What was found
RT WING LOWER SURFACE L/E; #6 SLAT NOSE SKIN AT ACTUATOR RIBS. CRACK AROUND FASTENER SKIN. CRACK CONFIRMED IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK FOUND AT 2ND FWD O/B FASTENER. CRACK LENGTH :0.157. REMOVED INBD CENTER, OTBD COVE SKIN & PARTIAL FLEX SKIN SECTION IAW SRM 51-40-02-0G-0; REMOVED FASTENER FROM REPAIR AREA, CUTOUT DAMAGE AREA IAW SRM 57-42-01-2R-8 FIG 202; PERFORMED HFEC AT CUT OUT IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS. PERFORMED HFEC HOLE PROBE INSPECTION ON ALL REMOVED FASTENER LOCATIONS WITHIN REPAIR AREA IAW NDTM PART 6; 51-00-00; PROCEDURE 16. NO CRACKS. FABRICATED DOUBLER AND FILLER IAW SRM 57-42-01-2R-8.