What was found
INSPECTION FOUND A 1.25 INCH CRACK IN LT I/B MLG DOOR AFT LOWER PAN. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 28. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.25 INCH CRACK IN LT I/B MLG DOOR AFT LOWER PAN. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 28. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28.