An engine diagnostic system, proposed for the F100 engine, was tested in five specially modified Tactical Air Command F-15 aircraft during a 16-month flight evaluation. After more than 3300 engine operating hours encompassing almost 900 flights during the flight evaluation, these aircraft provided a data base, still being analyzed, that has shown successful demonstration of the original functional characteristics. Four general design requirements, recording engine operating time/low cycle fatigue event detection, engine trim, and trend and performance data collection were demonstrated. Also, validation of maintenance actions taken and indicated needed maintenance were successfully demonstrated.
F100 engine diagnostic system status to date
1981-01-01
Conference paper
No indication
English
F100 engine diagnostic system status to date
AIAA | 1981
|F15/F100 engine diagnostic system
AIAA | 1979
|F100 Engine Diagnostic System (EDS) - Summary of results
AIAA | 1984
|SAE Technical Papers | 1980
|Fuel Control System of the F100 Engine
NTIS | 1981