As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXFOLIATION CORROSION OVER BEAM OF C2 LOWER DOOR JAMB. FASTENERS WERE REMOVED IAW SRM 51-30-5. CORROSION REMOVED IAW SRM 51-10-3 PAR 26. THICKNESS FOUND OUT OF LIMITS IAW SRM 53-05 FIG 123 SHEET 2. REPAIR DOUBLERS, FILLER AND SPACER WERE FABRICATED AND INSTALLED IAW SRM'S 53-05, FIG 123 SHEET 3 AND 51-10-3 P 14-21.