Airbus H130: Difference between revisions
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=Operators= | =Operators= | ||
*Fusion: [[Griffin]] | *[[Fusion: LA]]: [[Griffin]] | ||
[[Category:Aircraft]] | [[Category:Aircraft]] |
Revision as of 09:06, 5 August 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