What was found
C1 LT WING OB LEADING EDGE UPPER RIB CRACKED 12 INCH OB OF IB END. REPAIRED BY STOP DRILLING AND INSTALLING REPAIR ANGLE IAW SRM 57-2-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C1 LT WING OB LEADING EDGE UPPER RIB CRACKED 12 INCH OB OF IB END. REPAIRED BY STOP DRILLING AND INSTALLING REPAIR ANGLE IAW SRM 57-2-0.