What was found
INSPECTION FOUND A 0.8 INCH CRACK IN R-1 DOOR CUTOUT AFT LOWER CORNER OUTER SKIN, STA 328-344, S16R TO S17R. A REPAIR WAS INSTALLED IAW SRM 53-10-01, REPAIR 2, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 0.8 INCH CRACK IN R-1 DOOR CUTOUT AFT LOWER CORNER OUTER SKIN, STA 328-344, S16R TO S17R. A REPAIR WAS INSTALLED IAW SRM 53-10-01, REPAIR 2, FIGURE 201.