What was found
DURING CHECK-C MAINT, THE LT WING NUMBER 2 L/E SLAT O/B END, THE T/E WEDGE HAD A BULGE THAT WAS DELAMINATING. APPLIED HOT BOND REPAIR ON NR 2 SLAT APPROX 4 IN BY 3.5 DOUBLER PER SRM 57-43-02 AND 51-70-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, THE LT WING NUMBER 2 L/E SLAT O/B END, THE T/E WEDGE HAD A BULGE THAT WAS DELAMINATING. APPLIED HOT BOND REPAIR ON NR 2 SLAT APPROX 4 IN BY 3.5 DOUBLER PER SRM 57-43-02 AND 51-70-10.