What was found
RT AFT FUSELAGE TO VERTICAL AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-090, DATED 21 SEPT 2016. NDT PERFORMED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT AFT FUSELAGE TO VERTICAL AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-090, DATED 21 SEPT 2016. NDT PERFORMED.