Dassault FALCON 2000EX
Service difficulty reports · 118
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'FALCON2000EX' 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 aircraft_model_key = 'FALCON2000EX' 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 DXTA2013101005533Handle · inoperativeGEAR HANDLE WOULD NOT MOVE TO RETRACT GEAR AFTER TAKEOFF.SDR 2013FA0000433Duct · crackedDURING CLIMB OUT, CREW RECEIVED A NR 2 PYLON BLEED OVERHEAT CAS MESSAGE. COMPLIED WITH QRH2 PROCEDURE, AND MESSAGE WENT OUT. DURING POST FLIGHT MX INSPECTION, REVEALED THE SENSE LINE ON DUCT BOSS FITTING CRACKED 75 PERCENT AROUND BASE OF FITTING. REPLACED SDR CA130430007Engine · malfunctioned(CAN) ON DESCENT FROM FL470, THE CREW NOTICED A PULSATING VIBRATION WHICH WAS FELT THROUGHOUT THE ACFT. THE AUTO-THROTTLE DISENGAGED AND THE CREW PRESSED THE EVENT BUTTON BEFORE MANUALLY RETARDING THE NR 1 ENGINE TO IDLE. THE ENGINE HAD AN APPARENT FLAMEOUT SDR BKEA2013FA0000162Line · unsecureAPPROX 4 AND A HALF HOURS INTO FLIGHT, WHITE ADVISORY ANNUNCIATION AUTOPILOT FAIL OCCURRED. AUTOPILOT SWITCHED FROM CHANNEL 1 TO 2. MINUTES LATER, SAME ANNUNCIATION OCCURRED AND AUTOPILOT SWITCHED FROM CHANNEL 2 TO 1. ABOUT TEN MINUTES LATER, YELLOW CAUTIOSDR CA130311004Oil System · low pressure(CAN) DURING THE FIRST FLIGHT OF THE DAY, THE ACFT HAD TO DIVERT DUE TO LOW OIL PRESSURE PROBLEMS. SOME MAINTENANCE WAS PERFORMED AND WHEN THE ACFT DEPARTED, THE PILOT RECEIVED ANOTHER LOW OIL PRESSURE, DOWN TO 42 PSI ACCOMPANIED BY A LOUD NOISE, WHICH FORCEDSDR 2013F00064Flt Controls · malfunctionedENROUTE, IN LEVEL FLIGHT AT FL400. SAW A WHITE CAS MESSAGE STATING THAT THE AUTOPILOT HAD FAILED. ENSURED SYS HAD SWITCHED TO THE OTHER AUTOPILOT. WHITE CAS MESSAGE WENT AWAY. OVER THE NEXT SEVERAL MINUTES, WHITE CAS MESSAGE REPEATED ITSELF AND THEN RECESDR CA121211004Analyzer · malfunctioned(CAN) ENROUTE AT 45.000 CLEAR SKIES, CREW EXPERIENCED VERY STRONG VIBRATION, 24 ON THE SCALE, ITT WAS 895-900 OIL PRESSURE 40 PSI ON ENGINE NR 1. WHEN THEY PULLED THE ENGINE BACK TO IDLE IT WAS STILL VIBRATING. THEY SHUTDOWN THE ENGINE AND LANDED. AT THE RASDR CA121126002Ejector · leaking(CAN) WITH A PARKED ACFT, AFTER ENGINE SHUTDOWN, FUEL WAS NOTED LEAKING FROM THE NACELLE. OPENING THE COWLINGS REVEALED A LEAK AT THE FUEL EJECTOR TANK, PRE SB 26285. THE TANK WILL BE REPLACED BEFORE THE ACFT IS RETURNED TO SERVICE.SDR ZESA2012111912Engine · power lossAPPROXIMATELY 2.5 HRS AT 41,000FT, ENTERED INTO TURBULANCE AND WAVE ACTION. NR 2 ENGINE STARTED COMPRESSOR STALLING, THE N1 STARTED DROPPING AND THE ITT STARTED CLIMBING, THE THROTTLE WAS UNRESPONSIVE AND UPON SURPASSING 988C WITH THE N1 AT 46 PERCENT THE PISDR CA120918004Fuel Sys · leaking(CAN) THE CUSTOMER REPORTED A FUEL LEAK FROM THE DRAIN OF THE ECOLOGY VALVE AFTER ENGINE SHUTDOWN. HE ESTIMATED AROUND 10 LITERS OF FUEL DROPPED ON GROUND IN THE 2 MINUTES FOLLOWING ENGINE SHUTDOWN. TROUBLESHOOTING IS ON-GOING.SDR CA120503008Indicator · failed(CAN) HAD OCCASIONAL CAS MESSAGE, XX MID-WING FUEL PROBE FAIL. AS PART OF THE TROUBLESHOOTING WE HAD REMOVED THE PROBE TO CHECK FOR CONTACT DAMAGE, PRESENCE OF MOISTURE AND TO INSPECT THE WIRING TO IT. IT WOULD DISAPPEAR FOR A TIME AND THEN RETURN. FINALLY SSDR CA120503007Switch · failed(CAN) DURING 60 DAY INSPECTION, DISCOVERED HEATING UNIT WITHIN PITCH AFU, FAILED ITS SELF TEST. INTEGRAL THERMAL SWITCH FOUND TO HAVE FAILED OPEN. INSTALLED REPAIRED REPLACEMENT UNIT.SDR CA120411009Engine · vibration(CAN) DURING CRUISE, THE PILOT NOTICED VIBRATION BOTH FELT AND DISPLAYED ON THE COCKPIT DISPLAY. THE THROTTLE WAS RETARDED TO IDLE, LOWERING THE VIBRATION. AT THE SAME TIME AN OIL FILTER CAUTION MESSAGE WAS REPORTED ALONG WITH A CHIP LIGHT. THE PILOT ELECTEDSDR BKEA2012F00068Engine · multiple failAT ABOUT 10,000 FEET IN LAST STAGE OF CLIMB, NR 1 ENGINE OIL PRESSURE CASS MESSAGE ILLUMINATED, PULLED POWER BACK FOLLOWED BY A NR 1 ENGINE VIBRATION CASS MESSAGE. A COUPLE OF MINUTES LATER NR 1 ENGINE OIL FILTER CASS MESSAGE. PROCEDED TO PULL POWER BACK ANDSDR CA111129010Pressure Switch · leaking(CAN) CAS MSG, HYD QTY 2 LOW, HYD QTY WAS AT 56% THEN 44% ON LANDING. FOUND PARK BRAKE ACCUMULATOR SWITCH LEAKING, SWITCH REPLACED IAW AMM CHAP 32-42-05-900-802. FUNCTIONAL TEST OF PARK BRAKE ACCU CO. PN ON 1203P0224, SN ON 108, PN OFF G1052-1 & SN OFF 468.SDR CA110914012Pump · leaking(CAN) WHILE CARRYING OUT A FAN BALANCE/VIBE SURVEY ON NR 1 ENGINE, IT WAS NOTED THAT THE HYD PUMP WAS "WEEPING" SOME HYD FLUID AT CASE SPLIT LINE AND AROUND PAD AREA. ALSO, WHILE OPERATING, YOU COULD NOT STAND TO WRAP YOUR HAND AROUND THE PX LINE DUE TO A VERSDR CA110427003Engine · power loss(CAN) IFSD DURING REVENUE FLIGHT AFTER POWER REDUCTION ON CLIMB, CREW REPORTED ENGINE NOISE FOLLOWED BY A BANG AND N1 ROLLBACK TO 70 PERCENT. THE PILOT SHUTDOWN THE ENGINE AND DECLARED AN EMERGENCY. A SUCCESSFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. TROUBLSDR CA110321018Extinguisher · empty(CAN) DURING BASIC INSPECTION FOUND NR 1 FIRE EXTINGUISHER AT ZERO.
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