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BELL UH-1Y Venom
From SKYbrary Wiki
UH1Y
| Aircraft | |||
|---|---|---|---|
| Name | UH-1Y Venom | ||
| Manufacturer | BELL | ||
| Wing | Rotary | ||
| Position | Four-blade main rotor | ||
| Tail | Four-blade tail rotor | ||
| WTC | Medium | ||
| Type code | H2T | ||
| Engine | Turboshaft | ||
| Engine count | Multi | ||
| Position | Above cabin | ||
| Landing gear | Skids | ||
| Mass group | 3 | ||
|
| |||
BELL UH-1Y Venom
Description
The Bell UH-1Y Venom is a twin-engine medium size utility helicopter, part of the United States Marine Corps' H-1 upgrade program. The UH-1Y is currently in low-rate production to replace the USMC's aging fleet of UH-1N Twin Huey light utility helicopters first introduced in the early 1970s. The UH-1Y was to have been re-manufactured from UH-1Ns, but in 2005 it was approved for the aircraft to be built as new.
Technical Data
| Wing span | 14.88 m48.819 ft |
|---|---|
| Length | 17.78 m58.333 ft |
| Height | 4.5 m14.764 ft |
| Powerplant | 2 x General Electric T700-GE-401C turboshaft, 1,546 shp continuous (1,150 kW) each. |
| Engine model | General Electric CT7 |
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 | 135 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 | 83008,300 kg 8.3 tonnes kg |
Ceiling | FL200 | ROD | ft/min | APC | |||||||||||||
| WTC | M | Range | 350350 nm 648,200 m 648.2 km 2,126,640.422 ft NM |
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Accidents & Serious Incidents involving UH1Y
None on SKYbrary