EC725 Caracal / H225M

Aircraft type
Military

Data given for the Airbus Helicopters EC725 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
4.6 m
15.09 ft
Length
16.79 m
55.09 ft
Main rotor diameter
16.2 m
53.15 ft
Tail rotor diameter
3.15 m
10.33 ft
Width
3.38 m
11.09 ft
Fuel
Fuel capacity
1,949 l
515 us gal
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

Manufacturer Name
Airbus Helicopters EC725 Caracal / H225M
Military

Engine models

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