What was found
CRACK ON LOWER TAIL SECTION SKIN WRI: 53-10/2763. REPAIRED THE LOWER TAIL SECTION SKIN CRACK BETWEEN STA2319-STA2370, S-45L-45R PER PER SRM53-00-01 REPAIR 6 FIGURE 202. THIS IS A CATEGORY B REPAIR PER SRM53-00-01 REPAIR 6 FIGURE 202. THE INSPECTION THRESHOLD IS 18750FC FROM THE TIME THE AIRPLANE WAS DELIVERED. THE INTERVAL IS 10000FC. INSPECTION METHOD: INTERNAL HFEC (RECOMMENDED), EXTERNAL LHEC(ALTERNATIVE). DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100