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Tatra T.101

General Aviation and Light Aircraft

The Tatra T.101 was a two-seat monoplane general aviation aircraft built in 1937 by Ringhoffer-Tatra, the Czech industrial firm better known for its cars and trucks. Ringhoffer-Tatra had begun making aircraft in 1935 by building the Avro 626 Avian and the Bucker Bu 131 Jungmann under licence, and the T.001 of 1937 was its first own design. The T.101 developed from that aircraft with a larger wingspan and a bigger tail unit. Only one was built, registered OK-TAO, but in 1938 it flew from Prague to Khartoum, a distance of about 4,330 kilometres, and it set an altitude record for two-seat aircraft with engines under four litres, later raised to 7,470 metres. It was powered by a Tatra T100 four-cylinder air-cooled inverted inline piston engine of 77 kilowatts. A replica built by the brothers Ivo and Jiri Sklenar first flew in October 2009.

Facts
Year
1937 1
Year
1938 2
Engine Class
Piston 1
Power (kW)
77 1
Top Speed (km/h)
215 1
Mass (kg)
500 1
Maximum Mass (kg)
1100 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Tatra T.101 (Wikipedia)

Of Make

Source Tatra T.101 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Tatra T.101 (Wikipedia)Lead
Quote, Lead
The Tatra T.101 is a two-seat monoplane general aviation aircraft that was built in 1937 by Ringhoffer-Tatra.

Originated In

Also in Geography Atlas: where this subject originated.

Source Tatra T.101 (Wikipedia)Operational history
Quote, Operational history
In 1937 a prize was offered for the longest flight by an aircraft of Czechoslovak origin.
Sources
1. Tatra T.101 (Wikipedia)
  • Lead
    The Tatra T.101 is a two-seat monoplane general aviation aircraft that was built in 1937 by Ringhoffer-Tatra.
  • Specifications, powerplant power
    Powerplant: 1 × Tatra T100 4-cylinder air-cooled inverted in-line piston engine, 77 kW (103 hp)
  • Specifications, empty weight
    Empty weight: 500 kg (1,102 lb)
  • Specifications, maximum mass
    Max takeoff weight: 1,100 kg (2,425 lb)
  • Specifications, maximum speed
    Maximum speed: 215 km/h (134 mph, 116 kn)
  • Operational history
    In 1937 a prize was offered for the longest flight by an aircraft of Czechoslovak origin.
View the Source
2. Aviators.cz: Tatra T-101.1 (Aviators.cz)
Aviators.czHistory of the T-101, maiden flight
Quote, History of the T-101, maiden flight
On the 17th January 1938 pilot Matena took the aircraft on its maiden flight
View the Source
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