What was found
INSPECTION FOUND A 1 INCH CRACK IN LT WING FILLET PANEL. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-51-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN LT WING FILLET PANEL. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-51-0.