As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT OTBD FLAP; INBD LOCATION NR 2 MOUNTING SURFACE IS CORRODED. REMOVED CORROSION AND SOLD LIMITS IAW CMM 57-44-08. ETCHED; FLAP-PEENED; CLEANED; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-11-01 AND BSOPM 20-10-02. PRIMED SURFACE; MATERIAL ID FOR SHIM; FABRICATED; PRIMED AND INSTALLED SHIM IAW CMM 57-44-08.