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The Vehicle Heath Management System tracks the usage of selected aircraft
components throughout their useful lives. Parts usage is computed for
each aircraft operation and applied to parts in the maintenance management
system. The aircraft configuration information correctly allocates the
actual usage to the installed parts. Several usage indicators (flight
hours, landing cycles, calendar time) may be applied against each tracked
component. Usage indicators may be categorized as either operational or
structural, but they are tracked against parts in the same manner. Usage
can be manually updated for usage accumulated outside of the normal aircraft
operations, such as engine running time in a test cell. |
Structural Usage Processing
Structural
usage processing is a means of determining life usage to the airframe
structural components. Regime recognition and structural usage accumulation
recognizes that different flight maneuvers and operations can produce
different amounts of damage to a part. This approach provides a more accurate
measure of the remaining life of a component than if using flight hours
alone. This is analogous to the operational usage indicators typically
used for the dynamic components of the aircraft. Structural usage indicators
are determined through algorithms based upon the aircraft conditions (e.g.
weight, configuration, etc.) and flight maneuvers undertaken during any
given flight. Goodrich is currently working with Helicopter Original Equipment Manufacturer 's (OEM) and airworthiness authorities to provide structural usage benefits to operators. |