What was found
RIGHT FORWARD VERTICAL STAB FUSELAGE ATTACHMENT DRAG ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR IAW REO 690-55-31, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FORWARD VERTICAL STAB FUSELAGE ATTACHMENT DRAG ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR IAW REO 690-55-31, REV A.