As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ETOPS - #2 ENGINE INLET COWL EXTERNAL SKIN IS CRACKED/PUNCTURED @ APPROX. 5:30 POSITION 1" FROM AFT EDGE EXTENDING 9 1/4" FWD. // REMOVED #2 AIR INTAKE COWL PER AMM 71-61-41-000-802-A. 1724236 3/3/21 REPLACED AND INSTALLED #2 AIR INTAKE COWL PER AMM 71-61-41-400-802-A. OPS CHECK, LEAK CHECK GOOD. OK FOR SVC. COWL, NOSE; AIR OFF 43-7111-9-0003 02478 ON 43-7111-9-0003 02144