What was found
DURING CHECK-C MAINT, COCKPIT FLOOR SUPPORT ANGLE HAD CORROSION AT STA 148 TO 157, CENTER FLOOR SUPPORT APPROX LBL 12. INSTALLED NEW FLOOR SUPPORT PER SRM 51-1-0 WITH BOLTS PER SRM 51-30-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, COCKPIT FLOOR SUPPORT ANGLE HAD CORROSION AT STA 148 TO 157, CENTER FLOOR SUPPORT APPROX LBL 12. INSTALLED NEW FLOOR SUPPORT PER SRM 51-1-0 WITH BOLTS PER SRM 51-30-0.