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Farman F.90

Pioneer and Early Aviation Aircraft

The Farman F.90 was a single-engined biplane transport carrying six passengers, built and developed in France in the early 1920s. It appeared in 1921 as a single-bay biplane with unstaggered rectangular wings, the upper plane held high above the fuselage on four vertical centre-section struts, and a deep flat-sided fuselage with a passenger compartment lit by four small windows on each side. The pilot sat in an open cockpit behind the cabin. It was first powered by a 260 horsepower Salmson nine-cylinder radial and later re-engined with 380 horsepower Bristol Jupiters as the F.91. The one F.90 built won the 1922 Grand Prix de Paris and took the Zenith Cup fuel consumption competition in both 1923 and 1926, but it brought no orders and was not put into production.

Facts
Year
1921 1
Engine Class
Piston 1
Power (kW)
190 1
Units Built
1 1
Top Speed (km/h)
180 1
Engine
Salmson AZ 9 radial 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Farman F.90 (Wikipedia)

Of Make

Source Farman F.90 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Farman F.90 (Wikipedia)Operational history, Farman pilots
Quote, Operational history, Farman pilots
Flight trials began in 1921, conducted by Farman pilots Lucien Coupet and Jules Landry.

Originated In

Also in Geography Atlas: where this subject originated.

Source Farman F.90 (Wikipedia)Lead, place
Quote, Lead, place
It was built and developed in France in the early 1920s.
Sources
1. Farman F.90 (Wikipedia)
  • Design and development, appearance
    The F.90 passenger transport appeared in 1921.
  • Lead, type
    The Farman F.90 was a single engine biplane transport, carrying 6 passengers.
  • Design and development, engine
    The F.90 was initially powered by a 260 hp (194 kW) Salmson AZ 9 9-cylinder radial engine
  • Specifications, powerplant
    Powerplant: 1 × Salmson AZ 9 9-cylinder air cooled single row radial, 190 kW (260 hp)
  • Specifications, power
    Powerplant: 1 × Salmson AZ 9 9-cylinder air cooled single row radial, 190 kW (260 hp)
  • Specifications, maximum speed
    Maximum speed: 180 km/h (110 mph, 97 kn)
  • Design and development, production
    Only one F.90/1 was built.
  • Operational history, Farman pilots
    Flight trials began in 1921, conducted by Farman pilots Lucien Coupet and Jules Landry.
  • Lead, place
    It was built and developed in France in the early 1920s.
  • In Group: Early Commercial Airliners and Transports, Lead, role
    The Farman F.90 was a single engine biplane transport, carrying 6 passengers.
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