Dassault FALCON 2000
Service difficulty reports · 527
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 = 'FALCON2000' 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 = 'FALCON2000' 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 2012FA0000283Pressure Switch · leakingACFT LOST HYD FLUID FROM THE NR 2 SYS, ROOT CAUSE DISCOVERED TO BE A PARKING BRAKE ACCUMULATOR PRESSURE SWITCH (150GC) PN: 7G1052-1 SN:303, WHICH INTERNALLY FAILED AND LEAKED FLUID FROM A PRESSURE RELIEF VENT HOLE. A NEW SWITCH PN: 1203P0224 WAS INSTALLED ANDSDR DXTA2012032004926Hmu · failedCRUISING AT FL390 "FADEC 2" LIGHT ILLUMINATED ON MWP FOLLOWED IMMEDIATELY BY A ROLL BACK TO FLIGHT IDLE OF NR 2 ENGINE. CREW COMPLETED CHECKLIST ITEMS. EIED 2 DISPLAYED A "F2A WF SOFT FAULT". ENGINE 2 REMAINED AT FLIGHT IDLE FOR ABOUT 20 MINS. DURING DESCENT SDR DXTA2012031904925Pressure Switch · inoperativeAMBER BRAKE PRESSURE ANNUNCIATOR ILLUMINATED DURING TAKEOFF ROLL, FOLLOWED BY A RED TAKE OFF CONFIGURATION ANNUNCIATOR. ABORTED TAKEOFF AT 60 KTS. TROUBLESHOT AND FOUND RT BRAKE PRESSURE SWITCH R145GC SHORTED. R & R PRESSURE SWITCH. OPS AND LEAK CHECKED GSDR DXTA2012031204916Unknown · unknownON LANDING AND APPLYING NORMAL BRAKES, ACFT PULLED SHARPLY TO THE RT. NEEDED LT STEERING TO TRACK CENTER OF RUNWAY. PERFORMED A GENERAL VISUAL INSPECTION OF ALL FOUR BRAKES WITH NO FINDINGS. NO MESSAGES NOTED ON EIED. NO MINELLO'S FLAGGED. BLED ALL FOUR BRASDR DXTR20120207001Retaining Clip · missingPASSENGER SEAT BELT ) FOUND WITH RETAINING CLIP MISSING. R & R SEAT BELT.SDR CA120213012Engine · surges(CAN) DURING MAINTENANCE FLIGHT, ON TAKEOFF THE CREW FELT 1 ENGINE SURGING. PILOT RETARDED POWER LEVER TO IDLE. ACFT RETURNED TO BASE FOLLOWED BY UNEVENTFUL LANDING. TROUBLESHOOTING ONGOING.SDR DXTA2012020304862Autothrottle Sys · malfunctionedNR 2 ENGINE THROTTLE INOPERATIVE. DURING CLIMB FROM 13000 TO 15000 FT, ENGINE AND WING ANTI ICE ON, TAT 0, AUTO THROTTLE ON, MANUAL SPEED, ACCELERATING FROM 300 TO 350 KIAS. AUTO THROTTLE DISENGAGED, APR ON, NR 2 ENGINE SURGING. RETARDED NR 2 ENGINE TO TOP OSDR DXTA2011121204821Engine · malfunctionedIN CRUISE AT FL340, EXPERIENCED A LOUD VIBBRATION FROM THE NR 1 ENGINE AND A POWER ROLL BACK. FADEC ATTEMPTED ONE RE-LIGHT AND HEARD AN INCREASING, LOUDER VIBRATION AND PROCEEDED WITH A PRECAUTIONARY ENGINE SHUTDOWN WITH NO EXCEEDED ENGINE PARAMETERS NOTE. NSDR DXTA2011113004805Fadec · malfunctionedCRUISE ALTITUDE 43000', NR 2 ENGINE BEGAN TO SLOWLY LOSE POWER. POWER DECLINED TO APPROX 50 PERCENT. PRECAUTIONARY LANDING. AT LOWER ALTITUDES THROTTLE HAD LITTLE EFFECT CONTROLLING ENGINE. ENGINE WOULD NOT ACCELERATE ABOVE FLT IDLE REGARDLESS OF THROTTLE SDR DXTA2011112904804Probe · inoperativeAFTER LANDING & APU START, AMBER ECU OVERHEAT MWP LIGHT ILLUMINATED. NOT GETTING ANY AIR FROM APU AT TIME. NOTICED THE ECU OVERHEAT LIGHT, CREW NOTICED A BURNING ODOR IN COCKPIT & GALLEY AREA. AFTER SECURING ACFT & OPENING FORWARD SERVICE COMPARTMENT DOOR,SDR DXTA2011112804801Engine · surgesRT ENGINE WAS SURGING AFTER TAKEOFF. SURGING SHOWED ON ITT, N1, AND FUEL FLOW. SURGING WAS FIRST NOTICED AFTER POWER REDUCTION TO MAX CLIMB DETENT. CHECKED FOR FAULTS ON EIED NO FAULTS NOTED. ACCOMPLISHED ENGINE RUNS IAW MM 72-00-00. ACCOMPLISHED MULTIPLE ESDR DXTA2011111404786Proximity Sensor · defectiveON TAKEOFF, "AUTO SLATS" LIGHT ILLUMINATED. ATTEMPTED TO RETRACT GEAR BUT HANDLE LOCKED. MAINTAINED 3 GREEN LIGHTS. LANDED UNEVENTFULLY. AFTER LANDING, NOTED LT STEERING AND BRAKE WARNING. TECHS HAVE RETRIEVED FAULTS CODES IN THE BSCU FOR TROUBLESHOOTING.SDR DXTA2011102804768Apu · odorON DESCENT AT ABOUT 25,000 FEET A STRONG ACRID SMELL WAS NOTICED PRIMARILY IN THE COCKPIT AND NOT THE CABIN. NO SMOKE WAS VISUALLY DETECTED. RAN APU AND ODOR WAS DETECTED. FOUND APU WAS JUST CHANGED 10-24-11 FOR OIL IN ECS SYS, SUSPECT DECONTAMINATION CHECKSDR DXTA2011101704752Uplock · inoperativeON TAKEOFF, DURING GEAR RETRACTION GEAR HANDLE LIGHT REMAINED FLASHING AND ALL 3 RED DOOR LIGHTS WERE ILLUMINATED. ABNORMAL CHECKLIST WAS FOLLOWED, LANDING GEAR EXTENDED AND 3 GREEN LOCKED LIGHTS ILLUMINATED. LANDING WAS UNEVENTFUL. POSTFLIGHT WAS NORMAL. SDR FV7R20111101001Electronic Unit · failedUNIT SMOKING AND EMITTING "BURNING" SMELL. THIS UNIT WAS REMOVED FROM NR M910CS. THE CAUSE OF FAILURE IS ASSIGNABLE TO AN INTERNAL COMPONENT FAILURE Q14 LOCATED ON THE CPU ASSY. ENGINEERING HAS BEGUN A FAILURE ANALYSIS TO IDENTIFY THE ROOT CAUSE. SIMILAR COMSDR DXTA2011091204720Fan · failedAFTER DEPARTURE AND CLIMBING OUT, HEARD SOMETHING THAT SOUNDED LIKE A CIRCUIT BREAKER POP. ABOUT 1 MINUTE LATER, SMELLED AN ELECTRICAL BURNING ODOR. FOUND IRU NR 1 COOLING FAN AND IRU NR 2 COOLING FAN INOP AND BURNED. REPLACED IRU NR 1 COOLING FAN AND IRU SDR DXTA20110804705Duct · leakingBATTERY TEMP INDICATED 120 DEGREES WITH AMBER LIGHT. POWERED UP ACFT PERFORMED DIGITAL BATTERY TEMP MONITOR TEST, WITH NO DEFECTS NOTED. BELT HAD BEEN REPLACED FOR SIMILAR ISSUE NOT LONG AGO. FOUND LT ENG BLEED "Y" DUCT JUST ABOVE FWD SVCC BAY ENTRY DOOR TO SDR DXTA2011080904701Connector · dirtyRED UNLOCK LIGHT DID NOT EXTINGUISH AFTER TAKEOFF. NORMAL HYD PRESSURES. PERFORMED CHECKLIST & GEAR EXTENDED NORMAL. PERFORMED MLG SWINGS. VERIFIED DISCREPANCY, MLG MOVED TO UPLOCK POSITION, BUT BOTH MLG DOORS DID NOT, NLG & DOORS MOVED TO UP POSITION BUT SDR DXTA2011080504687Bearing · wornVIBRATION AND GRINDING IN THE NOSEGEAR/COCKPIT FLOOR AREA. STARTED AROUND 200 KIAS AND INCREASED WITH SPEED. UPON SLOWING AND LOWERING THE NOSE, VIBRATION CEASED BELOW 200 KIAS. TROUBLESHOT AND FOUND THE UPPER NOSE GEAR FOLLOW UP DOOR WITH EXCESSIVE PLAY LASDR DXTA2011080404683Skin · looseEXPERIENCED A LOW FREQUENCY CONTINUOUS & SOMETIMES PULSATING VIBRATION DURING CLIMB & DECENT. OCCURRED AT ABOUT FL 200 UNTIL CRUISE. STARTING ABOUT 280KT IAS & CONTINUING UNTIL ABOUT .82M. IN CRUISE, SEEMED TO DIMISH ABOVE .82M & REOCCURED ABOUT .78M SLOWING.SDR DXTA2011072604672Motor · failedDURING ARRIVAL, DETECTED AN ELECRICAL ODOR OF SMOKE IN COCKPIT. POSSIBLY DUE TO CO-PILOT'S WINDSHIELD WIPER STICKING IN UP POSITION. REPLACED WINDSHIELD WIPER MOTOER IAW MM 24-000, 30-402, 30-407 34-003.SDR DXTA2011072204665Apu · odorSTRONG BURNED OIL ODOR IN COCKPIT AND SOMETIMES THE CABIN WHEN ON THE GROUND APU RUNNING. INSTALLED REPAIRED APU IAW MM 49-000. TESTED AND CHECKED GOOD.SDR DXTA2011070904648Brake · malfunctionedAMBER BRAKE LIGHT ILLUMINATED ON MWP DURING GEAR EXTENSION AND NEVER WENT OUT. IT WAS ACCOMPANIED BY A RT BRAKE RED THAT FAILS TO RESET. REMOVED CONNECTORS CLEANED AND INSPECTED. NO DEFECTS NOTED. PERFORMED OPS TEST OF BSGU 2, OPS CHECK GOOD IAW MM 32-466.SDR UVVR2011062900016Shroud · corrodedNOSE SECTION AVIONICS COOLING FAN PROTECTOR CORRODED ON THE AFT SIDE OF FRAME 0.SDR UVVR2010060900015Structure · corrodedEXTERNAL WING SUPPORT STRUCTURE CASTING CORRODED ON NUMEROUS AREAS,LOCATED AT LT SPAR ADJACENT TO THE LT MLG ACTUATOR CYLINDER, FOUND DURING C INSPECTION.SDR DXTA2011063004639Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. 3 RED LIGHTS DISPLAYED ON GEAR PANEL. GEAR EXTENDED NORMALLY.SDR DXTA2011062704636Indication Sys · malfunctionedAFTER WEIGHT CAME OFF OF WHEELS, STALL WARNING STARTED AND COULD NOT BE SILENCED. ALL 3 RED MOVING LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. UPON GEAR EXTENSION, ALL 3 RED MOVING LIGHTS EXTINGUISHED. AMBER GRND PROX WAS DISPLAYING IN THE ATTITUDE INSDR DXTA2011062204631Control Panel · malfunctionedALL THREE RED MOVING LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. UPON GEAR EXTENSION, ALL THREE RED MOVING LIGHTS THEN EXTINGUISHED. REPLACED CONFIGURATION PANEL (30C2) WITH A REPAIRED PANEL IAW MM 34-003. LANDING GEAR EXTENSION LOCATIONED TESTED GOOSDR DXTA2011062004625Brake Pads · wornLOSS OF BRAKE AUTHORITY. ON LANDING, THE BRAKING AUTHORITY DIMINISHED TO THE POINT OF USING FULL BRAKE. INVESTIGATED AND FOUND NR 2 AND 3 BRAKES WERE WORN BEYOND LIMITS. REMOVED NR 2 BRAKE AND INSTALLED O/H BRAKE ASSY. REMOVED NR 3 BRAKE ASSY AND INSTALLEDSDR DXTA2011061704620Pump · leakingENROUTE, LOST NR 1 HYD FLUID QTY. NEAR ZERO LEVEL ON LANDING. ON POST FLIGHT INSPECTION, HYD FLUID WAS VISABLE DRIPPING FROM THE NR 2 NACELLE. VERIFIED LEAKS AT REGULATOR ON HYD PUMP. R & R NR 2 FWD HYD PUMP IAW MM 29-104, REV DATE 05/2009. RAN ENGINE NO SDR CA110611002Bypass Switch · malfunctionedCLASS 3 MESSAGE ON EIED F1B TWF LOCAL FAULT AND F1B TWF SOFT FAULT. CARRIED OUT MX CHECK ON ACFT SYS AND FOUND NR 1 ENGINE HYDRO MECHANICAL UNIT (HMU) CHANNEL B FAILED. IN CONTACT WITH MFG RECOMMENDATIONS REPLACED THE NR1 ENGINE HMU PN 5085T40G04, SN OFF BECHSDR DXTA2011052704595Shaft · wornCRUISING ALONG AT FL400 THE LT ENGINE FLAMED OUT WITH NO INDICATIONS WHAT SO EVER. HAD AN X ON THE N2 VIBRATION. ELECTED NOT TO RESTART AND DIVERTED. NO CHIP, FILTER DETECTOR MESSAGES. DISASSEMBLED FRONT SUMP & FOUND TOWERSHAFT DISENGAGED FROM BEVEL GEARSSDR DXTA2011052604591Hmu · malfunctionedCLIMBING THROUGH 10,000 FT, A CHANGE IN ENGINE PITCH SOUND. NR 2 ENGINE FUEL FLOW REPEATEDLY DROPPED 200 PPH FROM NORM & N1 DROPPED ABOUT 2 % FROM NORM. LASTED 2 SECONDS & WITH 3 DROPS IN 1 MINUTE & INDICATIONS RETURNED TO NORM. SAME SERIES OF DROPS OCCUREDSDR CA110606011Sensor · malfunctionedTHESE FAILURES HAVE BEEN REPORTED ON THE OIL LEVEL SENSORS FOR THE APU. UNITS P/N 722446 S/N (1) 725A (2) 990 (3) 651 (4) 1039 SO FAR FOR TROUBLESHOOTING WE HAVE CHECKED THE APU STARTER/GENERATOR TO ENSURE IT IS NOT CAUSING ANY VIBRATION. WOULD LIKE TO VERIFYSDR DXTA2011041904550Fan · obstructedIN FLIGHT, "RED DISPLAY TEMP" DISPLAYED ON CAPTAIN PFD AND ATTITUDE INDICATOR DISAPPEARED. PULLED OUT CAPTAIN'S PFD AND FOUND SCREEN OVER COOLING FAN VENT COMPLETELY COVERED WITH LINT, FUZZ, & DEBRIS. CLEANED OFF SCREEN AND REINSTALLED CAPTAIN'S PFD. OPS CHSDR CWQD.2011.05Resistor · overtempRT HALF OF CENTER WINDSHIELD NOT HEATING. TROUBLESHOT TO RT WINDSHIELD RESISTOR BOX BROKEN OFF AT CONNECTION POINT AND GROUND WIRE AT TERMINAL NR 3 OVERHEATED.SDR DXTA2011030844981Control Unit · inoperativeAT FL400 AMBER "BRAKE" ANNUNCIATOR ILLUMINATED, AND RT BRAKE MINELCO. REMOVED NR 1 BSCU AND INSTALLED AND INSPECTED BSCU IAW MM 32-445 PERFOMRED AN OPS CHECK REF MM 32-446.SDR DXTA2011030804497Brake Sys · warning lightAT FL400 AMBER "BRAKE" ANNUNCIATOR ILLUMINATED, AND RT BRAKE MINELCO.SDR 2011FA0000074Power Supply · shortedF/A SMELLED SMOKE AND SAW SMOKE COMING FROM BEHIND THE MICROWAVE OVEN. ON FEB. 4, 2011, THE ARTICLE IN QUESTION WAS RECEIVED AT REPAIR STATION. INVESTIGATION FOUND THAT A WIRE INSIDE THE METAL POWER SUPPLY BOX HAD CHAFED ON AN ADJACENT COMPONENT. THE METAL SDR DXTA2011020704453Control Cable · disconnectedON TAKEOFF FLAP RETRACTION FLAP ASYM WARNING LIGHT ILLUMINATED FOLLOWED BY A TRIP OF THE FLAP CONTROL CIRCUIT BREAKER. ACFT WAS LANDED WITH EXISTING FLAP AND SLAT CONFIGURATION. REMOVED PANEL 571BB, FOUND CABLE OFF OF ALP TRANSMITTER (LT). FOUND LT TRANSMISDR DXTA2011020304445Brake · frozenACFT DEPARTED. AFTER GEAR EXTENSION WITH 3 GREEN DOWN AND LOCKED, NO AMBER ANNUNCIATORS ILLUMINATED. IAW CONTAMINATED OPS PROCEDURES PARKING BRAKE WAS EXERCISED 3 TIMES AND STOWED. BRAKE PRESSURE ANNUNCIATOR NOT ILLUMINATED. AFTER A MATTER OF SECONDS AMBERSDR DXTA2011012604437Brake Sys · malfunctionedBRAKE PRESSURE STILL APPLIED WHEN FOOT BRAKES ARE RELEASED. FEELS AS THOUGH LT BRAKE STILL ENGAGED AFTER FOOT PEDAL PRESSURE IS RELEASED. ACFT PULLS LEFT WHILE TAXING AT 5 - 10 KNOTS, WHEN BRAKES ARE APPLIED & RELEASED. ALSO BRAKE PRESSURE LIGHT ILLUMINATESSDR DXTA2011012504433Slat · damagedON FLAP-SLAT RETRACTION AFTER TAKEOFF, THE YELLOW NIPS LIGHT REMAINED ON. IWA THE CHECKLIST, RE-EXTENDED SLATS-FLAPS, EXTENDED NORMALLY AND NIPS LIGHT WENT OUT. RETRACTED FLAPS-SLATS AND NIPS LIGHT REMAINED ON. UPON INVESTIGATION, THE RT SLAT HAS A WRINKLE INSDR DXTA2011012104425Apu · leakingDURING TAKEOFF WITH ENGINE ICE ON AND WING ICE ON AFTER TAKEOFF, IN TAKE OFF POWER DETENT, AN ODOR OF BURNING OIL OR EXHAUST WAS PRESENT IN COCKPIT. THIS ODOR DECREASED ONCE POWER WAS BROUGHT OUT OF TAKE OFF DETENT AND WITH GASPERS OPENED. TROUBLESHOT AND FSDR DXTA2011011804416Proximity Switch · intermittentAFTER TAKEOFF, ON GEAR RETRACTION THE NOSE GEAR RETRACTED NORMALLY, BOTH MLG REMAINED GREEN & GEAR DOOR LIGHTS ILLUMINATED RED. WHEN GEAR HANDLE MOVED TO THE GEAR DOWN POSITION ALL 3 GEARS SHOWED DOWN AND GREEN AND THE RED GEAR DOOR LIGHTS WERE EXTINGUISHED. SDR 2011FA0000056Card · corruptedNAVIGATIONAL CHART INFORMATION RESIDES ON A PCMCIA CARD (PLUG IN HARD DISK), WHICH IS STORED IN SLOT OF DATABASE MANAGEMENT UNIT (DMU). TROUBLESHOOTING REVEALED THAT THE PCMCIA CARD WAS CORRUPTED WITH THE "RECYCLER VIRUS". IN ADDITION TO THE PCMCIA CARD, THE MSDR CA110124014Compressor · stalledPOWER ROLL BACK DURING CRUISE AT FL410, LOUD NOISES SOUNDING LIKE COMPRESSOR STALLS WERE HEAR FOR APPROX 10 SEC. AFTER WHICH THE ENG POWER ROLLED BACK TO IDLE. THE FLIGHT WAS DIVERTED AND LANDED SAFELY. TROUBLESHOOTING IS ON-GOING. (SDR 2011020500132/DXTA2011SDR DXTA2011010604399Engine · malfunctionedDURING CRUISE AT FL410 IN CLEAR AIR THE LT ENGINE MADE WHAT SOUNDED LIKE COMPRESSOR STALL NOISES (BANGING, ABOUT 3 PER SECOND) FOR ABOUT TEN SECONDS AND THEN ROLLED BACK TO IDLE. DURING THE DESCENT ALL PARAMETERS WERE CHECKED TO BE NORMAL AND THE ENGINE RESPONSDR DXTA2010121904365Microwave Oven · odorON DESCENT THE F/A WAS USING THE MICRO-WAVE WHEN SHE SMELLED SMOKE AND SAW SMOKE COMING FROM BEHIND THE MICRO-WAVE. WHEN PULLING OUT THE TRASH BIN THERE WAS ALSO A DEFINITE ODOR OF SMOKE. VERIFIED SOURCE OF SMOKE IN CABIN, ORIGINATED FROM WIRING INSIDE MICROWSDR DXTA2010112904330Relay · malfunctionedSTABILIZER TRIM IS INOPERATIVE WHEN TRYING TO TRIM NOSE UP FROM EITHER YOKE CONTROL SWITCH. IT WILL TRIM NOSE DOWN FROM YOKE SWITCHES. EMERGENCY STAB TRIM WILL TRIM THE STAB IN BOTH DIRECTIONS. PRIMARY STAB TRIM CONTROL CONFIRMED DISCREPANCY FOUND NOSE DOWN
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