What was found
ON AFT WING TO FUSELAGE FAIRING SUPORT STRUCTURE FOUND LH ANGLE BS 939, RT ANGLE BS 939, AND ANGLE ARE CORRODED. (REFERENCE SRM 53-82-55-001-002-A01 SHEET 5 OF 5 ITEMS 96, 97 AND 98). REMOVED AND REPLACED CORRODED ANGLES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON AFT WING TO FUSELAGE FAIRING SUPORT STRUCTURE FOUND LH ANGLE BS 939, RT ANGLE BS 939, AND ANGLE ARE CORRODED. (REFERENCE SRM 53-82-55-001-002-A01 SHEET 5 OF 5 ITEMS 96, 97 AND 98). REMOVED AND REPLACED CORRODED ANGLES.