H125 Technical Information | Civil Helicopters - Airbus

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Introduction

Airbus’ H125 continues to lead the single-engine helicopter market in all mission segments, benefitting from its high performance and multi-role capacity.

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Technical description

Performance

Hover ceiling OGE @ MTOW, ISA 3,871 m (EASA certification) 12,700 ft (EASA certification) Hover ceiling IGE @ MTOW, ISA 4,420 m 14,500 ft Fast cruise speed @ MTOW 252 km/h 136 kts Max range @ fast cruise speed 630 km 340 NM Max endurance @ fast cruise speed 4 hr, 27 min 4 hr, 27 min Flight envelope (temperature) -40°C to ISA +35°C limited to 50°C -40°C to ISA +35°C limited to 50°C Max altitude flight 7,010 m 23,000 ft

Dimensions

D-value 12.94 m 42.45 ft Rotor diameter 10.69 m 35.07 ft Cabin internal volume (excl. pilot's area) 3.00 m³ 105.94 cu ft

Characteristics

Crew + passengers 1 pilot + 6 pax or 2 pilots + 4 pax 1 or 2 pilots + up to 6 passengers Max takeoff weight (MTOW - dual hydraulics) 2,370 kg 5,225 lb Max takeoff weight with external load 2,800 kg 6,173 lb Useful load 1075 kg 2373 lb Standard fuel tank capacity 425 kg 937 lb Engine type Safran Helicopter Engines Arriel 2D Safran Helicopter Engines Arriel 2D Takeoff power 710 kW / 952 shp 710 kW / 952 shp

Configuration

Four passengers

The one pilot and four passenger configuration is ideal for VIP or private and business aviation. With forward-facing seats and a spacious cabin, passengers can make the most of their time in the air.

Five passengers

The H125’s standard seating configuration of one pilot and five passengers complements commercial transport operations. Passengers benefit from ample legroom and a comfortable ride.

Six passengers

The six-passenger configuration is often used by tourism and sightseeing operators. The H125’s compact cabin means every passenger has the opportunity for breath-taking views.

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