Bell Helicopter Bell 206LT Twin Ranger
Light Utility Helicopter
The Bell 206LT Twin Ranger is a twin-engined seven-seat light utility helicopter produced by the US-American manufacturer Bell Helicopter Textron , produced in Bells commercial helicopter plant in Mirabel, Quebec (Canada).
The Bell 206LT Twin Ranger is a twin-engined variant of the
Bell 206L Long Ranger. A conversion to twin engine configuration is available for all Long Ranger variants.
Propulsion | 2 Turboshaft Engines |
Engine Model | Allison 250-C20R |
Engine Power (each) | 336 kW | 450 shp |
Speed | 250 km/h | 135 kts 155 mph |
Service Ceiling | 3.048 m | 10.000 ft |
Range | 430 km | 232 NM 267 mi. |
Empty Weight | 1.246 kg | 2.747 lbs |
max. Takeoff Weight | 2.018 kg | 4.450 lbs |
Rotor Blades (main/tail) | 2/2 |
Main Rotor Diameter | 11,28 m | 37 ft 0 in |
Tail Rotor Diameter | 1,65 m | 5 ft 5 in |
Rotor Disc Area | 99,9 m² | 1075 ft² |
Length (Fuselage) | 9,81 m | 32 ft 2 in |
Length | 13,02 m | 42 ft 9 in |
Height | 3,14 m | 10 ft 4 in |
First Flight | 04.04.1984 |
Production Status | out of production |
Total Production | <20 |
Developed from | Bell 206L-4 |
ICAO Code | B06T |
FAA TCDS | H2SW |
Data for (Version) | Bell 206LT |