Overview
The Bell 407 is a single-engine turbine helicopter developed from earlier Bell designs. Introduced in the 1990s, it offers improved performance and cabin comfort. The aircraft is widely used in corporate, emergency medical, and utility operations.
Live Fleet Activity (B407)
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Specifications
Units
- Engine
- 1 × Rolls-Royce Model 250-C47E/4
- Engine type
- Turboshaft
- Power
- 862 shp · 643 kW
- Avionics
- AP-85 Two-Axis Autopilot, Garmin G1000H/G1000H NXi
- Wing tips
- No winglets
- Seats
- 7
- Crew
- —
- Cabin width
- 3 ft 11 in · 1.20 m
- Cabin height
- 3 ft 11 in · 1.20 m
- Cabin length
- 6 ft 7 in · 2.00 m
- Exterior length
- 41 ft 8 in · 12.70 m
- Tail height
- 10 ft 10 in · 3.30 m
- Fuselage diameter
- 4 ft 7 in · 1.40 m
- Wing span
- 35 ft 0 in · 10.67 m
- Baggage volume
- 18 ft³ · 0.5 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 6,000 lb · 2,700 kg
- Max landing weight
- —
- Max payload
- 2,550 lb · 1,150 kg
- Fuel capacity
- 130 gal · 500 L · 400 kg (Jet A)
- Max cruise speed
- 133 kt · 153 mph · 246 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 337 nm · 390 mi · 620 km
- Fuel burn
- 3.39 nm/gal · 1.66 km/L
- Ceiling
- 20,000 ft · 6,100 m
- Rate of climb
- 1,850 ft/min · 9 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery
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Live fleet activity details
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