What was found
INSPECTION FOUND A 2 CRACK IN FORWARD CARGO DOOR PAN ON LOWER SIDE OF DOOR NEAR NR 2 FRAME. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 8. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-4, 51-30-02, AND 51-30-7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 CRACK IN FORWARD CARGO DOOR PAN ON LOWER SIDE OF DOOR NEAR NR 2 FRAME. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 8. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-4, 51-30-02, AND 51-30-7.