What was found
STRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-15L. PERFORM EO-95204-REQ1 REV.1 AND EI NO.F2025A53M-2012 REV.2. VERIFY REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15 REQUIREMENTS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-15L. PERFORM EO-95204-REQ1 REV.1 AND EI NO.F2025A53M-2012 REV.2. VERIFY REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15 REQUIREMENTS.