As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON MAIN DECK CARGO DOOR FUSELAGE LOWER FRAME SUPPORT FITTING, NR 1 HOLE NR A, B AND C FOUND CRACKED AND HOLE DIAMETER REACHED 0.560". SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.