As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GREATER THAN 10 PERCENT MATERIAL LOSS INDICATION NOTED AT BS 441 CIRCUMFERENTIAL SPLICE FWD SKIN PANEL BETWEEN STR 1920R. REPAIRED AFT UPR SKIN STA 440 STR 19 IAW FEDEX SRM 53-30-3 AND INITATED PART 5 OF 7-5330-7-2319G FOR BS 441 BETWEEN STR 19-20 FWD SKIN.