What was found
L/H AFT VERTICAL STAB TO FUSELAGE DRAG ANGLE CRACKED . CORRECTIVE ACTION: REPAIRED L/H AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018 REV A, DATED 2016-11-10 REFER TO AVMAX W/O: 80989 W/C: 1184.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
L/H AFT VERTICAL STAB TO FUSELAGE DRAG ANGLE CRACKED . CORRECTIVE ACTION: REPAIRED L/H AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018 REV A, DATED 2016-11-10 REFER TO AVMAX W/O: 80989 W/C: 1184.