What was found
LT WING INBOARD MAIN FLAP OUTBOARD AFT WEDGE PANEL LOWER SKIN DELAMINATED 27IN BY 11IN AND EXTENDS TO AFT EDGE. R&R MAIN FLAP PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING INBOARD MAIN FLAP OUTBOARD AFT WEDGE PANEL LOWER SKIN DELAMINATED 27IN BY 11IN AND EXTENDS TO AFT EDGE. R&R MAIN FLAP PER SRM.