What was found
RIGHT WING L/E INTERIOR UPPER RIB CRACK AT STA XFS 693.000. 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.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING L/E INTERIOR UPPER RIB CRACK AT STA XFS 693.000. 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.