Dassault FALCON 10
Service difficulty reports · 134
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 = 'FALCON10' 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 = 'FALCON10' 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 CA050518015Embellisher · crackedEMBELLISHER ON RIGHT WHEEL IS CRACKED. RT EMBELLISHER REPLACED WITH NEW UNIT.SDR CA050608010Separator · making metal(CAN) DURING OIL CHANGE, METAL FOUND IN OIL AND FILTER. SOURCE OF METAL FOUND TO BE AIR/OIL SEPARATOR ALUMINUM LIGAMENTS. PART CHANGED AS PER SB TFE731-72-3696 TO NEWPART NUMBER 3075781-1.SDR CA050322009Flow Divider · leaking(CAN) DURING GROUND RUN, FUEL WAS OBSERVED TO BE LEAKING FROM THE RT AFT ENGINE AREA. THE PROBLEM WAS FOUND TO BE A LEAKING FUEL FLOW DIVIDER. THE PART WAS REPLACED, A SATISFACTORY GROUND RUN AND LEAK CHECK WAS CARRIED OUT AND THE AIRCRAFT WAS RETURNED TO SERVSDR 2005FA0000462Bolt · brokenA BROKEN BOLT WAS NOTICED DURING A TIRE PRESSURE CHECK. THE WHEEL COVER WAS REMOVED TO INVESTIGATE. ALL TEN BOLTS WERE NDT`D BY PAG PARTICLE INSP AND 3 OTHER BOLTS WERE FOUND CRACKED. PART CYCLES (LANDINGS) SINCE O/H IS 176 CSO. (K)SDR CA041222008Amplifier · inoperative(CAN) DURING FLIGHT, THE CREW NOTICED THAT THE RT FUEL QUANTITY GAUGE HAD DROPPED TO ZERO. THE LOW LEVEL LIGHT DID NOT ILLUMINATE, ASSURING THE CREW THAT THIS WAS AN INDICATION PROBLEM ONLY. THE RT QUANTITY AMPLIFIER WAS REPLACED AND THE SYSTEM WAS PROPERLY CSDR CA041222009Indicator · failed(CAN) DURING CRUISE FLIGHT THE RT FUEL FLOW GAUGE FAILED. GAUGE WAS REPLACED AND SYSTEM TESTED SERVICEABLE.SDR CA041222007Sensor · open(CAN) DURING PREFLIGHT CHECKS, THE LT ENGINE FIRE WARNING FAILED TO TEST. TROUBLESHOOTING REVEALED A FAILED FIRE LOOP. FIRE LOOP WAS REPLACED WITH NEW PRIOR TO FURTHER FLIGHT.SDR 2004FA0000908Hose · collapsedDURING ENGINE RUN-UP, PHYSICALLY CHECKED LEADING EDGE FOR HEAT AND FOUND COLD. RT IB ANTI-ICE FLEXHOSE WAS REMOVED AND VISUALLY INSPECTED. FOUND THE INNER LINING HAD COLLAPSED, BLOCKING AIRFLOW THROUGH HOSE. HOSE WAS REPLACED WITH NEW. FAULTY HOSE WAS MARKSDR PRI2004F00000Pump · inoperativeNR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILED IN FLIGHT. UPON REMOVAL OF FAILED PUMP. INSPECTION FOUND ONE PLUG O-RING HANGING OUT ALLOWING FLUID TO ESCAPE. (WP19200407082)SDR Q752004F00000Actuator · leakingDURING CLIMB OUT, SLATS RETRACTED NORMALLY. THEN A MASSIVE HYDRAULIC LEAK APPEARED ON OB LEFT WING. NR 1 HYDRAULIC SYSTEM BEGAN TO EMPTY. LANDING GEAR WAS LOWERED AND LANDING WAS MADE NORMALLY. AFTER INVESTIGATING PROBLEMS WAS LT, OB SLAT ACTUATOR. THE RESDR GQR2004F00000Pump · wornDURING FLIGHT CREW NOTICED THERE WAS A LARGE DISCREPANCY BETWEEN INDICATED FUEL QUANTITY AND AMOUNT OF FUEL USED AS SHOWN ON FLIGHT MANAGEMENT SYSTEM. UPON LANDING CREW NOTICED FUEL DRIPPING FROM SEVERAL AREAS ON THE UNDERSIDE OF THE AIRCRAFT. FUEL WAS FOUNDSDR 2004FA0000533Control Rod · chafedTIP FROM AUG 03 AC 43-16A RUDDER CONTROL ROD CHAFED. RUDDER CONTROL ROD CRANK AT FRAME NR 37. FOUND YAW DAMPNER ATTACHMENT PIN INSTALLED 180 DEGREE OUT. COTTER KEY AND NUT CHAFED THE ELEVATOR SERVO HYDRAULIC LINE, NO DAMAGE TO LINE NOTED. ID TAG GOUGED. CSDR R1765Pushrod Tube · chafedINSPECTED RUDDER PUSH-PULL TUBE IAW SDRS AND ALERTS ARTICLE IN AVIATION MAINTENANCE MAGAZINE DATED OCTOBER 2003. FOUND ELEVATOR SERVO PRESSURE LINE CHAFED RUDDER PUSH-PULL TUBE. SUSPECTED LINE WAS TIGHTENED WITH A PRELOAD THAT TWISTED THE LINE TO RUB THE TUBSDR UO22003F00003Altimeter · failedREMOVED UNIT FROM AIRCRAFT DUE TO UNIT LEAKING AND SHIPPED TO INSTRUMENT SERVICES, INC. FOR REPAIR. REINSTALLED UNIT AFTER REPAIR AND UNIT FAILED LEAK TEST. REMOVED UNIT AND WILL SENT UNIT BACK REPAIR STATION.SDR R1561Pushrod Tube · chafedDURING INSPECTION FOR HYDRAULIC SEEP AT BOTTOM OF RUDDER, FOUND ELEVATOR SERVO PRESSURE LINE CHAFFED THROUGH RUDDER PUSH-PULL TUBE. SUSPECTED LINE WAS TIGHTENED WITH A PRELOAD THAT TWISTED THE LINE TO CHAFE ON THE RUDDER PUSH-PULL TUBE. THE LINE WAS LOOSENEDSDR UO22003F00000Control Box · malfunctionedANTISKID TEST PROBLEM. INTERMITTENTLY, THE RIGHT LIGHT WOULD NOT COME ON DURING TEST. DISCONNECTED THE LT AND RT INPUT CONNECTORS FROM THE ANTISKID CONTROL BOX. ALL INPUTS TO THE BOX WERE CHECKED. NO DEFECTS WERE FOUND. TRIED ANTISKID TEST PUSHBUTTON. WHSDR WTX2003F00000Plug · meltedPILOT REPORTED NR 1 ENGINE WOULD NOT START DUE TO LACK OF STARTER ROTATION. TRACED PROBLEM TO MELTED STARTER/GENERATOR PYLON FEED THROUGH PLUG. OUTBOARD TERMINAL END OF PLUG AND TERMINAL END OF CABLE HAD MELTED. IAW SNL AND MM. (PTRS SW15200305957) 3456.SDR CA030107015Line · chafed(CAN) R/H ENGINE FLUCTUATING. OVERSHOOTING & CAUSING THROTTLE SPLIT IN ALTITUDE, LEAK CHECKED THE PRESSURE SENDING LINE FROM THE ENGINE COMPUTER TO THE ENGINE INLET PRESSURE & TEMPERATURE SENSOR (P2T2). FOUND LINE LEAKING IN PYLON. LINE WAS TOUCHING HARD AGAINSDR 2002FA0000690Turbine · damagedAFTER TAKEOFF AND DURING CLIMBOUT, THE PILOT EXPERIENCED A COMPUTER GENERATED AUTOMATIC ROLL BACK OF POWER ON THE NR 1 ENGINE. THE NR 2 ENGINE WAS BROUGHT BACK TO A MATCHING POWER SETTING. IT WAS THEN NOTICED THAT THE NR 1 ENGINE ITT WAS MORE THAN 100 DEGREESDR 2002FA0000580Line · chafedNR 1 HYDRAULIC SYSTEM LOST ALL FLUID ON FLIGHT. DISCOVERED HYDRAULIC LINE CHAFFED THROUGH. LINE HAD CHAFFED AGAINST ANOTHER LINE (PN F10A751127) IN AFT BAY. INSPECT SYSTEM COMPONENTS FOR POTENTIAL DAMAGE.SDR GLA2002F00000Bolt · backed outTAKEOFF, AC WAS CLIMBING THROUGH WHEN NR1 ENG CHIP DETECTOR/LOW PRES WARNING LIGHT ILLUMINATED. ENG WAS SHUT DOWN AND SAFE SINGLE ENG LANDING WAS MADE. INVESTIGATION REVEALED NR1 ENGINE OIL PUMP HAD RUPTURED AND FAN ASSY WOULD NOT ROTATE. ENG WAS REMOVED ANSDR CA020207001Squat Switch · contaminated(CAN) LOSS OF PRESSURIZATION AFTER TAKEOFF. RECTIFICATION: MOISTURE WAS FOUND ON THE LT LANDING GEAR SQUAT SWITCH 9G1. SUSPECT SQUAT SWITCH 9G1 WAS COLD SOAKED, CLEANED AND LUBED. PASSENGER OXYGEN MASK HAD NO OXYGEN FLOW. SYSTEM IS OPERATING IAW F10 MSDR JGV2001F00011Wheel · crackedDISASSEMBLED WHEEL TO INSPECT AFTER A CRACK WAS NOTED IN THE OUTBOARD WHEEL HALF. REMOVAL OF PAINT REVEALED A CRACK RADIATING FROM A LIGHTENING HOLE INWARD TOWARD THE BEARING RACE AT A 45 DEGREE ANGLE AND ABOUT 1.5 INCHES IN LENGTH. FURTHER INVESTIGATION REVSDR IY22001F00000Carbon Seal · failedBACKGROUND: POST SB CARBON SEALS HAVE COMMON PROBLEM WITH SEAL RUNNERS FAILING DUE TO CARBON BUILDUP. THE SEAL RUNNER IS MFG FROM CERAMIC MATERIAL AND TENDS TO BREAK DUE TO THIS CO-KING. RESULTS: TYPICAL DAMAGE SUSTAINED FROM THIS RUNNER FAILURE IS AS FOLSDR SW15200110653Carbon Seal · failedTHE NR 5 CARBON SEAL COKED AND FAILED CAUSING OIL STARVATION ON THE NR 5 BEARING WHICH SUBSEQUENTLY FAILED. THE CARBON SEAL WAS INSTALLED.SDR 20010322CW010Bearing · failedUNIT REMOVED FOR SEVERE VIBRATION. DRIVE END BEARING HAD FAILED. BEARING RACE WAS RUSTED IN LINER OF END BELL AND COULD NOT FLOAT. RECOMMEND LUBRICATION ON BEARING RACE WHEN INSTALLED.SDR CA010307008Controller · failed(CAN) NR 1 CONTROLLER INSTALLED PROBLEM IN DESCENT LOST PRESSURE ON/AT 4,000 FEET. NR 2 CONTROLLER INSTALLED UNIT WOULD NOT PRESSURIZE IN AIR. NR 3 OUR CONTROLLER REPAIRED. INSTALLED AND FLIGHT TESTED OK.SDR G1FR100YHose · failedAFTER COMPLETING A MFG 1200 HR B INSPECTION, A MAINTENANCE GROUND RUN OPERATIONAL CK OF THE WING ANTI-ICE SYSTEM WAS REQUIRED AND ACCOMPLISHED. NO HEAT WAS NOTICED AT RT OUTBOARD SLAT WITH ANTI-ICE WINGS SELECTED AND GREEN OPERATIONAL LIGHT ILLUMINATED. FURTSDR 20010212CW002Windshield · crackedAIRCRAFT DEPARTED CMI IN VFR CONDITIONS AND DURING CLIMB OUT THROUGH 15,000 FT, THE CO-PILOT''S FWD WINDSHIELD OUTER PANE CRACKED. PILOT ELECTED TO RETURN TO CMI. AIRCRAFT LANDED WITHOUT INCIDENT.SDR 20001227SH013Duct · damagedPILOT REPORTED THE WING DEICE SYSTEM WAS INOPERATIVE. AFTER VERIFYING ELEC PORTION OF SYS WAS FUNCTIONING, A GROUND OPER CHK PERFORMED. DISCOVERED VERY LITTLE FLOW GETTING TO RT SLATS, LT SLATS APPEARED TO BE GETTING SUFFICIENT HEAT, BUT BOTH SIDES ARE REQUISDR CA001128009Fuel Control · failed(CAN) RT ENGINE UNCONTROLLED ACCELERATION AFTER 10 MINS AT CRUISE ALT 39,000 DESCENDED DOWN TO 21,000 ENGINE OK HAD CONTROL.CHANGED (1) FCU, P/N 3076800-8 S/N ON A3538PT/OFF A 4778T(2) PT2 SENSOR P/N 3070816-4 (3) ENGINE COMPUTER P/N 949572-8 S/N ON 94-576/OFSDR CA001107022Tube · broken(CAN) WHILE TAXIING OUT FOR DEPARTURE, THE PILOTS WERE CONDUCTING FLIGHT CONTROL CHECKS AND FOUND CO-PILOTS R/H RUDDER PEDAL NOT RESPONDING PROPERLY. THE PILOT THEN PUSHED ON HIS RUDDER PEDAL. AFTER DOING SO, THE CO-PILOTS PEDALHAD NO EFFECT AT ALL. THE FLIGHTSDR CA001019011Bolt · wrong part(CAN) ENGINE AFTERBODY LT FOUND SEVERAL FASTENERS WERE NOT NAS 1303 PER FALCON 10 I.P.C. 54-22-05 PAGE 1-1 - INCORRECT HARDWARE, REPLACED BY CORRECT HARDWARE PER FALCON 10 IPC 54-22-05 PAGE 1-1.SDR 20000925SH002Tire · separatedNR 3 MLG TIRE TREAD SEPARATED FROM THE CASTING ON LANDING. TREAD DAMAGED UNDERSIDE OF RIGHT INBOARD FLAP AND RIGHT LOWER COWL. TIRE APPEARED TO BE PROPERLY INFLATED AND NOT EXCESSIVELY WORN. TIRE DID NOT DEFLATE AFTER SEPARATION. TIRE S/N 91570060. SUBMITSDR CA000801026Fuel Control · failed(CAN) LEFT ENGINE MAJOR POWER FLUCTUATION, COMPUTER OFF NO CHANGE. OIL PRESSURE LIGHT ON 10-15 SEC. OIL PRESSURE RECOVERED. HYD. PUMP DROP TO 2000 PSI TANK LIGHT ON. 1) ENGINE GROUND UN ADJ. (IDLE, ADJ.) 1/2 TURN FLUCTUATION STOPPED ON HIGH POWER.. OIL PRESSURSDR 20000523SH030Relay · failedDURING AIRFRAME INSPECTION, THE REVERSE CURRENT RELAY WAS REMOVED FOR INSPECTION AND RECERTIFICATION. THE RELAY, WHICH WAS FUNCTIONING NORMALLY WHEN REMOVED, WAS ROUTED TO A RATED REPAIR STATION FOR CHECK AND RECERTIFICATION. UPON RETURN FROM VENDOR, UNIT WASSDR 20000516SH017Flap Track · crackedDURING A 4A+ INSPECTION, 57-10-02 PAGE 601 STATES TO INSPECT THE NR 1 AND NR 3 FLAP TRACKS FOR CRACKS. FOUND NR 1 LT INBD TRACK TO HAVE A CRACK 70MM IN LENGTH AND LOWER TRACK FLANGE TO BE DISPLACED 15MM DOWNWARD. FALCON HAS A SB F-10-235 TO INSTALL STRONGERSDR CA000501017Actuator · failed(CAN) ON DECENT, FOUND HORIZONTAL STAB NORMAL MODE U/S. SELECTED EMERGENCY STAB AND LANDED.FOUND STAB ACTUATOR NORMAL MODE MOTOR U/S.SDR CA000222005Engine · leaking(CAN) OIL PRESSURE FLUCTUATIONS EXPERIENCED, POWER WAS REDUCED BUT OIL WARNING CAME ON. CORRECTIVE ACTION WAS TAKEN TO SHUT ENGINE DOWN. OIL QUANTITY DOWN 4 QUARTS. REPORT TO FOLLOW. OIL LOSS WAS DUE TO BREATHER VALVE LEAK AND VIBRATIONS WERE EXPERIENCED DSDR 2000ZZZX213Turbine Blade · failedONE EACH, THIRD STAGE LOW PRESSURE TURBINE BLADE FAILED DUE TO STRESS RUPTURE. AIRCRAFT LANDED SAFELY. POSSIBLE CAUSE WAS THE OPERATION OF BLADE IN EXCESS OF RECOMMENDED HOURS AS SET IN ALLIED SB 72-3494. RECOMMEND ENGINE MFG INCLUDE TURBINE BLADES IN SB 72SDR 99ZZZX4413Bracket · damagedSLAT (OUTBOARD) NR 3 RAIL MOUNT BRACKET ATTACHED TO SLAT RUBBING LEADING EDGE CAUSING DAMAGE TO THE BRACKET. THIS HAS ALSO BEEN NOTICED ON FALCON10, SN 131.SDR 99ZZZX4616Hydraulic Pump · failedTHE SERIAL NUMBERED PUMP WAS INSTALLED ON THIS ARICRAFT AS A REPLACEMENT OF AN OVERHAULED PUMP BY THIS VENDOR (THE ZEE CO) WHICH FAILED AFTER 157 HOURS OF OPERATION. THIS PUMP, SN AH-49579A, WAS IN OPERATION ONLY 87.9 HOURS BEFORE IT HAD A FAILURE WHICH CAUSEDSDR CA991209089Blade · missing(CAN) ENGINE AT OVERHAUL FACILITY, REPORT TO FOLLOW.SDR 99ZZZX4447Pump · failedIN 12-98 THIS S/N PUMP WAS INSTALLED ON ACFT AS REPLACEMENT. IN 9-99, THIS PUMP FAILED DURING RETURN TRIP. AFTER REMOVAL, PUMP CHECKED AND FOUND SHAFT ROTATING BUT NOT CONNECTED TO INTERNAL PUMP, SUSPECTED A SHEARED INTERNAL SHAFT. PUMP RETURNED TO VENDOR. SDR CA991007093Outflow Valve · failed(CAN) AIRCRAFT FAILED TO PRESSURIZE, AIR CONDITIONING VALVE FAILED CLOSED.SDR CA991007092Connecting Rod · failed(CAN) COMPRESSOR CONNECTING ROD FAILURE AT JOURNAL.SDR 99ZZZX4158Hinge · failedTHE PILOT REPORTED THERE WAS AN ABNORMAL 'THUMP' NOISE COMING FROM THE NOSE GEAR AREA WHEN THE GEAR WAS RETRACTED ON SEVERAL OCCASIONS. AN INVESTIGATION REVEALED THE CENTER RT NOSE LANDING GEAR DOOR BELLCRANK/HINGE WAS BROKEN IN HALF. AN INSPECTION OF THE ENSDR CA990915083Track · cracked(CAN) RIGHT INBOARD FLAP TRACK FOUND CRACKED. TRACK REPLACED.SDR 99ZZZX3322Bearing · failedOVERVOLTAGE CONDITION RESULTING IN OVERHEATING AND PARTIAL INTERNAL FAILURE OF STARTER/GENERATOR. SUBMITTER RECOMMENDED BEARING INSPECTION INTERVAL TO BE INCLUDED IN FALCON MOUNT MANUAL TIME LIMIT (CHAPTER 5-20-00). SUSPECT BEARING FAILURE CAUSED OVERVOLTAGESDR 99ZZZX4011Tire · failedDURING ATTEMPTED TAKEOFF AT OAK, BOTH LEFT MAIN TIRES FAILED AT 100 KNOTS. TAKEOFF WAS ABORTED. INSPECTION REVEALED DAMAGE TO BOTH MAIN WHEELS, LEFT FLAP AND LEFT MAIN LANDING GEAR DOOR. AIRCRAFT FERRIED AFTER WHEEL AND TIRE ASSEMBLIES REPLACED.
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