As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT FUSELAGE TO RUDDER DRAG ANGLE CRACKED AT WHERE WL 102.50 CROSSES REAR SPAR DATUM 67.50 PERCENT. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED CRACKED DRAG ANGLE IAW SRM 51-42-34-001-001-A01 LOCATED DRILLED AND DEBURRED NEW DRAG ANGLE ON LT FUSELAGE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW DRAG ANGLE IAW SRM 51-42-21-001-001-A01 AND SRM 51-42-27-001-001-A01 AND DWG BA670-35002.