What was found
**CORROSION** ON FUSELAGE SKIN AT BODY STATION 696; RBL 5; WL 305. / [01] REMOVED CORROSION ON FUSELAGE SKIN BS696 RBL5 WL305;1'X1' AREA I.A.W SRM 51-10-02-0G-01 AND ARM90-7023-01 TABLE 3001 ZONE 1; [02] VERIFIED REMOVED CORROSION ON FUSELAGE SKIN BS696 RBL5 WL305;1'X1' AREA I.A.W SRM 51-10-02-0G-01 AND ARM90-7023-01 TABLE 3001 ZONE 1; [03] HFEC INSP BLEND IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [04] UT INSP BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.036' ADJACENT TO 0.040'. EQUIP ID#: ATS2031 S/N: 170515011; [05] DAMAGE ON FUSELAGE SKIN BS696;RBL5;WL305 FOUND TO BE OUT LIMITS I.A.W ARM90-7023-01 TABLE 3001 ZONE 1 ORIGINAL MATERIAL THICKNESS IS 0.040' REMAINING MATERIAL TICKNESS IS 0.036'; [06] VERIFIED DAMAGE ON FUSELAGE SKIN BS696;RBL5;WL305 FOUND TO BE OUT LIMITS I.A.W ARM90-7023-01 TABLE 3001 ZONE 1 ORIGINAL MATERIAL THICKNESS IS 0.040' REMAINING MATERIAL TICKNESS IS 0.036'; [07] REFER TO FAULT TTG8Q005BHK5 FOR REPAIR RESOLUTION.; [08] REFER TO FAULT TTG8Q005BHK5 FOR REPAIR RESOLUTION; QC VERIFIED.; [09] VERIFIED NDI COMPLETE; [10] REFER TO FAULT TTG8Q005BHK5 FOR REPAIR RESOLUTION; QC VERIFIED; [11] REFER TO EA 21-153-01632 SUMMARY REQUIREMENT; BARCODE: TTG8Q005N4KF.