What was found
PIT, Q5, TOP SKIN AND CORE BOND, 3.5 INCH AREA. DELAMINATION, NR 4 SLAT OB END TOP SURFACE. REMOVED DAMAGE, INSTALLED NEW CORE SECTION AND DOUBLER IAW SRM 51-70-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT, Q5, TOP SKIN AND CORE BOND, 3.5 INCH AREA. DELAMINATION, NR 4 SLAT OB END TOP SURFACE. REMOVED DAMAGE, INSTALLED NEW CORE SECTION AND DOUBLER IAW SRM 51-70-10.