As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON INTERNAL FUSELAGE SKIN STA Y=1021 BTW LONG 13L-14L AT PAX CABIN. CRACKS ON FUSELAGE/SKIN AND DOUBLER/STA 1022 & L-13-L14 WERE REPAIRED WITH ETI-17-16-149 REV 3 AND ER/A 551741-14 REV ORIGINAL. PERFORM GVI ON EXTERNAL SURFACE, EVERY 3000 FLIGHT CYCLES UNDER LOG 2773773 PER ER/A 551741-14 SEC II.