Engineering:Blériot-SPAD S.37
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Short description: 1920s French aircraft
| Blériot-SPAD S.37 | |
|---|---|
| Role | Airliner |
| Manufacturer | Blériot |
| First flight | 9 September 1920 |
| Number built | 1 |
The Bleriot-SPAD S.37 was a small French airliner developed soon after World War I.
Design
The S.37 was a sedan-style airliner where the passengers were placed in open cabin in front of the pilot.
Specifications
Data from [1]
General characteristics
- Crew: 1
- Capacity: 3 pax
- Length: 7.30 m (23 ft 11 in)
- Wingspan: 9.72 m (31 ft 11 in)
- Height: 2.80 m (9 ft 2 in)
- Wing area: 31.5 m2 (339 sq ft)
- Empty weight: 1,066 kg (2,350 lb)
- Gross weight: 1,716 kg (3,783 lb)
- Powerplant: 1 × Hispano-Suiza 8Fa 8-cylinder V inline engine, 200 kW (270 hp)
- Propellers: 2-bladed fixed-pitch propeller
Performance
- Maximum speed: 190 km/h (120 mph, 100 kn)
See also
Related development
References
- ↑ "SPAD S-37 - avion de transport civil - Un siècle d'aviation française". Aviafrance.com. https://www.aviafrance.com/spad-s-37-aviation-france-146.htm. Retrieved 2019-02-04.
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