What was found
STRINGER CRACK, FWD SIDE OF STA 2360 S-10L. (REPAIR). REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15 REQUIREMENTS. PERFORM EO-95258-REQ1 REV.1 AND EI NO. F2025A53M-2155 REV.0 AND EGAT WORK SHEET NO.50702.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRINGER CRACK, FWD SIDE OF STA 2360 S-10L. (REPAIR). REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15 REQUIREMENTS. PERFORM EO-95258-REQ1 REV.1 AND EI NO. F2025A53M-2155 REV.0 AND EGAT WORK SHEET NO.50702.