What was found
DURING CHECK-C MAINT, THE FLOOR PAN WAS CORRODED AT STA 1022 TO 1041, RL18. REMOVED CORROSION BY CUSP MEMBRANE CUTOUT PER SRM 53-05, VIEW U OF FIG 4F.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, THE FLOOR PAN WAS CORRODED AT STA 1022 TO 1041, RL18. REMOVED CORROSION BY CUSP MEMBRANE CUTOUT PER SRM 53-05, VIEW U OF FIG 4F.