CASA C-202 Halcón
|First flight||May 15, 1952|
|Primary user||Spanish Air Force|
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.
Data from Jane's All The World's Aircraft 1961–62
- 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 kW (775 hp) each each
- Maximum speed: 375 km/h (233 mph)
- Cruising speed: 335 km/h (208 mph)
- Range: 1,208 km (750 miles)
- Service ceiling: 7,250 m (23,780 ft)
- Related development
|Wikimedia Commons has media related to CASA C-202 Halcón.|
- Taylor 1961, p. 129.
- take-off power
- at 2,900 m (9,500 ft)
- 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.