As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING OTBD FLAP, OTBD FWD HINGE SIDE LOAD FITTING SPOT FACE FOUND CORRODED. REWORKED IAW CMM 57-44-09 REVISION 78. NEW SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.