As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING FLAP FAIRING 633 CB FWD CENTER STIFFENER ANGLE IS CRACKED. REMOVED STIFFENER IAW A310-200 SRM 51-40-21; PG 22. INSTALLED A NEW STIFFENER IAW A310-200 SRM 51-40-21; PG 9; PARAGRAPH B. THE STIFFENER WAS FABRICATED ON N/R N01416 23416.