Blériot 105
The Bleriot 105 was a biplane passenger aircraft built by Louis Bleriot in the mid-1920s, derived from the SPAD S-45.
| Blériot 105 | |
|---|---|
| Role | Cabin monoplane |
| National origin | France |
| Manufacturer | Blériot Aéronautique |
| First flight | 4 August 1924 |
| Number built | 1 |
| Developed from | Bleriot-SPAD S.45 |
Specifications
Data from [1]
General characteristics
- Crew: 1
- Capacity: 18 passengers
- Length: 15.69 m (51 ft 6 in)
- Wingspan: 26.84 m (88 ft 1 in)
- Height: 5.95 m (19 ft 6 in)
- Wing area: 125.00 m2 (1,345.5 sq ft)
- Empty weight: 3,000 kg (6,614 lb)
- Gross weight: 5,500 kg (12,125 lb)
- Powerplant: 4 × Hispano-Suiza 8Fb V-8 inline piston, 220 kW (300 hp) each
Performance
- Maximum speed: 154 km/h (96 mph, 83 kn)
- Service ceiling: 2,900 m (9,500 ft)
References
- "Blériot Bl-105 - avion de transport civil - Un siècle d'aviation française". aviafrance.com. Retrieved 2019-02-03.
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