What was found
NICK ON FUSELAGE SKIN AT BS 867 S-25L REPAIRED IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 103, DATED MAR 10, 2011, SECTION 53-30-3, FIGURE 48. HFEC OPEN HOLE INSPECTION OF ALL FASTENER HOLES COMMON TO THE REPAIR IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 103, DATED MAR 10, 2011, SECTION 53-30-3 AND BOEING 737 NDT MANUAL D6-37239, PART 5, 51-00-00, FIGURE 16. NO DEFECTS EVIDENT. HFEC INSPECTION OF CUT OUT EDGES IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 103, DATED MAR 10, 2011; SECTION 53-30-3 AND BOEING 737 NDT MANUAL D6-37239, PART 5, 51-00-00, FIGURE 23. NO DEFECTS EVIDENT (NDT11-0845). REFERENCE NON-ROUTINE WORK ORDER NR 1014379, DATED 5 JULY 2011.