As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CHECK-C MAINT, THE RT WING AFT FLAP SECTION, 5 FT O/B OF FUSELAGE HAD HOLE IN COMPOSITE LOWER SURFACE 0.90 IN BY 0.5 IN, LOCATED 13 INCHES AFT OF L/E. INSTALLED HOT BOND ON AFT FLAP O/B OF FUSELAGE PER SRM 51-70-10 AND 57-53-01. REPAIR WAS 2 IN BY 3 IN.