H225 Technical Information - Airbus

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Technical description

Performance

Hover ceiling OGE ISA 1,554 m 5,100 ft Hover ceiling IGE ISA 2,396 m 7,861 ft Maximum speed, Vne 324 km/h 175 kts Recommended cruise speed 263 km/h 142 kts Max range with standard fuel tanks at SL 850 km 459 nm Max range + standard + central tanks + pod 1,130 km 610 NM Max endurance + stand. fuel tanks SL/Aux fuel 4 hr, 10 min / 5 hr, 43 min 4 hr, 10 min / 5 hr, 43 min Max altitude flight 6,095 m (PA) 20,000 ft (PA)

Dimensions

D-value 19.50 m 63.98 ft Rotor diameter 16.20 m 53.14 ft Internal volume 15.50 m3 547.30 cu.ft

Characteristics

Crew + passengers 1 or 2 pilots + 19 passengers 1 or 2 pilots + 19 passengers Max takeoff weight (MTOW) 11,160 kg (increase up to 24,603 lb) Max takeoff weight with external load 11,200 kg 24,692 lb Useful load 5,401 kg 11,907 lb Max cargo sling load 4,750 kg 10,472 Ib Standard fuel tank capacity 2,044 kg 4,506 lb Standard + aux. fuel tank capacity 2,771 kg 6,108 Ib Engine type 2 x Safran Helicopter Makila 2A1 2 x Safran Helicopter Makila 2A1 Takeoff power 1,567 kW / 2,101 shp 1,567 kW / 2,101 shp One engine inoperative (OEI 30s) 1,784 kW / 2,392 shp 1,784 kW / 2,392 shp

Configurations

19 seats

Passenger and offshore transport

11 seats

VIP transport

8 seats

Search and rescue operations

Documents

Brochures

Brochure H225

Missions

Mission-Powerline Brochure

Brochure Mission Powerline

Mission-HEMS Brochure

LIFE SAVING

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Firefighting

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