Engine Spesifications

• Crew: two, pilot and co-pilot 
• Capacity: 51 passengers, 35 paratroops, 18 stretchers or four HCU-6/E pallets 
• Payload: 6,000 kg (13,100 lb) 
• Length: 21.40 m (70 ft 2 1⁄2 in) 
• Wingspan: 25.81 m (84 ft 8 in) 
• Height: 8.18 m (26 ft 10 in) 
• Wing area: 59.10 m2 (636.1 sq ft) 
• Airfoil: NACA 653-218 
• Aspect ratio: 11.27:1 
• Empty weight: 9,800 kg (21,605 lb) 
• Max. takeoff weight: 15,100 kg (33,289 lb) 
• Powerplant: 2 × General Electric CT7-9C3 turboprops, 1,305 kW (1,750 hp) 
• Cruise speed: 450 km/h (248 knots, 286 mph) at 4,575 m (15,000 ft) 
• Stall speed: 156 km/h (84 knots, 97 mph) 
• Range: 4,355 km (2,350 nmi, 2,706 mi) 
• Service ceiling: 7,620 m (25,000 ft) 
• Rate of climb: 7.8 m/s (1,780 ft/min)