Beechcraft XT-36
The Beechcraft XT-36 (company designation Model 46) was an American twin-engine trainer-transport aircraft project of the early 1950s. Planned to carry two crew and 12 passengers as a transport, or one instructor and three students as a trainer, the aircraft was intended to become a standard United States Air Force type, as well as licensed production being set up by Canadair as the CL-16.
The project was started in 1951, with the rising demand for new aircrew due to the Korean War, Beechcraft was awarded a contract for the construction of the type, and built a new assembly plant for the production line. In 1953, however, shortly before the first flight of the prototype was to occur, changing priorities resulted in the cancelation of the programme.[1]
Variants
- XT-36A
- Military designation for Beech Model 46 trainer for the USAF; prototype completed but not flown.
- CL-16
- Licensed production by Canadair.
Specifications (estimated)
Data from The Beechcraft T-36[2]
General characteristics
- Crew: two to four
- Capacity: 12 passengers
- Wingspan: 70 ft 0 in (21.34 m)
- Gross weight: 25,000 lb (11,360 kg)
- Powerplant: 2 × Pratt & Whitney R-2800 radial, 2,300 hp (1,716 kW) each
Performance
- Maximum speed: 350 mph (564 km/h)
- Cruise speed: 300 mph (483 km/h)
- Range: 650 miles (1,047 km)
- Service ceiling: 34,000 ft (10,370 m)
See also
- Aircraft of comparable role, configuration and era
- Related lists
References
- Notes
- Bibliography
External links
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Beechcraft designation |
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Military |
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Drone |
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Hawker business jet line |
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Unmanned |
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Piston-engined |
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Turboprops |
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Jets |
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Advanced Trainer |
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Basic Combat |
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Basic Trainer |
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Primary Trainer (1924-1948) |
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Trainer (1948-1990) |
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"T-1", "T-2", "T-3" and "T-6" have also been assigned since 1962 in a separate sequence.
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General |
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Military |
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Accidents/incidents |
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Records |
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