Jump to content

Blériot 135

From Wikipedia, the free encyclopedia

135
General information
TypeAirliner
ManufacturerBlériot
Primary userAir Union
Number built2, including one conversion
History
Introduction date1924
First flight19 July 1924
Developed fromBlériot 115
Developed intoBlériot 155

The Blériot 135 (or Bl-135) was a French airliner of the 1920s, a development of the Blériot 115 with more powerful, radial engines. One of the two built was a converted 115, the other new. Both served with Air Union on their Paris–London route from mid-1924.

Variants

[edit]
Bleriot 135
Four-engined airliner.
Bleriot 136
Projected five-seat day-bomber version. Not built.

Operators

[edit]
France

Specifications

[edit]

General characteristics

  • Crew: Two pilots and one radio operator
  • Capacity: 8 passengers
  • Length: 14.45 m (47 ft 5 in)
  • Wingspan: 25.00 m (82 ft 0 in)
  • Height: 4.96 m (16 ft 3 in)
  • Wing area: 126.0 m2 (1,356 sq ft)
  • Empty weight: 3,218 kg (7,094 lb)
  • Gross weight: 5,300 kg (11,684 lb)
  • Powerplant: 4 × Salmson 9Ab , 172 kW (230 hp) each

Performance

  • Maximum speed: 190 km/h (118 mph, 103 kn)
  • Range: 570 km (355 mi, 308 nmi)
  • Service ceiling: 5,100 m (16,730 ft)

References

[edit]
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 162.
  • Barfoot, John. "R.E.8 Pilot: Lieutenant William Lefevre Oxley Parker13 Squadron, RFC." The '14–'18 Journal 2006. Sydney: The Australian Society of World War 1 Aero Historians, 14.
  • aviafrance.com