What was found
PHX - DURING B-CHECK, NR 1 ENGINE TAILCONE HAS CRACK ON AFT LOWER END OF TAILCONE. REPAIRED TAILCONE BY WELDING CRACK CONDITION PER AC 43-13-1A. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PHX - DURING B-CHECK, NR 1 ENGINE TAILCONE HAS CRACK ON AFT LOWER END OF TAILCONE. REPAIRED TAILCONE BY WELDING CRACK CONDITION PER AC 43-13-1A. (M)