Airbus Helicopters H135
Overview
The Airbus Helicopters H135 is a helicopter aircraft manufactured by Airbus Helicopters, with the profile centered on its civil helicopter role. The current production-status field is listed as In Production. The listed configuration provides for a crew of 1 or 2 pilots and passenger capacity of Up to 5 or 6 passengers. Power is provided by 2 Safran Helicopter Engines or Pratt & Whitney Canada Arrius 2B2 Plus or PW206B3 engines. Recorded dimensions include length 40.22 ft overall D-value, wingspan 34.10 ft main rotor diameter, height 12.8 ft. Maximum takeoff weight is listed as 6,570 lb standard; 6,834 lb alternate gross weight. Listed performance includes maximum speed 136 kt VNE kt, range 342 nmi with standard fuel nautical miles. Its ICAO type designator is EC35. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
Specifications
| ICAO Type Code | EC35 |
|---|---|
| Crew | 1 or 2 pilots |
| Passenger Capacity | Up to 5 or 6 passengers |
| Length | 40.22 ft overall D-value |
| Wingspan / Rotor Diameter | 34.10 ft main rotor diameter |
| Height | 12.8 ft |
| Max Takeoff Weight | 6,570 lb standard; 6,834 lb alternate gross weight |
| Max Speed | 136 kt VNE |
| Range | 342 nmi with standard fuel |
| Engine Manufacturer | Safran Helicopter Engines or Pratt & Whitney Canada |
| Engine Model | Arrius 2B2 Plus or PW206B3 |
| Engine Count | 2 |
Data verification status: Partially Verified