As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(LOG 1874559) DURING INSPECTION FOUND SEVERAL PREVIOUS BLEND OUTS ON EXTERNAL SKIN OF FUSELAGE BTW STA= 340 AND STA= 360 STRINGERS 17 AND 19 LH SIDE. SKIN OF FUSELAGE BTW STA= 340 AND STA= 360 STRINGERS 17 AND 19 LH SIDE WERE REPAIRED PER ERA 592771-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND ETI-37-21-421 REV. 1.