What was found
TWO INCH CRACK IN SHEETMETAL IN ENG NR 2 AT 12.30 POSITION IN EXHAUST END. STOPPED DRILLED PER MT78-00. CRACK BEYOND ALLOWABLE MM LIMITS. REPLACED CNA MM 78-11-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TWO INCH CRACK IN SHEETMETAL IN ENG NR 2 AT 12.30 POSITION IN EXHAUST END. STOPPED DRILLED PER MT78-00. CRACK BEYOND ALLOWABLE MM LIMITS. REPLACED CNA MM 78-11-11.