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Avia 156
Type of aircraft From Wikipedia, the free encyclopedia
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The Avia 156 was a 1930s Czechoslovak six-passenger commercial transport airliner for both mail and passengers, designed by Robert Nebesář and built by Avia. The type performed well but only one was built.[1]
![]() | You can help expand this article with text translated from the corresponding article in Czech. (March 2020) Click [show] for important translation instructions.
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Development
The Avia 156 was a single-engined high-wing cantilever monoplane that first flew in 1934. Powered by a Hispano-Suiza 12Ydrs inline piston engine, it had fixed tailwheel landing gear.[1]
Specifications
Data from [1]
General characteristics
- Crew: two
- Capacity: six
- Length: 10.55 m (34 ft 7 in)
- Wingspan: 15.10 m (49 ft 6 in)
- Wing area: 38 m2 (410 sq ft)
- Empty weight: 2,305 kg (5,082 lb)
- Max takeoff weight: 3,790 kg (8,356 lb)
- Powerplant: 1 × Hispano-Suiza 12Ydrs inline piston engine, 630 kW (850 hp)
Performance
- Maximum speed: 350 km/h (220 mph, 190 kn)
- Cruise speed: 330 km/h (210 mph, 180 kn)
- Range: 950 km (590 mi, 510 nmi)
- Service ceiling: 6,200 m (20,300 ft)
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References
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