N200CR
Service difficulty reports · 17
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2025FA0000158Anti-Ice Valve · failedWHILE 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 2023FA0000772Valve · failedDURING SINGLE POINT PRESSURE REFUELING, ONE OF THE THREE SYSTEM VENT VALVES FAILED TO OPEN. THIS FAILURE RENDERED THE SINGLE POINT PRESSURE REFUELING INOPERATIVE.SDR 2022FA0000753Bleed Valve · failedAFTER 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 2022FA0000500Electrical Box · overheatedWHILE 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. SPECIFICALLSDR 2021FA0000417Bleed Valve · failedTHIS 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 PLSDR 2021FA0000416Bleed Valve · failedRH COLD BLEED VALVE FAILURE DURING RIGHT ENGINE START SEQUENCESDR 2021FA0000288Symbol Generator · failedTHIS REPLACEMENT ADVANCED GRAPHICS MODULE (AGM) #3 FAILED UPON INSTALL AND POWERUP. THIS WAS A "NO FAULT FOUND" BENCH TESTED SPARE FROM HONEYWELL.SDR 2021FA0000287Symbol Generator · failedON INITIAL POWER UP ADVANCED GRAPHICS MODULE (AGM) #3 FAILED.SDR 2021FA0000159Control System · inoperativeDURING 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 BRSDR 2020FA0000555Gcu · over voltageDURING 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 2020FA0000554Gcu · low voltageDURING 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 DESDR 2020FA0000154Servo Valve · leakingDURING A MAINTENANCE VISUAL INSPECTION THE BRAKE SERVO VALVE WAS FOUND TO BE LEAKING.SDR 2020FA0000153Servo Valve · leakingDURING A MAINTENANCE VISUAL INSPECTION THE BRAKE SERVO VALVE WAS FOUND TO BE LEAKING.SDR 2020FA0000083Module · failedGPS 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 2020FA0000055Igniter Box · inoperativeDURING 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 2019FA0000059Probe · faultyDURING 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 TROUBLESHOOTINGSDR 2018FA0000483Starter · making metalDURING A 12 MONTH INSPECTION, THE PNEUMATIC STARTER CHIP DETECTOR/PLUG WAS FOUND TO HAVE THE PRESENCE OF FERROUS METALS.
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