Transport Atlas

How The World Moves
Sign In
Text size
100%
Theme
Vehicle

Yakovlev AIR-12

General Aviation and Light Aircraft

The Yakovlev AIR-12 was a long-range sport aircraft designed and built in the Soviet Union in the late 1930s, intended for record-breaking long-distance flights. It had a welded steel tube nose structure, plywood-skinned wooden wings of high aspect ratio and a fabric-covered rear fuselage, with a pilot and a passenger or navigator in two closed cockpits and a 100 hp Shvetsov M-11 radial engine, later replaced by a 150 hp M-11Ye. Flight testing began in August 1936, and on 21 September 1936 Yulian Piontkovskiy flew it from Moscow to Kharkiv to Sevastopol and back to Kharkiv, about 2,000 km in 10 hours 45 minutes. A flight in October 1937 covered 1,444 km but was not recognised by the FAI because no official observer was present.

Facts
Year
1936 1
Engine Class
Piston 1
Top Speed (km/h)
235 1
Mass (kg)
558 1
Maximum Mass (kg)
1204 1
Engine
Shvetsov M-11 5-cylinder air-cooled radial piston engine 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Yakovlev AIR-12 (Wikipedia)

Of Make

Source Yakovlev AIR-12 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Yakovlev AIR-12 (Wikipedia)Lead
Quote, Lead
The Yakovlev AIR-12 was a long-range sport aircraft designed and built in the Soviet Union during the late 1930s.

Originated In

Also in Geography Atlas: where this subject originated.

Source Yakovlev AIR-12 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
designed and built in the Soviet Union during the late 1930s
Sources
1. Yakovlev AIR-12 (Wikipedia)
  • Lead
    The Yakovlev AIR-12 was a long-range sport aircraft designed and built in the Soviet Union during the late 1930s.
  • Operational history, flight testing
    Flight testing of the AIR-12 commenced in August 1936
  • Specifications, powerplant
    Powerplant: 1 × Shvetsov M-11 5-cylinder air-cooled radial piston engine
  • Specifications, engine fitted
    Powerplant: 1 × Shvetsov M-11 5-cylinder air-cooled radial piston engine
  • Specifications, empty weight
    Empty weight: 558 kg
  • Specifications, maximum weight
    Max takeoff weight: 1,204 kg
  • Specifications, maximum speed
    Maximum speed: 235 km/h
  • Lead, country of origin
    designed and built in the Soviet Union during the late 1930s
View the Source
Comments (0)
No comments yet. Be the first to share a thought.
Reader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.