Specifications
Broker
Aircraft Details
Offered "as is" Ex-Works China with valid EcoA. Aircraft based in Ordos City, Inner Mongolia, China. PAX Utility configuration with right-hand side electric & de-iced external mirror, cargo swing (1,400 kg capacity), dual sliding doors, vertical reference window, and capabilities for extended cargo swing. Equipped with Garmin G500 flight deck, ADS-B, Garmin GTN 650H GPS/VHF/VOR, Garmin GNC 255A VHF/VOR, Garmin GTX 335R Mode S transponder, and Kannad AP-H extended range ELT. Features dual controls, heavy duty blade pins, Thales Avionics 200A starter-generator, enhanced external paint, short protective skid shoes, reinforced sand-protection strips on main and tail rotor blades, tail rotor arch, and engine flushing device. Airframe total time: 800 hours. Powered by SAFRAN ARRIEL 2D engine. Interior and exterior both from 2018. VFR flight rules, single pilot operation.
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.