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

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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

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  1. ^ "Blériot Bl-105 - avion de transport civil - Un siècle d'aviation française". aviafrance.com. Retrieved 2019-02-03.