As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/W O/B AFT FLAP ACCESS PANEL NR 588KT AFT SUPPORT I/B AREA CORROSION CRACK REVEALED. CORROSION BLEND OUT 0.055" BY 1" BY 3" EXCEED SRM 57-50-01 FIG 3. LIMIT AFT SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 4 AND HFEC INSP C/OUT AS PER NTM PART6 51-00-0 FIG 4. RESULT NO CRACK FOUND AT CUT LINE AND FIBERGLASS T/E WEDGE REPAIRED AS PER SRM 51-40-12 PART 4D FIG 11.