What was found
UPPER SKIN OF FLAP T/E WEDGE DELAMINATED. REMOVED PREVIOUS REPAIR AND FABRICATED AND INSTALLED NEW REPAIR IAW SRM 51-70-10. DEFECT SIZE: 2 INCH DIAMETER DELAMINATION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER SKIN OF FLAP T/E WEDGE DELAMINATED. REMOVED PREVIOUS REPAIR AND FABRICATED AND INSTALLED NEW REPAIR IAW SRM 51-70-10. DEFECT SIZE: 2 INCH DIAMETER DELAMINATION.