As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK EVIDENCE ON FUSELAGE SKIN LOCATED ON STA Y=1037 AND L-14L. SUMMARY OF NRC 0180: AREA WAS REPAIRED ON FUSELAGE SKIN LOCATED ON STA Y=1037 AND L-14L PER PRI 624765-14 REV 2 AND PER ER/A 624765-14 REV ORIG SECTION I. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE FROM DATE OF APPROVAL ONLY (07MAR25) REF LP 0849461. ASSOCIATED ER/A 14-624765 ADDED FOR AC 9571. (LP #0849867)