Aircraft › Airbus Helicopters › Airbus Helicopters H135 (EC135) › Airbus Helicopters EC135 T2+
Airbus Helicopters EC135 T2+
The EC135 T2+ was certified by EASA in February 2006 as a small rotorcraft on skids, with a bearingless four-blade main rotor 10.20 meters across and a ten-blade Fenestron tail rotor. Its two Safran Arrius 2B2 turboshaft engines run as independent freewheel turbines. One pilot flies it from the right seat with up to seven passengers. The maximum take-off weight is 2,910 kg, or 2,950 kg under approved supplements on later serial numbers, and the maximum operating altitude is 20,000 feet. It stands 3.35 meters high, and the modified fuel tank of later serial numbers holds 700 litres of usable fuel.
- Engines
- Two Safran Arrius 2B2 turboshafts mounted above the fuselage
- Max takeoff weight
- 6,400 lb (2,910 kg)
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Specifications
| Height | 11 ft 0 in (3.35 m) |
|---|---|
| Ceiling | 20,000 ft (6,100 m) |
| Fuel capacity | 180 US gal (700 L) |
| Status | In service |
| Type codes | ICAO EC35 |
Who flies it now
45 flights by other operators
From flights seen in US airspace in the last 14 days (public flight data).
In the air now
No aircraft of this type in the air right now
Flights of this type in the air now, from public flight data.