As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON FUSELAGE SKIN LONGERON 10 RH BETWEEN STA.207 AND 218. FUSELAGE SKIN WAS REPAIRED (PERMANET REPAIR) PER ER/A 576287-14 REV ORIGINAL AND ETI-88-19-022 REV. 2 GENERAL VISUAL INSPECTION ON REPAIR WILL BE MONITORING EVERY 8000 CYCLES UNDER L.P. 0981635 PER ERA 576287-14 REV ORIGINAL SECTION II. (LP0983470)