As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER CRACK, FWD SIDE OF STA 2598 S-8L LEVEL 2. (REPAIR). VERIFY REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15 REQUIREMENTS. PAPER FINAL COMPLETED. ACCOMPLISHED REPAIR I.A.W UPS EO-95140-REQ1 REV.1 AND EGAT EI NO.F2025A53M-2076 REV.0 AND SRM 53-80-03-2R-2 REV.46 / TR53-152 AND EGAT WORK SHEET NO.50682.