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Model 33 Plebe
Role Military trainer
National origin United States
Manufacturer Temco Aircraft
First flight 1953
Number built 1
Developed from Temco Buckaroo
Developed into Temco 58

The Temco Model 33 Plebe was an American two-seat training aircraft built by Temco Aircraft and evaluated by the United States Navy, only a prototype was built.

Design and development[]

Developed from the earlier Temco Buckaroo, the Plebe was a single-engined low-wing monoplane with a retractable tricycle landing gear. The Plebe was powered by a 225 hp (168 kW) Continental O-470-3 piston engine with a two-bladed tractor propeller. The two crew sat in tandem with dual controls under a sliding canopy. First flown in 1953 the Plebe was evaluated by the United States Navy to meet the requirement for a primary/basic trainer. A contract was placed for the competing Beechcraft Mentor and only the prototype Plebe was built.

Specifications[]

Data from [1]

General characteristics

  • Crew: 2
  • Length: 31 ft 3 in (9.52 m)
  • Wingspan: 24 ft 1 in (7.33 m)
  • Height: 9 ft 2 in (3.00 m)
  • Empty weight: 1800 lb (816 kg)
  • Gross weight: 2500 lb (1134 kg)
  • Powerplant: 1 × Continental O-470-13, 225 hp (168 kW)

Performance

  • Maximum speed: 192 mph (308 km/h)
  • Range: 518 miles (834 km)

See also[]

References[]

Notes
All or a portion of this article consists of text from Wikipedia, and is therefore Creative Commons Licensed under GFDL.
The original article can be found at Temco Model 33 Plebe and the edit history here.
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