As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C AFTER I/B FLAP O/B SEGMENT REMOVAL, FOUND FWD O/B SEGMENT MOST O/B AFT END 01/EA ANGLE CRACKED. THE ABOVE MENTIONED CRACKED AREA ANGLE REMOVED PER SRM 51-35-01.V.2R.38. NEW T-FAB & MAT USED S2931361X7075T6511 PER EN1063-06. HFEC C/OUT FOUND NO EVIDENT OF CRACK AT FAB T-ANGLE REWORKED AREA, REPAIR ACCOMPLISHED PER EN1063-06. NEW TEE HOLES TRANSFERRED & NEW TEE INSTALLED PER SRM 51-21-01V.2.R38.