As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKS ( 2 EA ) ON DORSAL FIN L/E ACCESS PANEL 6301A CUTOUT AT VERTICAL STABILIZER. DORSAL FIN L/E ACCESS PANEL 6301A CUTOUT AT VERTICAL STABILIZER WAS REPAIRED (AS PERMANENT) PER ER/A 516509-14MA (SECTION I) REV 4 AND SRM 51-30-2 AND 51-30-5.