What was found
INSPECTION FOUND A 1.25 INCH CRACK IN RT O/B FOREFLAP LEADING EDGE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 57-50-4 AND 51-30-2, PAGE 7.
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 RT O/B FOREFLAP LEADING EDGE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 57-50-4 AND 51-30-2, PAGE 7.