What was found
LT WING LATERAL WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE IS CRACKED AT FUSELAGE FRAME 50. REMOVED AND REPLACED THE LT LATERAL WING UPPER ANGLE FROM FS 48-50 IAW SRM 51-40-02 AND IAW CPM 51-21-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING LATERAL WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE IS CRACKED AT FUSELAGE FRAME 50. REMOVED AND REPLACED THE LT LATERAL WING UPPER ANGLE FROM FS 48-50 IAW SRM 51-40-02 AND IAW CPM 51-21-06.