Airbus H130: Difference between revisions

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(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 = 2x ??? shp
| 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
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=Operators=
=Operators=
*Fusion [[Griffin]]
*[[Fusion: LA]]: [[Griffin]] N844GN
 
[[Category:Aircraft]]

Latest revision as of 17:01, 5 October 2018

Airbus H130
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