As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
OUT OF LIMITS FOR THICKNESS REMAIN ON PREVIOUS BLEND OUT, STA Y= 355 BETWEEN LONGERON 18 LT TO 19 LT AT OUTER FUSELAGE SKIN. AREA OUT OF LIMITS WAS REPAIRED. PERFORMED GENERAL VISUAL INSPECTION, INITIAL 8000 CYCLES REPETITIVE EVERY 8000 CYCLES IAW SRM 53-04-2.