As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C, DURING THE REPAIR ASSESSMENT PROGRAM INSPECTION - BS 560 - 566 STR 38R - 39R EXISTING REPAIR DOUBLER THICKNESS AT FWD CARGO DOOR FWD LOWER CORNER AREA OUT OF SRM REPAIR LIMITS. FWD CARGO DOOR FWD LOWER CORNER AREA REPAIRED AS PER SRM 52-00-03 FIG 4 REFER RAP - SEQUENCE 42 - 17 FOR DETAIL INSTRUCTION.