What was found
DOT#52 A-043 CABIN FLOOR PANEL 231VF HAS PULLED FIBERS IN CORNERS <[01]. REFER TO FAULT TTG8Q010E6U4 WHERE EA 25-153-01240 WAS ADDED AS A SUBTASK.;[ 02] AUDIT C/W.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DOT#52 A-043 CABIN FLOOR PANEL 231VF HAS PULLED FIBERS IN CORNERS <[01]. REFER TO FAULT TTG8Q010E6U4 WHERE EA 25-153-01240 WAS ADDED AS A SUBTASK.;[ 02] AUDIT C/W.