What was found
UPON INSPECTING THE NR 2 ENGINE FIREWALL, FOUND AN APPROX 2 1/4 INCH CRACK IN AFT WEB AT 8 O'CLOCK POSITION APPROX 6" FROM FLEX ADAPTER. REPAIR WILL BE MADE IAW SRM 54-10-01, 54-10-03 FIG 1 AND M/M 51-30-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON INSPECTING THE NR 2 ENGINE FIREWALL, FOUND AN APPROX 2 1/4 INCH CRACK IN AFT WEB AT 8 O'CLOCK POSITION APPROX 6" FROM FLEX ADAPTER. REPAIR WILL BE MADE IAW SRM 54-10-01, 54-10-03 FIG 1 AND M/M 51-30-0.