What was found
FUSELAGE TO VERTICAL ATTACH POINT LT DRAG ANGLE CRACKED AT FRAME 67. REPAIRED LT DRAG ANGLE IAW REO 690-55-31-004. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE TO VERTICAL ATTACH POINT LT DRAG ANGLE CRACKED AT FRAME 67. REPAIRED LT DRAG ANGLE IAW REO 690-55-31-004. MAJOR REPAIR.