As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DISBOND - SKIN , LT WING T/E OUTBD FLAP INBD LWR. (REPAIR). IAW SRM 57-53-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.55. PERFORM REPAIR AS BELOW STEP:1.1 REMOVED THE DISBOND MATERIALS AND CLEANED. MEASURE THE DAMAGE SIZE AND LOCATION (L:4.5", W:2", 1.3" FROM AFT EDGE, 0.5" FROM INBD EDGE). BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260F FOR 130 MINUTES AND KEEP A MINIMUM VACUUM OF 22 IN/HG.CONDITION CHECK IS SATISFACTORY.