What was found
INSPECTION FOUND A 2 INCH CRACK IN MAIN CABIN DOOR PAN FRAME LOWER FORWARD CORNER IN CUTOUT FOR LOWER HINGE ARM. THE DOOR PAN WAS REPLACED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN MAIN CABIN DOOR PAN FRAME LOWER FORWARD CORNER IN CUTOUT FOR LOWER HINGE ARM. THE DOOR PAN WAS REPLACED IAW SRM 51-30-2.