# Service difficulty reports: N200CR A list on [N200CR](https://openairdocs.org/aircraft/N200CR.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 2025FA0000158](https://openairdocs.org/sdr/2025FA0000158.md): Anti-Ice Valve · failed · Feb 24, 2025 · N200CR · Amd FALCON2000EX · Engine Anti-Icing System > WHILE IN CRUISE FLIGHT, CREW SELECTED RIGHT ENGINE ANTI-ICE. THE ENGINE ANTI-ICE VALVE OPENED PROPERLY. ONCE CLEAR OF ICING CONDITIONS, THE CREW SELECTED THE RIGHT ENGINE ANTI-ICE VALVE TO CLOSE BUT IT FAILED IN THE OPEN POSITION. - [SDR 2023FA0000772](https://openairdocs.org/sdr/2023FA0000772.md): Valve · failed · Nov 20, 2023 · N200CR · Amd FALCON2000EX · Aircraft Fuel System > DURING SINGLE POINT PRESSURE REFUELING, ONE OF THE THREE SYSTEM VENT VALVES FAILED TO OPEN. THIS FAILURE RENDERED THE SINGLE POINT PRESSURE REFUELING INOPERATIVE. - [SDR 2022FA0000753](https://openairdocs.org/sdr/2022FA0000753.md): Bleed Valve · failed · Dec 6, 2022 · N200CR · Amd FALCON2000 · Compressor Bleed Valve > AFTER REPLACING OUR CURRENT BLEED AIR SYSTEM CROSSBLEED VALVE FOR FAILURE, WE REPLACED WITH AN OVERHAUL EXCHANGE UNIT. WE THEN EXPERIENCED AN INTERMITTENT FAILURE OF THE REPLACEMENT VALVE. REPLACEMENT VALVE 8130 SHOWS PART WAS RESTOCKED AS "NO FAULT FOUND." - [SDR 2022FA0000500](https://openairdocs.org/sdr/2022FA0000500.md): Electrical Box · overheated · Jun 13, 2022 · N200CR · Amd FALCON2000EX · Electrical Power System Wiring > WHILE TAXIING AFTER LANDING AND APU START WAS INITIATED. AFTER APU START THE APU GEN FAILED TO CONNECT. CYCLES OF THE APU GEN SWITCH FAILED TO CONNECT. SUBSEQUENT TROUBLESHOOTING REVEALED EVIDENCE OF "HOT SPOTS" IN THE LH MAIN ELECTRICAL BOX PANEL. SPECIFICALL - [SDR 2021FA0000417](https://openairdocs.org/sdr/2021FA0000417.md): Bleed Valve · failed · Dec 10, 2021 · N200CR · Amd 20F5 · Engine Bleed Air System > THIS IS THE REPLACEMENT RH COLD AIR BLEED VALVE FROM THE FAILURE OF THE SAME VALVE YESTERDAY. THE PREVIOUS REPLACEMENT WAS REMOVED FOR THE SAME DISCREPANCY AND COULD NOT BE REPRODUCED BY THE MANUFACTURER. THIS PART WAS RETURNED TO THE SPARES CIRCULATION AND PL - [SDR 2021FA0000416](https://openairdocs.org/sdr/2021FA0000416.md): Bleed Valve · failed · Dec 9, 2021 · N200CR · Amd 20F5 · Engine Bleed Air System > RH COLD BLEED VALVE FAILURE DURING RIGHT ENGINE START SEQUENCE - [SDR 2021FA0000288](https://openairdocs.org/sdr/2021FA0000288.md): Symbol Generator · failed · Oct 14, 2021 · N200CR · Amd FALCON2000EX · Central Display > THIS REPLACEMENT ADVANCED GRAPHICS MODULE (AGM) #3 FAILED UPON INSTALL AND POWERUP. THIS WAS A "NO FAULT FOUND" BENCH TESTED SPARE FROM HONEYWELL. - [SDR 2021FA0000287](https://openairdocs.org/sdr/2021FA0000287.md): Symbol Generator · failed · Oct 11, 2021 · N200CR · Amd FALCON2000EX · Central Display > ON INITIAL POWER UP ADVANCED GRAPHICS MODULE (AGM) #3 FAILED. - [SDR 2021FA0000159](https://openairdocs.org/sdr/2021FA0000159.md): Control System · inoperative · May 27, 2021 · N200CR · Amd FALCON2000EX · Rudder Control System > DURING OUR INITIAL DESCENT INTO NEW ORLEANS INTERNATIONAL, WE DISCOVERED THE RUDDER TRIM WAS INOPERATIVE WHEN TRYING TO USE IT FOR COORDINATED FLIGHT IN THE DESCENT. THIS SYSTEM IS UNMONITORED IN THE FALCON 2000LX EASY II AIRCRAFT. NO CAS MESSAGE OR CIRCUIT BR - [SDR 2020FA0000555](https://openairdocs.org/sdr/2020FA0000555.md): Gcu · over voltage · Dec 17, 2020 · N200CR · Amd FALCON2000EX · AC Generation System > DURING ENGINE START AND TAXI, THE RIGHT NR 2 GENERATOR, SWITCH BREAKER TRIPPED, INDICATING A SYSTEM OVER-VOLTAGE. ONE RESET ATTEMPT RESULTED IN THE SAME OVER-VOLTAGE. THE AIRCRAFT WAS SHUT DOWN AND REPAIRS WERE MADE. THIS REPAIRED PART FROM FALCON REVEALED - [SDR 2020FA0000554](https://openairdocs.org/sdr/2020FA0000554.md): Gcu · low voltage · Nov 27, 2020 · N200CR · Amd FALCON2000EX · AC Generation System > DURING CRUISE FLIGHT AT FL400, WE EXPERIENCED A NR 2 ENGINE GENERATOR CONTROL UNIT "UNDER-VOLTAGE" INDICATION. THE SYSTEM AUTOMATICALLY COMPLETED A LOAD SHED OF NON-ESSENTIAL ITEMS. WE FOLLOWED THE CHECKLIST, STARTED THE APU, AND CONTINUED OUR TRIP TO THE DE - [SDR 2020FA0000154](https://openairdocs.org/sdr/2020FA0000154.md): Servo Valve · leaking · Feb 12, 2020 · N200CR · Amd FALCON2000EX · Landing Gear Brake System > DURING A MAINTENANCE VISUAL INSPECTION THE BRAKE SERVO VALVE WAS FOUND TO BE LEAKING. - [SDR 2020FA0000153](https://openairdocs.org/sdr/2020FA0000153.md): Servo Valve · leaking · Feb 12, 2020 · N200CR · Amd FALCON2000EX · Landing Gear Brake System > DURING A MAINTENANCE VISUAL INSPECTION THE BRAKE SERVO VALVE WAS FOUND TO BE LEAKING. - [SDR 2020FA0000083](https://openairdocs.org/sdr/2020FA0000083.md): Module · failed · Jan 11, 2020 · N200CR · Amd FALCON2000EX · Global Positioning System > GPS MODULE #1 FAIL UPON COMPLETION OF DIGITAL CHART LOAD INTO THE AIRCRAFT'S INDS. FOLLOWING THE GPS #1 FAIL WE RECEIVED A TERRAIN #1 FAIL AS WELL. - [SDR 2020FA0000055](https://openairdocs.org/sdr/2020FA0000055.md): Igniter Box · inoperative · Dec 30, 2019 · N200CR · Amd FALCON2000EX · Exciter > DURING NR 1 ENGINE START THE IGNITOR/EXCITER BOX FAILED TO SEND IGNITION SIGNAL TO THE ENGINE FOR SUCCESSFUL START. ENGINE NR 1 FADEC AUTOMATICALLY ABORTED START. - [SDR 2019FA0000059](https://openairdocs.org/sdr/2019FA0000059.md): Probe · faulty · Mar 8, 2019 · N200CR · Amd FALCON2000EX · Fuel Quantity Sensor > DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THE AUTOMATIC REFUELING SYSTEM WAS ONLY ALLOWING PARTIAL OPENING OF THE RT WING REFUELING FUEL VALVE, CAUSING IMPROPER FUEL DISTRIBUTION BASED ON QUANTITY COMMANDED BY THE REFUELING PANEL. EXTENSIVE TROUBLESHOOTING - [SDR 2018FA0000483](https://openairdocs.org/sdr/2018FA0000483.md): Starter · making metal · Nov 16, 2018 · N200CR · Amd FALCON2000EX · Engine Starter > DURING A 12 MONTH INSPECTION, THE PNEUMATIC STARTER CHIP DETECTOR/PLUG WAS FOUND TO HAVE THE PRESENCE OF FERROUS METALS. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N200CR' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N200CR/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.