What was found
FUSELAGE SKIN EXTERIOR CRACK, BS2370, S-15L, L=0.7" IAW SRM 53-00-01, REPAIR 1 AND ER/A 488628-14 REV ORIGINAL. PERFORMED FUSELAGE SKIN EXTERNAL REPAIR, THIS IS A CATEGORY"B" REPAIR INSP REQUIREMENTS. INSPECTION THRESHOLD: AFTER REPAIR 1500 FLIGHTS METHOD: INTERNAL HFEC, INTERVAL 6000R/C REF: NDT, PART6, 51-00-00, FIG4. EXTERNAL LFEC, INTERVAL:1500 F/C REF: NDT, PART6 , 53-30-00, FIG 5, DEFERRED.