As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FLC WEB CORRODED IN X2 SPOTS BS 620 - 640 JUST OTBD OF S27L. BLENDED CORROSION ON FLC WEB BS 620, STR 27L. NOMINAL THICKNESS .036 REMOVED .006 OF MATERIAL REMAINING THICKNESS .030. REMOVED CORROSION IAW 53-00-04-1A-1 DETAIL II. R & R WEB IAW SRM 51-40-02 PARAGRAP 4 AND DWG 143N5359. (1381786)