What was found
INSPECTION FOUND A .5 INCH CRACK IN LT O/B MIDFLAP I/B MOST RIB. THE CRACK WAS STOP DRILLED AND A REINFORCING ANGLE WAS INSTALLED IAW SRM 51-40-3 AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN LT O/B MIDFLAP I/B MOST RIB. THE CRACK WAS STOP DRILLED AND A REINFORCING ANGLE WAS INSTALLED IAW SRM 51-40-3 AND 51-10-2.