What was found
INSPECTION FOUND A 1.5 INCH CRACK AT AFT LIGHTENING HOLE OF C-1 CARGO DOOR WEB. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, PAGE 6B, 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK AT AFT LIGHTENING HOLE OF C-1 CARGO DOOR WEB. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, PAGE 6B, 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-11.