What was found
INSPECTION FOUND A 6 INCH CRACK IN FORWARD BAGGAGE BIN DOOR INNER SKIN AT BOTTOM AFT SIDE. THE CRACK WAS STOP DRILLED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 52-05, 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 FORWARD BAGGAGE BIN DOOR INNER SKIN AT BOTTOM AFT SIDE. THE CRACK WAS STOP DRILLED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 52-05, FIGURE 26A.