As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT CARGO COMPARTMENT, CEILING SUPPORT BETWEEN FR56/FR57 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y450 TO -Y963. REMOVED CORROSION FROM CEILING AT SUPPORT PANEL FR56/FR57 -Y450 TO -Y953. IAW A300 SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063.MATERIAL LOSS IS .002 REMAINING MATERIAL IS .061 T98828.FOUND TO BE NEGLIGIBLE DAMANGE IAW A300 SRM 51-73-11.