What was found
FOUND CRACK AT RT HORIZONTAL STAB LOWER SKIN AT 138.70, 33 INCHES FROM THE FWD SPAR. ACCOMPLISHED REPAIR IAW SRM 55-10-01 REPAIR 11. DIP REQUIRED FOR DETAILED VISUAL & LFEC INSPECTIONS, BEGINNING AT THRESHOLD 56,000 FLIGHT CYCLES & REPEAT INSPECTIONS EVERY 9,000 FLIGHT CYCLES THEREAFTER. SEE TABLE 204 & FIGURE 206. INSPECT AT THRESHOLD OF 56,000 FLIGHT CYCLES AFTER REPAIR INSTALL & REPEAT AT INTERVALS OF EVERY 9000 FLIGHT CYCLES THEREAFTER IAW SRM 55-10-01 REPAIR 11 DIP CONTROL 33576.