What was found
LEFT VERTICAL TO FUSELAGE FWD DRAG ANGLE IS CRACKED. CUT & REMOVED CRACKED SECTION OF DRAG ANGLE. FABRICATED ANGLE, FILLER & INSTALLED IAW REO 670-55-31-085 REV A DATED 09 MAY 2016.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT VERTICAL TO FUSELAGE FWD DRAG ANGLE IS CRACKED. CUT & REMOVED CRACKED SECTION OF DRAG ANGLE. FABRICATED ANGLE, FILLER & INSTALLED IAW REO 670-55-31-085 REV A DATED 09 MAY 2016.