What was found
RIGHT WING L/E INTERIOR UPPER RIB CRACKED .5 INCH AT STA XFS 717.000. STOP DRILLED PER SRM 57-2-5. FABRICATED REINFORCING ANGLE PER SRM 57-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM 57-2-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING L/E INTERIOR UPPER RIB CRACKED .5 INCH AT STA XFS 717.000. STOP DRILLED PER SRM 57-2-5. FABRICATED REINFORCING ANGLE PER SRM 57-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM 57-2-5.