What was found
LEFT WING TRAILING EDGE WEB SUPPORT ANGLE, ATTACHED TO FLAP DEFLECTION RIB AND AFT OF NR 1 ENGINE PYLON CRACKED IN RADIUS. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING TRAILING EDGE WEB SUPPORT ANGLE, ATTACHED TO FLAP DEFLECTION RIB AND AFT OF NR 1 ENGINE PYLON CRACKED IN RADIUS. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02.