What was found
DURING C2 CHECK INSPECTION, FOUND CRACK IN TWO FLOOR PANEL SUPPORT ABOVE 1 INCH AND 1.5 INCH AT STA 1541 RBL 0 TO RBL 30, LBL 0 TO LBL 30. REPAIRED CRACKED AREA USING REPAIR DOUBLERS PER MD11 SRM53-00-01 FIG 5,VOL1 REV 36.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C2 CHECK INSPECTION, FOUND CRACK IN TWO FLOOR PANEL SUPPORT ABOVE 1 INCH AND 1.5 INCH AT STA 1541 RBL 0 TO RBL 30, LBL 0 TO LBL 30. REPAIRED CRACKED AREA USING REPAIR DOUBLERS PER MD11 SRM53-00-01 FIG 5,VOL1 REV 36.