As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON BORES AND INTERIOR SIDES OF FITTING AT RT SLAT NO .0 STA XIS=40. AREAS WERE REWORKED AND MEASURED THEREFORE OUT LIMITS IAW SRM 57-02, PAR 9C(1) AND TABLE 1 WITH DIAMETER FWD HOLE 0.9385" AND AT HOLE 0.9385" BUSHINGS WERE FABRICATED IAW SRM 57-02, PAR 9 C(2).