Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 9JLA2022101331840Actuator · defectiveDURING POST FLIGHT CHECKS IT WAS DISCOVERED A TAIL DE-ICE FAULT CODES RATC 18 AND LATC 18. THE MAINTENANCE TEAM DETERMINED THE LEFT HORIZONTAL LEADING EDGE DEICE ACTUATOR WAS DEFECTIVE. THE ACTUATOR WAS REMOVED, AND A SERVICEABLE UNIT WAS INSTALLED. OPS CHECKSSDR 9JLA2022101331839Manifold · failedTHE FLIGHT CREW REPORTED THAT ON LANDING, AMBER "GROUND SPOILER FAIL" CAS MESSAGE WAS POSTED. INBD SPOILERS FAILED TO DEPLOY. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE GROUND SPOILER MANIFOLD WAS DEFECTIVE. THE DEFECTIVE UNIT WAS REMOVED, AND A SERVISDR 9JLA2021120831806Actuator · defectiveTHE FLIGHT CREW REPORTED THAT THE HORIZONTAL STABILIZER TRIM FAILED IN FLIGHT, THE FLIGHT CREW ELECTED TO DIVERT FLIGHT AND LAND TO INVESTIGATE THE FAULT. THE APPROACH AND LANDING WAS UNEVENTFUL. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE HORIZONTALSDR 9JLA2021120731804None · noneTHE FLIGHT CREW REPORTED THAT THE RIGHT ENGINE EXPERIENCED COMPRESSOR STALL DURING TAKEOFF POWER. THIS CONDITION WAS ALLOWED PER MEL AND OPERATIONS WERE CONTINUED WITH NO RESTRICTIONS. THE MAINTENANCE VENDOR DETERMINED THE FAULT WAS INTERNAL WITH THE ENGINE RESDR 9JLA2021093022798Control Module · defectiveTHE FLIGHT CREW REPORTED THAT AN AMBER STAB TRIM FAIL CAS MESSAGE POSTED ON TOP OF DESCENT. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE STABILIZER TRIM ELECTRONIC CONTROL MODULE WAS FAULTY. THE UNIT WAS REMOVED AND A REPAIRED UNIT WAS INSTALLED. OPS SDR 9JLA2021081222789Ecu · defectiveTHE FLIGHT CREW REPORTED AT APPROX. 1 HOUR INTO FLIGHT A YAW DAMPENER 1 AND 2 FAIL CAS AMBER MESSAGE WAS POSTED ALONG WITH A RUDDER FAULT CYAN CAS MESSAGE. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED A DEFECTIVE RUDDER ELECTRONIC CONTROL UNIT. THE DEFECTIVSDR 9JLA2021072922790Pressure Sensor · defectiveTHE FLIGHT CREW REPORTED THAT DURING CLIMB OUT RECEIVING A RIGHT BLEED FAULT CAS MESSAGE. THE CREW RAN THE CHECKLIST AND ELECTED TO RETURN BACK TO THE AIRPORT AND LAND. LANDING WAS UNEVENTFUL. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE FAULT HAD BEEN SDR 9JLA2021007012278Wire Harness · defectiveTHE FLIGHT CREW REPORTED THAT AFTER LANDING AN ANTI-SKID FAIL CAS MESSAGE WAS DISPLAYED. THE MAINTENANCE TEAM DETERMINED THAT THE RIGHT HAND OTBD MAIN LANDING GEAR WIRING HARNESS WAS DEFECTIVE. THE HARNESS WAS REPLACED WITH A NEW UNIT. OPS CHECKS GOOD, NO DEFESDR 9JLA2021032422780Control Box · defectiveTHE FLIGHT CREW REPORTED THAT A "STAB TRIM FAIL" CAS MESSAGE ILLUMINATED AND THEN CLEARED IN FLIGHT. THE MAINTENANCE TEAM TROUBLESHOT AND FOUND THAT STABILIZER TRIM ELECTRONIC CONTROL MODULE WAS DEFECTIVE. THE UNIT WAS REMOVED AND A INSPECTED/TESTED UNIT WAS I
Other aircraft with N143RL · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N143RL is registered now to the first aircraft listed.