Dassault FALCON 7X
Service difficulty reports · 56
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 = 'FALCON7X' 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 = 'FALCON7X' 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 2026FA0000521Actuator · unsecureDURING REMOVAL OF THE WING LOWER SURFACE REMOVABLE PANELS (T57-10-01-90-801-01/02 ENCLOSED), AND ESPECIALLY DURING REMOVAL OF ACCESS PANELS (PARAGRAPH 3.E.FIG 2), TECHNICIANS NOTICED THAT SCREWS WERE NOT TIGHTENED CORRECTLY ON THE RH MIDDLE SLAT OUTBOARD HOOK SDR 2026FA0000246Power Supply · looseDURING APPLICATION OF SB F7X-630 ON AIRCRAFT, FOUND FEEDER (0V) NUT OF BACK UP WINDSHIELD DE-ICING POWER SUPPLY M1001DG NOT TIGHT.SDR 2026FA0000148Generator · failedPIREP: N369CA SN 087 DEPARTED KHOU TO KIAD. DURING AIRCRAFT CLIMB THE PILOT IDENTIFIED AN AMBER CAS MESSAGE. "ELEC: GEN 2 FAULT". THE CREW ACCOMPLISHED THE ASSOCIATED CHECKLIST. THE PILOT DECLARED AN EMERGENCY WITH ATC AND REQUESTED IMMEDIATE VECTORS FOR RETURSDR 2026FA0000146Fuel Tank · misinstalledFOLLOWING REMOVAL OF BOTH WINGS FOR CENTRAL WING PANELS REPLACEMENT, ACCESSES ARE PERFORMED IN THE FEEDER TANKS. PIPES, BRACKETS, PUMPS WERE REMOVED. DURING THESE ACCESSES, COMPONENTS IN THE FEEDERS TANKS ARE DISCOVERED INSTALLED WITHOUT PRC & PAINT PROTECTIONSDR 2026FA0000127Fuel Sys · contaminatedPOLLUTION FOUND IN FUEL TANKS AFTER REMOVAL OF BOTH WINGS - FOLLOWING REMOVAL OF BOTH WINGS FOR REPLACEMENT OF LOWER PANELS AFTER 2C INSPECTION PERFORMED IN 2025, WE FOUND CONTAMINATION IN THE WINGS, IN THE CENTRE TANK, IN THE THREE FEEDERS’ TANKS, IN THE FILTSDR 2026FA0000092Fuel Filter · misinstalledDURING INSPECTION/CLEANING OF THE FUEL FILTERS, THE FILTER OF THE BOOSTER PUMP 2 WAS DISCOVERED IN THE HYDRAULIC BAY, BETWEEN HYDRAULIC PIPES. FILTER WAS NOT INSTALLED AS PER AMM.SDR 2026FA0000062Wire Harness · chafedAIRCRAFT CURRENTLY IN MAINTENANCE. DURING REMOVAL OF FUEL GAUGE 1203 QJ FOUND FUEL TANK CENTER FUSE C1 HARNESS WITH SIGN OF CHAFING.SDR 2025FA0000838Housing · wrong partRH4 CABIN SEAT ROLLER HOUSING IS WRONG MANUFACTURING SPEC. COMPLIED WITH B/E AEROSPACE NTO-431193-001 REV A. CHANGE THE IDENTIFIED CORNERS OF FLOOR FITTING P/N 431193-15. COLLINS DRAWING 431193-15 REV D.SDR 2025FA0000680Pump · malfunctionedCREW REPORT - N927CA SN 279 DEPARTED KPHL TO KBCT. ENROUTE TO KBCT THE PILOT IDENTIFIED A HYDRAULIC PUMP FAIL ON THE B SYSTEM. THE CREW PERFORMED CHECK LIST. THE CREW CONTINUED ON THE FLIGHT PATH AND THIRTY TO FORTY MINUTES LATER, THEY LOST ALL FLUID IN THE BSDR 2024FA0000432Clamp · separatedDURING SCHEDULED "2C" INSPECTION FOUND RIGHT INBD WING ANTI ICE DISTRIBUTION SYSTEM PIPE AT THE VICINITY OF RIBO1 CLAMP (REF IPC 30-11-40-20 ITEM 140A) FAILURE AND COMPLETE SEPARATION FROM PIPE PREVENTING WING ANTI ICE HEAT TO INBD LEADING EDGE AND ALLOWING UNSDR OCC82024031900025Power Supply · failedMAU#1 CHANNEL B CIRCUIT BREAKER WAS POPPING OUT AND WHEN TROUBLESHOOTING FOUND THE MAU#1. POWER SUPPLY #2 PCB BURNT INTERNALLY CAUSING THE SYSTEM TO GO OFF LINE.SDR 2023FA0000407Engine · stalledIN CRUISE THE # 1 ENGINE DID AN UNCOMMANDED SHUTDOWN. THE CREW RESTARTED THE ENGINE BUT OBSERVED THAT THE ITT WAS HIGHER THAN THE OTHER ENGINES. THE POWER LEVER FOR THE # 1 ENGINE WAS BROUGHT BACK TO IDLE AND THE AIRCRAFT DIVERTED TO KTEB.SDR K5SR202306270001Control Unit · faultyAIRCRAFT N988NW FALCON 7X S/N 174 DEPARTED SLC RUNWAY 35. ALL NORMAL FROM POWER UP, ACCELERATION, LIFT-OFF. AT GEAR RETRACTION, WE GOT AN CAS MESSAGE “GEAR: RETRACT FAIL” FOLLOWED CLOSELY BY “GEAR: DOOR NOT CLOSED” AND “BRAKE: BOTH SYSTEMS FAIL”. THEY COULD ALSDR 9JLA2023032239213Power Supply · defectiveTHE FLIGHT CREW REPORTED THAT UPON AIRCRAFT POWER UP RECEIVING AN EMERGENCY LIGHTS NO1 BATTERY FAIL FAULT MESSAGE. THE MAINTENANCE TEAM FOUND THE NO1 EMERGENCY POWER SUPPLY WAS DEFECTIVE. THE UNIT WAS REMOVED AND REPLACED WITH A REPAIRED POWER SUPPLY. OPS CHECSDR 9JLA2022112339206Pitot Head · failedFLIGHT CREW REPORTED THAT DURING FLIGHT RECEIVING AN ADS MESSAGE THAT THE NO1 AIR DATA PITOT PROBE HEAT HAD FAILED. THE MAINTENANCE PROVIDER CONFIRMED THE DISCREPANCY AND REMOVED AND REPLACED THE NO1 PITOT PROBE WITH ARE REPAIRED UNIT. OPS CHECKS WERE SATISFACSDR 9JLA2022120139205Generator · faultedTHE FLIGHT CREW REPORTED THAT THE NO3 ENGINE GENERATOR FAILED DURING CLIMB AFTER TAKEOFF. THE FLIGHT CREW ELECTED TO RETURN BACK TO THE AIRPORT AND LAND SO THE MAINTENANCE TEAM COULD EVALUATE. THE BASE MAINTENANCE TEAM CONFIRMED DISCREPANCY AND REPLACED THE GESDR 2022F00399Gearbox · crackedRECEIVED WO TO PERFORM FWD HYD PUMP SEAL REPLACEMENT ON GEARBOX ENG#3 DUE TO SUSPECT ENGINE OIL LEAK. NOTED HYD LEAK INSTEAD OF OIL LEAK. NOTED ALSO LOWER ENGINE COWL ENGINE OIL CONTAMINATED.
PERFORMED ENGINE RUN UP AND FOUND CRACK ON GEARBOX.SDR 2022FA0000503Receiver · unreliableWEATHER RADAR DOES NOT WORK PROPERLY WE HAVE REMOVED AND REPLACED RTU 4X GETTING OUR ORIGINAL BACK MINUS MOD S. OUR ORIGINAL UNIT FAILED. PRIOR TO OPERATION IT WAS WORKING FINE. THE AIRCRAFT WAS PAINTED IN JANUARY 2019 AT DASSAULT FACTORY PAINT SHOP MERIGNAC FSDR 2022FA0000504Receiver · unreliableWEATHER RADAR DOES NOT WORK PROPERLY WE HAVE REMOVED AND REPLACED RTU 4X GETTING OUR ORIGINAL BACK MINUS MOD S. OUR ORIGINAL UNIT FAILED. PRIOR TO OPERATION IT WAS WORKING FINE. THE AIRCRAFT WAS PAINTED IN JANUARY 2019 AT DASSAULT FACTORY PAINT SHOP MERIGNAC FSDR CWQA20220303001Pcb · failedDURING APPROACH CREW RECEIVED BAG FAN FAULT (CAUTION), FOLLOWED BY AFT DIST BOX OVHT (WARNING CAS MESSAGE).
EMERGENCY DECLARED, CHECKLIST FOLLOWED AND UNEVENTFUL LANDING PERFORMED.
MESSAGES WENT AWAY SHORTLY AFTER RAT DEPLOYMENT IAW CHECKLIST.
MAINTENANCE ESDR QV1Y2021111117971Oxygen System · leakingF7X S/N 033 REGISTRATION N7X WAS INDUCTED AT JET AVIATION BASEL UNDER PROJECT BN7X0002 TO TROUBLESHOOT A SUSPECTED PASSENGERS OXYGEN LEAK. THE TROUBLESHOOTING PERFORMED UNDER PROJECT BN7X0002 WORK ORDER 4000 CONFIRMED THAT THE ELECTRICAL FLOW CONTROL UNIT (EFCSDR CWQA20211028001Pump · leakingDURING CRUISE, CREW RECEIVED HYD A LOW QUANTITY MESSAGE. CHECKLIST FOLLOWED, DEACTIVATED HYD A PUMP, EMERGENCY DECLARED, MANUAL GEAR EXTENSION PERFORMED, AND UNEVENTFUL LANDING PERFORMED.
MAINTENANCE REMOVED AND REPLACED LEAKING #1 ENGINE HYDRAULIC A1 PUMP, SDR CWQA20210122001Control Unit · malfunctionedDURING APPROACH CREW SELECTED SLATS AND FLAPS FIRST POSITION SF1, FOLLOWED BY FLAP FAIL AND FLAP ASYMMETRY MESSAGE. CHECKLIST FOLLOWED, EMERGENCY DECLARED, AND UNEVENTFUL LANDING PERFORMED. MAINTENANCE EVALUATION COULD NOT DUPLICATE PROBLEM, FLAPS INSPECTIONSDR JGVR20201118001Bolt · shortN55LC REJECTED TAKEOFF ON 16 NOV 2020 DUE TO THRUST REVERSER CAS MESSAGE WITH TO POWER APPLIED (THRUST REVERSER NOT STOWED). REMOVED LOWER T/R ACTUATOR ACCESS PANEL AND NOTED LOWER "S HOOK" BOLT HAD FALLEN OUT, NOT ALLOWING S HOOK TO OPEN AND T/R TO FULLY STOSDR 2020FA0000452Life Raft · partial deployDURING REMOVAL OF THE NUMBER THREE LIFE RAFT FOR OVERHAUL, ONE OF THE BREAK AWAY BANDS BROKE AND THE RAFT PARTIALLY INFLATED ON THE HANGAR FLOOR. ONLY HALF OF THE RAFT INFLATED AND THE OTHER HALF WAS STUCK TO THE OPEN PORTION OF THE RAFT. THE RAFT WAS LAST OSDR 2020FA0000121Terminal · damagedTHE SUPPLY CABLE AND POSITIVE TERMINAL ON THE LT WINDSHIELD DEICING POWER SUPPLY, L1001DG, PN16N24334 HAD BEEN SEVERELY HEAT DAMAGED. THE THREE DEICING POWER SUPPLIES WERE REPLACED FOR AN UPGRADE ON 23 MARCH 2017. REMOVE AND REPLACED DAMAGED POWER SUPPLY. RSDR CA190731004Seal · failed(CAN) DURING FLIGHT, NO. 3 ENGINE STARTED TO SURGE AND THE SURGING ACCOMPANIED BY FLUCTUATION IN ENGINES PARAMETERS. THE CREW ALSO FELT VIBRATION AND ELECTED TO DIVERT AND LANDED UNEVENTFULLY. AFTER TROUBLESHOOTING AND DATA REVIEW, THE ENGINE WILL BE REMOVE DUSDR CA190808011Engine · vibration(CAN) ON JULY 19 2109 AFTER DEPARTURE LEVELING OFF AT FL200 APPROXIMATE 15 MIN INTO THE FLIGHT, THE CREW HEARD A LOUD BANG ON THE STARBOARD SIDE OF THE AIRCRAFT AND IMMEDIATELY THE AIRCRAFT YAWED TO THE RIGHT AND "HIGH VIB #3" WAS DISPLAYED ON THE CAS. THE PILSDR BKEA2019070200001Control Unit · malfunctionedAPPROXIMATELY AT 12:00 PM I ARRIVED AT KHPN FROM A FLIGHT FROM KATL, AND RENTED A VEHICLE TO KTEB TO ANSWER A CALL FOR MAINTENANCE OVERSITE ON AIRCRAFT S/N-036. THE PIC DECLARED AN EMERGENCY ON LANDING INTO KTEB AIRPORT FROM KOXC AIRPORT. UPON LANDING WITH EMESDR CA190426001Engine · vibration(CAN) THE CREW REPORTED A HIGH VIBRATION CAS MESSAGE WAS RECEIVED ON #3 ENGINE WHEN THE THROTTLES WERE ADVANCED (PRIOR TO TAKE-OFF). THE TAKE-OFF WAS ABORTED JUST AS THEY STARTED TO ROLL, WELL BELOW V1. TROUBLESHOOTING IS GOING ON. (TC# 20190426001)SDR BKEA201904010001Cabin Pressure · malfunctionedAIRCRAFT DEPARTED, ONCE THE THE AIRCRAFT HAD REACHED ALTITUDE ABOVE FL350, UNABLE TO KEEP PRESSURE CONTROL EITHER VIA AUTO OR MANUAL, CABIN CLIMB OR DESCENT VARIES AT ABOUT 450FPM.BELOW FL340 NORMAL OPS.AIRCRAFT RETURNED TO FOR REPAIRSSDR 7P9A2019F00108Quick Disconnect · misinstalledSHORTLY AFTER REACHING CRUISE LEVEL 40 MINUTES INTO THE FLIGHT THE HYD THE CAPTAIN NOTICED THE SYNOPTIC PAGE DISPLAYED A SPIKE ON THE HYDRAULIC PRESSURE. ABOUT 10-15 LATER (50 TO 55 MINUTES INTO THE FLIGHT) THE CREW STATED A HYD A LOW QTY, FOLLOWED BY HYD A LOSDR 2018FA0000012Warning Message · illuminatedCLIMBING THROUGH A THICK OVERCAST. TURNED ALL ENG AND WING ANTI-ICE ON AT APPROXIMATELY 9000FT. CAME OUT OF CLOUDS BETWEEN FL 330 AND FL 340. IN THE PROCESS OF TURNING THE ANTI-ICE SYS OFF, THE WING ANTI-ICE WAS TURNED OFF FIRST. THE INSTANT THE WING ANTI-SDR 2017FA0000538Valve · failedTHE PARK EMERGENCY VALVE IS THE LAST REVERSIONARY MANUAL MECHANICAL BACK UP IN CASE OF BRAKE BY WIRE OR TOTAL HYDRAULIC FAILURE. THIS VALVE WAS INSTALLED ON AUGUST 16 2017. IT CAME FROM SPARES IN A REPAIRED CONDITION FROM A VENDOR FAA REPAIR STATION. THREE SDR 2017FA0000537Valve · failedTHE PARK EMERGENCY VALVE IS THE LAST REVERSIONARY MANUAL MECHANICAL BACK UP IN CASE OF BRAKE BY WIRE OR TOTAL HYDRAULIC FAILURE. THIS VALVE WAS INSTALLED AUGUST 30 2017. IT CAME FROM SPARES IN AN OVERHAULED CONDITION FROM A VENDOR FAA REPAIR STATION. TWO WESDR CA151125001Check Valve · dirty(CAN) DURING FLIGHT, THE CREW GOT A HIGH OIL PRESSURE WARNING ON NR 2 ENGINE. THE FLIGHT WAS DIVERTED WHERE IT LANDED SAFELY. ACFT MFG PERSONNEL CLEANED THE OIL PRESSURE CHECK VALVE AND THE ACFT WAS RELEASED FOR SERVICE.SDR CA151031006Filter · bypassing(CAN) CREW REPORTS AN ENGINE NR 3 FUEL FILTER BYPASS AND A SLOW ACCELERATION DURING TAKEOFF. THE FUEL FILTER WAS REPLACED AND AFTER A GROUND RUN UP OF 10 MIN. AT N1:80 PERCENT, NO MORE MESSAGE.SDR CA151007002Engine · unknown(CAN) AN ABORTED TAKEOFF DUE TO HIGH ITT ON NR 2 ENGINE. TROUBLESHOOTING ONGOING. CUSTOMER CONFIRMED THAT THEY HAD SURGE BEFORE THE EVENT.SDR CA150727001Oil System · low pressure(CAN) THE ACFT HAD AN ISSUE WITH NR 3 ENGINE OIL PRESSURE RUNNING MUCH HIGHER THAN NR 1 & 2 ENGINES. THE ACFT WAS DIVERTED. PRELIMINARY RESULTS REVEALED, CARBON IN THE PRESSURE ACTUATING VALVE, PAV. TROUBLESHOOTING ONGOING.SDR CA150306008Warning System · activated(CAN) A CHIP DETECTOR INDICATION WAS OBSERVED IN FLIGHT. THE CREW ELECTED TO RETURN TO THE AIRPORT OF ORIGIN TO INVESTIGATE. TROUBLESHOOTING ON GOING.SDR 2015FA0000022Wheel · vibrationCREW REPORTED VIBRATION FROM NOSE WHEELS AFTER TAKEOFF. CREW CALLED TOWER AND RETURNED TO BASE WITHOUT INCIDENT.SDR CA150120013Engine · malfunctioned(CAN) DURING CLIMB, PILOT REPORTED A LOUD NOISE AND NR 1 ENGINE VIBRATIONS. REDUCED POWER, VIBRATIONS REDUCED. TRIED TO PUT A LITTLE MORE POWER, VIBRATIONS INCREASED. RETURNED TO DEPARTURE AIRPORT. THE PRELIMINARY TROUBLESHOOTING REVEALED A LARGE TRACE OF OISDR CA141010007Engine · overtemp(CAN) DURING CLIMB PILOT NOTED ITT EXCEEDANCE, REDUCED THRUST.SDR CA140804004Engine · malfunctioned(CAN) DURING TAXI, THE PILOTS RECEIVED A CAUTION MESSAGE ASSOCIATED WITH FAULT CODE P3 SENSOR MIS-COMPARE ON NR 2 ENGINE. ACFT RETURNED TO HANGAR FOR TROUBLESHOOTING AND THE FAULT COULD NOT BE REPRODUCED. ON THE FOLLOWING FLIGHT, DURING CLIMB AT FL120 WHEN POSDR CA140630007Autothrottle Sys · malfunctioned(CAN) WHILE IN CRUISE, THE PILOTS REPORTED THAT ON 2 OCCASIONS THE NR 2 ENGINE THROTTLE, AUTO THROTTLE MODE, MOVED BACK UN-COMMANDED WHILE THE ALL 3 ENGINE PARAMETERS REMAINED UNCHANGED. MFG IS AWAITING ENGINE DATA DOWNLOAD FOR TROUBLESHOOTING PURPOSES. MFGSDR CA140314003Engine · fluctuatesAFTER CLIMBING TO THEIR ASSIGNED ALTITUDE AT FL400 AND INCREASING SPEED TO MAX CRUISE, THE CREW HEARD 2 LOUD NOISES. AT THE SAME TIME THEY SAW THAT ENGINE 2 PARAMETERS WERE FLUCTUATING INCLUDING DECREASING ROTOR SPEED AND RAPID TEMPERATURE INCREASE. A TEMP EXSDR CA140117005Engine · failed(CAN) IT WAS REPORTED THAT WHILE IN CRUISE, THE ENGINE NO1 HAD A CHIP LIGHT WARNING, THE VIBRATION LEVEL BECAME HIGH AND A HUMMING NOISE COULD BE HEARD. THE CREW SHUTDOWN THE ENGINE IAW CHECKLIST AND LANDED SAFELY. THE ENGINE WILL BE REMOVED FOR INVESTIGATIONSDR 2013FA0000665Feeder Cable · overheatedGENERATOR FEEDER CABLE, WHICH TERMINATES AT FRAME 46 BULKHEAD CONNECTOR, HAD OVERHEATED.SDR CA130128012Oil System · low pressure(CAN) THE PILOT SHUTDOWN THE NR 2 ENGINE DUE TO A LOW OIL PRESSURE INDICATION. THE FSR REQUESTED A CHIP DETECTOR, OIL FILTER INSPECTIONS AND ENGINE DATA DOWNLOAD. AWAITING RESULTS.SDR CA130117004Engine · malfunctioned(CAN) DURING REVENUE FLIGHT, A FEW MINUTES AFTER TAKEOFF, THE PILOT NOTICED AN HIGH OIL PRESSURE IN THE RED BAND. THE PILOT REDUCED POWER AND EACH SUBSEQUENT TENTATIVE TO INCREASE POWER, THE MOP WAS CLIMBING IN THE RED ZONE. THE ENGINE WAS SHUTDOWN BY THE PIL
Back to Dassault FALCON 7X