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 BETWEEN 2 FASTENERS AT ATTACH ANGLE FROM FUSELAGE TO VERTICAL STABILIZER, 7 INCHES FROM AFT END OF THE STABILIZER AT RT SIDE. STOP DRILLED SMALL CRACK PER SRM 53-05, FIG 23. ACCOMP HIGH FREQ EDDY CURRENT PER NDT 51-00-03. CHECKED STOP DRILL. INSTALLED DOUBLER PER SRM 53-05 FIG 23. INSTALLED HI-LOKS PER SRM 51-30-5.