What was found
INSPECTION FOUND A .5 CRACK IN FLOOR PANEL ATTACH ANGLE AT FS 680, LBL 4. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 CRACK IN FLOOR PANEL ATTACH ANGLE AT FS 680, LBL 4. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3.