H130 Technical Information

Performance

Hover ceiling OGE	9,700 ft
Hover ceiling IGE	11,250 ft
Fast cruise speed	128 kts
Max* range with standard fuel tanks at SL	327 NM
Max* endurance with standard fuel tanks SL	4h00 min
Flight envelope (Temperature)	-40°C to ISA +35°C limited to 50°C
Max altitude flight	23,000 ft

Dimensions

D-value	41.47 ft
Rotor diameter	35.07 ft
Cabin internal volume	130.70 cu. ft

Characteristics

Crew + passengers	1 pilot + up to 7 passengers or 2 pilots + up to 6 passengers
Max takeoff weight (MTOW)	4,512 lb
Max takeoff weight with external load	6,724 lb
Useful load	2,306 lb
Standard fuel tank capacity	937 lb
Engine type	Safran Helicopter Engines Arriel 2D
Takeoff power	710 kW / 952 shp

Configurations

Six seats for passenger transport

The single pilot and six passenger configuration is ideal for passenger transport, private and business aviation and VIP travel. Rear-facing “club seating” can be installed to create an arrangement favorable for work or conversation.

Seven seats for tourism flights

The single pilot and seven passenger layout is conducive to high-volume tourism flights, with passengers facing forward and seated on a raised theatre-style platform for maximum access to exterior views.