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Beechcraft XT-36

Military Aircraft

The Beechcraft XT-36, company designation Model 46 and intended production designation T-36A, was an American twin-engine trainer-transport aircraft project of the early 1950s by the Beech Aircraft Company. The United States Air Force started the project in 1951 on an expedited basis, driven by rising demand for aircrew during the Korean War and an anticipated shortage of North American TB-25 trainers, and it was meant to serve in both trainer and transport roles. Changing requirements led to delays, design difficulties and spiraling development costs, and the aircraft was ultimately deemed unnecessary and canceled before the prototypes flew. One prototype with Beech serial number J-1 was built but never flown. The estimated specifications describe a twin radial-engined aircraft with a 70 foot wingspan and a 25,000 pound gross weight.

Facts
Year
1951 1
Engine Class
Piston 1
Status
Cancelled 1
Top Speed (km/h)
560 1
Maximum Mass (kg)
11,340 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Beechcraft XT-36 (Wikipedia)

Of Make

Source Beechcraft XT-36 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Beechcraft XT-36 (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
was an American twin-engine trainer-transport aircraft project of the early 1950s by the Beech Aircraft Company

Originated In

Also in Geography Atlas: where this subject originated.

Source Beechcraft XT-36 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
The project was initiated by the United States Air Force on an expedited basis
Sources
1. Beechcraft XT-36 (Wikipedia)
  • Design and development, project start
    The project was started in 1951
  • Lead
    was an American twin-engine trainer-transport aircraft project of the early 1950s
  • Specifications (estimated)
    Pratt & Whitney R-2800 radial piston engines
  • Lead, cancellation
    canceled before the prototypes flew
  • Specifications (estimated), gross weight
    Gross weight: 25,000 lb (11,340 kg)
  • Specifications (estimated), maximum speed
    Maximum speed: 350 mph (560 km/h
  • Lead, manufacturer
    was an American twin-engine trainer-transport aircraft project of the early 1950s by the Beech Aircraft Company
  • Lead, country of origin
    The project was initiated by the United States Air Force on an expedited basis
View the Source
Allison T38 (Wikipedia)
Has Part: Allison T38, Applications
Quote, Has Part: Allison T38, Applications
Beechcraft XT-36 (planned for retrofit; project cancelled)
View the Source
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