As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ACCOMPLISHMENT OF SID ITEM 53-2-1 AND .5 INCH LONG CRACK WAS FOUND IN THE FUSELAGE SKIN FROM RIVET TOWARDS CENTER OF LEFT NR 3 EMERGENCY EXIT OPENING, LOWER AFT CORNER. A PATCH WAS FABRICATED AND INSTALLED AS PER VIEW 'A' OF CV 640(340D) SB NR 53-1.