What was found
INSPECTION FOUND COCKPIT FLOOR PANEL ATTACH ANGLE CORRODED AT BS 304-280, WL 208.1, LBL 40. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND COCKPIT FLOOR PANEL ATTACH ANGLE CORRODED AT BS 304-280, WL 208.1, LBL 40. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.