Introduction

Airbus’ H215M responds to military requirements for a proven cost-effective, high-performing and versatile medium-heavy utility helicopter.

Technical Description

  • EXPH-1020-128

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
4 hr, 00 min
Max endurance with aux fuel tank
6 hr, 05 min

Dimensions
D-value
18.70 m
Rotor diameter
15.60 m
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 - Safran Helicopter
2 x Makila 1A1 Turboshaft
Takeoff power
1,357 kW / 1,819 shp

Documents

Brochures

Military Range Brochure

Brochures

Military Range Brochure

Topics in focus

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