What was found
LONGERON CHORD FWD END AT STA 1220 TO 1238 CORRODED. AFTER CORROSION REMOVED, NDI SHOWED 10 INCH CRACK DUE TO INTERGRANULAR CORROSION. REPAIRED IAW ASA CKF-EXB-080 SUPP SHEETS 1 & 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LONGERON CHORD FWD END AT STA 1220 TO 1238 CORRODED. AFTER CORROSION REMOVED, NDI SHOWED 10 INCH CRACK DUE TO INTERGRANULAR CORROSION. REPAIRED IAW ASA CKF-EXB-080 SUPP SHEETS 1 & 2.