What was found
INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B FLOOR PANEL EDGE AT FS 927 - 1003. THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 53-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B FLOOR PANEL EDGE AT FS 927 - 1003. THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 53-01.