What was found
INSPECTION FOUND A 0.65" CRACK IN FUSELAGE SKIN AT THE R-2 DOOR UPPER HINGE CUTOUT UPPER FORWARD CORNER. THE SKIN WAS REPAIRED IAW SRM 53-60-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 0.65" CRACK IN FUSELAGE SKIN AT THE R-2 DOOR UPPER HINGE CUTOUT UPPER FORWARD CORNER. THE SKIN WAS REPAIRED IAW SRM 53-60-01.