What was found
INSPECTION FOUND A .625 INCH CRACK THROUGH FASTENER AT R-1 DOOR OUTER SKIN LOWER FORWARD CORNER ABOVE GATE. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-40-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .625 INCH CRACK THROUGH FASTENER AT R-1 DOOR OUTER SKIN LOWER FORWARD CORNER ABOVE GATE. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-40-1.