As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON FUSELAGE SKIN STA. 1494 BTW LONGERONS 3 AND 4 LH SIDE. PERMANENT REPAIR SCTION I WAS PERFORMED ON FUSELAGE SKIN STA. 1494 BTW LONGERONS 3 AND 4 LH SIDE. PER ETI- 90-19-016 REV. 1 AND ER/A 577192-14 REV. ORIGINAL. PERFORM WITHIN EVERY 3,000 CYCLES AFTER INSTALLATION OF SECTION I PERMANENT REPAIR: LOG 1032923 PER ER/A 577192-14 REV. ORIGINAL.