As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LH IB MAIN FLAP TE WEDGE ASSY ADDITIONAL DISBOND UPPER AND LOWER SKINS WHILE PERFORMING TAP TEST FOUND ADDITIONAL AREAS OF DISBOND TO UPPER AND LOWER SKINS OF TE WEDGE. FOUND LOWER SKIN DISBOND 30 IN. L X 12 IN. W. FOUND UPPER SKIN DISBOND OF 27.5 IN. L X 6 IN. W.<[01] REMOVED LH IB MAIN FLAP TE WEDGE PER SRM 51-40-02;[02] REFERENCE TTG8Q0100PEW FOR REPLACEMENT WEDGE INSTALLATION