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 DXTA200601501Proximity Switch · faultyHAD LT AND RT MINELCO'S FOR STEERING AND BRAKES. RAN FAULT CODES AND GOT 315, 334, 415, 434. DID A RESET AND STEERING MINELCO'S RESET, BUT NOT BRAKES. RAN FAULT CODES AND HAVE 315 AND 415 AGAIN. ON DEPARTURE, THE GEAR DID NOT RETRACT FIRST, BUT ON RECYCLE SDR 917133O-Ring · cutWHILE IN CRUISE FLT AT FL 340, NOTICED OIL PRESSURE ON RT ENGINE DROP INTO YELLOW. IT CONTINUED TO DROP 1 PSI EVERY 2 TO 4 MINUTES AND EVENTUALLY ENDED UP IN THE RED AT 17 PSI BEFORE SHUTTING ENGINE DOWN ON THE GROUND. OIL TEMP WAS 67 DEGREES C, OIL QUANTITY SDR C4S2006F00000Window · crackedDURING POST FLIGHT INSPECTION, FOUND SEVERAL (5) SMALL CRACKS (.25 INCH APPROX) IN THE LEFT REAR COCKPIT SIDE WINDOW VERY AFT EDGE, MIDDLE OF THE WINDOW. THE CRACKS WERE IN THE IB PANE. THE DEFECTIVE PART WILL BE REPLACED WITH A NEW UNIT (K)SDR DXTA200601480Warning Message · activatedON THE TAKEOFF ROLL, PRIOR TO A/S ALIVE CALL GOT THE MASTER WARNING W/ BOTH THE RED AND YELLOW BRAKE LIGHTS ON.SDR DXTA200601469Transmitter · faultedAFTER FLAP RETRACTION LOW FUEL ONE AND TWO LIGHTS CAME ON. FOLLOWED BY APU FAULT LIGHT (APU MASTER WAS OFF). CABIN LOST PRESSURE. LOW FUEL LIGHTS WERE INTERMITTENT. DURING OUR DESCENT BACK INTO BTV, OIL PRESSURE GAUGE ON LEFT ENGINE ROLLED DOWN TO 14 PSI. OSDR DXTA200601460Brake Assy · noisyHAVING LIGHT TO MODERATE BRAKING DURING LANDING AND DURING TAXI, THE BRAKES WILL SLIP AS IF ON ICING CONDITIONS. ALSO PRESENT IS A GRINDING NOISE DURING BRAKING TO A FULL STOP. REMOVED ALL FOUR WHEEL CAPS AND INSPECTED WHEEL SPEED TRANSDUCERS AND DRIVE TUBESSDR DXTA200601457Pcb · malfunctionedDURING GEAR EXTENSION, WHEN HANDLE WAS PUT DOWN, THE GEAR DID NOT EXTEND THE GEAR HANDLE WAS FLASHING AND THE GEAR DOORS (MAIN) LIGHTS WERE ILLUMINATED. NOTHING MECHANICAL MOVED. GEAR HANDLE WAS PLACED IN UP POSITION AND RE-CYCLED, GEAR DEPLOYED NORMAL. REMSDR XTA200601457Circuit Board · failedDURING GEAR EXTENSION, WHEN HANDLE WAS PUT DOWN, THE GEAR DID NOT EXTEND THE GEAR HANDLE WAS FLASHING AND THE GEAR DOORS (MAINS) LIGHTS WERE ILLUMINATED. NOTHING MECHANICAL MOVED. GEAR HANDLE WAS PLACED IN UP POSITION AND RE-CYCLED, GEAR DEPLOYED NORMAL. RESDR PA06005Pressure Switch · failedPILOT REPORTED LOSS OF NR 1 HYD FLUID, LEFT SIDE. TROUBLESHOOTING REVEALED THE LEFT HYDRAULIC SYSTEM PRESSURE SWITCH IN THE TAIL COMPARTMENT FOR THE HYDRAULIC SYSTEM RUPTURED INTERNALLY CAUSING THE FLUID/PRESSURE LOSS. REPLACED THE LEFT HYDRAULIC SYSTEM PRESSDR 2006FA0000670Computer · intermittentALL 3 FMS INTERMITTENTLY RESETS IN FLIGHT WITH INFORMATION RETURNING AT RANDOM.SDR DXTA200601448Apu · inoperativeON GROUND AT HPN AFTER RIGHT ENGINE START SMOKE STARTED BLOWING OUT OF BOTH COCKPIT GASPERS. PAX AND CREW OVERHEAD ANNUNCIATORS ILLUMINATED AFTER ENGINE SHUTDOWN SMOKE DISAPPEARED AND APU BLOWS NORMAL AIR. REMOVED AND REPLACED APU P/N 3800548-2, S/N P-387 WISDR DXTA200601444Fuel Filter · unknownTAXIING IN, RT ENG SHUTDOWN & RECEIVED FOLLOWING EIED MESSAGE -F2B T2 RANGE FAULT-. DOWNLOADED FADEC'S & SENT TO MCC. PERFORMED 2 STARTS ON NR 2 ENG, BOTH START NORM. RAN ENG AT LOW PWR 5 MINS, OPS CHECKS NORM. GAINED ACCESS TO RT TZ SENSOR, FOUND EXCESSIVSDR DXTA200601422Carbon Seal · failedAPPROX. 1.5 HOURS INTO FLIGHT LT ENGINE OIL PRESSURE GAUGE STARTED SHOWING INTERMITTENT. ON DESCENT OUT OF FL370 OIL PRESSURE STARTED DROPPING SLOWLY, CONTINUED TO MONITOR THEN OIL PRESSURE WENT <30 PSI MASTER CAUTION. REMOVED STARTER CARBON SEAL P/N 3056647SDR DXTA200601412Probe · malfunctionedON TAKE OFF ROLL NO AIRSPEED READOUT ON RIGHT SIDE. ERRONEOUS WIND READOUTS NOTED OF 40 -40 TO -60 KTS. TAKEOFF ABORTED. - REMOVED RT SIDE PITOT PROBE PN 50520 SN 1960 AND INSTALLED NEW PITOT PROBE P/N 50520 S/N 3772 IAW F2000 MM PROCEDURE 20-000. PERFORM OPESDR DXTA200601409Starter · failedNR 2 ENGINE HAD NORMAL START, DURING START FOR NR 1 ENGINE NO N2 ROTATION WAS OBSERVED. NR 2 WAS SHUTDOWN THEN APPROXIMATELY 1 MIN. LATER NR 1 ENGINE COWLING BLEW OPEN. ALL BLEED VALVE SWITCHES WERE IN "AUTO" POSITION. INSPECTED ENGINE & FOUND AIR STARTER TURSDR DXTA200601395Water Heater · failedELECTRIC BURNING SMELL IS PRESENT AT THE INTERSECTION OF THE GALLEY AND THE CABIN. DETERMINED ELECTRICAL BURN SMELL DUE TO WATER HEATER FAILURE. WATER HEATER ISOLATED AND DEFERRED IAW MEL 25-7 AND SUPPLEMENTAL MAINT PROCEDURES.SDR 2006FA0000444Cowling · separatedAC WAS RETURNING TO HOME FIELD AFTER MAINTENANCE WHEN CREW HEARD A LOUD NOISE AND ELECTED TO RETURN TO DEPARTURE. AFTER ENGINE SHUT-DOWN, IT WAS DETERMINED THAT THE LT ENGINE UPPER AND LOWER COWLING HAD SEPARATED FROM THE AC IN FLIGHT. SB CONCERNING COWLING SDR 2006FA0000443Cowling · separatedAIRCRAFT WAS RETURNING TO HOME FIELD AFTER MAINTENANCE WHEN CREW HEARD A LOUD NOISE AND ELECTED TO RETURN TO DEPARTURE. AFTER ENGINE SHUTDOWN, IT WAS DETERMINED THAT THE LT ENGINE UPPER AND LOWER COWLING HAD SEPARATED FROM THE AC IN FLIGHT. SB CONCERNING COWSDR DXTA200601347Transmitter · inoperativeAFTER T/O W/FLAPS AT 20 DEGREES AT 400 FT AGL FLAP HANDLE PLACED IN UP POS THE FLAP ASYM + GONG CAME ON AND THE SLATS DID NOT RETRACT. INSTALLED A REPAIRED FLAP TRANSMITTER (LT) IAW MM CHAPTER 27-509. COMPLETED OPERATIONAL CHECK IAW MM CHAPTER 27-502. NO DEFSDR DXTA200601269Pcb · inoperativeUNCORRECTABLE T/O CONFIGURATION MASTER CAUTION ON TAKEOFF ROLL. ALL PARAMETERS WERE MET. BRAKES, FLAPS, AIRBRAKES, TRIM, AND AUTOPILOT WERE IN CORRECT POSITION. NO MESSAGES ON EIED EITHER. CAN'T CORRECT. AUDIO WARNING, "NO TAKEOFF", ALSO CAME ON. REMOVEDSDR DXTA200601262Brake Assy · malfunctionedDURING OCF AT 80KTS WHEN BRAKES APPLIED, LEFT TOE BRAKE -MORE PEDAL TRAVEL- AND AIRCRAFT PULLS HARD LEFT. ITEM IS UNDER INVESTIGATION.SDR DXTA200601249Adc · failedDURING TAKEOFF ROLL, BELOW 50KTS, "AUTO SLATS" ANNUNCIATOR CAME ON, NO AIRSPEED OR ALTITUDE INFO ON NR 1 PFD. ADC MESSAGES ON EIED AFTER CLEARING THE RWY. TROUBLESHOT SYSTEM, REMOVED & REPLACED PILOTS ADC OPS CHECKS GOOD. PITOT/STATIC LEAK CHECK AND ADC FUNCSDR DXTA200601240Cooling Fan · failedAPPROX 5 TO 10 MINUTES AFTER T/O, FLIGHT ATTENDANT AND CREW NOTICED ACRID SMELL COMING FROM AREA OF CLOSET BEHIND CAPT'S SEAT. REMOVED ALL ITEMS FROM CLOSET, CHECKED BEHIND PANEL COVERING AVIONICS BOXES, ALL FELT NORMAL TEMPERATURE. SMELL PERSISTED FOR 5-10 SDR DXTA200601237Access Door · warning lightDOOR WARNING LIGHT CAME ON DURING THE TAKEOFF ROLL. TAKEOFF WAS ABORTED AND ALL DOORS WERE VERIFIED CLOSED. DEFERRED IAW NJA FALCON 2000 MEL, FERRIED AIRCRAFT TO CMH FOR REPAIR. COMPLETED DOOR INDICATION TEST IAW F2000 MM 52-701. NO DEFECTS NOTED.SDR DXTA200601224Starter Gen · seizedWHILE SITTING ON THE RAMP WITH APU RUNNING. THE CABIN LIGHTS FLICKERED AND AN ELECTRICAL BURNING SMELL WAS PRESENT. SHUT DOWN APU. TOOK ALL PWR OFF. THERE WERE NO CB'S POPPED. THE SMELL WAS ONLY PRESENT IN THE CABIN. APU WILL NOT START. GAINED ACCESS TOSDR CA060129014Engine · odor(CAN) THE ENGINE WAS REPORTED TO EXHIBIT OIL SMELL IN CABIN AIR ACCOMPANIED BY HIGH OIL CONSUMPTION. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20060129014)SDR DXTA200501152Control Module · malfunctionedON GEAR RETRACTION NOSE WHEEL RETRACTED, MAIN GEAR DID NOT RETRACT , MAIN GEAR DOOR LIGHTS REMAINED ON, "AUTO SLATS" LIGHT ILLUMINATED, NOSE WHEEL STEERING MINELCOS DISPLAYED RED AND NOSE WHEEL STEERING WAS INOPERATIVE ON LANDING. - REPLACED R/H NOSE GEAR PROXSDR DXTA200501140Fire Warning · illuminatedNR 2 ENGINE FIRE FAULT LIGHT IS ILLUMINATED. ITEM IS UNDER INVESTIGATION.SDR DXTA200501106Sensor · malfunctionedDURING FLIGHT LEFT MAIN LANDING GEAR OVERHEAT LIGHT ILLUMINATED. RESEARCHED TECH DATA. GAINED ACCESS TO WHEEL WELL INSPECTED FOR ANY VISUAL DAMAGE OR DEFECTS, FOUND NONE AT THIS TIME. PERFORMED GEAR WELL OVERHEAT TEST AND TEST PASSED. CONTACTED LMCC FOR HISDR DXTA200501102Controller · failedAT FL360 AN IMMEDIATE LOSS OF CABIN PRESSURIZATION WAS EXPERIENCED. CABIN PRESSURIZATION IMMEDIATELY WENT ABOVE 10,000 FEET. EMERGENCY DESCENT WAS INITIATED TO 15,000 FEET. AFTER LEVEL OFF AUTOMATIC CABIN PRESSURE CONTROLLER WAS FLASHING A CODE OF AO16. AFSDR DXTA200501085Steering Sys · malfunctionedDURING T/O ROLL, NOSEWHEEL STEERING WOULD NOT ENGAGE UNTIL STEERING WAS TURNED PASSED 45 DEGREES EITHER SIDE. DURING TAXI NWS WORKED INTERMITTENTLY. PERFORMED OPERATIONAL TEST OF STEERING CONTROL SYSTEM WITH NO DEFECTS NOTED PER FALCON 2000 M/M 32-500.SDR CA051129011Engine · malfunctionedDURING CLIMB, THE ENGINE EMITTED A LOUD NOISE AND SHUT DOWN UNCOMMANDED. SUBSEQUENT INSPECTION REVEALED DAMAGE TO THE TURBOMACHINE. P&WC WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR DXTA200501033Pitot Head · obstructedON TAKEOFF ROLL AFTER 50 KTS & BEFORE 80 KTS PILOTS AIRSPEED FAILED CO-PILOTS PFD INDICATED YELLOW IAS MISCOMPAIR FLAG, NR 2 EIED DISPLAYED FLA ADC MN RANGE SOFT FAULT, FIB ADC MN RANGE SOFT FAULT, FZA ADC MN RANGE SOFT FAULT F2B MN RANGE SOFT FAULT. ABORTED SDR DXTA200501015Position Switch · inoperativeON FINAL APPROACH AT 170K THE GEAR HANDLE WAS PUT DOWN, BUT JUST THE 3 RED LTS CAME ON AFTER 20 SEC THE GEAR HANDLE STARTED TO FLASH. THE GEAR WAS EXTENDED USING THE EMER GEAR PULL HANDLE. 3 GREEN CAME ON. - REMOVED L/H MLG DOOR PROX SWITCH, P/N 803682, S/N 07SDR DXTA200501010Adc · inoperativeON TAKEOFF ROLL. EXPERIENCED AN ADC FAILURE. TAKEOFF WAS ABORTED. REMOVED AND REPLACED NR 1 ADC, SYSTEM OPERATIONALLY CHECKS NORMAL IN ACCORDANCE WITH FALCON 2000 MAINTENANCE MANUAL CHAPTER 34-100 AND 34-104. ALL WORK PERFORMED BY DUNCAN AVIONICS TEB.SDR DXTA200500966Pressure Switch · leakingTOTAL LOSS OF HYDRAULIC FLUID ON THE NR 1 HYD SYSTEM IN FLIGHT. REMOVED NR 1 HYDRAULIC SYSTEM PRESSURE SWITCH CODE (L30GI) P/N 7G979, S/N 1722 AND REPLACED WITH NEW SWITCH P/N 7G979 , S/N 2784. REMOVED NR 1 & NR 2 ENGINE HYDRAULIC PUMPS AND INSPECTED FLUID ASDR DXTA200500946Position Switch · malfunctionedAFTER TAKEOFF GEAR HANDLE WAS SELECTED UP, GEAR STARTED TO RETRACT WITH THREE RED LIGHTS, GEAR THEN STOPPED INTRANSIT WITH MAIN GEAR RED AND GREENS SEEN AND GEAR HANDLE FLASHING. AFTER SELECTING GEAR DOWN, GEAR WENT DOWN NORMALLY. TROUBLESHOT FOR LANDING GEASDR DXTA200500928Pcb · inoperativeUPON GEAR EXTENSION, GOT THE FOLLOWING INDICATIONS, THE 3 RED LIGHTS NO GREEN THE EXTENSION PROCESS THEN STOPPED. HEARD A CLICKING SOUND COMING FROM BEHIND US. JUST AS THE GEAR HANDLE STARTED FLASHING THE EXTENSION PROCESS FINISHED. REMOVED PCB 10GW AND INSSDR DXTA200500925Hydraulic System · leakingCOMPLETE LOSS OF THE NR 1 HYDRAULIC SYSTEM IN FLIGHT AT FL410. HYD QTY DROPPED TO 15 PERCENT, PRESSURE FELL TO 100PSI. UPON LANDING HYDRAULIC FLUID NOTED ALL OVER BELLY OF ACFT AND COVERING INSIDE OF "HELLHOLE" COMPLIED WITH NORMAL AND ABNORMAL CHECKLIST PERSDR DXTA200500921Control System · malfunctionedFLAP SLATS NIPS LIGHT OUT IN FLIGHT. LEFT SLAT NOT RETRACTING COMPLETELY, FLAPS/SLATS DEPLOYED AT CRUISE.SDR DXTA200500833Potentiometer · failedFLAP CONTROL CIRCUIT BREAKER POPPED IN CRUISE FLIGHT. FLAP HANDLE WAS NOT MOVED AND REMAINED IN UP POSTION. INSTALLED REPAIRED LT POTENTIOMETER IAW FALCON 2000 M/M 27-509.SDR DXTA200500830Warning Light · illuminatedBRAKE LIGHT ILLUMINATED IN FLIGHT, DOWNLOADED FAULT CODE 335. RESEARCHED COOL CODE: CHECK RT WHEELS. WHEELS CHECK GOOD. NO DEFECTS DETECTED. WORK PERFORMED IAW CHAPTERS 45-308 AW 32-404 OF THE FALCON 2000 M/M.SDR DXTA200500800Fan · odorMODERATE TO STRONG BURNING ODOR WAS NOTICED IN COCKPIT AFTER DEPARTURE, ODOR BECAME FAINT AND THEN STRONGER SEVERAL TIMES. REMOVED AND REPLACED NR 4 PDU COOLING FAN ASSY. WITH A NEW FAN ASSEMBLY. OPS CHECK GOOD NO ODOR NOTED IN CABIN. WORK PERFORMED IAW FALCOSDR DXTA200500719Contact · dirtyON TAKEOFF ROLL, RED MASTER DOOR LIGHT CAME ON. ALL DOORS WERE CLOSED AND LOCKED. MEL'D IAW NETJETS FALCON MEL. ALL DOORS WERE OPEN & CLOSED, AND FOUND CONTACTS ON EMERGENCY EXIT DOOR TO BE DIRTY , CLEANED AND REINSTALLED DOOR AND OPS CHECK SYSTEM AND FOUNSDR DXTA200500721Fadec · malfunctionedDURING NR 2 ENGINE START - INITIALLY EXPERIENCED SURGING NOISE WHICH EVOLVED INTO EXTREMELY VIOLENT VIBRATION RESULTING IN SHAKING ENTIRE A/C AND THEN IT IMMEDIATELY BEGAN RAPID RISE TO YELLOW ARC PRIOR TO MANUAL SHUTDOWN. REPLACED NR 2 B FADEC IAW FALCON 200SDR 2005FA0000472Wire Harness · shortedFRACTURED WIRE HARNESS UNDER COPILOT SEAT ARCED AND SHORTED, SPARKS AND COPPER GLOBULES. POSSIBLE FIRE HAZARD IF PAPERS, ETC. UNDER SEAT. CIRCUIT BREAKER WAS SLOW TO RE-ACT. HARNESS NEEDS TO BE MORE RUGGED WITH ATTENTION TO ROUTING AND CLAMPING. (K)SDR DXTA200500585Fire Detector · false activationDURING DESCENT (16000 FT) FIRE BELL SOUNDED LT WHEEL WELL OVERHEAT AND BAGGAGE FIRE ILLUMINATED AT SAME TIME. BAGGAGE LIGHT EXTINGUISHED AFTER 5 SECS, WHEEL WELL REMAINED ON. EXECUTED PHASE 1 CHECKLIST. LIGHT EXTINGUISHED ON IT'S OWN AT 200 KTS BEFORE GEAR SDR DXTA200500570Proximity Switch · failedLANDING GEAR HANDLE FLASHED RED FOLLOWED BY LN3 GEAR CONTROL C/B POPPING. FOLLOWED ABNORMAL GEAR EXT CHECKLIST W/ONE RESET OF C/B GEAR EXTENDED NORMALLY AND LANDING GEAR CONTROL C/B POPPED AGAIN. REMOVED BAD SWITCH AND INSTALLED NEW PROXY SWITCH AT LT MAIN LSDR DXTA200500564Actuator · malfunctionedAFTER GEAR RETRACTION LEFT GEAR RED LIGHT INDICATOR DID NOT GO OUT. INSPECTION AFTER LANDING, GEAR DOOR WAS CLOSED BUT RED LIGHT REMAINED ON. REMOVED AND REPLACED THE LT MLG DOOR UPLOCK WITH A SERVICEABLE -REPAIRED- UNIT PER THE F-2000 M/M 32-300. ALL CHECKSDR DXTA200500556Warning Light · illuminatedON TAXI OUT AMBER BRAKE LIGHT ILLUMINATED AND RT BRAKE MINELCO TRIPPED. COMPUTER SHOWS CODE 424 RIGHT PEDAL SWITCH. ITEM IS UNDER INVESTIGATION.
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