As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN HAS GOUGES AT THE AFT CARGO DOOR FRAME 64 BETWEEN STRINGER 27R AND 28 R. BLENDED GOUGES AT THE AFT CARGO DOOR FRAME 64 BETWEEN STRINGER 27R AND 28R. ORIGINAL THICKNESS ARE 0.236 AND 0.315 IAW A300-600 SRM 53-17-12. REMAINING THICKNESS IS 0.214 AND 0.214 AND 0.285. FOUND TO BE IN LIMITS IAW A300-600 SRM 53-10-12. ALODINED AND PRIMED IAW A300-600 51-40-10. PAINTED IAW A300-600 SRM 51-40-12.