Dassault FALCON 20-F5
Service difficulty reports · 26
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 = 'FALCON20F5' 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 = 'FALCON20F5' 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 KC8A202607240004Fire Warning · false activationAPU FIRE WARNING BEFORE TAKEOFF. VISUALLY CHECKED APU AND AFT COMPARTMENT, NO EVIDENCE OF SMOKE OR FIRE NOTED. FIRE DETECTION SYSTEM CHECKS GOOD PER THE FALCON 20-F5 MM 26-10-00. SUSPECT APU WAS RUNNING DURING TAKEOFF.SDR KC8A20260410003Elec Connector · shortedLOSS OF PRESSURIZATION DURING CLIMB OUT OF KBHM, CABIN WARNING LIGHT ILLUMINATED ACCOMPANIED BY THE AURAL WARNING, NO RESPONSE SELECTING MANUAL CONTROL. CREW DECLARED AN EMERGENCY AND DIVERTED TO KHSV. MAINTENANCE FOUND CONDITION VALVE CIRCUIT BREAKER POPPED. SDR KC8A20250623002Fire Warning · false activationINTERMITTENT APU FIRE WARNING AFTER TAKE-OFF FROM KSUS. CREW SHUT DOWN APU AND ACTIVATED APU COMPARTMENT FIRE EXTINGUISHER. RETURNED TO KSUS. MAINTENANCE AT KSUS INSPECTED APU AND COMPARTMENT FOR HEAT OR FIRE DAMAGE, NO DEFECTS NOTED. DEFERRED APU SYSTEM IN ACSDR KC8A2024072678Fire Warning · false activationCREW NOTICED APU FIRE WARNING LIGHT ILLUMINATED, NO SECONDARY INDICATIONS OF APU OPERATION. FIRE BOTTLE DISCHARGED AS PRECAUTION. AIRCRAFT, APU, AND COMPARTMENT INSPECTED FOR FIRE DAMAGE. NO DAMAGE OR DEFECTS NOTED. APU AND FIRE EXTINGUISHING FOR APU DEFERRED SDR 2CJA2021103000005Clamp · brokenAFTER LOADING OUR PASSENGERS AND TAXIING OUT TO RUNWAY 27R WE LIFTED OFF AT 21:29Z. APPROXIMATELY 2 MINUTES AFTER TAKEOFF WHILE WE WERE CLIMBING AT ABOUT 3900 FEET THE #2 ENGINE CHECKLIST AND UPON PULLING THE #2 FUEL SHUTOFF HANDLE THE FIRE ZONE 1R LIGHT WENTSDR DJSR201910243001Trim System · out of limitsDURING TAKEOFF PHASE, YOKE HIT MECHANICAL STOP BEFORE AIRPLANE PITCH DOWN OCCURRED. CREW TRIMMED TAIL PLANE ACTUATOR NOSE DOWN, WHICH CORRECTED THE PROBLEM. CREW RETURNED TO DEPARTURE AIRPORT.SDR DJSR201910248001Feel Unit · erraticAFTER TAKEOFF PITCH CONTROL ARTIFICIAL FEEL BECAME ERRATIC/SLUGGISH. ABORTED FLIGHT AND RETURNED TO DEPARTURE AIRPORT.SDR BQVD201411030001Servo Valve · bypassingRIGHT BRAKE ANTISKID DID NOT TEST PRIOR TO LANDING. REDUCED BRAKING ON RIGHT BRAKE IN SYSTEM "A". BRAKING NORMAL ON SYSTEM "B". FOUND RIGHT MAIN LANDING GEAR ANTI-SKID SERVO VALVE BYPASSING BRAKE FLUID PRESSURE WITH ANTI-SKID SYSTEM ON OR OFF.SDR BJYA20090507001Fire Warning · false activationAFTER TAKEOFF, AT ABOUT 7000 MSL THE ACFT EXPERIENCED AN "APU FIRE INDICATION". CREW FOLLOWED THEIR EMERGENCY PROCEDURES CHECK LIST AND DISCHARGED THE APU FIRE BOTTLE. THE SOLE INDICATION WAS THE LIGHT. THE CREW HAD NO ASSOCIATED SCENTS OR FUME AND NO OTHERSDR 4006Outflow Valve · failedAIR CONDITIONING VALVE CIRCUIT BREAKER POPPED AFTER TAKEOFF AND WOULD NOT RESET WHICH PREVENTED THE AIRCRAFT FROM PRESSURIZING. THE PILOTS REMAINED AT LOWER ALTITUDE WHILE FOLLOWING PROPER PROCEDURES AND LANDED AT THE NEXT AIRPORT. THE PART WAS REPLACED AND THSDR 2007FA0000049Seal · deterioratedDETERIORATED APU EXHAUST DUCT SEAL BETWEEN THE DUCT FLANGE AND AIRCRAFT SKIN ALLOWED HOT EXHAUST GASSES TO ENTER THE TAILCONE AREA RESULTING IN HEAVY SOOT BUILDUP AND HEAT DAMAGE TO WIRE BUNDLES AND ELECTRICAL CONNECTORS AND STRUCTURAL COMPONENTS ADJACENT TO TSDR PAZR200620412Plug · corrodedDURING THE COURSE OF REPLACING THE LT MLG ASSEMBLY, THE TECHNICIAN, UPON VISUAL INSPECTION AFTER REMOVAL OF MLG ASSY, FOUND SIGNS OF CORROSION ON THE PLUG, P/N MY20112-1605. UPON FURTHER DISASSEMBLY, IT WAS NOTED THAT THE CORROSION HAD GONE THROUGH THE PLUG. SDR 379002Control Switch · burnedON PREFLIGHT CHECK, MECHANIC IN THE COCKPIT OBSERVED SMOKE COMING FROM THE OVERHEAD PANEL. UPON FURTHER INSPECTION, MAINTENANCE PERSONNEL FOUND DAMAGED "NO SMOKING" AND "SEAT BELT" SWITCHES. THESE SWITCHES HAD BEEN PREVIOUSLY REPLACED AS A RESULT OF A NOISE SDR CA040105008Squat Switch · frozen(CAN) ON LANDING THE PIC COULD NOT ACTIVATE THE NORMAL BRAKES AND THE NOSE WHEEL STEERING. PIC USED NR 2 BRAKE SYSTEM AND DIFFERENTIAL POWER TO CONTROL THE AC. SQUAT SWITCH WAS REMOVED, CLEANED AND RE-INSTALLED. NORMAL BRAKES AND NOSE WHEEL STEERING FUNCTION SDR UO22003F00013Relief Valve · leakingTHE AIRCRAFT WAS CLIMBING TO 37,000 FT WHEN THE LOW HYDRAULIC RESERVOIR HEAD PRESSURE LIGHT COME ON. THE PILOT DESCENDED TO 20,000 FT IAW THE FLIGHT MANUAL. WE FOUND THAT THE NR 2 HYDRAULIC RESERVOIR OVER PRESSURE RELIEF VALVE WAS LEAKING. THE VALVE WAS PURSDR 20000427SH021Seat · brokenCO-PILOT SEAT: LARGE CRACK IN OUTBOARD VERTICAL TUBE OF BACKREST FRAME. ALSO, MULTIPLE CRACKS IN SEAT PAN. PILOT SEAT: MULTIPLE CRACKS IN SEAT PAN. (X)SDR 20000427SH013Seat · crackedCO-PILOT SEAT: LARGE CRACK IN OUTBOARD VERTICAL TUBE OF BACKREST FRAME. ALSO, MULTIPLE CRACKS IN SEAT PAN. PILOT SEAT: MULTIPLE CRACKS IN SEAT PAN. (X)SDR 2000ZZZX581Valve · malfunctionedRIGHT WING REFUEL VENT VALVE OPERATES INCORRECTLY AFTER OVERHAUL. WHEN POWER IS APPLIED TO THE 'OPEN' CIRCUIT, VALVE RUNS TO THE CLOSED POSITION AND THE VALVE POSITION INDICATOR (MECHANICAL INDICATES CLOSED. ELECTRICALLY, THE VALVE INDICATES OPEN.SDR 99ZZZX3647Indicator · reads lowGAUGE INSTALLED. ENGINE GROUND RUN AND FUNCTIONED NORMALLY. ON NEXT FLIGHT, CREW NOTICED TEMPERATURE WAS READING LOW. REPLACED GAUGE.SDR 99ZZZX265Control Cable · damagedWHILE PERFORMING RECENT REQUIREMENT OF 1,500 HOUR LUBE ON CONTROL COLUMNS, FOUND 3 OUT OF 4 UPPER CABLES, AND 1 OUT OF 2 LOWER CABLES, WITH BROKEN STRANDS WHERE THEY RUN OVER PULLEYS. P/N'S: MY2021520810-1, 1 EACH. MY20215-20820-1, 2 EACH. MY20215-20830, 1 SDR 99ZZZX264Control Cable · damagedWHILE PERFORMING RECENT REQUIREMENT OF 1,500 HOUR LUBE ON CONTROL COLUMNS, FOUND 3 OUT OF 4 UPPER CABLES, AND 1 OUT OF 2 LOWER CABLES, WITH BROKEN STRANDS WHERE THEY RUN OVER PULLEYS. P/N'S: MY2021520810-1, 1 EACH. MY20215-20820-1, 2 EACH. MY20215-20830, 1 SDR 98ZZZX4184Line · crackedDURING MAINTENANCE, FOUND DRIP OF HYDRAULIC FLUID ON BEND IN LINE, WHICH WOULD REFORM WHEN WIPED AWAY. CRACK WAS NOT READILY VISIBLE UNTIL LINE WAS DISCONNECTED AT AFT END IN ORDER TO SPREAD THE LINE A BIT AT THE BEND RADIUS. SUBMITTER STATED REPLACED THIS SSDR 97ZZZX2868Servo · leaksLEFT AILERON SERVO LEAKED EXCESSIVELY IN-FLIGHT, CAUSED LOSS OF NR 1 HYDRAULIC SYSTEM. SUBMITTER BELIEVES PISTON O-RING SEALS RUPTURED OR ROLLED. NOT SURE UNTIL INVESTIGATED.SDR 97ZZZX2867Servo · leaksLEFT AILERON SERVO LEAKING EXCESSIVELY WITH NO SYSTEM PRESSURE APPLIED OTHER THAN 21 PSI ON HYDRAULIC TANK (HEAD PRESSURE). BELIEVE PISTON O-RING SEALS SPLIT OR ROLLED. NOT SURE UNTIL AERO PRECISION REPAIR AND OVERHAUL, INC., FL, HAS HAD AN OPPORTUNITY TO INSDR 97ZZZX1015Engine · power lossPILOT NOTES: AFTER RE-FUEL, THE ACFT LOST PWR ON T/O APPROX 200 FEET AGL. NR 2 ENG EGT WENT RED LINE APPROX 780 DEGREES FAHRENHEIT AND RPM HAD ROLL BACK. A POP WAS HEARD IN THE CABIN BY PASSENGERS. (POSSIBLE COMPRESSOR STALL). PILOT WENT TO FLT IDLE WITH SDR 97ZZZX1249Actuator · leaking9-15-96 FOUND FAN FLAP ACTUATOR LEAKING BADLY ON T/R DEPLOY. ACTUATOR WAS REPAIRED 6-21-96. P/N AND S/N LISTED. 6-29-96. APPROX 66 HOURS AND 74 CYLCES PRIOR TO CURRENT TIME, FOUND SAME P/N AND POSITION, ACTUATOR LEAKING. THIS ACTUATOR S/N 735 HAD APPROX 1
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