EC225 Super Puma / H225

Aircraft type

Data given for the Airbus Helicopters EC225 LP Super Puma in basic configuration.

Manufacturer Airbus Helicopters
Aircraft family Helicopter
Engine type Turboshaft
Engine count 2
ICAO code EC25

Technical specifications

Design
Main rotor blades
5
Main rotor count
1
Tail rotor blades
4
Tail rotor count
1
Dimensions
Height
4.97 m
16.31 ft
Length
16.49 m
54.1 ft
Main rotor diameter
16.2 m
53.15 ft
Tail rotor diameter
3.15 m
10.33 ft
Width
3.96 m
12.99 ft
Fuel
Fuel capacity
2,588 l
684 us gal
Performance
Service ceiling
20,000 ft
6,100 m
Speed limits
Vne
175 kt
324 km/h / 201 mph
Weight limits
MLW
11,000 kg
24,250 lb
MTOW
11,000 kg
24,250 lb

Aircraft models

Engine models

Manufacturer Name Cont. T/O
Safran Helicopter Engines Makila 2A 1303 kW 1303 kW
Safran Helicopter Engines Makila 2A1 1303 kW 1303 kW