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B06T /
BELL B-206LT TwinRanger
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B06T / Revision as of 09:42, 5 December 2014 by Timo.Kouwenhoven (talk | contribs)
Revision as of 09:42, 5 December 2014 by Timo.Kouwenhoven (talk | contribs)
| Aircraft | ||||||
|---|---|---|---|---|---|---|
| Name | B-206LT TwinRanger | |||||
| Manufacturer | BELL | |||||
| Body | Narrow | |||||
| Wing | Rotary | |||||
| Position | Two-blade main rotor | |||||
| Tail | Two-blade tail rotor | |||||
| Type code | H2T | |||||
| Engine | Turboshaft | |||||
| Engine count | Multi | |||||
| Position | Above cabin | |||||
| Landing gear | Skids | |||||
| Mass group | 1 | |||||
|
| ||||||
BELL B-206LT TwinRanger
Description
The Bell 206LT is a two-bladed, twin-engine helicopter, manufactured by Bell Helicopter.
Technical Data
| Wing span | 10.16 m33.333 ft |
|---|---|
| Length | 12.11 m39.731 ft |
| Height | 2.83 m9.285 ft |
| Powerplant | 2 x Allison 250-C20R turboshaft, 450 shp (335 kW) each. |
| Engine model | Allison 250 |
Performance Data
| Take-Off | Initial Climb (to 5000 ft) |
Initial Climb (to FL150) |
Initial Climb (to FL240) |
MACH Climb | Cruise | Initial Descent (to FL240) |
Descent (to FL100) |
Descent (FL100 & below) |
Approach | ||||||||||
| V2 (IAS) | kts | IAS | kts | IAS | kts | IAS | kts | MACH | TAS | 120 kts | MACH | IAS | kts | IAS | kts | Vapp (IAS) | kts | ||
| Distance | m | ROC | 1470 ft/min | ROC | ft/min | ROC | ft/min | ROC | ft/min | MACH | ROD | ft/min | ROD | ft/min | MCS | kts | Distance | m | |
| MTOW | 14511,451 kg 1.451 tonnes kg |
Ceiling | FL135 | ROD | ft/min | APC | |||||||||||||
| WTC | Range | 347347 nm 642,644 m 642.644 km 2,108,412.075 ft NM |
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Accidents & Serious Incidents involving B06T
None on SKYbrary