As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT FUSELAGE SKIN AROUND VACUUM VENT HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. REMAINING MATERIAL OUT OF LIMITS PER SRM 53-41-11. REMOVED EXISTING FASTENERS PER SRM 51-42-11. CUT OUT DAMAGED SKIN AREA IAW SRM 53-41-11. FABRICATED DOUBLER AND FILLERS PER SRM 53-41-11. LOCATED AND DRILLED PER SRM 53-41-11 FIG 205. INSTALLED DOUBLER AND FILLERS IAW SRM 53-41-11 FIG 205.