What was found
DOT#28 A-043 AFT CABIN FLOOR PANEL 241WF HAS PULLED FIBERS <[01]. REPAIRED IAW EA 25-153-00249 AND SRM 53-00-50-2R-1.;[ 02] C/W. AUDIT COMPLETE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DOT#28 A-043 AFT CABIN FLOOR PANEL 241WF HAS PULLED FIBERS <[01]. REPAIRED IAW EA 25-153-00249 AND SRM 53-00-50-2R-1.;[ 02] C/W. AUDIT COMPLETE.