What was found
DURING C-CHECK, RIGHT WING, INBOARD FOREFLAP HAS A 2.5 INCH CRACK AND 1.5 INCH NARROW DENT ON UPPER SURFACE OUTBOARD IN INBOARD END. REPAIRED CORE AND INSTALLED FIBERGLASS OVERLAY IAW SRM IAW SRM 51-40-06. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, RIGHT WING, INBOARD FOREFLAP HAS A 2.5 INCH CRACK AND 1.5 INCH NARROW DENT ON UPPER SURFACE OUTBOARD IN INBOARD END. REPAIRED CORE AND INSTALLED FIBERGLASS OVERLAY IAW SRM IAW SRM 51-40-06. (M)