What was found
SURFACE CORROSION AT FLIGHT DECK FLOOR SKIN PANEL BETWEEN STA 259.5 AND STA 270 ;S-17L ;WL 208.1. REMOVED THE CORROSION IAW SRM. 51-10-02-0G-0. PERFORMED UT THICKNESS INSPECTION ON REWORKED AREA IAW NDT PART 4 51-00-00 PROCEDURE 3. MIN. THICKNESS IS 0.059'. ORIGINAL MAT 0.063' MATERIAL REMAINING 0.059' MATERIAL REMOVED 0.004', FOUND TO BE WITHIN LIMITS IAW SRM 53-10-51-1A-1 FIG 105 DETAIL C. TREATED AND PRIMED AREA IAW AMM51-21-72-370-804.