What was found
ACFT HAS A CRACK LT FWD UPPER CORNER RING PAN BETWEEN BS Y=674 TO Y=693. LT FWD UPPER CORNER RING PAN BETWEEN BS Y=674 TO Y=693 WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 487747-14 MA, REV A AND 493648-14 MA REV A, D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ACFT HAS A CRACK LT FWD UPPER CORNER RING PAN BETWEEN BS Y=674 TO Y=693. LT FWD UPPER CORNER RING PAN BETWEEN BS Y=674 TO Y=693 WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 487747-14 MA, REV A AND 493648-14 MA REV A, D.