Dassault FALCON 900
Service difficulty reports · 144
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 = 'FALCON900' 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 = 'FALCON900' 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 CA030428008Seal · cracked(CAN) WHILE PERFORMING THE BASIC (MONTHLY) INSPECTION, FOUND SEAL/SHIELD P/N FGFB 583800308 CRACKED, BRACKETS BROKEN. BECAUSE OF THE BROKEN BRACKETS CAUSED THE SEAL/SHEILD TO CHAFE ON THE INNER FORWARD SKIN OF BOTH THRUST REVERSER DOORS IN THE STOWED POSITISDR 2003FA0000307Proximity Switch · failedAFTER TAKEOFF WHEN THE GEAR HANDLE WAS PLACED UP ALL THREE GREEN LIGHTS EXTINGUISHED. A LOUD METALLIC GRINDING TYPE NOISE WAS NOTED AFTER SEVERAL SECONDS (10-15) THE NOISE STOPPED AND THE GREEN LIGHT FOR THE NOSE GEAR ILLUMINATED. AT THIS TIME THE GEAR HANDLE SDR 2003FA0000316Proximity Switch · failedAFTER TAKEOFF WHEN THE GEAR HANDLE WAS PLACED UP ALL THREE GREEN LIGHTS EXTINGUISHED. ALOUD METALLIC GRINDING TYPE NOISE WAS NOTED AFTER SEVERAL SECONDS 10-15 THE NOISE STOPPED AND THE GREEN LIGHT FOR THE NOSE GEAR ILLUMINATED. AT THIS TIME THE GEAR HANDLE WASSDR 40002Proximity Switch · out of adjustLANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. CONFIRMED GEAR DOWN AND LANDED AT DEPARTURE AIRPORT. RAMP AND TAXIWAY WERE SNOW AND SLUSHY. RUNWAY WAS DRY. A FERRY PERMIT WAS OBTAINED TO GO TO MAINTENANCE. AIRCRAFT WAS JACKED UP, SWANG GEAR, WHERE NO DEFECTSDR 40001Proximity Switch · failedLANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED NOSE GEAR LEFT PROXIMITY SWITCH (3GF). ALL WORK DONE IN ACCORDANCE WITH M/M CHAPTERS 32-300, 32-611, AND 32-303. FUNCTION TEST OK.SDR 040Skin · gougedDURING SCHEDULED MAINTENANCE EVENT, FOUND GOUGING AND CHAFING PRESENT ON LT THRUST REVERSER DOOR SKIN. DAMAGE WAS MAPPED AND SENT TO MFG ENGINEERING FOR EVALUATION. MFG ENGINEERING DETERMINED DAMAGE IS NOT ACCEPTABLE, AND GRANTED EXTENSION FOR SERVICE PENDINSDR 2003FA0000026Line · crackedDURING CRUISE FLIGHT, NR 2 OIL LIGHT ON MASTER WARNING PANEL CAME ON. POWER LEVER WAS REDUCED TO IDLE, OIL PRESSURE INDICATION CONTINUED TO FALL TO LESS THAN 25 PSI, THIS TOOK APPROXIMATELY 15-20 SECONDS. CHECKLIST WAS CALLED, NR 2 ENGINE WAS SHUT DOWN. CREW SDR AUS20021000Coffeemaker · faulty(AUS) COFFEEMAKER FAILED. SMOKE AND FUMES EMANATING FROM COFFEE MAKER.SDR AUS20020999Bellcrank · failed(AUS) BAGGAGE COMPARTMENT DOOR BELLCRANK BROKEN. LOWER FUSELAGE PANEL TORN BY BROKEN BELLCRANK.SDR AUS20020872Roller · worn(AUS) LEADING EDGE SLAT ROLLERS WORN.SDR AUS20020659Display · faulty(AUS) ADVISORY DISPLAY FROZE. AIRCRAFT IS RAAF FALCON 900 A26-077.SDR AUS20020660Transmitter · faulty(AUS) RT ANGLE OF ATTACK TRANSMITTER FAULTY. INVESTIGATION FOUND THAT THE INTERNAL POTENTIOMETER WAS OPEN CIRCUITED. AIRCRAFT IS A RAAF FALCON 900 A26-076.SDR AUS20020862Acm · leaking(AUS) TURBOCOOLER LEAKING OIL. SUSPECT CAUSED BY INTERNAL SEAL FAILURE.SDR AUS20020662Controller · faulty(AUS) ATC CONTROLLER FAULTY. INVESTIGATION FOUND THE CONTROLLER HAD ANUNSERVICEABLE PHOTOELECTRIC CELL. AIRCRAFT IS AN RAAF FALCON 900A26-070.SDR AUS20020661Transmitter · faulty(AUS) RT ANGLE OF ATTACK TRANSMITTER FAULTY. INVESTIGATION FOUND THAT THE INTERNAL POTENTIOMETER WAS SHORT CIRCUITED. AIRCRAFT IS A RAAF FALCON 900 A26-073.SDR 2002FA0000587Retainer · brokenUPON AIRCRAFT ARRIVAL AND SUBSEQUENT SHUTDOWN, MECHANICS HEARD A SCRAPING AND A THUNKING SOUND FROM THE NR 1 ENGINE AS THE ENGINE WAS SPOOLING DOWN. WHEN THE FAN ASSY WAS TURNED BY HAND, THE SAME NOISES CAN BE HEARD AND FELT. INSPECTION OF THE OIL FILTER REVSDR AUS20020449Adc · faulty(AUS) AIR DATA COMPUTER (ADC) FAULTY.SDR AUS20020448Gauge · faulty(AUS) ENGINE ITT GAUGE DIGITAL READOUT DIFFERENT TO ANALOGUE READOUT.SDR AUS20020521Engine · overtemp(AUS) NR 2 ENGINE ITT EXCEEDED LIMITS.SDR CA020220010Starter Gen · failed(CAN) DURING START SEQUENCE, NR 2 ENGINE FAILED TO ROTATE, START SEQUENCE WAS CANCELLED, AND TRIED A SECOND TIME WITH NO ROTATION OF ENGINE. FAULT WAS TRACED TO THE STARTER GENERATOR, UNIT WAS REPLACED WITH A NEW AND START SEQUENCE WAS OK. NR 2 ENGINE STARTED SDR AUS20020522Proximity Switch · faulty(AUS) LT NOSE LANDING GEAR DOOR PROXIMITY SWITCH INTERMITTENT INOPERATION.SDR AUS20011444Compressor · leaking(AUS) AIR CONDITIONING SYSTEM TURBO COMPRESSOR OIL LOSS. SUSPECT CAUSED BY FAILURE OF AN INTERNAL SEAL. RAAF AIRCRAFT REGISTRATIONA26-074.SDR AUS20011105Wheel · cracked(AUS) MAIN WHEEL INBOARD HALF CRACKED ADJACENT TO BRAKE TANG. FOUND DURING EDDY CURRENT INSPECTION.SDR RO462097Stator · separatedENGINE RETURNED FOR MAINTENANCE WHEN AIRCRAFT WAS EXPERIENCING ENGINE TEMPERATURE LIMIT AT TAKE OFF AND SUBSEQUENT HUNG STARTS. THE INNER HUB OF THE 4TH LOW COMPRESSOR STATOR WAS FOUND SEPARATED DURING ENGINE MAINTENANCE DISASSEMBLY. MAJOR ENGINE COMPONENT DSDR AUS20011101Wheel · cracked(AUS) MAIN WHEEL INBOARD HALF CRACKED ADJACENT TO BRAKE TANG. FOUND USING EDDY CURRENT INSPECTION.SDR AUS20010900Indicator · failed(AUS) NR 1 ENGINE ITT INDICATOR INTERNAL FAILURE.SDR AUS20010899Transmitter · failed(AUS) NR 3 ENGINE OIL PRESSURE TRANSMITTER FAULTY.SDR AUS20011104Wheel · cracked(AUS) MAIN WHEEL INBOARD HALF CRACKED ADJACENT TO BRAKE TANG. FOUND DURING EDDY CURRENT INSPECTION.SDR JGV2001F00012Bearing Cage · corrodedDURING NOSE GEAR INSTALLATION INSPECTION OF BALL JOINT FOUND CORROSION ON OUTBOARD DIAMETER OF BEARING CAGE. NO OBVIOUS SIGNS OF CORROSION PROTECTION DURING ORIGINAL INSTALLATION. PROBABLE CAUSE: WHEEL WELL ENVIRONMENT WITHOUT USE OF CORROSION PROTECTION.SDR AUS20011103Wheel · cracked(AUS) MAIN WHEEL INBOARD HALF CRACKED ADJACENT TO BRAKE TANG. FOUND DURING EDDY CURRENT INSPECTION.SDR AUS20011102Wheel · cracked(AUS) MAIN WHEEL INBOARD HALF CRACKED ADJACENT TO BRAKE TANG. FOUND DURING EDDY CURRENT INSPECTION.SDR AUS20010653Clevis · cracked(AUS) MAIN ENTRY DOOR COMPENSATING SPRING CLEVIS CRACKED ACROSS ALL THREE CABLE ATTACHMENT LUGS. AIRCRAFT SERIAL NUMBER A26-074.FLEET INSPECTION FOUNDTHE CLEVIS CRACKED ON ALL OTHER AIRCRAFTIN THE RAAF FLEET. THIS DEFECT WAS RECEIVED FROM THE RAAF AND ISENTERESDR AUS20010589Oxygen Mask · leaking(AUS) PILOTS OXYGEN MASK LEAKING AT OXYGEN SUPPLY QUICK DISCONNECT. THIS DEFECT WAS RECEIVED FROM NO34 SQUADRON RAAF AND IS FOR INFORMATION ONLY. AIRCRAFT SERIAL A26-073.SDR 20010413CW010Battery · unapproved partTWO UNAUTHORIZED CELLS INSTALLED IN BATTERY BLOCK. UNAUTHORIZED CELLS REPLACEMENTS PERFORMED USING UNACCEPTABLE PRACTICES. RECOMMEND REPLACEMENT OF ENTIRE CELL BLOCK.SDR 20001018SH004Hydraulic Line · brokenDURING ROUTINE MAINTENANCE CHECK FLIGHT, CREW NOTICED NR 2 HYDRAULIC SYSTEM PRESSURE LOW. AIRCRAFT LANDED UNEVENTFULLY. INVESTIGATION FOUND HYDRAULIC LINE BROKEN AT B-NUT FITTING. CAUSE UNKNOWN. SUBMITTER STATED AT TIME OF THIS REPORT, NR 2 SYSTM WAS BEINGSDR 20000914SH015Hydraulic Line · brokenDURING ROUTINE MAINTENANCE CHECK FLIGHT, CREW NOTICED NR 2 HYDRAULIC SYSTEM PRESSURE LOW. AIRCRAFT LANDED UNEVENTFULLY. INVESTIGATION FOUND HYDRAULIC LINE FRACTURED NEAR B-NUT FITTING. CAUSE UNKNOWN. NEW LINE INSTALLED, SYSTEM SERVICED AND FUNCTION CHECKEDSDR 20000831SH014Screen · missingDURING AIRCRAFT INSPECTION FOUND PART OF APU INLET SCREEN MISSING PART OF ITS WIRE MESH. SUSPECTED PART WAS INGESTED BY APU DURING OPERATION. BORESCOPED APU INLET COMPRESSOR AND DAMAGE TO LEADING EDGES OF ALL THE BLADES WAS FOUND. THE APU INLET SCREEN IS THSDR 20000828SH033Skin · corrodedCORROSION OF FUSELAGE SKIN AT LOWER FRAME 10 UNDER FORWARD END OF PANEL 130A. THE DOMED HOTPLATES ARE RETAINING WATER. THIS PANEL IS REMOVED ONLY AT 2C INSPECTION. SUBMITTER RECOMMENDED REMOVAL AT EACH C-INSPECTION TO INSPECT FOR CORROSION. AC TT: 6,845.8SDR 20001113SH018Fire Detector · malfunctionedPILOT''S FLIGHT SQUAWK - ''BAG COMP FIRE WARNING LT CAME ON IN-FLIGHT AND EXTINGUISHED. ISOLATED BAG COMP WITH ''NO HEAT'' SWITCH. CONFIRMED NO FIRE''. SERVICE CENTER TROUBLESHOT TO FAULTY DETECTOR. (X)SDR 20000913SH036Skin · corrodedAIRCRAFT FUSELAGE SKIN AT APU EXHAUST BETWEEN FRAMES 33 AND 34 CORRODED. DAMAGED AREA REMOVED AND SKIN REPLACEMENT REPAIR DONE. (X)SDR 20000817SH028Wire · chafedACFT TT: 9,308.4 HOURS. CYCLES: 6,485. ACFT FERRIED FOR PURPOSE OF REPAIRING CHAFED WIRES ON LOWER SIDE OF LT NAV TRANSCEIVER TRAY LOCATED AT LT FRAME STA 10. ACFT EXPERIENCED AN ELECTRICAL FIRE AS A RESULT OF WIRE CHAFING ON THE TRAY. SEVERAL WIRES WERESDR 20000721SH025Skin · corrodedAIRCRAFT FUSELAGE SKIN AT APU EXHAUST BETWEEN FRAMES 33 AND 34 CORRODED. DAMAGED AREA WAS REMOVED AND SKIN REPLACEMENT REPAIR DONE. ACTT: 5,062.5 HOURS. (X)SDR 20000721SH022Skin · corrodedAIRCRAFT FUSELAGE SKIN AT APU EXHAUST BETWEEN FRAMES 33 AND 34 CORRODED. DAMAGED AREA WAS REMOVED AND SKIN REPLACEMENT REPAIR DONE. (X)SDR 20000721SH026Skin · corrodedCORROSION OF FUSELAGE SKIN AT LOWER FRAME 10 UNDER FORWARD END OF PANEL 130A. THE DOMED NUTPLATES ARE RETAINING WATER. THIS PANEL IS REMOVED ONLY AT 2C INSPECTION. SUBMITTER RECOMMENDED REMOVAL AT EACH C-INSPECTION TO INSPECT FOR CORROSION. ACTT: 5,062.5 SDR 20000721SH021Skin · corrodedCORROSION OF FUSELAGE SKIN AT TOWER FRAME 10 UNDER FORWARD END OF PANEL 130A. THE DOMED NUTPLATES ARE RETAINING WATER. THIS PANEL IS REMOVED ONLY AT 2C INSPECTION. SUBMITTER RECOMMENDED REMOVAL AT EACH C-INSPECTION TO INSPECT FOR CORROSION. ACTT: 4,868.6 SDR 20000620SH006Window · crackedWINDOW CRACKED IN-FLIGHT. (X)SDR 20000403SH007Retainer · brokenDISASSEMBLED ENGINE BECAUSE OF BAD S.O.A.P. SAMPLE. FOUND NR 3 SEAL RUNNER RETAINER BROKEN. (X)SDR 2000ZZZX624Cooling Fan · failedTWO HOURS AFTER TAKEOFF, A HEAVY ELECTRICAL ODOR AND SMELL WAS NOTICED BY THE CREW IN THE CENTER PEDESTAL AREA. A PRECAUTIONARY LANDING WAS EXECUTED. MAINTENANCE FOUND THE SOURCE OF THE SMOKE FROM THE NR 3 IRS COOLING FAN INVERTER. THE DEFECTIVE INVERTER ANSDR 2000ZZZX623Cooling Fan · failedTWO HOURS AFTER TAKEOFF, A HEAVY ELECTRICAL ODOR AND SMELL WAS NOTICED BY THE CREW IN THE CENTER PEDESTAL AREA. A PRECAUTIONARY LANDING WAS EXECUTED. MAINTENANCE FOUND THE SOURCE OF THE SMOKE FROM THE NR 3 IRS COOLING FAN INVERTER. THE DEFECTIVE INVERTER ANSDR CA000203009Power Supply · shorted(CAN) A NOISE WAS HEARD EMANATING FROM THE LT VALANCE LIGHTING. UPON INVESTIGATION, AN ELECTRICAL ARC WAS FOUND OCCURING BETWEEN 2 WIRES COMING OUT OF THE LIGHTING POWER SUPPLY.
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