Agusta-Westland AW109LUH: Difference between revisions
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| Line 14: | Line 14: | ||
| EngineQ = 2 | | EngineQ = 2 | ||
| TakeoffPower = 2x 714 shp | | TakeoffPower = 2x 714 shp | ||
| FuelCapacity = 193 Imperial Gallons | | FuelCapacity = 193 Imperial Gallons (1,073 Ibs) | ||
| Passengers = 7 | | Passengers = 7 | ||
| Crew = 2 | | Crew = 2 | ||
| Line 27: | Line 27: | ||
*Fuel Economy: 2.3nm per Imperial Gallon | *Fuel Economy: 2.3nm per Imperial Gallon | ||
*Jet A-1: 5.56 Ibs/gallon | *Jet A-1: 5.56 Ibs/gallon | ||
*Fuel Burn: 451 Ibs/Hour @ 156 Knots | |||
*Flight Duration at 156 Knots: 2h 20min | |||
[[Category:Aircraft]] | [[Category:Aircraft]] | ||
Revision as of 19:47, 14 November 2016
| Agusta-Westland AW109LUH | ||||
|---|---|---|---|---|
| Type | Helicopter | |||
| Passengers | 7 | |||
| Crew | 2 | |||
| Range | 500 nm | |||
| Cruise Speed | 153 knots | |||
| Fuel Capacity | 193 Imperial Gallons (1,073 Ibs) | |||
| 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
- Jet A-1: 5.56 Ibs/gallon
- Fuel Burn: 451 Ibs/Hour @ 156 Knots
- Flight Duration at 156 Knots: 2h 20min