EC135 P2 (CPDS)

Aircraft model
Manufacturer Airbus Helicopters
Aircraft family Helicopter
Aircraft type Airbus Helicopters EC135 / H135
Engine type Turboshaft
Engine count 1

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
10.2 m
33.46 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
155 kt
287 km/h / 178 mph
Weight limits
MLW
2,835 kg
6,250 lb
MTOW
2,835 kg
6,250 lb

Engine models

Manufacturer Name Cont. T/O
Pratt & Whitney Canada PW206B2 321 kW 333 kW