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
Documents
Brochures
Brochure H225
Missions
Mission-Powerline Brochure
Mission-HEMS Brochure
Mission Firefighting Brochure
Mission Search and Rescue Brochure
Brochure Mission Police
Infographics
H225 infographic
- Brochures
- Missions
- Infographics
Brochure H225
Mission-Powerline Brochure
Mission-HEMS Brochure
Mission Firefighting Brochure
Mission Search and Rescue Brochure
Brochure Mission Police
H225 infographic

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