What was found
OUTBOARD END, WEDGE - TOP SURFACE DISBOND. INSTALLED NEW CORE SKIN & DOUBLER PER SRM 51-71-10, 51-70-09, DEFECT SIZE: 2 INCHES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
OUTBOARD END, WEDGE - TOP SURFACE DISBOND. INSTALLED NEW CORE SKIN & DOUBLER PER SRM 51-71-10, 51-70-09, DEFECT SIZE: 2 INCHES.