What was found
A 1.5" AND A .5 INCH CRACK EXIST AT NR 2 ENGINE O/B T/R UPPER L/E FLANGE REF 78-31-00-6. REMOVED AND REPLACED NR 2 ENG O/B T/R IAW A300-600 AMM 71-13-03-4-05 OPS CHECK GOOD IAW A300-600 AMM 71-03-4-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 1.5" AND A .5 INCH CRACK EXIST AT NR 2 ENGINE O/B T/R UPPER L/E FLANGE REF 78-31-00-6. REMOVED AND REPLACED NR 2 ENG O/B T/R IAW A300-600 AMM 71-13-03-4-05 OPS CHECK GOOD IAW A300-600 AMM 71-03-4-05.