What was found
A 3.5" INCH CRACK EXIST AT NR 2 ENGINE T/R I/B L/E UPPER POSITION LOCATED ON BRACKET SUPPORT FLANGE REF 78-31-00-6. REMOVED AND REPLACED NR 2 ENG I/B T/R IAW A300-600 AMM71-13-03-4-05, OPS CHECKED GOOD IAW A300-600 AMM 71-13-03-4-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 3.5" INCH CRACK EXIST AT NR 2 ENGINE T/R I/B L/E UPPER POSITION LOCATED ON BRACKET SUPPORT FLANGE REF 78-31-00-6. REMOVED AND REPLACED NR 2 ENG I/B T/R IAW A300-600 AMM71-13-03-4-05, OPS CHECKED GOOD IAW A300-600 AMM 71-13-03-4-05.