H225 technical information

CDPH-1626-046

Technical description

Performance

Hover ceiling OGE ISA
1,554 m
Hover ceiling IGE ISA
2,396 m
Maximum speed, Vne
324 km/h
Recommended cruise speed
263 km/h
Max range with standard fuel tanks at SL
850 km
Max range + standard + central tanks + pod
1,130 km
Max endurance + stand. fuel tanks SL/Aux fuel
4 hr, 10 min / 5 hr, 43 min
Max altitude flight
6,095 m (PA)

Dimensions

D-value
19.50 m
Rotor diameter
16.20 m
Internal volume
15.50 m3

Characteristics

Crew + passengers
1 or 2 pilots + 19 passengers
Max takeoff weight (MTOW)
11,160 kg
Max takeoff weight with external load
11,200 kg
Useful load
5,401 kg
Max cargo sling load
4,750 kg
Standard fuel tank capacity
2,044 kg
Standard + aux. fuel tank capacity
2,771 kg
Engine type
2 x Safran Helicopter Makila 2A1
Takeoff power
1,567 kW / 2,101 shp
One engine inoperative (OEI 30s)
1,784 kW / 2,392 shp

Configurations

19 seats

for passenger and offshore transport

19 seats Offshore Configuration H225

11 seats

for VIP transport

11 seats VIP Configuration H225

8 seats

SAR

SAR Configuration H225

Documents

Brochures

Civil Range Brochure

Civil Range Brochure

Missions

Mission-Powerline Brochure

Brochure Mission Powerline

Mission Search and Rescue Brochure

Brochure Mission Search and Rescue

Brochure Mission Police

Brochure LAW ENFORCEMENT

Infographics

Civil Range Brochure

Civil Range Brochure

Mission-Powerline Brochure

Brochure Mission Powerline

Mission Search and Rescue Brochure

Brochure Mission Search and Rescue

Brochure Mission Police

Brochure LAW ENFORCEMENT

The latest on the H225

The latest on the H225

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