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 W6JA20161020011Proximity Switch · faultyAFTER TAKEOFF, RT MLG INDICATION READ DOWN GREEN POSITION WITH HANDLE AND GEAR IN THE UP POSITION. THE RT MLG INDICATION PROXIMITY SWITCH WAS FOUND TO BE FAULTY. FAULTY PROXIMITY SWITCH WAS REPLACED WITH A NEW UNIT, P/N OFF: D23336000-1, S/N OFF: 03138, P/N SDR W6JA20160719008Circuit Breaker · trippedON APPROACH, THE FLAP CONTROL CIRCUIT BREAKER TRIPPED. FLAPS REMAINED IN THE RETRACTED POSITION WITH THE SLATS DEPLOYED. ON LANDING, MAINTENANCE VISUALLY INSPECTED FLAPS, RESET THE FLAP CONTROL CIRCUIT BREAKER, PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM TO FULSDR DXTA2016042106227Contactor · unserviceableAFTER STARTING THE ENGS WE GOT AN APU FAULT CAS MSG. SHUTDOWN THE APU THEN THE ESS BUS TURNED AMBER ON THE ELEC SYNOPTIC. SHUTDOWN ENGS & POWERED DOWN ACFT. FOUND ESS BUS 7 1/2 CB POPPED ON THE J BOX ABOVE THE NR 1 BATTERY. ALSO NOTED ELEC SMELL IN FWD SERSDR CA160222004Check Valve · failed(CAN) UPON ACFT SHUTDOWN, CAS MESSAGE, BRAKE ACCUMULATOR, DISPLAYED. BRAKE ACCUMULATOR PRESSURE WOULD NOT HOLD RENDERING PARK BRAKE INEFFECTIVE. ACFT HAD AN IDENTICAL PROBLEM 18 MONTHS EARLIER THAT WAS THE RESULT OF A FAILED HYD CHECK VALVE, PN L95H07-202 UPSDR DXTA2016011106164Apu · contaminatedSHORTLY AFTER STARTING THE APU, ACFT CABIN FILLS WITH NOXIOUS FUMES OF AN OILY NATURE. REMOVED CONTAMINATED APU & INSTALLED A REPAIRED APU. OPS & LEAK CHECKED GOOD. WORK DONE IAW MM 49-10-01-900-802, 53-71-01-900-801, 24-33-01-900-801 & AND MM 49-24-14.SDR DXTA2016011106163Apu · smokeWHEN STARTING APU AFTER LANDING, LINE SERVICE OBSERVED WHITE SMOKE, A FLAME COMING OUT OF THE EXHAUST & FUEL LEAKING FROM APU. THE CABIN ALSO HAD AN EXTREMELY STRONG ODOR OF JET FUEL. R & R APU FUEL FLOW DIVIDERIAW MM 49-30-58. LEAK & OPERATIONS CHECKED GOSDR CA160105005Roller · loose(CAN) RIGHT INBD GEAR DOOR UPLOCK ROLLER SUPPORT FOUND LOOSE ON MOUNT SERRATIONS. NUTS HAD BACKED OFF. NUTS TIGHTENED AND DOOR OPERATED THRU SEVERAL CLOSING CYCLES AND CHECKED SERVICEABLE. FOUND LT SIDE STARTING TO LOOSEN OFF AS WELL. NUTS TO BE REPLACED ONSDR DXTA2015122906144Apu · odorUPON ARRIVING AT THE AIRPORT, NOTICED A MUSTY & OILY ODOR IN THE CABIN & COCKPIT. THIS SMELL PERSISTED & BECAME STRONGER WITH APU USAGE & WHILE INFLIGHT. UPON LANDING WE BOTH FELT A BURNING SENSATION IN BOTH OUR EYES. THE OILY ODOR IS MUCH STRONGER IN THE CSDR CA151228003Fadec · unknown(CAN) THE CUSTOMER REPORTED AN ENGINE #2 IFSD ON TRANSITION TO THE TAXIWAY WITH A NOISE OBSERVED (ITT 500) AND A NO DISPATCH MESSAGE. CREW OBSERVED FADEC FAULT CODES: 2A-AF-IGV AND 2B-AH-IGV (ACTUATOR). TROUBLESHOOTING ONGOING.SDR CA151201005Engine · fluctuates(CAN) THE FLIGHT DEPARTED WITHOUT ISSUES NOTED. THE ACFT REFUELED AND DEPARTED FOR FINAL INTENDED DESTINATION. AFTER 1 HR INTO THE FLIGHT AT 40 KFT THE ACFT RAN INTO HEAVY TURBULENCE WITH ALTITUDE FLUCTUATIONS OF 400 FT TOTAL AND SPEED FLUCTUATIONS OF 40 KNOSDR CA151127002Engine · malfunctioned(CAN) CREW EXPERIENCED MODERATE TO SEVERE TURBULENCE. THEY WERE UNABLE TO MAINTAIN ALTITUDE AND TRACK. THEY REQUESTED LOWER AND STARTED TO DESCEND, THIS WAS NOT POSSIBLE DUE TO AN INCREASE IN VERTICAL SHEAR. AT THIS POINT, THE BELIEVED THEY HAD A COMPRESSOR STSDR CA151130021Unknown · odor(CAN) REPORTS OF OIL ODOR IN CABIN AT TAKEOFF AND LANDING. IT IS UNKNOWN AT THIS TIME FROM WHICH ENGINE THE ODOR IS COMING FROM, TROUBLESHOOTING IS ON-GOING.SDR CA151130009Engine · vibration(CAN) IN LEVEL FLIGHT, AT FL400 THE LT ENGINE BEGAN VIBRATING BADLY. POWER WAS REDUCED, BUT THE VIBRATION CONTINUED AND THE ITT BECAME VERY HOT. THE ENGINE WAS THEN SHUTDOWN MANUALLY. 2 PILOTS, 1 PASSENGER. THE CREW LANDED AT INTENDED DESTINATION. TROUBLESSDR DXTA2015111306125Valve · failedIN LEVEL FLIGHT AT FL400 THE LT ENG BEGAN VIBRATING BADLY. POWER WAS REDUCED, BUT THE VIBRATION CONTINUED & THE ITT BECAME VERY HOT. THE ENG WAS THEN SHUTDOWN MANUALLY. R & R PRESS REGULATING & SHUTOFF VALVE IAW G450 CMP 361106 & G450 CMP 361215. OPERATIONSDR CA151117015Compressor · stalled(CAN) WHILE IN CRUISE AT FL410, THE NR 2 ENGINE EXPERIENCED COMPRESSOR STALLING FOR A DURATION OF APPROXIMATELY 4 MIN. THE ENGINE WAS SHUTDOWN AND THE FLIGHT DIVERTED. AN UNEVENTFUL LANDING WAS PERFORMED. TROUBLESHOOTING IS ON-GOING.SDR CA151117007Compressor · damaged(CAN) IN FLIGHT AT FL45, THE CREW HEARD TWO COMPRESSOR STALLS FOLLOWED BY POWER ROLLBACK AND FLAMEOUT. NO OTHER DETAILS ON THE CIRCUMSTANCES ARE AVAILABLE. INSPECTION FOUND PLASMA COATING DAMAGE INSIDE THE COMPRESSOR. ENGINE TO BE REMOVED.SDR CA151102004Vane · worn(CAN) NR 2 ENGINE SURGE AT FL 450 ACFT WAS BROUGHT TO A LOWER ALTITUDE AT FL 360, NO ISSUE. WENT UP TO FL 400, NO ISSUE. CONTINUES TO FL 450 AND ENGINE STARTED TO SURGE. ACFT DIVERTED THE 4TH STAGE COMPRESSOR METCO COATING IS WORNED OUT. IT IS A KNOW ISSUSDR CA150929014Pressure Switch · faulty(CAN) DURING FLIGHT, 1 ENGINE ANTI ICE OVERPRESSURE CAS MESSAGE CAME ON. DUE TO BAD WEATHER AT DESTINATION, PILOT DECIDE TO DIVERTED AND LAND. ACFT GROUNDED. NR 1 ENGINE ANTI ICE OVER PRESSURE SWITCH FOUND AT FAULT. PN: 01ND36204-7.SDR CA150727006Warning Message · illuminated(CAN) ACFT WAS DESCENDING WHEN FROM THE NR 2 ENGINE, A NO DISPATCH CAS MESSAGE POPPED OUT FOLLOWED BY 3 LOUD NOISE. ALL THE ENGINE PARAMETERS WERE NORMAL AND THE PILOT DECIDED TO REDUCE THE ENGINE POWER AND DIVERT THE ACFT TO ANOTHER AIRPORT. THE PILOT LANDESDR CA150713007Vane · damaged(CAN) CUSTOMER REPORTS ENG SURGE AT FL 430. ACFT DESCENDED TO FL 330 & CONTINUED TO DESTINATION. UNEVENTFUL LANDING WAS COMPLETED. NO INJURIES REPORTED, DURING TROUBLESHOOTING, HPC BORESCOPE REVEALED COATING DAMAGES AT THE 4TH STAGE VANE COATING. THE ENG WSDR 9JLA2015061114804Uplock Actuator · defectiveTHERE HAVE BEEN SEVERAL REPORTS FROM THE FLIGHT CREW ABOUT A FALSE INTERMITTENT WARNING WITH THE GEAR HANDLE FLASHING RED NORMALLY 45 MIN INTO FLIGHT. THE GEAR HANDLE LIGHT ALWAYS CLEARED DURING THE APPROACH TO LANDING. EACH REPORT WAS MET WITH TROUBLESHOOTINSDR CA150604006Unknown · odor(CAN) ACFT WAS ON DESCENT WHEN THE CREW HAD OIL ODOR AND SMOKE IN CABIN. AFTER AN UNEVENTFUL LANDING, GROUND CREW REPORTED A LOW OIL LEVEL. AS THE ACFT FLEW BACK TO ITS BASE, OIL ODOR AND SMOKE IN CABIN APPEARED AGAIN DURING THE DESCENT. TROUBLESHOOTING ONGOSDR CA150325014Engine · shutdown(CAN) THE CREW REPORTED AN IN-FLIGHT SHUTDOWN. THEY WERE FLYING AT FL450 WHEN THEY ENCOUNTERED SEVERE TURBULENCE JUST BEFORE THE IFSD. THEY DESCENDED TO FL 410 AND RESTARTED THE AFFECTED ENGINE BUT THEY NOTICED THAT THE ITT WENT TO YELLOW, APPROXIMATELY 800 SDR DXTA2015021705980Terminal · burnedAFTER ENGINE START, TURNED ON THE WINDSHIELD HEAT. WITHIN 1 TO 2 MINUTES SMOKE & FIRE CAME OUT OF THE CENTER GLARE SHIELD. SHUT EVERYTHING DOWN & THE SMOKE & FIRE STOPPED. FOUND ELECTRICAL COMPONENTS, TERMINAL & CONTACTOR DAMAGED. R & R TERMINAL & CONTACTOSDR CA150224003Engine · malfunctioned(CAN) ENGINE SUFFERED AN IFSD AT 41,000 FT AND THE CREW PERFORMED A MANUAL RELIGHT. PILOT REPORTED COMPRESSOR SURGE EVENT WHEN TRYING TO GET FROM 41000 FT TO 43000 FT DUE TO WEATHER CONDITIONS. DESCENDED TO 37000 FT AND ENGINE RECOVERED AFTER REDUCING POWER SSDR DXTA2014122205951Pitot Line · obstructedAT FL 390, THE AUTOPILOT & AUTO THROTTLES DISENGAGED. THE PILOT'S SIDE AIRSPEED WENT UP 30 KTS ABOVE MMO & ALTITUDE WENT UP 200 FT. ON THE ECL ACTIVE ABNORMAL RECEIVED SIX MESSAGES, AUTO SLATS, ALT MISCOMPAIR, IAS MISCOMPAIR, AIL FEEL, ADS1 FAIL, MACH TRIM FSDR DXTA2014121505947Engine · failedAFTER TAKEOFF, THE NR 2 ENGINE OIL PRESSURE WENT TO ZERO MOMENTARILY. THEN BEGAN FLUCTUATING BETWEEN 40 - 60 PSI. AS THE POWER WAS REDUCED FOR LEVEL FLIGHT THE OIL PRESSURE STABILIZED. AS POWER WAS ADDED, OIL PRESSURE WOULD NOT INCREASE NORMALLY. ON RETUSDR CA141204008Engine · overtemp(CAN) DURING FLIGHT AT 33,000 FT THE PILOT REPORTED THAT THE LT ENGINE ITT WENT IN THE YELLOW BAND. ITT REPORTED TO HAVE GONE TO 850 DEG. THE PILOT RETARDED THE THROTTLE TO LOWER ITT AND ELECTED TO DIVERT FOR A SAFE LANDING. TROUBLESHOOTING.SDR CA141202023Unknown · odor(CAN) CUSTOMER CALLED TO REPORT OIL ODOR IN CABIN. CREW IS NOT SURE WHAT ENGINE MAY BE CAUSING THE ODOR BUT IT IS BELIEVED THAT THE LT CF0239 IS MOST LIKELY INVOLVED.SDR CA141202006Engine · flamed out(CAN) IN CRUISE AFTER A 25 MINUTES OF FLIGHT, THE PILOT NOTICED ONE ENGINE FLAMED OUT AND RELIGHTED AFTER A SHORT DELAY. THE AIRCRAFT WAS REDIRECTED BACK TO DEPARTURE AIRPORT WHERE IT LANDED SAFELY. TECHNICIANS ARE RETRIEVING ENGINE DOWNLOAD AT THIS TIME.SDR CA141025006Oil System · low pressure(CAN) DURING APPROACH THE CREW EXPERIENCED FLUCTUATING OIL PRESSURE AND A LOW OIL PRESSURE CAS MASTER CAUTION IN THE COCKPIT. THE CREW FOLLOWED THE CHECKLIST AND PULLED THE ENGINE BACK TO IDLE. PRESSURE THEN, WAS AT 30 PSI. JUST BEFORE LANDING, CREW EXPERIENCESDR EBVR20140930002Stop Fitting · misinstalledRT NR 7 SLAT TRACK STOP FOUND TO BE INSUFFICIENTLY TORQUED AND TO HAVE INCORRECT LOCK WASHER INSTALLED.SDR EBVR20140930001Stop Fitting · misinstalledRT NR 7 SLAT TRACK STOP FOUND TO BE INSUFFICIENTLY TORQUED AND TO HAVE INCORRECT LOCK WASHER INSTALLED.SDR CA141008006Unknown · odor(CAN) THE OPERATOR REQUEST ASSISTANCE TROUBLESHOOTING MINOR OIL ODOR IN CABIN DURING DESCENT. THE CREW HAD NOTED ODOR ON PREVIOUS TRIPS TOO. TROUBLESHOOTING IS ONGOING.SDR EBVR201409050001Stop · damagedHARDWARE FOR THE NR 7 SLAT STOP WAS LOOSE EVEN THOUGH THE SAFETY TAB WAS IN PLACE AND UNBROKEN. THIS LOCATION HAS BEEN PART OF A DISCUSSION OF AN ISSUE THAT HAS BEEN FOUND ON FACTORY INSTALLED WINGLET INSTALLATION BUT THIS ACFT HAS THE STC WINGLET MODIFICATIOSDR CA140812008Duct · cracked(CAN) UPON ARRIVAL, CREW GOT BAGGAGE COMPARTEMENT OVERHEAT. THEY PHYSICALLY CHECKED AND IT WAS IN FACT OVERHEATED, AFTER INVESTIGATION FOUND APU BLEED AIR DUCT BLOWN.SDR CA140721011Engine · surges(CAN) REVIEW OF THE GBS FILES INDICATES THAT THE ENGINE ENCOUNTERED A DROP IN P3, BY APPROXIMATELY 15 PSI, POSSIBLY DUE TO AN ENGINE SURGE. THE CAUSE OF SURGE IS NOT APPARENT AND INVESTIGATION IS CONTINUING.SDR CA140630008Engine · warning message(CAN) SHORTLY AFTER DEPARTURE, THE CREW GOT AN OIL FILTER CAUTION MESSAGE FOLLOWED BY A DROP IN OIL PRESSURE OF 20 PSI. POWER WAS REDUCED TO IDLE AND FLIGHT RETURNED TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL LANDING WAS MADE WITH ENGINES RUNNING. DURING THSDR CA140530005Wire · shorted(CAN) FLIGHT RECORDER CIRCUIT BREAKER, 551FZ, TRIPPED, ONE SECOND LATER STDBY FLIGHT RECORDER CIRCUIT BREAKER, 561FZ, TRIPPED. RESET ATTEMPTED, DUE INFLIGHT. MAINTENANCE TROUBLESHOOTING DISCOVERED A WIRE, ID 36/22, ACTIVE +28VDC WHICH WAS A CAP AND STOWED WSDR CA140313002Linkage · brokenFOUND A BROKEN CONTROL LINKAGE ROD ON THE OVERSPEED SYSTEM DURING ROUTINE INSPECTION. THE HARDWARE WILL BE SENT TO SERVICE INVESTIGATION GROUP FOR FURTHER ANALYSIS. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND PROVIDE INFORMATION THROUGH SUBSEQUENT SERVISDR CA140224013Engine · vibration(CAN) DURING TAKEOFF, CREW REPORTED VIBRATION ON NR 2 ENGINE. THEY REDUCED THE POWER ON THIS ENGINE AND REQUESTED FOR DESCENT AND DIVERSION. ONCE POWER WAS REDUCED, THE VIBRATION STOPPED. INVESTIGATION IS ON-GOING.SDR CA140224006Engine · malfunctioned(CAN) DURING REVENUE FLIGHT, THE ACFT WAS AT FL 430 WENT THE AUTO THROTTLES RETARDED. THEN NR 2 ENGINE HAD IGNITION AND THE ITT ROSE TO 860 DEGREES C. THE CREW ELECTED TO SHUTDOWN NR 2 ENGINE AND THE ACFT LANDED SAFELY.SDR CA140203013Carbon Seal · leaking(CAN) THE CUSTOMER REPORTED AN EXCESSIVE OIL PRESSURE ON LT ENGINE DURING CLIMBOUT. THE CREW REDUCED POWER IN ORDER TO REDUCE OIL PRESSURE AND RETURNED. THE CREW PERFORMED UNEVENTFUL LANDING WITH BOTH ENGINES. THE CREW REPORTED OIL SMOKE FROM EXHAUST DURING SDR CA140203012Engine · flamed out(CAN) DURING CRUISE THE ENGINE SUFFERED 2 SUCCESSIVE FLAMEOUTS. PILOT REPORTED THAT THE NR 1 ENGINE HAD NO DISPATCH AFTER TAKEOFF AND ADDITIONALLY ENGINE NR 2 HAD LONG DISPATCH ON GROUND AFTER. NO MESSAGE ON STATUS/FAULT CODE PAGE IN FLIGHT. AT LEVEL 430 THSDR E4FR20140220001Bushing · missingDURING INSTALLATION OF RT ENGINE, BUSHING F2MB721550001 WAS NOT INSTALLED. INSTALLATION OF BUSHING IS NOT SPECIFIED IN THE AMM, TASK: 71-00-01-900-801 ENGINE INSTALLATION, BUT IS LISTED IN THE ILLUSTRATED PARTS CATALOG. FURTHER RESEARCH SHOWED THAT THIS PARTSDR 2014FA0000024Bleed Valve · defectiveDURING CLIMB, CREW RECEIVED A "BLEED OVERHEAT" ANNUNCIATOR. AFTER RUNNING ABNORMAL CHECKLIST, ANNUNCIATION RETURNED. ELECTED TO DIVERT. DAS PBI VERIFIED DISCREPANCY "HPV 2 FAILURE" MESSAGE WAS ACTIVATED ON THE EIED. STARTED NR 2 ENGINE, CYCLED THE HPV2 SWISDR DXTA2013112505580Microwave Oven · faultyFLIGHT ATTENDANT WENT TO USE THE MICROWAVE IN GALLEY & UPON STARTING THE MICROWAVE, WHITE ELEC SMOKE BEGAN SPEWING FROM BEHIND OR IN THE MICROWAVE. DESELECTED THE GALLEY MASTER SWITCH IN THE COCKPIT & THE SMOKE STOPPED. R & R THE GALLEY MICROWAVE ASSEMBLY WISDR CA131126011Apu · making metal(CAN) AIRCRAFT WAS ON THE RAMP WITH APU RUNNING, CREW NOTICE AN UNUSUAL ODOR IN CABIN, CREW VERIFIED APU EGT AN NOTICED EGT RISSING AT A FAST RATE, PILOT SHUTDOWN THE APU. MECHANIC WHEN ON SITE AND FOUND OIL FILTER FULL OF METAL.SDR CA131201001Seal · leaking(CAN) DURING FLIGHT, A LOW OIL PRESSURE WARNING OCCURRED. THE PILOT REDUCED POWER TO IDLE AND DIVERTED THE FLIGHT WHERE AN UNEVENTFUL LANDING WAS MADE. TROUBLESHOOTING FOUND AN OIL LEAK AT THE FORWARD HYDRAULIC PUMP DRIVE PAD FROM A FAULTY OIL SEAL. THE CONFIGSDR 2013FA0000602Power Cable · burnedRT GENERATOR WOULD NOT COME ONLINE. FOUND POSITIVE GENERATOR CABLE INSIDE RT PYLON TO BE BADLY BURNED AND SEPARATED FROM FEED THROUGH CONNECTOR. GEN CABLE INSIDE PYLON OVERHEATED TO THE POINT OF SEPARATION FROM THE FEED THROUGH CONNECTOR. CABLE CONNECTOR A
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