What was found
CORROSION AND CRACK ON COCKPIT FLOOR PANEL 120D. THE CORROSION WAS REMOVED IAW SRM 51-10-3 PAR. 26.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION AND CRACK ON COCKPIT FLOOR PANEL 120D. THE CORROSION WAS REMOVED IAW SRM 51-10-3 PAR. 26.