General characteristics

• Crew: one or two pilots • Capacity: four, including pilot Payload: 900 lb (408 kg) • Length: 21 ft 5 in (9.0 m) • Rotor diameter: 33 ft (10.1 m) • Tail rotor diameter: 4 ft 10 in (1.5 m) • Height: 10 ft 9 in (3.3 m) • Empty weight: 1,450 lb (657.7 kg) • Loaded weight: 2,500 lb (1,134 kg) • Powerplant: 1× Lycoming IO-540-AE1A5 6 cylinder, flat engine with fuel injection, 245 bhp (183 kW) • Fuel: 100 low lead (100LL) fuel or 100/130. • Main tank capacity: 31.6 US gallons (120 liters) • Main tank useable fuel: 30.6 US gallons (116 liters) • Auxiliary tank capacity: 18.5 US gallons (70 liters) • Auxiliary tank usable fuel: 18.3 US gallons (69 liters) • Performance Maximum speed: 130 kn (240 km/h; 150 mph) • Cruise speed: 110 kn (200 km/h; 130 mph) • Range: 300 nmi (560 km; 350 mi) • Altitude restrictions: 14,000 ft (4,300 m) density altitude or 9,000 ft (2,700 m) above ground level in order to be able to reach ground within 5 minutes in case of fire.

Performance

• Maximum speed: 130 kn (240 km/h; 150 mph) • Cruise speed: 110 kn (200 km/h; 130 mph) • Range: 300 nmi (560 km; 350 mi) • Altitude restrictions: 14,000 ft (4,300 m) density altitude or 9,000 ft (2,700 m) above ground level in order to be able to reach ground within 5 minutes in case of fire

See also: Bell 206 | Bell 407 | Eurocopter AS350