Specifications
Aircraft Details
• Located in Annecy, France; always hangared, never used for aerial work
• Private operation with only two pilots since delivery
• 910 total airframe hours, complete logs available, last periodic inspection completed
• Maintained by ROTOR TEAM - France
• Equipped with SAFRAN ARRIEL 2D engine (N1 cycles: 1043, N2 cycles: 567)
• Advanced avionics: Garmin G500H TXi Display, GTN 650H GPS/VHF/VOR/LOC/GS, GNC 255A VHF/VOR/LOC/GS, GTX 335R Mode S ADS-B Out, GMA 350H ICS, Kannad INTEGRA AP-H ELT
• VFR Day & Night package
• Additional features: Lean Instrument Panel with dual tablet holders, comfort layout with black carpet, dual controls, BOSE headset compatible ICS, USB ports, tinted and bulged windows, LH LED landing light, emergency floatation (fixed parts), cargo swing (1400 kg, fixed parts), extended cargo sling capability, pilot windshield wiper, heavy duty blade pins, high visibility red main rotor blade, hourmeter
• Hinged and sliding doors, corporate 5-seat configuration
• Comfort layout with black comfy carpet
• Airworthy status confirmed, full documentation available
About this Model
Overview
The Airbus H125 is a light, single-engine helicopter commonly selected for missions that prioritize hot-and-high performance, useful payload, and operational flexibility. It is widely used in utility, public service, aerial work, and passenger transport roles where landing options are limited and short turn times matter. Buyers typically evaluate it as a practical platform for mixed missions: moving people and equipment to remote sites, conducting aerial observation, and performing external-load tasks.
Mission Fit
The H125 is most at home in missions that demand strong out-of-ground-effect hover capability and predictable handling at altitude. It suits operators who need one helicopter to cover multiple roles—passenger moves, observation, and light utility—without a large support footprint. It is less aligned with missions that require higher passenger counts, extensive cabin amenities, or organizational requirements for twin-engine aircraft.
Cabin
Cabin experience is functional and mission-oriented, with configurations ranging from utility seating to more passenger-focused interiors depending on operator needs. Access and loading are generally designed around practical use—supporting frequent ingress/egress, gear carriage, and the option to prioritize rear-cabin volume or seating. Noise and vibration levels are typical of a single-engine light helicopter and vary with equipment fit and mission profile.