CASA C-202 Halcón

C-202 Halcón
Role transport
National origin Spain
Manufacturer CASA
First flight May 15, 1952
Primary user Spanish Air Force
Number built 20

The CASA C-202 Halcón was a twin-engine transport aircraft, constructed by CASA.

The Halcón was designed for use on Spain's international air routes. It had tricycle landing gear and a heated/air-conditioned cabin which could accommodate fourteen passengers. Twenty aircraft were initially ordered, and delivered to the Spanish Air Force with the designation T.6.

Operators

 Spain

Specifications (CASA-202)

Data from Jane's All The World's Aircraft 1961–62[1]

General characteristics

  • Crew: three
  • Capacity: 14 passengers
  • Length: 16.0 m (52 ft 6 in)
  • Wingspan: 21.58 m (70 ft 9 in)
  • Height: 6.06 m (19 ft 9 in)
  • Wing area: 57.4 m2 (617.6 ft2)
  • Aspect ratio: 8.11:1
  • Empty weight: 5,364 kg (11,828 lb)
  • Gross weight: 7,750 kg (17,088 lb)
  • Powerplant: 2 × ENMASA Beta B-41 nine-cylinder air-cooled radial engines, 578[2] kW (775 hp) each

Performance

  • Maximum speed: 375[3] km/h (233 mph)
  • Cruising speed: 335 km/h (208 mph)
  • Range: 1,208 km (750[4] miles)
  • Service ceiling: 7,250 m (23,780 ft)

See also

Related development

References

  1. Taylor 1961, p. 129.
  2. take-off power
  3. at 2,900 m (9,500 ft)
  4. Lambert 1956, p. 170.
  • Donald, David, ed. (1997). The Encyclopedia of World Aircraft. Prospero Books. p. 222. ISBN 1-85605-375-X.
  • Lambert, C.M. (10 February 1956). "Made In Spain: Part 2–The Work of CASA". Flight. Vol. 69 no. 2455. pp. 169–171.
  • Taylor, John W. R. (1961). Jane's All The World's Aircraft 1961–62. London: Sampson Low, Marston & Company.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.