Cassa 212

The C-212, AVIOCAR, series airplanes are twin-turboprop STOL transport airplanes, cantilever high wing monoplane. Non-retractable tricycle type landing gear. All metal construction with wing and fixed surfaces of the two-spar type, and monocoque fuselage, powered by two Garrett AiResearch Ltd. TPE 331-10-501C engines driving Hartzell propeller.

Dimensions Overall Length : 15.20 m (49 ft 10 in) Wing Span : 19.00 m (62 ft 4 in) Height : 6.30 m (20 ft 8 in) Volume : 22.03 m (776.8 ft)

Design Criteria Max. Take-Off Weight : 7,450 kg Max. Landing Weight : 7,350 kg Max. Zero Fuel Weight : 7,050 kg Max. Taxi Weight : 7,500 kg Cabin Data Main Comp. Total Length : 6.49 m (21 ft 3 in) Cargo Comp. Length : 5.00 m (16 ft 5 in) Floor Area : 10.5 m (113 ft) Volume : 22.03 m (776.8 ft) Number of Seat : Y 22 Doors Passenger Door : 700 mm x 1,580 mm Crew Door : 578 mm x 1,100 mm Emergency Door (forward) : 578 mm x 1,100 mm Emergency Door (sft) : 508 mm x 914 mm Powerplant : Rolls Royce RB 183 MK 555-15P/12 Turbofan Engine