As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING INNER CAVITY AREA OF THE FRUGER FLAP; AFT OF THE FIXED L/E; THE INBD LOWER HORIZONTAL ANGLE IS CRACKED. REMOVED LOWER ANGLE ASSY IAW SRM 51-40-21; PG 7. FABRICATED DIAPHRAM; 4 BRACKETS AND 2 SIDE ANGLES IAW DWGS A57242003 AND A572420078. ALODINED PARTS IAW SRM 51-21-10; PG 3. PRIMED AND PAINTED PARTS IAW A300-600 SRM 51-23-10; PGS 21-22. INSTALLED DIAPHRAM; 4 BRACKETS AND 2 SIDE ANGLES IAW SRM 51-40-21; PG 7.