
Where you'll see it
It did not enter production. It was powered by two 105 hp Walter Minor 4-III inline engines and reached about 350 km/h.
Related aircraft
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