What was found
INSPECTION FOUND A 1.2 INCH CRACK IN FORWARD CARGO DOOR AFT SIDE SEAL FLANGE AT LATCH CAM. THE CRACK WAS STOP DRILLED IAW SRM 52-05. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.2 INCH CRACK IN FORWARD CARGO DOOR AFT SIDE SEAL FLANGE AT LATCH CAM. THE CRACK WAS STOP DRILLED IAW SRM 52-05. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A AND 51-30-5.