What was found
LEFT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE IS CRACKED. CUT & REMOVED DAMAGED SECTION. FABRICATED & INSTALLED REPAIR IAW REO 670-55-31-083 REV A DATED 02 MAY 2016.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE IS CRACKED. CUT & REMOVED DAMAGED SECTION. FABRICATED & INSTALLED REPAIR IAW REO 670-55-31-083 REV A DATED 02 MAY 2016.