What was found
COCKPIT FLOOR PANEL 221 ALF LT SUPPORT ANGLE CRACKED AFT SECTION, APPROX FS 277.00 LBL 12. REMOVED AND REPLACED FLOOR SUPPORT ANGLE ON FS 277.00 & LBL 12 IAW SRM 51-42-06-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
COCKPIT FLOOR PANEL 221 ALF LT SUPPORT ANGLE CRACKED AFT SECTION, APPROX FS 277.00 LBL 12. REMOVED AND REPLACED FLOOR SUPPORT ANGLE ON FS 277.00 & LBL 12 IAW SRM 51-42-06-001-001-A01.