As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CMM 78-31-37 REV 23 FIG 35 ITEM 40B. THE 315A2101-41 INNER WALL BONDED PANEL HAS AN AREA OF DISBOND (PERF SKIN TO CORE) THAT MEASURES 1.5 X 24.5". AFTER REMOVING THE DISBONDED PORTION OF THE SKIN IT WAS DISCOVERED THAT THE PERF SKIN WAS PERPARED INCORRECTLY PRIOR TO ORIGINAL BONDING. THE DISBOND AREA KEEPS GROWING AND NOW MEASURES 5.5 X 33.5".