What was found
CRACK FWD UPPER CORNER RING PAN BETWEEN BS 503 TO 522 RT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, 51-10-3, PAR 14 & 21 AND ER/AS 487747-14MA REV A,AND 493648-14MA, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FWD UPPER CORNER RING PAN BETWEEN BS 503 TO 522 RT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, 51-10-3, PAR 14 & 21 AND ER/AS 487747-14MA REV A,AND 493648-14MA, REV A.