As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING OTBD FLAP INBD FWD HINGE SIDE LOAD FITTING FOUND CORRODED. REWORKED IAW CMM 57-44-08 REVISION 78. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306652 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.