What was found
LT AFT FUSELAGE TO VERTICAL FWD DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018, DATED 16 APR 2016. NDT PERFORMED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT AFT FUSELAGE TO VERTICAL FWD DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018, DATED 16 APR 2016. NDT PERFORMED.