What was found
CRACK ON FWD/UPPER CORNER RT RING PAN BETWEEN BS 886 TO 906 IN CPAX. RING PAN RT FWD /UPPER WAS REPAIRED IAW SRM 53-05, FIG 122, PAR 139 ER/A 487747-14 MA, REV A, 493648-14 MA REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FWD/UPPER CORNER RT RING PAN BETWEEN BS 886 TO 906 IN CPAX. RING PAN RT FWD /UPPER WAS REPAIRED IAW SRM 53-05, FIG 122, PAR 139 ER/A 487747-14 MA, REV A, 493648-14 MA REV A.