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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

Crew 1 or 2 pilots
Passengers Up to 5 or 6 passengers
Range 342 nmi with standard fuel
Max Speed 136 kt VNE

Specifications

ICAO Type CodeEC35
Crew1 or 2 pilots
Passenger CapacityUp to 5 or 6 passengers
Length40.22 ft overall D-value
Wingspan / Rotor Diameter34.10 ft main rotor diameter
Height12.8 ft
Max Takeoff Weight6,570 lb standard; 6,834 lb alternate gross weight
Max Speed136 kt VNE
Range342 nmi with standard fuel
Engine ManufacturerSafran Helicopter Engines or Pratt & Whitney Canada
Engine ModelArrius 2B2 Plus or PW206B3
Engine Count2

Data verification status: Partially Verified

Source: Airbus H135 Technical Information