The Honeywell F124 turbofan engine has what it takes to power today’s most advanced military jet trainers and light combat fighters.It has the highest thrust-to-weight ratio in its class, thanks to a unique single-stage design that maximizes engine performance. The F124 generates plenty of power without a costly and complex afterburning system – dramatically reducing fuel consumption, saving wear and tear on vital engine parts, and driving superior levels of reliability and availability.
The engine features advanced Full Authority Digital Electronic Control (FADEC) and an integrated Engine Monitoring System (EMS) to keep tabs on engine health, monitor usage and streamline troubleshooting. Modular design makes the engine faster and easier to repair, enabling maintenance teams to put training instructors and student pilots where they belong, back in the air, quickly and efficiently.
Safety is paramount in the flight training world and the T-100 provides an additional safety margin by using two F124 engines. The F124 offers all this and more, backed by the global resources of Honeywell and a reputation earned in producing some of the world’s best turbine engines over more than six decades.
Yes, we retrofit legacy systems (e.g., GE Frame 5, Siemens V94.2) with modern digital controllers, typically completing hardware integration within 4-8 weeks. Software migration requires additional validation time.
We recommend annual performance testing under ISO 3977-2 standards. Critical applications (e.g., offshore platforms) may require semi-annual tests with emissions compliance checks.
All rad-hard devices (e.g., FPGA, ADC) are QML Class V certified under MIL-PRF-38535 and tested to MIL-STD-883 Method 1019 for SEU tolerance. Full qualification reports are available upon request.
Our ASICs and power management ICs operate across -55°C to +175°C ambient temperatures, with derating curves provided in military temperature range (MTR) datasheets.
Our PMA parts (e.g., actuators, sensors) hold FAA/EASA Form 1 certification and match OEM form/fit/function. Installation requires SB/MB documentation per FAA AC 23.1529.
All NAS/MS fasteners include full DNA traceability: melt source (AMS 2301), heat/lot numbers, and AS9100-compliant MTRs with ultrasonic test reports.
AOG orders ship within 4 hours for stocked items (FAA-PMA, EASA Part 21G). Non-stock critical parts trigger priority manufacturing with 72-hour max turnaround.
Gas Turbine
Aircraft parts
