What was found
INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE OF C-2 DOOR INTERIOR SKIN. THE CRACK WAS STOP DRILLED, A WEB REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-30-2 AND 51-40-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE OF C-2 DOOR INTERIOR SKIN. THE CRACK WAS STOP DRILLED, A WEB REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-30-2 AND 51-40-2.