What was found
A 2 INCH SQUARE AREA OF DISBOND ON OUTBOARD END OF UPPER TAB SURFACE. REMOVED DAMAGED AREA OF SKIN AND CORE, PREPARED AND HOT BONDED NEW CORE INTO REPAIR AREA, FABRICATED REPAIR DOUBLER AND HOT BONDED PER SRM 51-70-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 2 INCH SQUARE AREA OF DISBOND ON OUTBOARD END OF UPPER TAB SURFACE. REMOVED DAMAGED AREA OF SKIN AND CORE, PREPARED AND HOT BONDED NEW CORE INTO REPAIR AREA, FABRICATED REPAIR DOUBLER AND HOT BONDED PER SRM 51-70-2.