N404FL
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
4 reports on file, 2012-01-18 – 2012-07-06.
Part: CONTROL UNIT — MALFUNCTIONED (ANTI SKID SYS) · airframe 6,404 hrs · 5,349 cycles
ON LANDING, CREW REPORTED LOSS OF BRAKING ACTION WITH THE ANTI-SKID SYSTEM ON. WITH ANTI-SKID SYSTEM TURNED OFF, THE BRAKES WORK NORMALLY. MX FOUND THE ANTI-SKID CONTROL UNIT FAILED.
Part: CONTROL VALVE — FAILED (ANTI SKID SYS) · airframe 6,402 hrs · 5,346 cycles
ON LANDING, CREW REPORTED LOSS OF BRAKING ACTION WITH THE ANTI-SKID SYSTEM ON. WITH ANTI-SKID SYSTEM TURNED OFF, THE BRAKES WORK NORMALLY. MX DETERMINED THE ANTI-SKID BRAKE CONTROL VALVE FAILED. THE VALVE WAS REPLACED.
Part: CONTROL VALVE — FAILED (ANTI SKID SYS) · airframe 6,402 hrs · 5,346 cycles
ON LANDING, CREW REPORTED LOSS OF BRAKING ACTION WITH THE ANTI-SKID SYSTEM ON. WITH ANTI-SKID SYSTEM TURNED OFF, THE BRAKES WORK NORMALLY. MAINTENANCE DETERMINED THE ANTI-SKID BRAKE CONTROL VALVE FAILED. THE VALVE WAS REPLACED
Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS)
DURING FLIGHT, LEFT HIGH FLOW PRESSURE RELIEF/SHUTOFF VALVE FAILED TO REGULATE LT ENGINE BLEED AIR RESULTING IN DOWN STREAM OVER PRESSURE CONDITION CAUSING THE OVER PRESSURE RELIEF VALVE TO OPEN PREVENTING WHICH FURTHER DAMAGED TO DOWN STREAM COMPONENTS. FAILING VALVE WAS RETURNED TO MFG ON 17 JAN 2012 FOR EVALUATION. MFG FAILURE ANALYSIS DETERMINED THE PISTON RETURN SPRING FRACTURED.