What was found
RIGHT WING CENTER LEADING EDGE INTERIOR RIB CRACKED .5 INCH AT XFS 310. STOP DRILLED CRACK PER SRM 57-2-0 PG 1-2. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2. INSTALLED ANGLE PER SRM 57-2-0 PG 1-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING CENTER LEADING EDGE INTERIOR RIB CRACKED .5 INCH AT XFS 310. STOP DRILLED CRACK PER SRM 57-2-0 PG 1-2. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2. INSTALLED ANGLE PER SRM 57-2-0 PG 1-2.