H215M technical information
Airbus’ H215M responds to military requirements for a proven cost-effective, high-performing and versatile medium-heavy utility helicopter.
Technical Description
Metric
Performance
| One-engine inoperative (OEI 2 min 30 s) | 1,400 kW / 1,877 shp |
| Standard fuel tank capacity | 1,567 kg |
| Max fuel tank capacity | 2,334 kg |
| Hover ceiling IGE | 2,800 m |
| Hover ceiling OGE | 1,650 m |
| Fast cruise speed | 258 km/h |
| Max range with standard fuel tanks at SL | 776 km |
| Max range with aux fuel tank | 1,165 km |
| Max endurance with standard fuel tanks SL / aux fuel tank | 4 hr, 00 min / 6 hr, 05 min |
Dimensions
| D-value | 18.70 m |
| Rotor diameter | 15.60 |
| Internal volume | 13.42 m3 |
Characteristics
| Crew + troops | 1 to 3 crew + 24 troops |
| Max takeoff weight (MTOW) | 9,000 kg |
| Max takeoff weight with external load | 9,350 kg |
| Useful load | 4,268 kg |
| Max External load | 4,500 kg |
| Engine type | 2 x Safran Helicopter Makila 1A1 Turboshaft |
| Takeoff power | 1,357 kW / 1,819 shp |
Imperial
Performance
| One-engine inoperative (OEI 2 min 30 s) | 1,400 kW / 1,877 shp |
| Standard fuel tank capacity | 3,455 Ib |
| Max fuel tank capacity | 5,147 Ib |
| Hover ceiling IGE | 9,196 ft |
| Hover ceiling OGE | 5,413 ft |
| Fast cruise speed | 139 kts |
| Max range with standard fuel tanks at SL | 419 NM |
| Max range with Aux fuel tank | 629 NM |
| Max endurance with standard fuel tanks SL / Aux Fuel tank | 4 hr, 00 min / 6 hr, 05 min |
Dimensions
| D-value | 61.35 ft |
| Rotor diameter | 51.18 ft |
| Internal volume | 473.86 cu. ft |
Characteristics
| Crew + troops | 1 to 3 crew + 24 troops |
| Max takeoff weight (MTOW) | 19,844 Ib |
| Max takeoff weight with external load | 20,615 lb |
| Useful load | 9,409 lb |
| Max External load | 9,920 lb |
| Engine type | 2 x Safran Helicopter Makila 1A1 Turboshaft |
| Takeoff power | 1,357 kW / 1,819 shp |
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