What was found
INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR INNER PAN AROUND AFT LOCKING CAM. THE CRACKED AREA WAS BLENDED OUT, TREATED, AND PRIMED IAW SRM 52-01, FIGURE 1, 51-10-3, AND 51-01, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR INNER PAN AROUND AFT LOCKING CAM. THE CRACKED AREA WAS BLENDED OUT, TREATED, AND PRIMED IAW SRM 52-01, FIGURE 1, 51-10-3, AND 51-01, FIGURE 1.