As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON EXTERNAL FUSELAGE SKIN BTW STA 1025 AND 1035 STRINGERS 13 AND 15 LH SIDE. EXTERNAL FUSELAGE SKIN BTW STA 1025 AND 1035 STRINGERS 13 AND 15 LH SIDEL WAS REPAIRED PER ER/A 582117-14 REV.ORIGINAL (SECTION I PERMANENT REPAIR) AND ETI-17-19-175 REV.2. (LP1310886)