What was found
INSPECTION FOUND A 6 INCH CRACK IN AFT CARGO DOOR INNER PAN AT AFT LATCH CLAMP. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 26A. A REPAIR ANGLE WAS INSTALLED IAW SRM 52-01, FIGURE 26A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 6 INCH CRACK IN AFT CARGO DOOR INNER PAN AT AFT LATCH CLAMP. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 26A. A REPAIR ANGLE WAS INSTALLED IAW SRM 52-01, FIGURE 26A.