Specifications
AI Description
- Model: H125
- Configuration: Utility/Passenger Transport
- Location: Oslo, Norway
- Condition: Used
- Good component status and well-maintained
- Crash-resistant fuel system: Yes
- Engine: Safran Arriel 2D
- Avionics:
- ADS-B equipped: Yes
- Radar altimeter: Yes
- ELT: Yes
- VFR day and night package with integrated flight display Garmin G500H TXI
- ELT – Kannad Integra AP-H
- ICS – Garmin GMA 350H
- Mode S – Garmin GTX 335R – ADS-B Out
- Avionic display system Garmin G500H TXI
- Lightweight data recorder (LDR)
- Static ports relocation
- Additional equipment:
- Dual controls: Yes
- Cargo hook: Yes
- Engine exhaust area black thermal painting
- Pilot’s windshield wiper
- RH side electric and de-iced external mirror
- Cargo swing capacity: 1,400 kg – 3,080 lb
- Capabilities for extended cargo swing
- Enlarged cockpit floor window (right side)
- LH landing light (swiveling in elevation and azimuth)
- Emergency flotation gear – fixed parts
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.