H130 (formerly EC130 / EC130 T2)
Airbus Helicopters — -
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General Information
Type: Helicopter
Usage Area: Civil Passenger Transportation / Tourist Flights / Sightseeing / VIP / Charter Service
Origin: Europe
Technical Specifications
Engine
1 × Safran Arriel 2D Turboprop/Turboshaft Engine
Engine Power
123 HP
Empty Weight
123 kg
Maximum Speed
123 km/h
Range
123 km
Fuel Capacity
123 L
Passenger Capacity
123
Body Material
Main rotor blades are made of composite material; fuselage and tail structure are also made of composite + modern lightweight construction (H130 is described as “light and modern” with composite materials + safety systems)
Featured Features
- The H130 is a single-engine, light/light-intermediate class civilian helicopter. It is used for passenger transport, VIP/tourist flights, emergency medical services (EMS), etc.
- Cabin volume (passenger compartment) approximately 3.70 m³ (130.7 ft³). Airbus +1
- Thanks to the “Fenestron” structure used as the tail rotor, the H130 operates very quietly in its class.
- There are different configuration options: passenger transport, emergency medical assistance (stretcher transport), VIP, tourist, etc. Therefore, values such as empty weight, useful load, number of seats may vary slightly.