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 DXTA2010112204314Circuit Board · malfunctionedDESCENDING THROUGH FL300, FLAP ASYM AMBER LIGHT STARTED TO BLINK & FLAP CONTROL BREAKER POPPED. FLAP ASYM LIGHT CONTINUED TO BLINK FOR ABOUT 30 SECONDS. ON GROUND, MCC ADVISED TO RESET FLAP BREAKER, DID NOT POP AGAIN. PERFORMED OPS TEST OF FLAPS IAW MM 27-81SDR DXTA2010111504305Duct · contaminatedBURNING ODOR WITH STRONG FUMES IN CABIN WITH APU RUNNING. TRACES OF OIL FOUND ON ECS FLOORBOARD. FOUND AIR DUCT CONTAMINATED. REMOVED CONTAMINATED DUCT AND INSTALLED NEW ASSY IAW MM 20-125 20-000 20-001.SDR DXTA2010110904300Selector · malfunctionedPERFORMING NORMAL APPROACH CHECKLIST, LOWERED LANDING GEAR AND CONFIRMED 3 GREEN & NO RED CALLOUT. WITHIN A MINUTE GEAR HANDLE BEGAN TO FLASH. ABANDONED APPROACH & PERFORMED LANDING GEAR EXTENTION MALFUNCTION CHECKLIST, LANDED UNEVENTFUL. REPLACED DEFECTIVESDR DXTA2010110804295Control Box · malfunctionedAFTER DEPARTURE LANDING GEAR WOULD NOT RETRACT. GEAR HANDLE WOULD NOT MOVE OUT OF THE DOWN POSITION. THE GEAR INDICATION WAS 3 GREEN AT ALL TIMES. REMOVED LANDING GEAR CONTROL BOX. APPLIED POWER TO PINS P & K TO ACTUATE SOLENOID. SOLENOID FAILED. INSTALLSDR DXTA2010110404289Proximity Switch · out of toleranceGEAR HANDLE WOULD NOT MOVE TO UP POSITION AFTER TAKEOFF. TROUBLESHOT L/G SYS AND FOUND THE LT & RT NLG PROXIMITY SWITCHES AND INBD & OTBD RT MLG PROXIMITY SWITCHES OUT OF TOLERANCES. ADJUSTED PROXIMITY SWITCHES TO WITHIN MINIMUM TOLERANCES AND PERFORMED SEVESDR DXTA2010102504269Window · crackedINNER MOST PANE OF DIRECT VISION CRACKED IN FLIGHT. CRACK IS ABOUT 20 INCHES LONG. REMOVED WINDOW AND INSTALLED NEW WINDOW. OPS CHECKED WINDOW HEAT SYS WITH NO DEFECTS. PRESSURIZED ACFT TO 4PSI AND LEAK CHECKED WINDOW WITH NO DEFECTS. ALL WORK ACCOMPLISHESDR 2010FA0001055Mount · delaminatedREMOVAL OF THE APU IS REQUIRED FOR COMPLETION OF SB THAT REPLACES THE APU FIREWALL. UPON DISASSEMBLY OF THE APU FROM THE APU SUPPORT TRUSS, FOUND SHOCK MOUNT DELAMINATING. INSPECTING OF THIS AREA WAS DETERIORATE UNTIL THE NEXT INSP INTERVAL FOR THIS PART. TSDR DXTA2010091304235Fire Bottle · dischargedNR 1 ENGINE FIRE BOTTLE INADVERTENTLY DISCHARGED IN FLIGHT. IT`S THE MIDDLE BOTTLE IN THE AFT SERVICE COMPARTMENT. CHECKED CARTRIDGE FIRING CIRCUIT FOR VOLTAGE AND FOUND NONE. REPLACED THE LT FIRE EXTINGUISHER AND ENGINE EXTINGUISHER CARTRIDGES. CONDUCTED TSDR DXTA2010091304231Brake · malfunctionedUPON TAXI OUT/BACK DISCOVERED ACFT PULLING TO LT. THIS CONDITION EXISTS WHETHER STEERING IS ENGAGED OR NOT. WHEN BRAKES ARE APPLIED TOGETHER USING EMERGENCY BRAKE OR PEDAL BRAKES, THE ACFT WILL TRACK STRAIGHT. WHEN BRAKES ARE APPLIED, A SQUEAKING/DRAGGING SOUNSDR 2010FA0001008Disc · failedDEFECT REPORTED AS BRAKE BINDING/OVERHEATING BRAKE UNIT S/N AUG86-2471. REMOVED BRAKE UNIT FITTING. FAST TAXI TEST CARRIED OUT. THE BRAKE LOCKED UP, WHEEL REMOVED OVERHEATING AGAIN EVIDENT & ROTATING DISC FELL OUT IN PIECES. BOTH BRAKES WERE O/H USING NEWSDR DXTA201009070422Proximity Switch · out of adjustAFTER TAKEOFF, WHEN RAISING THE LANDING GEAR, THE RT MLG DID NOT RAISE BUT THE NOSEWHEEL AND THE LT MLG RAISED, THEN THE LT MAIN CAME BACK DOWN. AT THAT TIME WE HAD LT AND RT GREEN ARROWS AND RED LIGHTS, AND NO RED OR GREEN NLG LIGHTS, NO FLASHING GEAR HANDLE SDR DXTA10082304201AControl Unit · faultyDURING ENROUTE CLIMB, PASSING FL300, AMBER BRAKE ILLUMINATED ON MWP WITH ASSOCIATED AMBER MASTER WARNING LIGHT. ALSO MX PANEL RED MINELCO ON RT BRAKE. DURING GEAR EXTENTION, AMBER BRAKE LGT EXTINGUISHED, THEN ILLUMINATED WITHIN 3 TO 5 SECONDS AFTER ANTI-SKIDSDR DXTA2010082404201Warning Light · illuminatedDURING ENROUTE CLIMB PASSING FL300 AMBER BRAKE ILLUMINATED ON MWP WITH ASSOCIATED AMBER MASTER WARNING LIGHT. ALSO, MX PANEL RED MINELCO ON RT BRAKE. DURING GEAR EXTENSION, AMBER BRAKE LIGHT EXTINGUISHED, THEN ILLUMINATED WITHIN 3 TO 5 SECONDS AFTER ANTI-SKIDSDR CA100903002Oil System · pressure lossIFSD, PILOT COMMANDED PILOT REPORTED THAT DURING FINAL APPROACH FOR LANDING, THE RT ENGINE OIL PRESSURE DROPPED DOWN SUDDENLY. PILOT SHUTDOWN THE ENGINE AS A PRECAUTION WHILE TAXIING.SDR DXTA2010080504185Brake Sys · malfunctionedAMBER BRAKE LIGHT COMES ON AFTER GEAR EXTENSION. LT BRAKE MENELCO RED. 329C, NR1 ELECTROSERVO FAILURE, BRAKES WERE A LITTLE LESS RESPONSIVE ON LT SIDE.SDR CA100817004Engine · failedDURING FLIGHT, WHILE AT CRUISE AT 40K, PILOT WITNESSED OIL FILTER IMPENDING BYPASS MESSAGE FOLLOWED BY DROP IN OIL PRESSURE TO 65PSI THEN 48PSI AND FINALLY 20PSI. PILOT SHUTDOWN THE ENGINE AND DECLARED AN EMERGENCY. ACFT LANDED WITHOUT INCIDENT.SDR DXTA2010072604175Computer · inoperativePILOT'S FLIGHT DIRECTOR FAILED IN FLIGHT AND COPILOT'S YD/MT LIGHT CAME ON AT SAME TIME. COPILOT'S FLIGHT DIRECTOR FAILED UPON LANDING. R & R NR1 AND NR 2 FCC-4002, FLIGHT CONTROL COMPUTERS AND PERFORMED GROUND OPS CHECKS IAW MM 34-022. NR 1 AND 2 FCC COMPUTESDR DXTA2010072104167Relay · inoperativePERFORMING THE EMERGENCY CHECKLIST FOR A LT WHEEL OVHT, MLG FAILED TO RETRACT. SEQUENCE STOPPED WITH 3 RED & 2 GREEN GEAR LIGHTS (GREEN WERE LT & RT MAINS) & MLG HANDLE FLASHING. DID NOT HEAR ANY MOVEMENT OF MLG IAW CHECKLIST, EXTENDED MLG & GOT 3 GREEN & NO SDR DXTA2010072004162Warning Light · illuminatedAMBER PITCH FEEL AFTER T/O LEAVING 5000 FT AT 240 KNOTS. DID NOT FEEL ANY CONTROL CHANGES. INSTALLED BREALEASH BOX TO SWITCH. ACCESSED FAULT HISTORY & FOUND NO FAULT CODES. PERFORMED TEST OF PITCH ARTHUR IAW MM 27-308 UPON MOVEMENT OF HORIZ STAB TO +1 DEG 15SDR DXTA2010052404098Uplock · malfunctionedAFTER TAKEOFF, DURING LANDING GEAR UP, WE GOT A GEAR UNSAFE INDICATION ALL (3) RED LIGHTS AND A FLASHING RED GEAR HANDLE. RETURNED TO AIRPORT GEAR DOWN WITH ALL INDICATIONS NORMAL (3) GREEN NO RED. REPLACED DEFECTIVE NLG UPLOCK ASSY IAW MM 32-322. OPS AND LEASDR 2010F00124Pin · loose((JGVR)) INFORMED BY API OF AN INCIDENT REPORTED TO THEM BY THE ACFT OPERATOR. THE REPORT TELLS OF A LOOSE PIN IN THE CONNECTOR THAT RESULTED IN AN INTERMITTENT FAULT INDICATION FOR THE NR 1 HYD PUMP SYS. IT APPEARS THE NR 11 PIN HAD PUSHED BACK EVEN THOUGHSDR DXTA2010042604074Engine · vibrationLT ENGINE ROLLED BACK TO IDLE AT FL430. ITT ROSE TO A YELLOW INDICATION ABOUT 875. SOME VIBRATION, ABOUT 24 ON VIB INDICATION. LANDED WITH ENGINE AT IDLE. R & R NR 1 ENGINE.SDR DXTA2010032604054Circuit Board · malfunctionedON GEAR EXTENTION AT 3000 AGL, FLAPS 10 GEAR DOOR LIGHTS AND GEAR LIGHTS NORMAL CYCLE INDICATIONS, HOWEVER GEAR HANDLE LIGHT FLASHING RED WITH ORAL GEAR WARNING. THIS CONDITION CONTINUED WITH FLAPS 20 AND FLAPS 40 AND AIRSPEEDS BTWN 155 - 170 KTS. CYCLED GEAR SDR DXTA2010032304046Servo Valve · defectiveRT BRAKE GRABS MUCH SOONER THAN THE LT BRAKE. DETERMINED RT BRAKE SERVO VALVE R251GC TO BE DEFECTIVE. REMOVED DEFECTIVE VALVE AND INSTALLED REPAIRED VALVE. BLED BRAKE SYS, OPS AND LEAK CHECKS GOOD. WORK ACCOMPLISHED IAW MM 32-418 AND 32-419.SDR DXTA2010022404001Pin · worn(ORIGINAL SUBMISSION DATE: 02/24/2010)
AFTER TAKEOFF, WHEN THE GEAR WAS SELECTED UP, A LOUD BANGING NOISE WAS HEARD ON LWR LT SIDE OF CAPTAINS SEAT AND SIDE PANEL. BANGING NOISE WAS CONSTANT UNTIL EXCELERATED PAST 160 KNOTS WHERE THE NOISE BECAME LOUDER BUTSDR DXTA2010022203999Squat Switch · malfunctionedAFTER TAKEOFF, GEAR WOULD NOT RETRACT. NOSE GEAR RED LIGHT WENT OUT, BOTH LT AND RT MAIN GEAR GREEN AND RED LIGHTS REMAINED ON WITH THE FLASHING GEAR HANDLE. ALL INDICATIONS NORMAL DURING GEAR EXTENSION. TROUBLESHOT SYS AND COULD NOT DUPLICATE. SERVICED NLGSDR DXTA2010021503985Engine · failedON TAXI, LT ENG ROLLED BACK TO COMPLETE FAILURE. NO MESSAGES, NO POPPED C/B`S, ALL ELECTRIC, IGNITION & PNEUMATIC SWITCHES IN NORMAL POSITION. ONLY INDICATIONS WERE: FAILED ENGINE, OIL, HYD, & GEN LIGHTS ILLUMINATED. ENVIRONMENTAL CONDITIONS AT TIME WERE VERY SDR DXTA2010F00035Warning System · malfunctionedON TAKEOFF, RED DOORS MASTER WARNING ILLUMINATED WITH AUDIBLE BELL, EXTINGUISHED IT 3 TIMES AND WOULD ILLUMINATE WITH GONG AGAIN. 4TH TRY IT EXTINGUISHGED AND WE LANDED WITHOUT INCIDENT. SMOOTH LANDING. LANDING WEIGHT 35200 LBS, 700 OVER MAX LANDING WEIGHT. RASDR DXTA2010021003978Line · disconnectedCOMPLETE LOSS OF NR 1 HYD SYS. INVESTIGATED FAILURE OF THE NR 1 HYD SYS AND FOUND THE SYS SUPPLY LINE FROM THE NR 1 SYS HYD ACCUMULATOR TO BE DISCONNECTED AT THE ACCUMULATOR AND AT THE OTHER END OF THE LINE. REPLACED LINE WITH NEW LINE. REPLACED NR 1 ENG SYSDR 2010F00028Warning Light · illuminatedAFTER A NORMAL TAKE-OFF THE F1A AND F1B "IMPENDING FUEL FILTER BY-PASS" ANNUNCIATED ON THE NR2 EIED. AFTER LANDING THE APU OIL TEST WAS INITIATED AND THE LT ENGINE "CHIP DETECTOR" INDICATOR ILLUMINATED "YELLOW" DURING THE TEST. INDICATOR RETURNED TO GREEN UPOSDR DXTA2010011103938Proximity Sensor · intermittentRT MLG FAILED TO RETRACT. FAULT CODE 415, BRAKE 2, COMPUTER STRUT PROXIMITY SWITCH FAILURE SHOWING. LANDED WITHOUT FURTHER INCIDENT. TROUBLESHOT SYS AND COULD NOT DUPLICATE DISCREPANCY. REPLACED PROXIMITY SWITCH 45GA WITH CUSTOMER SUPPLIED PART IAW MM 32-600SDR DXTA2010011103939Brake Sys · malfunctionedWHILE AT A SLOW TAXI AFTER LANDING WITH BRAKE PRESSURE APPLIED, THE BRAKE PRESSURE SEEMS TO RELEASE TEMPORARILY. NO BREAK MONELCOS TRIPPED. BLED ALL BRAKES TO ENSURE SYS IS FREE OF AIR. TAXIED ACFT BEFORE AND AFTER BLEEDING BRAKES ALL OPS CHECKS GOOD. WORK PSDR DXTA2009122103907Control Unit · inoperativeSHORTLY AFTER TAKEOFF THE LT EXT LIGHT AND RT EXT LIGHTS CIRCUIT BREAKERS POPPED AND THE ODOR OF ELECTRICAL SMOKE WAS NOTICED. T/S SYS. FOUND PULSE LIGHT CONTROL UNIT TO HAVE FAILED DUE TO EXPOSURE TO WATER. REMOVED AND REPLACED CONTROL UNIT WITH MODIFIED USDR 2009F00144Elt · false activationELT ACTIVATED AT FL410 AND STAYED ACTIVE UNTIL RESET AT MFG.SDR DXTA2009121403896Proximity Switch · inoperativeUPON GEAR RETRACTION BOTH MAIN GEAR REMAINED EXTENDED WITH GREEN MAIN GEAR LIGHTS AND RED MAIN GEAR DOOR LIGHTS ILLUMINATED. THE PROCEDURES IN THE 'LANDING GEAR ABNORMAL RETRACTION" CHECKLIST WERE FOLLOWED. GEAR EXTENDED NORMALLY, BUT UPON RETRACTION THE MAIN SDR DXTA2009111103854Servo Valve · inoperativeBRAKES GRAB, BOTH LEFT & RIGHT. REMOVED AND REPLACED LEAKING NR1 LT BRAKE SERVO VALVE WITH REPAIRED VALVE IAW W/C 32-418. BLED BRAKES IAW W/C 32-419. OPS TEST GOOD. CREW TAXIED ACFT. BRAKING REPORTED TO BE NORMAL. FOR DETAILS REF FAS WO 09-2945.SDR CA091103008Actuator · faulted(CAN) FUNCTIONAL CHECK OF THE HYD SHUT-OFF VALVES DETECTED A FAILURE OF THE NR 2 ENG FUEL SHUT-OFF VALVE STANDBY ACTUATOR. (THE 2 VALVES ARE WIRED IN SERIES.) THE INTERNAL SWITCH AND STANDBY MOTOR WINDINGS CIRCUIT SHOWS OPEN. ACTUATOR WAS REPLACED AND FAULT CSDR 2009FA0001073Pin · misinstalledREPORT TELLS THAT A FAULTY WIRING CIRCUIT CAUSED THE ACFT TO LOSE SLATS EXTENSION DURING A PRE-FLIGHT INSPECTION OF THE SLAT "STALL 2 TEST". IT APPEARS THAT THE NR 14 FEMALE CONNECTOR PIN ON THE CONNECTOR FOR PCB 414JE WAS NOT FULLY ENGAGED OR "SNAPPED" INTOSDR 2009FA0000983Module · malfunctionedPART RECEIVED FROM MFG AFTER "FUNCTIONAL TEST". THE PART WAS SHIPPED UNPROTECTED IN A SHIPPING CONTAINER. INSTALLED IN ACFT, SEVERAL CLEARABLE FAULTS APPEARED AND THE FOLLOWING FAULT CODE CAS MESSAGE "ANLGVZLAB ERR" 2130CPS001 WAS NOT CLEARABLE. AFTER TROUBSDR DXTA2009100703807Skin · puncturedDURING AIRCRAFT EXTERIOR INSPECTION FOUND 3" BOLT LODGED IN RT IB FLAP. BOLT PENETRATED THROUGH UPPER AND LOWER SKIN OF FLAP. REMOVED RIGHT INBD FLAP FOR REPAIR. INSTALLED NEW SKIN PANEL IAW SRM 51-10-04, 51-30-05, 51-30-07, AND MM 20-321. APPLIED PAINT FINISDR CA091110009Hydromech Unit · failed(CAN) TWICE DURING CLIMB THE LT ENG PWR ROLLED BACK. CREW REPOSITIONED THE THROTTLE AND POWER WAS RESTORED. REMAINDER OF THE FLIGHT WAS NORMAL. UPON ARRIVAL AT HOME BASE THE CREW REPORTED THE EVENT. MX CONDUCTED TROUBLESHOOTING INCLUDING INTERROGATION OF THESDR DXTA2009091603788Fire Detector · intermittentYELLOW FAULT LIGHT ON THE FIRE WARNING ILLUMINATED AT 3000 MSL, THEN EXTINGUISHED UPON LANDING. REMOVED AND REPLACED RT ENGINE FIRE/OVERHEAT DETECTOR WITH A NEW UNIT. PERFORMED A OPERATIONAL CHECK OF LOOP, OPS CHECKS GOOD. ALL WORK ACCOMPLISHED IAW MM 26-100.SDR DXTA2009090803778Circuit Board · defectiveCABIN DID NOT PRESSURIZE AFTER TAKEOFF. WHITE CAS MESSAGE "CABIN RATE" CAME ON DURING EACH CLIMB SEGMENT. REPLACED DEFECTIVE PRINTED CIRCUIT BOAD IAW MM 45-60-21. 32-600 AND 21-302. OPS CHECK GOOD.SDR DXTA2009083103769Monitor · odorPAX SMELLED SMOKE NEAR THE SIDE VALANCE AT THE MID CABIN. BURNING ODOR SEEMED TO GO AWAY WHEN LIGHTS WERE TURNED OFF. NO ODOR NOTICED IN REAR BAGGAGE, JUST IN MID CABIN AREA. REMOVED AND REPLACED CABIN MONITOR PER MM 25-000. OPS CHECK GOOD.SDR DXTA2009082403765Pressure Switch · malfunctionedFUEL-1 LIGHT ILLUMINATES IN FLIGHT CLIMB/CRUISE/DESCENT. LIGHT REMAINS ON AFTER XBP OPEN AND LT BOOST PUMP TURNED OFF. REMOVED LT FUEL PRESSURE SWITCH AND INSTALLED A NEW CUSOTMER SUPPLIED PRESSURE SWITCH. OPS AND LEAK CHECK GOOD. ALL WORK DONE IAW MM CH 28-SDR ZY8R20110722001Unknown · noisyEXPERIENCED AUDIBLE NOISE APPROX 2 HOURS IN TO ACOUSTIC ANALYSIS TEST FLIGHT THAT WAS BOTH HEARD AND DETECTED. THE NOISE RESONATED BETWEEN 70 AND 80 DECIBELS. AFTER REDUCING ENGINE POWER AND DESCENDING TO A LOWER ALTITUDE, THE NOISE WAS NO LONGER PRESENT.SDR DXTA2009071603730Landing Gear · failedAFTER NORMAL TAXI AND TAKEOFF, GEAR HANDLE WOULD NOT RELEASE (MULTIPLE ATTEMPTS). RETURNED FOR LANDING WITH "AUTOSLATS" ANNUCIATOR. APPEARED TO HAVE NOSEWHEEL STEERING UP TO CLEARING RUNWAY, AT K5, RAN OUT OF STEERING. LAST 1000 FT OF ROLLOUT, PLANE SHUTTERSDR JLT2009F00000Accessory Unit · damagedDURING A 75 HOURS SOAP SAMPLE AFTER MPI A WASHER WAS FOUND ON THE CHIP DETECTOR ON THE ACCESSORY GEAR CASE. IT WAS IDENTIFIED AS A WASHER FROM THE STARTER FAILURE THAT THE SHAFT CAUSED THE HOLDING PAD MOUNT TO BRAKE. THE LAST STARTER FAILURE WAS IN 2005. FRSDR DXTA2009070603718Unknown · odorSTRONG ODOR PRIMARILY ON CAPT SIDE OF COCKPIT. ELECTRICAL BURNING ODOR NOTICED ON ACFT SHUTDOWN. PULLED EFIS DISPLAYS AND FOUND ALL FANS CLEAN OF DEBRE AND OPERATION NORMAL. INSPECTED DV WINDOW HEAT CONNECTORS FOR ANY EVIDENCE OF ARCING, NOT FOUND. CHECKEDSDR DXTA2009070203714Monitor · odorA STRONG ELECTRICAL BURNING ODOR WAS NOTICED COMING FROM AREA NEAR GALLEY COAT CLOSET. MAIN CABIN AIRSHOW MONITOR CEASED TO FUNCTION. ON AFT BAGGAGE COMPARTMENT CB PANEL FWD MONITORS CB POPPED AND WAS NOT RESET. R & R CABIN VIDEO MONITOR WITH INSPECTED UNI
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