What was found
INSPECTION FOUND A 1/4" CRACK AT RIVET IN L-1 DOOR SKIN AND THE CORNER WAS BENT. THE CRACK WAS LOCATED AT THE UPPER AFT CORNER OF DOOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 32 AND 51-10-3B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1/4" CRACK AT RIVET IN L-1 DOOR SKIN AND THE CORNER WAS BENT. THE CRACK WAS LOCATED AT THE UPPER AFT CORNER OF DOOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 32 AND 51-10-3B.