What was found
INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF UPPER AFT CORNER OF L-1 DOOR PAN. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-40-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF UPPER AFT CORNER OF L-1 DOOR PAN. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-40-2.