What was found
LEFT FUSELAGE NR 1 AIR CONDITIONING COMPARTMENT DOOR CUT OUT UPPER AFT CORNER SKIN FOUND CRACK ABOUT 1 INCH IN LENGTH. DOOR CUTOUT UPPER AFT CORNER SKIN CARRIED OUT REPAIR AS PER SRM 53-20-15 REPAIR 3 FIGURE 201 REV 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122 INITIAL INSPECTION REQUIRED AT 4,000 FLIGHT CYCLES, REPETITIVE INSPECTION AT 4,000 FLIGHT CYCLES , METHOD: VISUAL INSPECTION AS PER SRM 53-20-15 REPAIR 3 TABLE 201 REV 56