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C-202 Halcón
Role	transport Type of aircraft
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.

 Spain

• Spanish Air Force

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 10 in)
• Height: 1.85 m (6.06 ft)
• Wing area: 57.50 m² (618.9 sq ft)
• Aspect ratio: 8.11:1
• Airfoil: NACA 23018 at root, NACA 23009 at tip
• Empty weight: 5,364 kg (11,826 lb)
• Gross weight: 7,750 kg (17,086 lb)
• Fuel capacity: 2,140 L (570 US gal; 470 imp gal)
• Powerplant: 2 × ENMASA Beta B-41 nine-cylinder air-cooled radial engines, 578 kW (775 hp) each (take-off power)

Performance

• Maximum speed: 375 km/h (233 mph, 202 kn) at 2,900 m (9,500 ft)
• Cruise speed: 335 km/h (208 mph, 181 kn)
• Range: 1,210 km (750 mi, 650 nmi) ^[2]
• Service ceiling: 7,250 m (23,790 ft)

Related development

• CASA C-201 Alcotán
• CASA C-207 Azor

• Donald, David, ed. (1997). The Encyclopedia of World Aircraft. Prospero Books. p. 222. ISBN 1-85605-375-X. {{cite encyclopedia}}: Missing or empty |title= (help)
• 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.