As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CORROSION ON CREASE BEAM FITTING AT STR 20R, BS 654+44 TO 654+66. REMOVED CORROSION AT CREASE BEAM FITTING AT STR 20R, BS 654+44 TO 654+66. AN AREA 1.00" BY 2.00" BY 0.005" DEEP. ORIGINAL THICKNESS 0.90". REMAINING THICKNESS IS 0.85" FOUND TO BE IN LIMITS IAW SRM 53-00-51/101 SHEET 63 DETAIL I - II. ALODINED AND PRIMED, IAW SRM 51-20-01. INSTALLED FASTENERS IAW SRM 51-40-02.