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AGUSTAWESTLAND AW-101
From SKYbrary Wiki
EH10
| Aircraft | |||||||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Name | AW-101 | ||||||||||||||||||||
| Manufacturer | AGUSTAWESTLAND | ||||||||||||||||||||
| Wing | Rotary | ||||||||||||||||||||
| WTC | Medium | ||||||||||||||||||||
| Type code | H3T | ||||||||||||||||||||
| Engine | Turboshaft | ||||||||||||||||||||
| Engine count | Multi | ||||||||||||||||||||
| Mass group | 3 | ||||||||||||||||||||
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AGUSTAWESTLAND AW-101
Description
The AgustaWestland AW101 (EH101 until June 2007) is a medium-lift helicopter for military applications but also marketed for civil use. The helicopter was developed as a joint venture between Westland Helicopters in the UK and Agusta in Italy (merged as AgustaWestland).
Technical Data
| Wing span | 18.59 m60.991 ft |
|---|---|
| Length | 22.85 m74.967 ft |
| Height | 6.65 m21.818 ft |
| Powerplant | 3 x Rolls-Royce Turbomeca RTM322-01 turboshafts, 1,725 kW (2,312 shp) each. |
| Engine model | Rolls-Royce/Turbomeca RTM322 |
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 | 151 kts | MACH | IAS | kts | IAS | kts | Vapp (IAS) | kts | ||
| Distance | m | ROC | ft/min | ROC | ft/min | ROC | ft/min | ROC | ft/min | MACH | ROD | ft/min | ROD | ft/min | MCS | kts | Distance | m | |
| MTOW | 1460014,600 kg 14.6 tonnes kg |
Ceiling | FL150 | ROD | ft/min | APC | |||||||||||||
| WTC | M | Range | 610610 nm 1,129,720 m 1,129.72 km 3,706,430.449 ft NM |
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Accidents & Serious Incidents involving EH10
None on SKYbrary