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 DXTA200803068Yaw Damper · inoperativeDURING LEVEL FLIGHT, ACCELERATING THROUGH 250KT AT 10,000 FT, THE AC EXPERIENCED A SUDDEN YAW TO THE RT WITH THE TRIM INDICATOR AT ZERO. INSTALLED A NEW YAW DAMPER SVL-86A OPS CHECKED GOOD. ALL WORK DONE IAW F-2000 MM 22-105 22-104SDR UG8A08P050601Skin · corrodedMISSING PAINT WITH MINOR CORROSION ON MIDDLE RT WING, UNDER THE SLAT, AT THE WING LIFTING POINT. CORROSION IS LOCATED ON WING PLANK AT LIFT POINT IN MACHINED CUTOUT. CUTOUT IS FILLED WITH SEALANT. CORROSION LOCATED UNDER SEALANT ON WING PLANK. REMOVED CORRSDR DXTA200803041Warning Light · illuminatedDOORS LIGHT ON MWP CAME ON AT 80 KTS DURING TAKEOFF. ADJUSTED SECONDARY CATCH ON BAGGAGE DOOR PERFORMED A DOOR WARNING CHECK, OPS CHECK GOOD REF FALCON 2000 MM 52-701SDR DXTA200803023Line · disconnectedUNCOMMANDED SHUTDOWN OF NR 2 ENGINE BY FADEC AFTER STARTUP. TROUBLESHOT TO A DISCONNECTED PS AIR LINE AT THE H2B FADEC. CONNECTED LINE PERFORMED NUMEROUS ENGINE STARTS AND RUNS NO DISCREPANCIES NOTED. ENGINE OPERATIONAL CHECK GOOD. ALL WORK IAW MM 71-002 AND SDR DXTA200803018Sensor · inoperativeBLEED OVERHEAT LIGHT CAME ON 2 MIN AFTER TAKEOFF. CHECKLIST ACCOMPLISHED AND CREW WAS UNABLE TO ISOLATE THE MALFUNCTION. FAULT CODE 404 AND 428. BLEED OVERHEAT COMES ON WITH APU BLEED ON AND ENGINE OFF. REMOVED & REINSTALLED TEMP SENSOR L70HU. OPS & LEAK CHSDR DXTA200803008Actuator · inoperativeNORMAL TRIM SYS FAILED INFLIGHT AND WOULD NOT RE-ENGAGE, (ELEVATOR). REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR WITH A REPAIRED/MODIFIED ASSEMBLY PER MM W/C 27-406, 27-404.SDR CA080423012Oil System · leaking(CAN) AFTER TAKEOFF, THE CREW NOTED OIL SMELL FOLLOWED BY VISIBLE VAPOR IN THE CABIN AIR AND OIL PRESSURE GAUGE FLUCTUATIONS. THE FLIGHT WAS DIVERTED TO AN ALTERNATE LANDING SITE. THE ENGINE WAS SHUTDOWN FOLLOWING LANDING. OIL WAS OBSERVED INSIDE THE BYPASS DUSDR DXTA200802995Shroud · contaminatedSTRONG ODOR OF HOT OIL DURING DESCENT. EVALUATED AND FOUND BURNED OIL IN APU BLEED AIR SHROUD. REMOVED APU P/N 3800548-2 S/N P-295 AND INSTALLED REPAIRED UNIT P/N 3800548-2 S/N P-358 (T.T. 3165, CYCLES 3212). RUN UP, LEAK CHECK, AND OPERATIONAL CHECK GOOD. SDR DXTA200802980Unknown · multiple failDURING DESCENT, AP TRIM FAIL LIGHT ILLUMINATED WITH ASSOCIATED AMBER CAS MESSAGE. REPLACED STAB CONTROL RELAYS- 504CH, 505CH, 506CH & 507CH. REPLACED STAB CONTROL PCB'S 502CH & 503CH. OPS CHECKED STAB CONTROL RELAY BOX DUE TO RELAY AND PCB REPLACEMENT. INSPECSDR DXTA20082980Trim System · malfunctionedDURING DESCENT AP TRIM FAIL LIGHT ILLUMINATED WITH ASSOCIATED AMBER (E).SDR DXTA20082919Cooling Fan · malfunctionedUPON LANDING, RED TEMP FOR CAPTIANS MFD DISPLAYED. IN ADDITION A SLIGHT SMELL OF ELECTRICAL SMOKE WAS EVIDENT UPON SHUTDOWN OF AVIONICS. T/S FOUND PILOTS MFD COOLING FAN INOP. REMOVED INOP FAM AND INSTALLED A NEW FAN. OPS CHECK GOOD I/A/W DA2000 MM 34-001.
SDR DXTA20082910Switch · out of adjustRED DOOR LIGHT CAME ON DURING T/O ROLL, APPROXIMATELY 100 YRDS AFTER BRAKE RELEASE AND FULL POWER. INSPECTED CONDITION AND ADJUSTMENT OF ALL DOOR SWITCHES AND PROX SENSORS, FOUND BAGGAGE BAY FWD SWITCH (43MV) OUT OF ADJUSTMENT AND STICKING. ADJUSTED AND CLEANSDR DXTA20082881Bulb · burned outWHEN PUTTING THE LANDING GEAR CONTROL HANDLE DOWN, THE LT MAIN (2) GREEN DOWN INDICATORS FAIL TO BOTH LIGHT. THE BOTTOM LT WILL NOT LIGHT CONSISTENTLY AT GEAR EXTENSION UNLESS YOU WIGGLE THE LIGHT. REMOVED AND REPLACED BOTH BULBS OPS CHECKED GOOD. REF: MM SECSDR 2008FA0000071Lanyard · missingACCESS COVER FOR THE EMERGENCY WINDOW HANDLE DOES NOT HAVE A LANYARD WHEN IT IS REMOVED. THE COVER HANGS BY THE WIRING THAT ILLUMINATES IT PUTTING STRESS ON THE SOLDERED CONNECTIONS TO BREAK CAUSING EITHER AN INOPERATIVE EMERGENCY LIGHT OR A SHORT CAUSING MORSDR DXTA200802827Pressure Switch · malfunctionedWHEN MAIN BRAKES ARE RELEASED BRAKE PRESSURE ANNUNICATOR ILLUMINATES, CHECKED LT AND RT SIDE, ONLY ILLUMINATES FOR LT SIDE. LT BRAKE MINELCO RED + RT AILERON MINELCO RED. (M-2B) REMOVED PRESSURE SWITCH ON THE LT SIDE P/N 7G1042 S/N 723. INSTALLED A NEW SWISDR DXTA200802811Pcb · inoperativeINTERCEPTED ILS LOCALIZER WITH AUTOPILOT ENGAGED ABOUT 3 MILES BEFORE GLIDESLOPE INTERCEPT AUTOPILOT ABRUPTLY PITCHED DOWN 4 TO 5 DEGREES THEN UP A FEW DEGREES WITH A SMALL AMOUNT OF BANK. REPLACED 2B10C CARD AND CHECKED IAW A/C SYS MANUAL, COMPLETED IAW MM 22SDR DXTA200802795Circuit Board · damagedBRAKES DO NOT WORK PROGRESSIVELY. THEY GRAB OR RELEASE SUDDENLY WHEN PRESSED OR RELEASED. INSPECTED ALL GEAR UPLOCK SWITCHES WIRING, NO DEFECTS NOTED. CHECKED UPLOCK SWITCHES ADJUSTMENTS AND GEAR UPLOCK LINKAGE, NO DEFECTS NOTED. REPLACED LANDING GEAR CONTROLSDR DXTA200802766Uplock Switch · malfunctionedGEAR SELECTED UP, GEAR RETRACTED NORMALLY, 3 RED DOOR LIGHTS REMAINED ON WITH RED GEAR UNSAFE LIGHT FLASKING. FOUND NLG UPLOCK WITH BROKEN INTERNAL SPRING. R & R NLG UPLOCK WITH MODIFIED UNIT. LEAK, OPS, AND ADJUSTMENT TEST GOOD I/A/W FALCON 2000 MM 32-300SDR DXTA200802763Proximity Sensor · malfunctionedAFTER TAKEOFF AND GEAR HANDLE SELECTED TO THE GEAR RETRACTION POSITION. NOSE GEAR RETRACTION MOVEMENT WAS FELT AND HEARD. 2 RED MAIN GEAR LIGHTS (NO NOSE LIGHT) ALONG WITH A RED FLASHING HANDLE LIGHT OCCURRED. REMOVED AND REPLACED LT & RT MLG PROX SWITCHES SDR DXTA200802752Adc · malfunctionedDURING TAKEOFF, TEN SECONDS AFTER FULL POWER WAS SET (AUTO SLATS) MESSAGE APPEARED. REPLACED ADC-850C AIR DATA COMPUTER NR 1 WITH AN OVERHAULED UNIT PER F2000 MM 34-103. COMPLETED LEAK CHECKS PER F2000 MM 34-100 & FAR 91.411 WITH NO LEAKS NOTED. OPS CHECKEDSDR DXTA200702729Probe · inoperativeRT AUTO SLAT LIGHT AT ROTATION ALONG WITH STALL EYEBROW. NO OTHER ABNORMAL INDICATIONS. STALL EYEBROW INDICATION UNTIL 200 KTS. AUTO SLAT LIGHT WENT OUT 15 MIN INTO FLIGHT. REMOVED LT AOA PROBE AND INSTALLED A MODIFIED AOA PROBE IAW FALCON 2000 AMM 27-813.SDR DXTA200702716Terminal Block · damagedUPON POWER APPLICATION FOR TAKEOFF, TAKEOFF CONFIGURATION ANNUNICATOR ILLUMINATED ACCOMPANIED BY ORAL WARNING. CONFIRMED DISCREPANCY. T/S PROBLEM TO INTERMITTENT GROUND AT JUNCTION BLOCK 4JM. RESEALED ALL PINS. PERFORMED FUNCTIONAL TEST OF TAKE-OFF SAFETIESDR DXTA200702694Warning System · malfunctionedMLG HANDLE BEGAN FLASHING 2-3 MIN AFTER MLG SHOWED DOWN & LOCKED & CONTINUED FLASHING FOR APPROX 3-5 MIN. FOUND SQUAT DISAGREEMENT INDICATOR TRIPED ON FAULT DISPLAY UNIT. ACCESSED CONNECTORS PL008 & PR008 IN LT & RT WW & OHMED BOTH CONNECTORS & RESET INDICATSDR DXTA200702685Proximity Sensor · inoperativeLT MAIN GEAR FAILED TO RETRACT. TROUBLESHOT, FAULT CD 000315 PRESENT ON BSCU1 DURING GEAR SWING. REMOVED PROX SENSOR 40GAA P/N D23336000-1, S/N 02551 AND INSTALLED REPAIRED PROX SENSOR 40GAA P/N D23336000-1, S/N 02555 IN ACCORDANCE WITH F2000EX EASY MM 32-315SDR DXTA200702683Engine · failedHAD AN UNCOMMANDED NR 2 ENGINE FAILURE AT FL430. WE OBSERVED A FADEC 2 MWP LIGHT AND THEN AN UNCOMMANDED SHUTDOWN OF THE ENGINE. REPLACED A FAILED RT ENGINE PER THE MM 54-010, 54-104, 54-106, 54-107, 71-000, 71-015 AND THE ENGINE LMM 72-00-00, 72-00-08, 72-70SDR 2008FA0000255Circuit Breaker · misinstalledMAU 1B AND AGM 2 FAIL IN FLIGHT AND RECOVERED AFTER 3 SECONDS. SHUNT (IPC 24-05-10, ITEM 210) INSECURED ON BREAKER, ELECTRIC ARC. ONE SCREW ON BREAKER L501X, TOO THREAD LENGTH OVERSIZED. RESULTS: EXCHANGE SHUNT AND BREAKERS. (K)SDR DXTA200702645Landing Gear · malfunctionedGEAR WOULD NOT EXTEND NORMALLY, WITH GEAR HANDLE DOWN, ONLY MAIN GEAR DOORS OPENED. 2 CYCLES SAME RESULT. GEAR CAME DOWN WITH EMERGENCY GEAR HANDLE PULLED. INSP, FAULT CODE 435 PRESENT DURING GEAR SWING. REMOVED LANDING GEAR SELECT HANDLE P/N 307-39. S/N 212SDR DXTA200702632Hydraulic System · reads lowNR 1 HYDRAULIC SYSTEM QUANTITY INDICATED IN THE RED ZONE FOR QUANTITY DURING TAKEOFF RUN. ABORTED TAKEOFF ENSUED AS A RESULT OF LOW HYDRAULIC QUANTITY. SERVICED HYD SYSTEM IAW MM CH 29-112.SDR DXTA200702595Transmitter · inoperativeAT THE INITIATION OF THE TAKEOFF ROLL AND AT APPROXIMATELY 60 KTS THE YELLOW CAS MESSAGE AOA HEAT NR 2 ILLUMINATED. REMOVED AND REPLACED ANGLE OF ATTACK TRANSMITTER WITH REPAIRED UNIT AS REQUIRED. OPS CHECK GOOD. HEAT TEST GOOD AT THIS TIME. WORK IAW MM 27-804SDR DXTA200702571Condesor · odorAFTER LANDING AND APU START, VERY STRONG ODOR OF RAW JET FUEL IS COCKPIT AND CABIN. RAN APU. NOTED MUSTY ODOR COMING FROM VENTS. AFTER 2 MINUTES ODOR BEGAN TO DISIPATE. REMOVED AND INSPECTED THE WATER SEPERATOR AND THE WATER SEPERATOR FILTER. NO DISCREPANSDR DXTA200702556Accumulator · leakingDURING CLIMBOUT THE NR 1 HYDRAULIC SYSTEM INDICATION DROPPED TO 10 PERCENT ON QUANTITY AND PRESSURE DROPPED AS WELL. NOTED LEAK FROM LT T/R ACCUMULATOR TO FILTER ASSY. REPAIRED LEAK AND SERVICED SYSTEM 1 RESERVOIR. PERFORMED SYSTEM 1 HYDRAULIC OPERATION TEST WSDR DXTA200702530Isolation Valve · malfunctionedWHEN BRAKES ARE APPLIED DURING LOW SPEED TAXI, BRAKES WILL RELEASE INTERMITTENTLY. 10-29-07 REPLACED DEFECTIVE BRAKE ISOLATION VALVE WITH UNIT INSPECTED BY EATON FH3R501L. REPLACED DEFECTIVE BRAKE SERVO VAVE WITH UNIT REPAIRED BY APRO XPER689K IN ACCORDSDR DXTA200702515Brake Assy · intermittentAIRPLANE BRAKES WORKING INTERMITENTLY. POWERED UP AIRCRAFT AND INTERROGATED CMC. NO FAULTS FOUND FOR BRAKE SYSTEM OR CAS MESSAGE PRESENT. PERFORMED BRAKE PRESSURE CHECKS ON SYSTEM 1 AND 2. NO DEFECTS NOTED. BLED BOTH BRAKE SYSTEM. BRAKE SYSTEM OPS CHECK GOODSDR DXTA200702475Unknown · odorBURNING RUBBER ODOR ENTERS COCKPIT DURING CLIMB 17000 TO 19000 FT AND LASTS FOR 30-40 SECONDS THEN DISAPPEARS. NO SMOKE VISIBLE, SEEMS TO ORIGINATE FROM LT SIDE OF COCKPIT IN THE AUDIO PANEL AREA. 09-28-07 VISUALLY INSPECTED DV WINDOW ELECTRICAL CONTACTS, SDR DXTA200702430Fire Warning · false activationBAGGAGE COMPARTMENT FIRE WARNING LIGHT AND ARUAL WARNING WITH MASTER WARNING AND CAS MESSAGE. M2B INSPECTED SENSOR AND PERFORMED BAGGAGE BAY FIRE WARNING TEST IAW F2000 MM 26-103 NO DEFECT NOTED.SDR DXTA200702410Computer · malfunctionedAP TRIM FAIL ILLUMINATED WITH (E) DISPLAYED ON PFD. OCCURRED IN CLIMB THROUGH FL400. REPLACED LEFT AND RIGHT FCC-4002 FLIGHT CTRL COMPUTERS I/A/W F2000 MM 34-003. PERFORMED A/P FUNCTIONAL TEST W/ NO DISCREPANCIES NOTED, I/A/W F2000 MM 22-100.SDR DXTA200702420Windshield · failedAT FL430 AFTER APPOX. 4 HOURS OF FLT TIME, THE COPILOT'S FRONT WINDSCREEN SHATTERED BUT DID NOT BREAK AWAY COMPLETELY. NO PRESSURIZATION WAS LOST. REPLACED CO-PILOT'S FRONT WINDSCREEN PANEL WITH A NEW PANEL PER F2000 MM 56-102. OPS CHECK WINDSHIELD HEAT GOOD SDR DXTA200702351Oven · odorWHITE ODORLESS SMOKE POURS OUT OF THE GALLEY CONVECTIVE OVEN WHEN OPERATING. CLEANED OUT INSIDE OF OVEN. OPERATED AT HIGHEST TEMPERATURE SETTING FOR 15 MINUTES. VERY MINIMAL SMOKE NOTED AFTER CLEANING. IAW F2000 M/M 20-314SDR DXTA200702343Coffeemaker · smokeBURNING SMELL AND SMOKE COMING FROM THE COFFEE POT. ISOLATED COFFEE POT AREA FROM WALL AND CONTINUED WITHOUT FURTHER INSTANCE. REMOVED AND REPLACED WIRE TERMINALS TO COFFEE POT- CHECK WIRES WITH METER WIRES CHECK GOOD AT THIS TIME- INSTALLED SAME COFFEE POT- SDR DXTA200702334Brake · malfunctionedWHEN MAIN A/C BRAKES ARE APPLIED BRAKES WILL GRAB THEN RELEASE, THEN GRAB WHILE BRAKES ARE APPLIED SMOOTHLY. [07-23-07] PERFORMED BRAKE PRESSURE CHECKS AND FOUND NO ABNORMAL PRESSURES. IAW F2000 MM 32-412. FOUND FAULT CODES FOR BSCU NR 1 AND 2 AND FOUND SDR DXTA200702311Circuit Board · inoperativeIN FLIGHT AT FL 430, MASTER CAUTION LIGHT ILLUMINATED, ACCOMPANIED BY AUDIBLE GONG. (FLAP ASYSTEMMETRY) CAUTION LIGHT ILLUMINATED (5) SECONDS LATER FLAP CONTROL CIRCUIT BREAKER IN OVERHEAD C/B PANEL POPPED. LANDED NO FLAP. REPLACED PCB CARD (50WW) WITH A NEW SDR DXTA200702294Unknown · odorINTERMITTENT BURNING ODOR FROM COCKPIT AIR ON GROUND AND DURING CLIMB. [07-12-07] INSPECTED COOLING SYSTEM. NO DEFECTS NOTED. INSPECTED APU INLET. FOUND NUMEROUS CUCADA INSECTS COVERING THE INLET SCREEN. CLEANED APU INLET. RAN COOLING SYSTEM NO FURTHER ODORSDR DXTA200702288Flap System · inoperativeFLAPS DID NOT EXTEND WHEN COMMANDED. TRIED 10, 20, AND 40 DEGREES AND THE FLAPS NEVER MOVED. THE SLATS EXTENDED NORMALLY. [07-12-07] PERFORMED FUNCTION TEST OF SLAT POSITION DETECTORS AND FLAP POSITION MICRO SWITCHES IAW FALCON 2000 M.M. CHAPT 27-802, ALL RSDR DXTA200702278Unknown · unknownRECEIVED A YELLOW MASTER CAUTION WARNING LIGHT UPON THROTTLE ADVANCE FOR TAKEOFF. [07-11-07] COMPLIED WITH TAKE-OFF SAFTIES INDICATION LOGIC AND ALARM TEST WITH NO DEFECTS NOTED IAW MM 31-301 AND 31-301. COMPLIED WITH ENGINE RUN AND OPERATIONAL CHECKS OF PCBSDR DXTA200702250Dau · inoperativeWE GOT THE NO TAKE-OFF AURAL WARNING WITH NO TAKEOFF ANNUCIATE LIGHT ON TAKE OFF. REMOVED AND REPLACED DATA AQUISITION UNIT (DAU-4000) WITH OVERHAULED UNIT. PERFORMED OPS CHECK OF DAV AND TAKEOFF WARNING SYSTEM. OPS CHECK GOOD. WORKSDR DXTA200702230Transducer · malfunctionedWHEN BRAKING AT LOW TAXI SPEEDS THE LT BRAKE RELEASES AND THE AIRCRAFT WILL PULL TO THE RT. PERFORMED FUNCTIONAL CHECK OF ANTI-SKID SYSTEM, BOTH CHANNELS AND BOTH SYSTEMS ARE WORKING IAW M/M 32-414 CHECKED WIRING FROM BOTH BSCU'S TO ALL TRANDUCERS AND SERVO VSDR DXTA200702220Proximity Sensor · inoperativeLANDING GEAR WAS EXTENDED USING ABNORMAL GEAR EXTENSION CHECKLIST BECAUSE, UPON TAKEOFF AT GEAR RETRACTION NEITHER MAIN GEAR CAME UP. REMOVED LT GEAR DOOR PROX SWITCH PN 803682, SN1408 INSTALLED PN 84799031 SN 2047. REMOVED RT GEAR DOOR PROX SWITCH PN 803682SDR DXTA200702216Proximity Sensor · inoperativeRED NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. SELECTED GEAR DOWN AND GEAR EXTENDED NORMALLY. ALL INDICATIONS NORMAL.REMOVED INOP NOSE GEAR UPLOCK DETECTOR AND INSTALLED A NEW UNIT IAW CH 32-600 OF THE MM OPS CHECK GOOD.SDR DXTA200702209Control Unit · intermittentWHEN BRAKING THE AIRCRAFT TO A FULL STOP AT LOW TAXI SPEEDS, LT BRAKE RELEASED AS PRESSURE ON THE BRAKE PEDALS IS LESSENED TO PREVENT NOSE DIP. IS MOST PRONOUNCED WHEN PARKING OR HOLDING SHORT. REMOVED OLD NR 2 BSCU AND REPLACED WITH REPAIRED UNIT. OPERATIONALSDR DXTA200702204Landing Gear · malfunctionedWHEN GEAR HANDLE WAS PUT IN THE DOWN POSITION, NOTHING HAPPENED. (M2B) - PERFORMED FUNCTIONAL TEST OF EXTENSION AND RETRACTION OF LANDING GEARS AND DOORS, LANDING SAFETIES, AND MAIN DOOR PROX SWITCHES AND GEAR ACTUATOR PROX SWITCHES, AND DOOR UP LOCK AND GEAR
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