As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHK IN TPE INSPECTION FOUND CRACK FROM VERT STAB ACCESS PNL 364FR. FOUND AFT FUSELAGE UPPER SKIN CHANNEL BOTH ENDS CRACKED AT STA 2065 BETWEEN X=13.65 AND X=-13.65 (REF EGAT NRC U05086). REPAIRED THE CHANNEL ON VERT STAB ACCESS PNL 364FR IAW MD-11F SRM VOL 1 53-00-01 REV 40. APPLIED PROTECTIVE COATING. CHECK NORMAL AND JOB COMPLETE.