As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:2C FUSELAGE INTERMEDIATE PRESSURE CLOSING PANEL IS CRACKED AT STA 1376, X= -31.5 AND BETWEEN Z= -25.613 & Z= -56.5. REPAIRED CRACKED FUSELAGE INTERMEDIATE PRESSURE CLOSING PANEL AT STA 1376, X= -31.5 AND BEWTEEN Z= -25.613 & Z= -56.5 IAW EA 011-5310-01-A8333 REV I/R AND EO MD11-5310-76895-A. (MAJOR)