What was found
CORROSION FOUND ON FLIGHT DECK FLOOR UPPER FLANGE OF BS 259.5; LBL 11 - RBL 11; WL 208 ; / [01] REMOVED FASTENER ON DAMAGED AREA FOR ACCESS I.A.W SRM 51-40-02-0G-0; [02] NO APPLICABILITY ENTRIES FOUND ON SRM <BR>DAMAGE TO BE REMOVE PER SRM 51-10-02-0G-0; [03] REMOVED DAMAGE ON BS 259.5 FLIGHT DECK FLOOR UPPER AFT FLANGE LBL11-RBL11 WL 208.5;22'X1.2' I.A.W SRM 51-10-02-0G-0; [04] VERIFIED CORROSION REMOVED; [05] ET INSPECTED BLEND AND HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23 AND 16; NO CRACKS NOTED.<BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.092'<BR><BR>CAL ID ATS1465 N600<BR>CAL ID ATS2031 E650; [06] NO ALLOWABLE LIMITS FOUND ON SRM FOR BS 259.5 FLIGHT DECK FLOOR UPPER AFT FLANGE LBL11-RBL11 WL 208.5 ORIGINAL MAT. THICKNESS IS 0.094' REMAINING MAT. THICKNESS IS 0.092'I.A.W.SRM 53-10-08-0I-3 CONTACTED ENGINEERING FOR REPAIR INSTRUCTIONS. ACCOMPLISHED REPAIR OF UPPER FLANGE OF CHORD AT BS 259.5 LBL 11 TO RBL 11 WL 208 IAW EA# 21-153-01901 AND EA# 21-153-01901-WIP1