Engineering:Couzinet 80
From HandWiki
80 | |
---|---|
Role | Trainer |
Manufacturer | Société des Avions René Couzinet |
First flight | 3 October 1933 |
Produced | 1 |
Developed from | Couzinet 30 |
The Couzinet 80 was a training aircraft built in France in the early 1930s.
Design
The Couzinet 80 was a four-seat low-wing monoplane of all-wood construction, based on the Couzinet 30.[1]
Specifications (variant specified)
Data from [1]
General characteristics
- Crew: 4
- Length: 11.25 m (36 ft 11 in)
- Wingspan: 16.16 m (53 ft 0 in)
- Height: 3.52 m (11 ft 7 in)
- Wing area: 34.4 m2 (370 sq ft)
- Empty weight: 1,623 kg (3,578 lb)
- Gross weight: 2,280 kg (5,027 lb)
- Powerplant: 2 × Salmson 9Nc 9-cylinder air-cooled radial piston engines, 101 kW (135 hp) each
Performance
- Maximum speed: 210 km/h (130 mph, 110 kn)
References
- ↑ 1.0 1.1 "Couzinet 80 - avion d'entrainement - Un siècle d'aviation française". Aviafrance.com. 2002-05-26. https://www.aviafrance.com/couzinet-80-aviation-france-9503.htm. Retrieved 2019-03-06.
![]() | Original source: https://en.wikipedia.org/wiki/Couzinet 80.
Read more |