N800WS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| JET LINX AVIATION, LLC (9JLA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
THE FLIGHT CREW REPORTED DELAMINATION OF THE RIGHT SPEED BRAKE. THE MAINTENANCE VENDOR REMOVED THE DEFECTIVE SPOILER PANEL AND INSTALLED A SERVICEABLE PANEL. OPS CHECKS OK AND THE AIRCRAFT WAS RETURNED TO SERVICE. NOTE SPOILER PANEL WAS SPLIT ALONG FORWARD INBOARD EDGE FOR SEVERAL INCHES.
THE FLIGHT CREW REPORTED THAT DURING CRUISE FLIGHT THE PILOTS SIDE WINDOW MADE A POPPING SOUND AND THEN THE OUTER PANE TO THE SIDE WINDOW CRACKED AND SHATTERED. THE FLIGHT CREW DECLARED AN EMERGENCY AND STARTED A DESCENT FOR LANDING. THE CREW SAID THEY HAD NO PRESSURIZATION ISSUES. THE LANDING WAS WITHOUT EVENT. NO CAUSE WAS FOUND THAT CAUSED THE WINDOW OUTER PANE TO FAIL. THE WINDOW WAS REMOVED AND A NEW WINDOW WAS INSTALLED. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURN TO SERVICE.
THE FLIGHT CREW REPORTED DURING FLIGHT AN AMBER CAS MESSAGE FUEL BOOST PUMP ON RH CAME ON AFTER TURNING FUEL TRANSFER FROM THE LEFT SIDE BACK TO OFF. THE MAINTENANCE VENDOR FOUND THE RIGHT HAND MOTIVE FLOW VALVE P/N 26430-05 S/N 0093 WAS DEFECTIVE. THE VALVE WAS REMOVED AND REPLACED WITH A REPAIRED UNIT. OPS AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT THEN WAS RETURNED TO SERVICE.
THE FLIGHT CREW REPORTED DURING FLIGHT RECEIVING AN AMBER ENGINE CONTROL FAULT RIGHT SIDE WHEN THE ANTI-ICE WAS TURNED ON. THE MAINTENANCE VENDOR TROUBLESHOT AND FOUND FAULT CODE VT ACTIVE. TROUBLESHOOTING WIRING AND FOUND CHANNEL B OTBD WING ANTI-ICE CIRCUIT RESISTANCE HIGH. CONNECTOR PE008 WAS REMOVED, THE PINS AND SOCKETS WERE CLEANED. REINSTALLED CONNECTOR. OPS CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.
THE FLIGHT CREW REPORTED THAT ON PREFLIGHT CHECKS THAT THE RUDDER BIAS CONTROLS FELT VERY WEAK ON BOTH SIDES. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE RUDDER BIAS ACTUATOR WAS DEFECTIVE. THE RUDDER BIAS ACTUATOR WAS REMOVED AND REPLACED WITH AN OVERHAULED UNIT. OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.
THE FLIGHT CREW INDICATED DURING THE PREFLIGHT CHECKLIST THAT THE RUDDER BIAS SYSTEM FELT VERY WEAK DURING OPERATIONS. THE MAINTENANCE VENDOR VERIFIED THE DISCREPANCY AND REPLACED THE RUDDER BIAS ACTUATOR WITH AN OVERHAULED UNIT. OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.
THE FLIGHT CREW REPORTED THAT IN FLIGHT RECEIVING A CAS MESSAGE INDICATING THAT THE LEFT WING ANTI-ICE SYSTEM FAILED. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE LEFT PYLON PRSOV (VD002) WAS DEFECTIVE. THE DEFECTIVE VALVE WAS REMOVED AND A SERVICEABLE CONDITION VALVE WAS INSTALLED. LEAK CHECK AND FUNCTIONAL CHECKS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.
THE FLIGHT CREW REPORTED IN FLIGHT THAT THE LEFT SIDE COLD AMBER ANTI-ICE INDICATION WITH ALL ANTI-ICE ON INFLIGHT. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE LEFT HIGH PRESSURE SHUTOFF VALVE WAS DEFECTIVE. THE PROSV VALVE WAS REPLACED WITH A INSPECTED PRSOV. LEAK AND OPERATIONS CHECKS, SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.