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 STABILIZER DRAG ANGLE ON LT SIDE. REMOVED AFT DRAG ANGLE ON LT SIDE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01. INSTALLED LT SIDE AFT DRAG ANGLE IAW SRM 51-42-13-001-001-A01, 52-42-21-001-001-A01 AND 51-42-22-001-001-A01, AND DWG PL BA670-35002. LOCATED AND DRILLED NEW DRAG ANGLE ON LT SIDE IAW SRM 51-40-11-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.