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Specifications (C-3605)
General characteristics
Crew: Two (pilot and winch operator)
Length: 12.03 m (39 ft 6 in)
Wingspan: 13.74 m (45 ft 1 in)
Height: 4.05 m (13 ft 3 in)
Wing area: 28.70 m2 (308.9 sq ft)
Aspect ratio: 6.58
Empty weight: 2,634 kg (5,807 lb)
Gross weight: 3,300 kg (7,275 lb)
Max takeoff weight: 3,716 kg (8,192 lb)
Fuel capacity: 510 litres (110 imp gal; 130 US gal)
Powerplant: 1 × Lycoming T53-L-7 turboprop, 820 kW (1,100 shp)
Propellers: 3-bladed Hamilton Standard 53C51, 3.05 m (10 ft 0 in) diameter
Performance
Maximum speed: 432 km/h (268 mph; 233 kn) at 3,050 metres (10,010 ft)
Cruising speed: 420 km/h (261 mph; 227 kn)
Stall speed: 98 km/h (61 mph; 53 kn) flaps down
Never exceed speed: 600 km/h (373 mph; 324 kn)
Range: 980 km (609 mi; 529 nmi) with 10% reserve
Service ceiling: 10,000 m (32,808 ft)
Rate of climb: 12.5 m/s (2,470 ft/min)
Wing loading: 129 kg/m2 (26 lb/sq ft) at max takeoff weight
Power/mass: 3.38 kg/shp (7.45 lb/shp) at max takeoff weight
Armament
SZW 52 target-towing winch, 2,000 metres (6,600 ft) cable; two underwing hardpoints for supply containers or smoke generators.
Avionics
28V DC electrical system; full blind-flying instrumentation.