What was found
INSPECTION FOUND A 3/8" CRACK IN C-2 DOOR EXTERIOR SKIN AT AFT UPPER CORNER OF DOOR HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3/8" CRACK IN C-2 DOOR EXTERIOR SKIN AT AFT UPPER CORNER OF DOOR HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 202.