Honeywell F125IN Turbofan Engine
F125IN Features

Key Features:

  • Best-in-class thrust to weight ratio
  • Minimal thrust deterioration
  • Modular engine design
  • Full Authority Digital Engine Control (FADEC)
  • Integrated engine health monitoring system
  • High reliability and durability
  • Over 500,000 hours of operation on the F124 – F125 engine series

Specifications:

Performance at Sea Level Static, Standard Day, Nominal Engine

  Intermediate Maximum
Thrust (lbf) 6,230 9,850
SFC (lbm/hr/lbf) 0.775 1.910
Inlet Airflow (lbm/s) 92.5 92.5
Overall Pressure Ratio 19.2 19.2
Bypass Ratio 0.46 0.46

 

Current Platforms/Applications:

The F125 engine powers AIDC’s Indigenous Defense Fighter (IDF) aircraft.
The F124 (non-afterburner variant of the F125IN) powers the following aircraft:

  • Alenia Aermacchi M-346 Advanced Jet Trainer
  • Aero Vodochody Czech Air Force L-159
  • Boeing/DARPA X-45A UCAV

 


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F125IN Turbofan Engine
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Force - F125IN engine and Interview with Arijit Ghosh
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Aeromag - Honeywell,
HAL celebrate 25 years
of engine production

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aeromag.in
Strategic Affairs - New Avenues with Garret Mikita
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Indian Defence Review
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indiandefencereview.com
SAIL HR Excellence Award
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epaper.timesofindia.com
Vayu – IAF Jaguars
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Vayu – Interview with Garret Mikita
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DefExpo Webcast
Interview with India Lead for Defense & Space
F125IN Screensaver
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