What was found
LEFT VERTICAL TO FUSELAGE DRAG ANGLE IS CRACKED. MAINTENANCE REPAIRED THE DRAG ANGLE IAW EC/TC REO 670-55-31-018.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT VERTICAL TO FUSELAGE DRAG ANGLE IS CRACKED. MAINTENANCE REPAIRED THE DRAG ANGLE IAW EC/TC REO 670-55-31-018.