What was found
CRACK ON RING PAN STRUCTURE AT AFT LOWER CORNERS BETWEEN BS 1022-1041 AND BS 1041-1060 LT SIDE. REPAIR PARTS WERE FABRICATED, AND INSTALLED IAW SRM 53-05, FIG 122 AND ER/A 487747-14MA, REV ORIGINAL AND REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RING PAN STRUCTURE AT AFT LOWER CORNERS BETWEEN BS 1022-1041 AND BS 1041-1060 LT SIDE. REPAIR PARTS WERE FABRICATED, AND INSTALLED IAW SRM 53-05, FIG 122 AND ER/A 487747-14MA, REV ORIGINAL AND REV A.