As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SKIN CRACKED AT NR 1 PYLON FWD STRUT ACCESS PANEL NR 452AL. CRACK FOUND TO BE OUT OF LIMITS LAW SRM 54-30-01. REMOVED DAMAGE LAW SRM 51-10-01. PERFORMED HFEC OF NR 1 PYLON TRIM OUT AT FWD ACCESS PANEL CUT OUT LAW NOT MANUAL PTS/51-00-00, NO DEFECTS NOTED. REPAIRED IAW WITH DRAWING NR 54301221-1.