What was found
CRACK ON TURBINE EXHAUST CASE S-RAIL APPROX 1700 O'CLOCK ON NR 3 ENGINE. WELD REPAIRED AND STRESS RELIEVED PER PWA ENGINE MANUAL 72-53-01, REPAIR 14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON TURBINE EXHAUST CASE S-RAIL APPROX 1700 O'CLOCK ON NR 3 ENGINE. WELD REPAIRED AND STRESS RELIEVED PER PWA ENGINE MANUAL 72-53-01, REPAIR 14.