Overview
The Bell 412 is a medium twin-engine helicopter introduced in the early 1980s. Developed from the Bell 212, it features a four-blade main rotor and improved performance. The aircraft serves civil and military operators worldwide.
Live Fleet Activity (B412)
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Specifications
Units
- Engine
- 1 × Pratt & Whitney Canada PT6T-3D Twin-Pac
- Engine type
- Turboshaft
- Power
- 1,250 shp · 932 kW
- Avionics
- Garmin GTN-750 NAV/COM/WAAS GPS, Helicopter Terrain Avoidance Warning System (H-TAWS) Capability, Power Situation Indicator (single indicator for quick pilot monitoring)
- Wing tips
- No winglets
- Seats
- 15
- Crew
- —
- Cabin width
- 8 ft 0 in · 2.43 m
- Cabin height
- 4 ft 1 in · 1.24 m
- Cabin length
- 7 ft 8 in · 2.34 m
- Exterior length
- 55 ft 10 in · 17.02 m
- Tail height
- 14 ft 11 in · 4.54 m
- Fuselage diameter
- 8 ft 6 in · 2.60 m
- Wing span
- 46 ft 0 in · 14.02 m
- Baggage volume
- 28 ft³ · 0.8 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 11,900 lb · 5,400 kg
- Max landing weight
- —
- Max payload
- 4,850 lb · 2,200 kg
- Fuel capacity
- 330 gal · 1,300 L · 1,000 kg (Jet A)
- Max cruise speed
- 124 kt · 143 mph · 230 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 356 nm · 410 mi · 660 km
- Fuel burn
- 1.25 nm/gal · 0.61 km/L
- Ceiling
- 20,000 ft · 6,100 m
- Rate of climb
- 1,350 ft/min · 7 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery
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Live fleet activity details
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