What was found
INSPECTION FOUND A 2.2 INCH CRACK IN VERTICAL FIN ATTACH ANGLE FOR PANEL ASSEMBLY AT FS 1431, ZFS -26.812. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2.2 INCH CRACK IN VERTICAL FIN ATTACH ANGLE FOR PANEL ASSEMBLY AT FS 1431, ZFS -26.812. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.