What was found
LT AFT DRAG ANGLE CRACKED WHERE THE VERTICAL STABILIZER MEETS THE FUSELAGE. REPAIRED IAW REO 670-55-31-091 REV DATED 2016-11-01. NDT PERFORMED. NO DEFECTS NOTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT AFT DRAG ANGLE CRACKED WHERE THE VERTICAL STABILIZER MEETS THE FUSELAGE. REPAIRED IAW REO 670-55-31-091 REV DATED 2016-11-01. NDT PERFORMED. NO DEFECTS NOTED.