As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT COCKPIT FLOOR SUPPORT AND ANGLE CORRODED. REMOVED CORROSION ON AFT COCKPIT FLOOR AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-00-101--001-A01 AND 51-21-06-001-001-A01. R & R AFT COCKPIT FLOOR SUPPORT ANGLE REF DWG CC670-34095 SRM 51-40-11-001-001-A01, 51-23-00-001-001-A01, 51-42-06-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.