What was found
CRACK AFT UPPER CORNER RING PAN BETWEEN BS 1022 TO 1041 RT SIDE. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122 AND 51-10-3 PAR 14 AND 21 AND ER/A'S 487747-14MA, 493648-14MA.
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 1022 TO 1041 RT SIDE. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122 AND 51-10-3 PAR 14 AND 21 AND ER/A'S 487747-14MA, 493648-14MA.