As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A CHECK INSPECTION, NR 2 ENGINE NOSE COWL, VISUALLY FOUND AFT INNER SKIN OF ACOUSTIC PANEL CRACKED THREE PLACES (AS VIEWED WITH COWL OPEN): 6 O'CLOCK/8 INCHES LONG; 06:45 O'CLOCK/11 INCHES LONG; 7 O'CLOCK/15 INCHES LONG. APPLIED INTERIM REPAIR IAW SRM 54-00-02,51-40-09 FIGURE 9 AND XEO 71-111707. VISUAL INSPECTION REQUIRED EVERY FLIGHT CYCLE UNTIL NOSE COWL REPLACED.