Category:Airbus H130

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Category:Airbus H130
Category: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

Pages in category "Airbus H130"

The following 2 pages are in this category, out of 2 total.