What was found
CRACK AROUND THE FASTENER AT NO.5 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. EDDY CURRENT INSPECTED AREA IAW NDT MANUAL PART 6; 51-00-00 PROCEDURE 23. EXTENT OF CRACK NOTED APPROX .100 INCHES. REMOVED DAMAGED PART IAW SRM 57-42-01-2R-8, STEPS 4.B.C. EDDY CURRENT INSPECTED DAMAGE TRIM OUT & SURROUNDING AREA IAW NDT MANUAL PART 6, 51-00-00 PROCEDURE 23. NO CRACKS FOUND. EDDY CURRENT INSPECTED OPEN HOLES COMMON TO REPAIR AREA IAW NDT MANUAL PART 6, 51-00-00 PROCEDURE 16. CRACK INDICATION NOTED AT FORWARD MOST OUTBOARD FASTENER HOLE COMMON TO ACTUATOR FITTING. NR 5 SLAT WAS REPAIRED ON ATS COMPONANTS WO 544729,REMOVAL AND INSTALLATION OF NR 5 SLAT ACCOMPLISHED ON FAULT TTG8Q009EAXR.