As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L1 CREW DOOR EXTERNAL LOWER SKIN HAS GOUGES .89-25. BLENDED AREA IAW-A300-SRM-51-73-10. MAX DEPTH WAS .003 (T04010) FOUND TO BE WITHIN LIMITS IAW-A300SRM-52-11-00. FIGURE 102. ORIGINAL THICKNES .09 REMAINING MATERIAL .0897. PERFORMED HFEC ON BLENDED AREA. NO DEFECTS FOUND.