Prior to the advent of the aging aircraft problem, the criterion for ensuring USN airframe safety was a damage index labeled FLE (Fatigue Life Expended). In retrospect, over several decades, the application of the FLE criterion has provided an exemplary, cost effective, structural-safety record. However, with today's realities, the structural engineering community is being directed to maintain airframes longer than originally envisioned and fly beyond the FLE criterion. Consequently, a reliability assessment will provide management with the needed technical support in order to make informed decisions regarding aging airframes and maintenance demands.
Structural Reliability Assessment Methodology - Why Now
1999
12 pages
Report
No indication
English
Aircraft , Environmental & Occupational Factors , Structural Analyses , Structural Mechanics , Fatigue life , Airframes , Structural engineering , Test and evaluation , Methodology , Cost effectiveness , Aging(Materials) , Damage , Structural properties , Reliability , Safety , Engineers , Indexes , Fle(Fatigue life expended)
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