As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA. Y=1437 AND BTW LONGERONS 12RH AND 13RH. SUMMARY OF NRC 00058 FUSELAGE SKIN STA Y=1437 AND BTW LONGERONS 12RH AND 13RH WAS REPAIRED (AS PERMANENT REPAIR) PER ER/A 577191-14 REV ORIGINAL AND ETI-90-19-015 REV 2.