As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CHECK-C MAINT FOUND CRACK AT CANT STA 1463 AND SUPPORT ANGLE AT TOP OF PYLON AND LEFT AFT FUSELAGE. ACCOMP HIGH FREQ EDDY CURRENT PER 51-00-01 PART 6 AND FOUND CRACK CONTAINED AT STOP DRILLED HOLES. REPAIRED PER SRM 54-04 FIG 10.