As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STAB LOWER LT DRAG ANGLE AFT OF 67.5 PERCENT, REAR SPAR DATUM CRACKED AT FWD END. REMOVED DRAG ANGLE IAW SRM 51-42-22-001-0013, DRILLED UP A TEMPLATE FOR NEW DRAG ANGLE. LOCATED AND DRILLED NEW DRAG ANGLE AND THEN COUNTER SUNK ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW DRAG ANGLE ON VERTICAL STAB IAW SRM 51-42-21-001-001-A01 AND 51-42-13.