What was found
CRACK ON LT RING PAN UPPER FWD CORNER BETWEEN BS 579 TO 598. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122, 51-10-3, PAR 14,21 AND ER/A 487747-14MA, REV A AND ER/A 493648-14MA, REV A. LONG OF CRACK IS 0.450".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LT RING PAN UPPER FWD CORNER BETWEEN BS 579 TO 598. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122, 51-10-3, PAR 14,21 AND ER/A 487747-14MA, REV A AND ER/A 493648-14MA, REV A. LONG OF CRACK IS 0.450".