Airbus H130: Difference between revisions
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Skca54admin (talk | contribs) (Created page with "{{Infobox Aircraft | Name = {{FULLPAGENAME}} | Image = H130.jpg | Type = Helicopter | CabinLength = ft | CabinWidth = ft | CabinHeight = ft | MTOW = 5,512 Ibs | MGW = Ibs...") |
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| EngineMakeModel = Turbomeca Arriel 2D | | EngineMakeModel = Turbomeca Arriel 2D | ||
| EngineQ = 1 | | EngineQ = 1 | ||
| TakeoffPower = | | TakeoffPower = 1x 952 shp | ||
| FuelCapacity = 93.5 Imperial Gallons (937 Ibs) | | FuelCapacity = 93.5 Imperial Gallons (937 Ibs) | ||
| Passengers = 6 or 7 | | Passengers = 6 or 7 | ||
Revision as of 21:38, 21 May 2017
| Airbus H130 | ||||
|---|---|---|---|---|
| Type | Helicopter | |||
| Passengers | 6 or 7 | |||
| Crew | 1 or 2 | |||
| Range | 327 nm | |||
| Cruise Speed | 127 knots | |||
| Fuel Capacity | 93.5 Imperial Gallons (937 Ibs) | |||
| Takeoff Power | 1x 952 shp | |||
| Rate of Climb | fpm | |||
| Altitude Ceiling | ft | |||
| Engine Type | Turbine | |||
| Engine Quantity | 1 | |||
| Engine | Turbomeca Arriel 2D | |||
| Max Takeoff Weight | 5,512 Ibs | |||
| (v1.02) | ||||
Notes
- Main Rotor Diameter: 41.5'
- Max Range (no reserve): 327nm
- Max Endurance (no reserve): 4h
- Jet A-1: 5.56 Ibs/gallon
Operators
- Fusion Griffin