As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ULTRASONIC INSPECTION IAW NDT MANUAL REVEALS THE THRUST REVERSER 315A2101-141 INNER WALL HAS AN AREA OF DISBOND 1.8 X 2.0" LOCATED 18.5" FROM AFT EOP AND 6.0" FROM UPR EOP IN THE FOOT PRINT OF THE NR 3 UPPER COMPRESSION PAD. VISUAL AREA OF DISCOLORATION C/T 315A2101-141 BONDED PANEL ASSY (INNERWALL) IML CENTERED 8.0 FROM LOWER AND 11.0 FROM AFT -141 EOP. ULTRASONIC INSPECTION IAW NDT MANUAL REVEALS A DELAMINATION WITHIN THE DISCOLORED AREA MEASURING APPROX 2.75" X 3.0".