What was found
RT WING CNTR L/E INTERIOR RIB CRACKED .5 INCH (LWR) AT XFS 385.000. STOP DRILLED CRACK PER SRM 57-2-1 PAR 7. FABRICATED REINFORCING ANGLE PER SRM 57-2-1 PAR 7. INSTALLED REINFORCING ANGLE PER SRM 57-2-1 PAR 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT WING CNTR L/E INTERIOR RIB CRACKED .5 INCH (LWR) AT XFS 385.000. STOP DRILLED CRACK PER SRM 57-2-1 PAR 7. FABRICATED REINFORCING ANGLE PER SRM 57-2-1 PAR 7. INSTALLED REINFORCING ANGLE PER SRM 57-2-1 PAR 7.