What was found
AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE ANGLE AT BS 939 WAS CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, 51-40-11, 51-45-00, AND 51-25-16.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE ANGLE AT BS 939 WAS CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, 51-40-11, 51-45-00, AND 51-25-16.