Agusta-Westland AW109LUH: Difference between revisions
Jump to navigation
Jump to search
Skca54admin (talk | contribs) No edit summary |
Skca54admin (talk | contribs) No edit summary |
||
| Line 11: | Line 11: | ||
| RoC = 1,700 fpm | | RoC = 1,700 fpm | ||
| EngineType = Turbine | | EngineType = Turbine | ||
| EngineMakeModel = Turbomeca Arrius 2K-2 | | EngineMakeModel = Turbomeca Arrius 2K-2 (714-shp each) | ||
| EngineQ = 2 | | EngineQ = 2 | ||
| TakeoffPower = | | TakeoffPower = 2x 714 shp | ||
| FuelCapacity = | | FuelCapacity = 193 Imperial Gallons | ||
| Passengers = 7 | | Passengers = 7 | ||
| Crew = 2 | | Crew = 2 | ||
| Line 20: | Line 20: | ||
| CruiseSpeed = 153 knots | | CruiseSpeed = 153 knots | ||
}} | }} | ||
*5-cell Fuel System | |||
*Main Rotor Diameter: 35' 6" | |||
*Max Range (no reserve): 500nm | |||
*Max Endurance (no reserve): 4h 46min | |||
*Fuel Economy: 2.3nm per Imperial Gallon | |||
[[Category:Aircraft]] | [[Category:Aircraft]] | ||
Revision as of 19:40, 14 November 2016
| Agusta-Westland AW109LUH | ||||
|---|---|---|---|---|
| Type | Helicopter | |||
| Passengers | 7 | |||
| Crew | 2 | |||
| Range | 500 nm | |||
| Cruise Speed | 153 knots | |||
| Fuel Capacity | 193 Imperial Gallons | |||
| Takeoff Power | 2x 714 shp | |||
| Rate of Climb | 1,700 fpm | |||
| Altitude Ceiling | 11,500 ft | |||
| Engine Type | Turbine | |||
| Engine Quantity | 2 | |||
| Engine | Turbomeca Arrius 2K-2 (714-shp each) | |||
| Max Takeoff Weight | 7,055 Ibs | |||
| (v1.02) | ||||
- 5-cell Fuel System
- Main Rotor Diameter: 35' 6"
- Max Range (no reserve): 500nm
- Max Endurance (no reserve): 4h 46min
- Fuel Economy: 2.3nm per Imperial Gallon