What was found
FOUND ONE CRACK DURING HFEC AT STABILIZER STA 138.70 2" AFT OF EXISTING REPAIR. ENDS OF CRACK MARKED. ACFT GROUNDED. REMOVED DAMAGE AND ACCOMPLISHED DOUBLER REPAIR IAW SRM 55-10-01-2R-11, FIG 204, REPAIR 11 IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD IS DUE AT 56000 FLIGHT CYCLES, REPEAT INTERNAL INSPECTIONS ARE REQUIRED AT 9000 FLIGHT CYCLES BY DETAILED VISUAL INSPECTION OR EXTERNAL LFEC INSPECTION IAW NDT PART 6 53-30-00, PROC 5 IAW SRM 55-10-01-2R-11.