As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENG THRUST REVERSER OUTBOARD COWL UPPER BIFURCATION PANEL INNER (NON PERFORATED) AND OUTER (PERFORATED) SKINS BOTH DELAMINATED FROM L/E TO T/E AND FROM SIDE TO SIDE TOTAL AREA OF DELAM IS BETWEEN 680 AND 700 SQ INCHES, EXCEEDS LIMITS OF MM. INSTALLED REPAIR PER AMM.