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Under the Contractual
Engineering Task, "Retrogression and Re-Aging (RRA) of 7057-T6 Corrosion Prone
Parts", UDRI will transition previously developed laboratory RRA procedures into a
robust Shop-level process to improve the corrosion resistance of 7075-T6 aircraft parts or
components. Using conventional and readily available heat-treating equipment, procedures
for the Shop RRA process ill be developed and
validated, and the process documented in a user-friendly process manual to allow for RRA
treatment by an Air Force, or independent, facility. To allow for maximum utility, the
developed Shop RRA procedures will be sufficiently generic to enable RRA-treatment of all types
of aircraft parts. UDRI will demonstrate the process by treating aircraft parts at an
Air Force facility or approved supplier, and will transition the process to the Air Force.
To enable treatment of parts that are still installed, or partially installed, on an aircraft,
UDRI will develop an in-situ RRA process. Utilizing portable equipment, in-situ RRA
process procedures will be developed, validated, and documented in a user's manual.
The prototype in-situ RRA equipment will be delivered to a selected Air Force facility, and
validation testing will be done by in-situ treating aircraft components without full
disassembly. At the conclusion of the program, the portable in-situ RRA equipment, along
with operating instructions for using and maintaining the prototype equipment, will be
delivered to the Air Force.
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