11/30/2009. Remarks by Johan Visschedijk: "The fourteen-passenger all-metal airliner was developed for domestic transport, and two prototypes were ordered by the Spanish Aviation Ministry in November 1948. Delayed by the late delivery of the 775 hp ENMASA (Empresa National de Motores de Aviation, S.A.) Beta 9C-29-750 nine-cylinder air-cooled radial engines, the first Halcón (Hawk) prototype flew in May 1952. In October 1953, an initial batch of production aircraft was authorized by the Spanish Aviation Ministry.

The second prototype was configured as an eight-passenger executive transport, with a lengthened fuselage, large windows in the rear fuselage. Fitted with two 1,300 hp Wright Cyclone R-1820-56 nine-cylinder air-cooled radial engines, and designated C-202B, it was first flown in 1956.

The engine shortage for the CASA C-201 also plagued the C-202, and in the event, only ten aircraft were produced (before the contract was cancelled in 1962, again without losses to CASA), and the ten aircraft went to the Spanish AF, designated T.6."

Span: Length: Height: Wing area: Empty weight: Loaded weight: Max speed: Cruise speed: Service ceiling:

C-202 70 ft 9 in (21.58 m) 52 ft 6 in (16.00 m) 19 ft 9 in (6.06 m) 617.6 sq.ft (57.40 sq.m) 11,580 lb (5,250 kg) 18,080 lb (8,200 kg) 230 mph (370 kmh) 205 mph (330 kmh) 23,950 ft (7,300 m)

C-202B 67 ft 6 in (20.58 m) 53 ft 7 in (16.33 m) 20 ft 11 in (6.37 m) 602.8 sq.ft (56.0 sq.m) 13,390 lb (6,071 kg) 21,273 lb (9,650 kg) 319 mph (514 kmh) 230 mph (370 kmh) 24,950 ft (7,600 m)