As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION, FOUND LOWER DOOR FRAME SUPPORT FITTING FOUND HOLE "A" CRACKED. REWORKED TO SIZE 0.560" CRACK STILL EXISTS. SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 117.