EC135 / H135

Aircraft type

Data given for the Airbus Helicopters EC135 T3 (CPDS) in basic configuration.

Manufacturer Airbus Helicopters
Aircraft family Helicopter
Engine type Turboshaft
Engine count 1
ICAO code EC35

Technical specifications

Design
Main rotor blades
4
Main rotor count
1
Tail rotor blades
10
Tail rotor count
1
Dimensions
Height
3.35 m
10.99 ft
Length
5.87 m
19.26 ft
Main rotor diameter
10.4 m
34.12 ft
Tail rotor diameter
1 m
3.28 ft
Width
1.56 m
5.12 ft
Fuel
Fuel capacity
671 l
177 us gal
Performance
Service ceiling
20,000 ft
6,100 m
Speed limits
Vne
150 kt
278 km/h / 173 mph
Weight limits
MLW
2,980 kg
6,570 lb
MTOW
2,980 kg
6,570 lb
MTW
3,000 kg
6,614 lb