As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE MAINTENANCE INSPECTION PROCESS IT WAS FOUND THE FUSELAGE SKIN WITH OIL CAN BETWEEN STA 500B AND STA 500B+10" AND BETWEEN STR 22L AND STR 23L. THE AFFECTED SKIN SECTION IS REPAIRED UNDER EO4502 INSTRUCTIONS AND APPROVED BY 8110-3.