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 20000717SH002Seal · odorINSTALLED NEW ARAMID FIBER SEALS P/N F2MA721406020B1 IN THE CABIN HOT AIR CHECK VALVE ASSY (140HD) PER FALCON SERVICE NEWSLETTER NR 8, ATA 21, DATED 9-1999. THE VALVE IS LOCATED IN THE BAGG COMPT ON LT SIDE. ACFT APU WAS RUN, SYS OPER AND LEAK CHECKED, OKAY.SDR 20000717SH001Engine · failedFLL - AFTER TAKEOFF, CREW SELECTED GEAR UP. CREW HEARD A LOUD BANG AND THE RT ENGINE HAD AN UNCOMMANDED SHUT DOWN, CREW LANDED AIRCRAFT BACK AT FLL AND UPON POST-FLIGHT, DETERMINED ENGINE HAD AN UNCONTAINED FAILURE . FURTHER INVESTIGATION REVEALED ENGINE CORSDR 20000710SH001Valve · failedCREW NOTED AMBER ''CREW'' LIGHT ON WHILE ON THE GROUND. LIGHT WOULD GO OUT IN MANUAL MODE. CREW DEFERRED AUTOMATIC MODE PER MEL 21-13. RELOCATED AIRCRAFT TO LIT. FALCON JET SERVICE CENTER FOUND A FAILED COCKPIT TEMPERATURE CONTROL VALVE IN THE AIR CONDITIONSDR 20000623SH020Contactor · defectiveCREW NOTICED A HOT SMELL WHEN PILOT''S WINDSHIELD HEAT WAS ON DURING FLIGHT. CREW DEFERRED PILOT''S WINDSHIELD HEAT PER MEL 30-6. RELOCATED AIRCRAFT TO AGS. GARRETT AVIATION FOUND A DEFECTIVE CONTACTOR IN THE PILOT WINDSHIELD HEAT SYSTEM WIRING. REPLACEMENSDR 20000623SH019Control Valve · failedCREW NOTICED AMBER ''CREW'' LIGHT ON IN-FLIGHT AND AMBER ''PAX'' LIGHT ON UPON LANDING. CREW DEFERRED MANUAL MODE PER MEL 21-14. RELOCATED AIRCRAFT TO AGS. GARRETT AVIATION FOUND A FAILED COCKPIT TEMPERATURE CONTROL VALVE IN THE AIR CONDITIONING SYSTEM. RESDR 20000510SH028Line · looseRIGHT ENGINE NR 2 SYSTEM HYDRAULIC PRESSURE LINE BECAME UN-SWAGED AT OUTBOARD END CAUSING COMPLETE DRAINAGE OF NR 1 HYDRAULIC SYSTEM. THIS OCCURRED IN-FLIGHT. FURTHER INVESTIGATION REVEALED IMPROPER SWAGING. TUBE WAS INSTALLED APPROXIMATELY 1 WEEK PRIOR TO ISDR 20000517SH001Sensor · looseFLIGHT CREW REPORTED ENCOUNTERING COMPRESSOR STALLS AND AIRCRAFT YAW TO LEFT CLIMBING THROUGH FL 230. LEFT ENGINE CONTROLS MOVED TO FLIGHT IDLE AND SHUT DOWN LT ENGINE. FLIGHT DIVERTED TO LIT DASSAULT SERVICE CENTER. INVESTIGATION REVEALED T2 SENSOR CONNECTSDR 20000328SH018Duct · crackedFOUND LEFT ALTERNATOR INTAKE DUCT CRACKED DURING A ROUTINE 600-HOUR ENGINE INSPECTION. (X)SDR 99ZZZX3912Valve · failedCREW ATTEMPTED TO START APU DURING QUICK TURN AND APU FAILED TO START. TOPPING ON VALVE ENABLE APU START. VALVE WAS REPLACED WITH NEW WHEN AIRCRAFT RETURNED HOME. IF APU IS REQUIRED IN CERTAIN CIRCUMSTANCES, IT MAY OR MAY NOT START DUE TO THE UNRELIABLE VALSDR 99ZZZX3913Valve · failedAFATER LANDING FOLLOWING A LONG FLIGHT AT FL 430, CREW ATTEMPTED TO START APU FOR A QUICK TURN. APU FAILED TO START. THEREFORE, LEFT NR 2 ENGINE RUNNING FOR CROSSBLEED START. TROUBLESHOOTING REVEALED THAT FUEL SOLENOID VALVE FAILED TO OPEN WHEN COMMANDED BYSDR 99ZZZX2212Proximity Switch · malfunctionedFLIGHT CREW SELECTED LANDING GEAR DOWN AND GOT THREE RED LIGHTS ON THE ANNUNCIATOR PANEL. AFTER A DELAY, THE LEFT MAIN AND RIGHT MAIN GEAR EXTENDED, BUT NOT THE NOSE. THE GEAR WAS EMERGENCY DEPLOYED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WASSDR 20000717SH019Chip Detector · contaminatedTWENTY MINUTES AFTER TAKEOFF, CREW WAS ALERTED BY A NR 1 ENGINE ''OIL'' LIGHT ON MASTER CAUTION PANEL. OIL PRESSURE WAS NORMAL. AIRCRAFT RETURNED TO HOME BASE (MMU). ENGINE CHIP DETECTOR INSPECTION REVEALED A CHIP ABOUT .1250 INCH LONG. DRAINED OIL FROM GEASDR 98ZZZX4185Battery Pack · disdchargedWHILE REPLACING AN EMERGENCY LIGHT BATTERY PACK, AN EXCHANGE UNIT WAS PURCHASED FROM FALCON JET (TEB). THE EXCHANGE UNIT WAS DISCHARGED WHEN RECEIVED, ALL OTHERS IN STOCK WERE ALSO FOUND DISCHARGED. THE ORIGINAL WAS STILL SERVICEABLE AND RE-INSTALLED IN THE SDR 98ZZZX4037Battery Pack · dischargedWHILE REPLACING AN EMERGENCY LIGHT BATTERY PACK, AN ECHANGE UNIT WAS PURCHASED FROM FALCON JET (TEB). THE EXCHANGE UNIT WAS DISCHARGED WHEN RECEIVED. ALL OTHERS IN STOCK WERE ALSO FOUND DISCHARGED. THE ORIGINAL WAS STILL SERVICEABLE AND RE-INSTALLED IN THE SDR 98ZZZX4026Actuator · failedRIGHT INBOARD FLAP DRIVE FAILED CAUSING UNSYMMETRICAL FLAP DEPLOYMENT INDUCING A CONTROLLABLE ROLL MOMENT. SUBMITTER SUGGESTED CAUSE AS PREMATURE WEAR.SDR 98ZZZX4187Water Tank · leakingTANK SPLITS OPEN AND LEAKS WATER INTO BELLY OF AIRCRAFT. FAILURES OCCUR ON END CAPS AND APPEAR TO BE DUE TO OBVIOUS MANUFACTURING DEFECTS. THIS IS THE THIRD FAILURE OPERATOR HAS EXPERIENCED.SDR CS1R075KDoor · not securedDURING TAKEOFF, ROLL DOOR WARNING ILLUMINATED AND CREW ABORTED TAKEOFF. AIRCRAFT RETURNED TO RAMP AND INSPECTION DETERMINED THE EMERGENCY EXIT WAS NOT FULLY SECURED.SDR 98ZZZX157Power Supply · failedON A TRANS-OCEANIC FLIGHT, THE NR 1 FMS CIRCUIT BREAKER TRIPPED. UPON RESETTING BY THE AIR CREW, THE NR 1 FMS COMPUTER BEGAN TO SMOKE. AIR CREW SHUT DOWN UNIT. UNIT RETURNED TO MANUFACTURER FOR REPAIRS. REPAIR BY MANUFACTURER REVEALED THE FAILURE WAS CAUSESDR 97ZZZX4256Harness · chafedFADEC WIRING HARNESS CHAFED WHERE IT PASSES THROUGH CLAMP. SUBMITTER STATED CLAMP NEEDS CUSHION TO PREVENT WIRE FROM BEING DAMAGED.SDR 97ZZZX2682Engine · failedRIGHT ENGINE COMPLETELY FAILED AFTER TAKEOFF AT APPROXIMATELY 200 FEET AGL. AFTER A SUCCESSFUL LANDING, ENGINE WAS EXAMINED AND FOUND THE FAN SEIZED; THE TURBINE BADLY DAMAGED. NO EVIDENCE OF FOD WAS FOUND. AWAITING EVALUATION FROM THE MANUFACTURER TO DETERSDR 97ZZZX2681Inlet · bolts looseAFTER ENGINE FAILURE, MORE THAN HALF THE BOLTS SECURING THE ENGINE INLET HA D UNSCREWED THEMSELVES. THE REMAINING WERE LOOSE. SUBMITTER SUSPECTS UNUSUAL ENGINE VIBRATION CAUSED THE BOLTS TO BACK OUT. THE INLET COULD POSSIBLY FALL OFF THE AIRCRAFT IN-FLIGHT.SDR 97ZZZX2485Line · crackedMAINTENANCE PERSONNEL NOTICED FUEL ON BOTTOM OF ENGINE COWL. FURTHER INVESTIGATION REVEALED A CRACKED WELD IN THE MAIN FUEL SUPPLY LINE WHERE THE FUEL PRESSURE SENDER IS LOCATED. LOCATION OF THE SENDER MAY IMPOSE UNDUE STRESS ON THE WELD.SDR JZBR14001Hmu · malfunctionINSTALLED HMU ON ENG FOR TEST AFTER C/W CFE 7388001. PERFORMED 2 NORMAL STARTS SATISFACTORILY. THE 3RD START ATTEMPT AND SUBSEQUENT ATTEMPTS FAILED. RE-INSTALLED ORIG HMU AND STARTS WERE NORMAL.SDR 96ZZZX5456Uplock · malfunctionLANDING GEAR DOORS WOULD NOT RETRACT AFTER GEAR UP SELECTED. RED LIGHTS ON GEAR PANEL WERE ON, GEAR HANDLE LIGHT FLASHING. THE CREW INDICATED THEY HAVE HAD SIMILAR PROBLEMS WITH THE LANDING GEAR ON THIS AIRCRAFT BEFORE. THEY REPLACED THE GEAR UPLOCK. UNABLSDR 96ZZZX5455Uplock · malfunctionLANDING GEAR DOORS WOULD NOT RETRACT AFTER GEAR UP SELECTED. RED LIGHTS ON GEAR PANEL WERE ON, GEAR HANDLE LIGHT FLASHING. THE CREW INDICATED THEY HAVE HAD SIMILAR PROBLEMS WITH THE LANDING GEAR ON THIS AIRCRAFT BEFORE. THEY REPLACED THE GEAR UPLOCK. UNABLSDR 96ZZZX5454Uplock · malfunctionLANDING GEAR DOORS WOULD NOT RETRACT AFTER GEAR UP SELECTED. RED LIGHTS ON GEAR PANEL WERE ON, GEAR HANDLE LIGHT FLASHING. THE CREW INDICATED THEY HAVE HAD SIMILAR PROBLEMS WITH THE LANDING GEAR ON THIS AIRCRAFT BEFORE. THEY REPLACED THE GEAR UPLOCK. UNABLSDR 96ZZZX2898Windshield · delaminatedPILOT'S FRONT WINDSHIELD OUTER PLY DELAMINATED AT FL 450. AN UNEVENTFUL EMERGENCY DESCENT AND LANDING WAS PERFORMED INTO WICHITA, KS. WINDSHIELD WAS SUBSEQUENTLY REPLACED AND AIRCRAFT RETURNED TO SERVICE.
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