As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK AT FWD END OF FUSELAGE TO VERTICAL STAB DRAG ANGLE ON RT SIDE. REMOVED AFT DRAG ANGLE ON RT SIDE IAW SRM 51-42-13-001-001-A01, 51-42-21-00-001-A0, 51-42-22-001-001-A01. INSTALLED NEW AFT DRAG ANGLE RT SIDE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-21186. LOCATED AND DRILLED UP NEW DRAG ANGLE ON RT SIDE IAW SRM 51-40-11-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.