Bell-407

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The Bell 407 is a four-blade ,single-engine , civil utility helicopter, a derivative of the Bell 206L-4. The 407 uses the four-blade, soft-in-plane design rotor with composite hub developed for the United States Army’s OH-58D Kiowa Warrior instead of the two-blade, semi-rigid, teetering, rotor of the 26L-4. The bell 407 is frequently used for corporate and offshore transport, as an air ambulance, law enforcement, electronic news gathering and move making. 

General characteristics

Ø  Crew: 1 pilot

Ø  Capacity: Typical seating configuration for seven comprising pilot and passengers, with five passengers in main cabin. Max hook capacity 1200 kg (2645 lb)

Ø  Length: 41 ft 8 in (12.7 m)

Ø  Rotor diameter: 35 ft 0 in (10.67 m)

Ø  Height: 11 ft 8 in (3.56 m)

Ø  Disc area: 962 ft² (89 m²)

Ø  Empty weight: 2,668 lb (1,210 kg)

Ø  Useful load: 2,347 lb (internal) (1,065 kg (internal))

Ø  MTOW: 6,000 lb (2,722 kg)

Ø  Powerplant: 1 × Allison 250-C47B turboshaft, 813 shp (606 kW)

Performance

Ø  Maximum speed: 140 knots (161 mp/h, 260 km/h)

Ø  Cruise speed: 133 knots (152 mp/h, 246 km/h)

Ø  Range: 324 nmi (372 mi, 598 km)

Ø  Service ceiling: 18,690 ft (5,698 m)