Blériot 106

Blériot 106
Role	Cabin monoplane
National origin	France
Manufacturer	Blériot Aéronautique
First flight	15 July 1924
Number built	1

The Blériot 106 was a 1920s French cabin monoplane designed and built by Blériot Aéronautique.^[1] First flown on 15 July 1924 the 106 was a single-engined shoulder-wing monoplane powered by a 480 hp (358 kW) Renault 12Jb inline piston engine.^[1] The pilot sat in an open cockpit behind the engine and an enclosed cabin had room for six passengers.^[1]

Specifications

Data from ^[1]The Illustrated Encyclopedia of Aircraft

General characteristics

Crew: 1
Capacity: 6 passengers
Length: 12.20 m (40 ft 0 in)
Wingspan: 18.00 m (59 ft 1 in)
Height: 3.50 m (11 ft 6 in)
Max takeoff weight: 2,700 kg (5,952 lb)
Powerplant: 1 × Renault 12Jb inline piston, 360 kW (480 hp)

Performance

Maximum speed: 180 km/h (112 mph; 97 kn)

References

Wikimedia Commons has media related to Louis Blériot aircraft.

Notes

1 2 3 4 Orbis 1985, p. 712

Bibliography

The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.

Aircraft produced by Blériot

I II III IV V VI VII VIII IX X XI XII XIII XIV XV XXI XXIII XXIV XXV XXVII XXXIII XXXVI XXXIX XLII XLIII XLIV 67 73 74 75 102 105 106 110 111 113 115 117 118 123 125 127 135 136 137 155 165 175 195 290 5190

This article is issued from Wikipedia - version of the 6/23/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.