Bell 212 with Mi-24

Bell-212

• Crew: 1
• Capacity: 14
• Length: overall including main rotor 17.46 m (57 ft 3 1/4 in)
• Length: fuselage 12.92 m (42 ft 4 3/4 in)
• Main rotor diameter: 14.69 m (48 ft 2 1/4 in)
• Height: 4.39 m (14 ft 4 3/4; in)
• Main rotor area: 169.5 m² (1,825 ft²)
• Empty: 2,517 kg (5,549 lb)
• Maximum takeoff: 5,080 kg (11,200 lb)
• Powerplant: 2x Pratt & Whitney Canada PT6T-03 or -3B, in Twinpac configuration, driving a common gearbox. 1,342 kW (1,800 shp)

Performance

• Maximum speed: (130 knots) at sea level
• Range: 439 km (237 nautical miles) at sea level with no reserves
• Service ceiling: 5,305 m (17,400 ft)
• Rate of climb: 532 m/min (1,745 ft/min)