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 2017FA0000382Channel · damagedFOUND THE CABLE CHANNEL STRUCTURE DAMAGED BY THE PASSENGER DOOR COMPENSATION SYSTEM MECHANISM. THE DAMAGED AREA WAS HIDDEN/COVERED WITH ALUMINUM HIGH SPEED TAPE.SDR DXTA2017021006368Door · slowON EXTENDING LANDING GEAR RECEIVED THREE GREEN DOWN AND LOCKED INDICATORS BUT THE GEAR HANDLE CONTINUED TO FLASH AND THE TWO MAIN RED GEAR DOOR LIGHTS STAYED ON. STARTED TO LOOK THROUGH THE CHECK LIST FOR THIS CONDITION AND ABOUT SIX MINUTES LATER THE GEAR DOSDR DXTA2016120306336Control Unit · faultedAFTER POWER UP ON THE RUNWAY, THE AMBER BRAKE PRESSURE AND AMBER BRAKE LIGHTS CAME ON. DURING TAXI IN, THE BRAKE PRESSURE LIGHT EXTINGUISHED BUT THE BRAKE LIGHT IS STILL ON. THE NR 1 BSCU REPLACEDSDR EBVR20161103001Frame · corrodedFRAME ZERO HAS CORROSION ON PREVIOUS REPAIR. REMOVE REPAIR, AND FAN ASSEMBLY FOR INVESTIGATION. REMOVED EXISTING REPAIR AND BLENDED CORROSION ON FRAME ZERO AROUND NOSE CONE FAN CUTOUT. REPAIRED CORROSION DAMAGE TO FRAME 0 IAW DRAWING F2MA211010B5 E01-1 AND CHASDR DXTR2016100301Skin · gougedTHE VERTICAL STABILIZER SKIN HAS A GOUGE ON THE LH & RH SIDE WHERE THE REAR FAIRING ASSY CONTACTS THE VERTICAL STABILIZER. ACCOMPLISHED MINOR REPAIR IAW AQRD ERO-861733 DATED OCT 03/2016.SDR EBVR20160831001Frame · corrodedCORROSION FOUND AT FRAME "0" DURING AN INSPECTION BELOW THE NOSE CONE FAN BOX. IAW E-MAIL FROM MFG ENGINEERING AT FRAME 0, EVALUATION OF AREA AFTER BLENDING OF CORROSION ITEM A AND D WILL REQUIRE A REPAIR. USED REPAIR DWG F2MA2110010A5 EO1-1 FOR THIS REPAIR.SDR DXTA2016081106276Proximity Switch · unserviceableMAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED PROXIMITY SWITCH, 5GBC, PN: D22858000-1, SN: B931 DUE TO INTERNAL FAILURE. INSTALLED REPAIRED PROXIMITY SWITCH AS STATED ABOVE IAW F2000 MM 32-61-49-900-801. REMOVED PCB CARD, 415JE, PN: C1381, SN: SDR DXTA2016080406275Circuit Board · unserviceableFOUL ODOR FOLLOWED BY HYD NR 2 ISOLATION LIGHT. RETURNED TO DEPARTURE. R & R PCB'S 413JE-421JE WITH SUPPLIED PARTS IAW AMM 24-00-00-910-801. PERFORMED ENGINE RUN UP AND FOUND NO FOUL ODOR AT THIS TIME. NO ISOL LIGHT AT THIS TIME. PARTS REPLACED: CIRCUIT BSDR EBVR20160816001Fitting · looseDURING CRUISE FLIGHT, CREW RECEIVED A CAS MESSAGE FOR LOW HYDRAULIC FLUID LEVEL ON NR 1 SYSTEM. AIRCRAFT LANDED. ON ARRIVAL AT AIRCRAFT MAINTENANCE CREW FOUND A LEAKING MS FITTING. NO PRIOR MAINTENANCE WAS DONE TO OR AROUND THAT FITTING OR LINE AT OUR FACILSDR DXTA2016050606235Printed Ckt Board · defectiveAFTER TAXING & BRIEFLY SETTING THE PARKING BRAKE, THE AMBER BRAKE ANNUNCIATOR & LT BRAKE MINELCO WERE INDICATING. NO OTHER BRAKE ABNORMALITIES WERE OBSERVED. COMPUTER CODES, LT 325 PEDAL SWITCH FAILURE. REMOVED A DEFECTIVE LT BRAKE PCB PN FE422 & SN 4475. SDR DXTA2016050506234Relay · failedWITHIN 5 MINUTES AFTER TAKEOFF AN ELEC BURNING RUBBER SMELL BECAME NOTICEABLE. SOURCE & LOCATION NOT DETECTABLE. ODOR SMELL MOST NOTICEABLE IN COCKPIT & SLIGHTLY NOTICEABLE IN CABIN. OPERATED WINDSHIELD HEAT & NOTICED THE LT WINDSHIELD HEAT WAS NOT WORKING SDR DXTA2016050406232Unknown · odorTHE SMELL OF BURNING RUBBER FILLED THE ACFT DESCENDING OUT OF 8000 FT. THE FLIGHT ATTENDANT THOUGHT THE SMELL WAS WORST WHEN GEAR WENT DOWN, ALSO THE TOP LEAD PAX RT CONTROL PANEL WAS VERY HOT. RAN APU & OPERATED AIR CONDITIONING SYS FULL HOT & FULL COLD WITSDR DXTA2016040606221Flashlight · odorUNUSUAL ODOR ISOLATED TO THE FLIGHT DECK, AFTER TAKEOFF & DURING ENTIRE TIME EN ROUTE. NO SMOKE JUST A STRONG ODOR AT ALTITUDE. POWERED UP ACFT, RAN ENGS & APU WITH NO ODOR, INSPECTED COCKPIT DISPLAYS NO DEFECTS NOTED. PERFORMED OPERATIONS CHECKS OF DISPLAYSDR DXTA2016032506215Bracket · bentDURING TAKEOFF & SELECTING THE GEAR HANDLE TO THE UP POSITION, THE MAIN GEAR DOOR PANEL LIGHTS ILLUMINATED & NO MAIN GEAR RETRACTION OCCURRED. NORMAL NOSE GEAR LIGHT & RETRACTION OCCURRED. NORMAL LG & DOOR INDICATIONS WHEN GEAR HANDLE WAS SELECTED DOWN. NO SDR DXTA2016021406186Warning System · activatedREPEAT SQUAWK AFTER TAKEOFF, THE TWO MAIN GEAR RED & GREEN LIGHTS REMAINED ILLUMINATED, NOSE GEAR LIGHTS EXTINGUISHED, & GEAR HANDLE STARTED FLASHING AFTER 15 SECONDS. UPON LANDING BOTH RT STEERING MINELCOS DISPLAYED.SDR DXTA2016021306184Control Handle · faultyAFTER TAKEOFF THE TWO MAIN GEAR RED & GREEN LIGHTS REMAINED ILLUMINATED, NLG LIGHTS EXTINGUISHED & GEAR HANDLE STARTED FLASHING AFTER ABOUT 15 SECONDS. ON LANDING ALL HYD, STEERING & BRAKE MINELCOS WERE TRIPPED. CODES 315 & 415 STRUT PROXIMITY SWITCH FAILURESDR DXTA2016020506179Switch Panel · burnedWHILE TROUBLESHOOTING, CONFERENCE TABLE READING LIGHT, FOUND SWITCH & SWITCH PANEL BURNT. REMOVED READING LIGHT SWITCH CAPSULE & FOUND CAPSULE & PANEL SIDE BURNT. REMOVED SWITCH PANEL, PN SPS-F90-5093, SN 040100670 & INSTALLED A REPAIRED SWITCH PANEL, PN SPSSDR DXTA2016020306178Display · inoperativeIMMEDIATELY AFTER ROTATION ON TAKEOFF, BOTH THE PILOT SIDE PFD & MFD WENT BLACK. TWO SECONDS LATER, SMOKE BEGAN TO RISE FROM IN FRONT OF THE GLARE SHIELD. THE COPILOT PFD HAD ALL RED FLAGS. NO CBS WERE POPPED & BOTH GENERATORS REMAINED ONLINE. PERFORMED ANSDR CWQA20151224001Wire · brokenDURING CRUISE AT FL430, CREW NOTICED SMOKE COMING FROM THE LOWER PORTION OF LT DIRECT VISION WINDOW. CREW LOCATED SOURCE & TURNED SIDE WINDOW HEAT OFF, THE SMOKE DISSIPATED & SMOKE WAS NO LONGER OBSERVED. CHECK LIST FOLLOWED, EMER DECLARED & UNSCHEDULED LANDSDR EBVR20150911001Skin · corrodedEXFOLIATION CORROSION PENETRATING FUSELAGE PRESSURE VESSEL FOUND AT UPPER AFT JUNCTION OF FRAME 7 AND STR L21, BELOW AND AFT OF THE MAIN ENTRY DOOR. THE UMBRELLA CABINET DIRECTLY ABOVE THE AREA OF CORROSION PROVIDES A SOURCE OF LIQUID TO FLOW UNDER THE FLOOR,SDR CA151030013Duct · contaminated(CAN) CUSTOMER HAS REPORTED EXPERIENCING ODOR OF BURNED OIL DURING DESCENT. ODOR REPORTED TO HAVE BECOME STRONGER WHEN TEMPERATURE IS WARMER BUT DID NOT SEEM TO DEPEND ON POWER SELECTION. ACFT IS CURRENTLY AT A MAINTENANCE FACILITY AND DURING INSPECTION OIL SDR BZUA2016F00014Unknown · odorCREW NOTICED AN ODOR IN THE COCKPIT CLIMBING OUT, ENROUTE AND STILL PERSISTENT. THE CREW ELECTED TO MAKE A PRECAUTIONARY LANDING. MAINTENANCE INSPECTED THE ACFT AND ENGINE. THE ODOR COULD BE ISOLATED BY SHUTTING THE LT ENGINE BLEED. THE ACFT WAS FERRIED WHSDR DXTA2015101206104Pump · failedLEFT OIL PRESSURE DROPPED TO 20 PSI. OIL ONE ANNUNCIATOR ILLUMINATED. SHUTDOWN NR 1 ENGINE IN-FLIGHT. SERVICED ENG OIL & STARTED ENG. VERIFIED OIL TO BE LEAKING OIL PUMP DRAIN. R & R ENG OIL PUMP & NR 1 HYD PUMP WITH OVERHAULED UNITS. SERVICED ENG OIL, SSDR DXTA2015010086104Warning System · activatedLEFT OIL PRESS DROPPED TO 20 PSI. OIL ONE ANNUNCIATOR ILLUMINATED. SHUTDOWN NR 1 ENG IN FLIGHT.SDR DXTA2015100606102Battery · malfunctionedDURING COCKPIT PREFLIGHT INSPECTION, LT PFD, MFD TURNING ON THEN GOING BLANK, FMS LT & RT START DOING THE SAME, RT SIDE PFD ALSO TURNING ON, THEN BLANK. APU RUNNING & GEN OPERATING. APPEARED TO BE CONTINUOUSLY SURGING. MCC SUGGESTED SHUTDOWN REBOOT, ON REBOSDR DXTA2015092506090Unknown · odorTHERE IS A STRONG MUSTY & MOLDY ODOR, LIKE DIRTY SOCKS. INSPECTED CABIN AC SYS CONDENSER FOR CLEANLINESS & INSPECTED CABIN RECYCLE VLVS INLET, NO DEFECTS NOTED. INSPECTED WATER SEPARATOR FILTER & CLEANED IAW AMM 21-52-18-100-801. REINSTALLED FILTER & RAN TSDR W6JA20150824005Pump · leakingLOSS OF NR 1 HYD RESERVOIR SYS FLUID IN FLIGHT TO 20%. NR 1 ENG HYD PUMP SYS NR 1 LIGHT ON & NR 2 ENG HYD PUMP SYS NR 1 LIGHT ON. PSI 200/600 FLUCTUATING. FOUND LEAK FROM NR 1 ENG HYD PUMP SYS NR 1. REMOVED NR 1 ENG HYD PUMP 1 & NR 2 ENG HYD PUMP 1. INSTASDR DXTA2015081706059Unknown · odorBAD ODOR FROM ENVIROMENTAL SYS WITH ENGS RUNNING. CHECKED BLEED AIR SYS, APPLIED HEAT TO MAX, INSPECTED THE APU INLET DUCTS, INSPECTED THE APU CARBON SEAL, PERFORMED A VACUUM CHECK OF APU GB VENT, AND RAN APU FOR ONE HOUR PERFORMING CHECKS, NOT ODOR DETECTED.SDR DXTA2015081706058Flashlight · odorCLIMBING 22000 FT, FIRST OFFICER SMELLED SOMETHING BURNING. DONNED THE OXYGEN MASKS, DECLARED AN EMERGENCY & LANDED IMMEDIATELY. PERFORMING AS MUCH OF THE APPROPRIATE EMERGENCY CHECKLIST AS POSSIBLE. CHECKED COPILOTS RECHARGEABLE FLASHLIGHT & FOUND TO BE SDR DXTA2015081106058Pitot Tube · obstructedAT 300 AGL, THE LT AIRSPEED DISAPPEARED. IT CAME BACK ON SHORTLY, SHOWING 80 KTS. FIRST OFFICER`S AIRSPEED WAS 220 KTS. LT AIRSPEED CLIMBED TO 270, WHILE THE RT DROPPED TO 120KTS. CONTINUED TO HAVE THREE DIFFERENT AIRSPEEDS & ALL CONTINUED TO FLUCTUATE BETSDR DXTA2015081006053Smoke Detector · failedN FLIGHT AT CRUISE THE FIRE BAG COMP LIGHT CAME ON WITH THE AUDIO WARNING. WE CHECKED THE BAGGAGE COMPARTMENT & A FIRE DID NOT EXIST. PERFORMED MULTIPLE FIRE TESTS IAW F2000 MM TASK 26-10-21-900-801 WITH NO DEFECTS NOTED. GENTLY MANIPULATED SMOKE DETECTOR &SDR CA150802002Engine · malfunctioned(CAN) PILOT REPORTED WHEN POWER REDUCED ON THE START OF A DESCENT FROM 41000 FT, AND NOTICED VIBRATION ON RT ENGINE FOLLOWED BY AN ITT, N1 AND N2 DROP. AUTO RELIGHT SEQUENCE WAS ACTIVATED AND ENGINE RECOVERED.SDR DXTA2015072706052Oven · smokeAPPROXIMATELY 40 MINUTES INTO FLIGHT, AFTER FLIGHT ATTENDANT STARTED USING OVEN, A STRONG ACRID ODOR ENTERED COCKPIT, ALSO NOTICED A SMOKEY HAZE IN MICROWAVE COMPARTMENT. OVEN USE WAS DISCONTINUED & ODOR DIMINISHED. R & R OVEN ASSEMBLY WITH A REPAIRED UNIT.SDR DXTA2015070806039Controller · malfunctionedDURING CRUISE RED MWS, CABIN LIGHT & AUDIBLE CAME ON. CABIN CLIMBING AT 500 TO 700 FT PM. FOLLOWED EMERGENCY CHECKLIST, EXECUTED RAPID DESCENT & DIVERTED. DUMP VALVE PRESSED. WHILE PERFORMING OPS TEST OF CABIN PRESSURE SYS IAW MM 21-32-00, FOUND THAT NEW PSDR DXTA2015061506031Unknown · sparksLIGHTNING STRIKE CAUSED SPARKS IN COCKPIT WHICH TRIPPED THE ANTI COLLISION FIN CIRCUIT BREAKER & WINGS CIRCUIT BREAKER. LEFT BLACK SINGE MARKS ON PANEL. BURNED ODOR IN COCKPIT & CABIN, NO FIRE OR SMOKE PRESENT. COMPLIED WITH AMM TASK 05-50-00-200-803. ACCESDR DXTA2015060906026Probe · out of limitsWINDSHIELD XFR LIGHT CAME ON INFLIGHT & SMOKE ODOR. TROUBLE SHOT & FOUND L512DG WAS NOT RECEIVING POWER. FOUND WINDOW PROBE TO BE OUT OF LIMITS, HIGH RESISTANCE. REMOVED DEFECTIVE PILOT WINDSHIELD 10SA & INSTALLED A NEW PILOT WINDSHIELD 10SA. PERFORMED ALL SDR DXTA2015020305974Hmu · failedON FINAL APPROACH & SHORTLY AFTER SELECTING FLAPS TO 10 DEGREES THE GEN 1 ANNUNCIATOR ILLUMINATED. APPROX 10 SECONDS LATER THE NR 1 ENG ROLLED BACK TO IDLE & SHUTDOWN WITH ALL APPROPRIATE ANNUNCIATOR ILLUMINATING AS WOULD BE OBSERVED ON A NORMAL ENG SHUTDOWNSDR DXTA2015012905972Cradle · odorINTERMITTENT DUSTY BURNING SMELL IN COCKPIT DURING FLIGHT. NO SMELL NOTED WHEN APU IS RUNNING. MUCH STRONGER IN COCKPIT THAN CABIN. OCCURS DURING CLIMB AND CRUISE, NOT DURING DESCENT WITH POWER REDUCED. SMELL SEEMED TO DISSIPATE WITH BLEED2 SWITCH OFF, OR CRESDR DXTA2015012105966Cradle · odorAN INTERMITTENT STRONG ACRID ODOR COMING FROM THE AREA BEHIND THE PILOTS SEAT. TECH FOUND THE BATTERIES AND CHARGERS WERE THE CAUSE OF THE ODOR. REMOVED AND REPLACED BOTH FLASHLIGHT ASSEMBLIES. OPS CHECKED GOOD.SDR DXTA2015011305959Unknown · odorA STRONG SMOKE LIKE ODOR DEVELOPED DURING CRUISE AT 41000 FEET. NO SMOKE WAS SEEN NO HEAT NOTICED & ALL CIRCUIT BREAKERS REMAINED SEATED. ODOR GOT STRONGER OVER TIME. EMERGENCY DECLARED AND AIRCRAFT DIVERTED. COMPLETED INSPECTION & CHECK & DECONTAMINATION OSDR DXTA2015010605957Arm · faultyDOOR LIGHT ILLUMINATED INFLIGHT AT FL350. AFTER RESETTING, IT ILLUMINATED FOUR MORE TIMES. NO LOSS OF PRESSURE NOTED. REMOVED FAULTY FORWARD CABIN DOOR PROXIMITY SWITCH STABILIZER ARM AND REPLACED. PERFORMED DOOR FUNCTIONAL CHECK. ALL WORK PERFORMED IAW MM SDR DXTA2014122305952Brake Sys · weakBRAKING WAS NOTICEABLY DIMINISHED DURING TAXI. RETRIEVED FAULT CODES. SWITCHED BSCU 1 & 2 IAW MM 32-41-02-900-801 AND PERFORMED OPS TEST OF BSCU IAW MM 32-41-02-710-801. NO FAULTS NOTED. CHECKED CONDITION OF CONNECTORS AND SWITCHES, NO FAULTS NOTED.SDR ZKFA2015F00012Engine · making metalDURING ACCOMPLISHMENT OF ENGINE SHUTDOWN CHECKLIST, FLIGHT CREW NOTED NR 2 ENGINE CHIP INDICATION. TECH REMOVED AND INSPECTED CHIP DETECTOR AND FOUND METAL CONTAMINATION ON BOTH COLLECTION POINTS, FORWARD AND AFT SUMP AREAS. SOAP SAMPLE WAS SUBMITTED FOR ANASDR DXTA201412205939Motor · failedSETTING SWITCH TO OFF WOULD NOT STOW WIPER. SHORTLY AFTER RECEIVED A STRANGE ODOR. 30 SECONDS LATER ODOR BECAME ELECTRICAL BURNING AND INCREASING IN INTENSITY. REMOVED FIRST OFFICER'S WINDSHIELD WIPER MOTOR AND INSTALLED A NEW WIPER MOTOR IAW MM 30-43-05-9SDR DXTA2014112105932Ahrs · failedCLIMBING THROUGH 4000 FT, DETECTED AN ODOR IN THE COCKPIT. CONTINUED THE CLIMB, LEVELING AT 16000 FT WHERE THE ODOR WAS THE STRONGEST. NO SMOKE WAS VISIBLE BUT SMELLED LIKE WIRE INSULATION BURNING. ISOLATING THE PNEUMATICS DID NOT REDUCE THE ODOR. REMOVED SDR DXTA2014111605927Brake Sys · unknownBRAKES AT SLOW SPEED TAXI & HIGH SPEED TAXI ARE LOCKING UP & PULLING TO THE RIGHT. JACKED STRUT & CHECKED FREEDOM OF WHEEL MOVEMENT, FOUND ACTION NORMAL. CHECKED TIRES FOR ANY EVIDENCE OF FLAT SPOTS, NONE NOTED. COMPLIED WITH TAXI CHECK, TAXI CHECKED NORMASDR ZKFA2015F00001Engine · making metalRT ENGINE CHIP INDICATION ON EIED DURING ACFT SHUTDOWN. ENGINE IS 12.5 HOURS OUT OF A NR 3 BEARING REPLACEMENT MAINTENANCE EVENT. ENGINE OIL SOAP WAS PERFORMED AND THE ENGINE REMOVED. THE MAJORITY OF THE DEBRIS WAS DETERMINED TO BE A 300-SERIES STAINLESS STSDR DXTA2014110505921Unknown · odorAN ACRID ODOR COMING FROM GLARE SHIELD VENTS ABOVE INSTRUMENT PANEL. RAN APU & USED APU BLEED AIR, RAN FOR SEVERAL MINUTES & NO ODOR WAS COMING FROM THE COCKPIT. RAN ENG 1 & 2 APPLIED BLEED AIR FROM BOTH ENGS FOR AN HOUR & NO ODOR WAS NOTED. ISOLATED ENG 1 SDR DXTA2014102405916Fire Warning · false activationCARGO BAY FIRE LIGHT ILLUMINATED & REMAINED ON UNTIL THE POWER LEVERS WERE RETARDED TO IDLE. NO FIRE INDICATIONS EXCEPT FOR FAINT SMOKE ODOR. RAN BOTH ENGINES AT CLIMB & CRUISE SETTINGS, COULD NOT REPLICATE FIRE LIGHT AT ANY POWER SETTING. CHECKED CONNECTIOSDR ZKFR2014102800001Bearing Cage · crackedDURING POWER-UP AND ENGINE START CHECKLIST FLIGHT CREW NOTED NR 2 ENGINE CHIP INDICATION YELLOW ON EIED. MAINTENANCE TECH REMOVED RT ENGINE CHIP DETECTOR AND DISCOVERED METAL CONTAMINATION ON DETECTOR. METAL CHIPS AND OIL FILTER WERE SENT OUT FOR SOAP LAB ANA
Back to Dassault FALCON 2000