What was found
DURING ROUTINE C-CHECK INSPECTION, AN EXTERIOR SKIN CRACK WAS NOTED. THE CRACK WAS NOTED AT THE NOSE WHEELWELL AFT LT OUTBOARD CORNER OF THE DOOR CUT OUT. THE CRACK, .0250 INCH IN LENGTH, TERMINATED IN A FASTENER HOLE. AN EXTERNAL REPAIR DOUBLER WAS INSTALLED IAW DRAWING HSE27-53-133, WHICH WAS FAA DER APPROVED, AND E.O. 53-DC8-122. (X)