As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW AREA. CPIL. SUMMARY OF NRC 00524: FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW AREA WAS REPAIRED PER PRI 617480-14 REV 1 AND ERA 617480-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617480.