Fatigue and Damage Tolerance
Airframe Fatigue and Damage Tolerance (F&DT) is used to define critical structural component lives, and produce an inspection and maintenance schedule to eliminate structural failure.
ROM collaborates with MR. Abraham Brot, a worldwide known expert in the field to provide fatigue analysis capabilities, including definition of fatigue spectrum, fatigue and damage tolerance analysis, inspection and maintenance instructions (inspection methods, threshold and intervals).
ROM uses its inhouse analysis capabilities to provide the baseline data for the fatigue analysis.
