What was found
INSPECTION FOUND A 4 CRACK IN R-1 DOOR INTERIOR FORWARD NR 2 BEAM. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 25. A J-ANGLE, FITTING, AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 52-05, FIGURE 25 AND 51-10-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 4 CRACK IN R-1 DOOR INTERIOR FORWARD NR 2 BEAM. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 25. A J-ANGLE, FITTING, AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 52-05, FIGURE 25 AND 51-10-3.