As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT ENGINE STRUT 2 AFT NACELLE STRUT FAIRINGS IN ACCESS PANEL 447BL INTERNAL PART IN HYDRAULIC SHUT OFF VALVE WITH BROKEN CONNECTOR.(<P>CONNECTOR OF HYDRAULIC SHUTOFF VALVE AND BACKSHELL WERE REPLACED (PN: BACC63BW14SC5S & PN: BACC10HV14) INSTALLATION TEST WAS SATISFACTORY I.A.W. SWPM 20-60-06. NO FURTHER DEFECTS NOTED.</P>)