Disassembly Inspection and Overhaul of X-22A Gear Reduction and Propeller Assemblies.
Final rept. May 77-Jul 78,
UNITED TECHNOLOGIES CORP WINDSOR LOCKS CONN HAMILTON STANDARD DIV
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This report presents the results of the disassembly inspection and overhaul of four Hamilton Standard designed and fabricated X-22A gear reduction and propeller assemblies. These units has operated intermittently since 1966 and had accumulated a total of 574 flight research hours. All functional components appeared to be in satisfactory condition and, following minor corrective action, the units were returned to service. Author