As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H ENGINE LOW PRESSURE TURBINE CASE COOLING TUBE SUPPORT ANGLE BRACKET; AT 4 OCLOCK POSITION; FORWARD FLANGE IS SEPARATED (SHEARED) FROM BRACKET. REMOVED AND REPLACED L/H ENGINE LOW PRESSURE TURBINE CASE COOLING TUBE SUPPORT ANGLE BRACKET; AT 4 O?CLOCK POSITION REF AMM 70-20-02.