What was found
CRACK AFT UPPER CORNER RING PAN BETWEEN BS Y=1231 TO Y=1250 LT SIDE. RING PAN AND SHIM WERE REPLACED IAW SRM 51-30-2, 51-30-5, SRM 51-30-3, PAR 14 AND 21, ER/A'S 493648-14MA, REV A AND 487747-14 MA, REV. A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK AFT UPPER CORNER RING PAN BETWEEN BS Y=1231 TO Y=1250 LT SIDE. RING PAN AND SHIM WERE REPLACED IAW SRM 51-30-2, 51-30-5, SRM 51-30-3, PAR 14 AND 21, ER/A'S 493648-14MA, REV A AND 487747-14 MA, REV. A.