What was found
RT WING L/E INTERIOR RIB CRACKED .5 INCH AT XFS 385 UPPER PART. STOP DRILLED CRACK PER SRM 57-2-0 PG 1-2. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2. INSTALLED REINFORCING 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.
RT WING L/E INTERIOR RIB CRACKED .5 INCH AT XFS 385 UPPER PART. STOP DRILLED CRACK PER SRM 57-2-0 PG 1-2. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2. INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2.