What was found
CRACK ON TOP OF RT ENG TAIL CONE. CRACK MEASURES 3.75" & RUNS LENGTHWISE ADJACENT TO PREVIOUS WELD. ACCEPTABLE AS IS WITHOUT REPAIR IAW V2500 SRM 54-40.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON TOP OF RT ENG TAIL CONE. CRACK MEASURES 3.75" & RUNS LENGTHWISE ADJACENT TO PREVIOUS WELD. ACCEPTABLE AS IS WITHOUT REPAIR IAW V2500 SRM 54-40.