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 = 'HA420' 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 = 'HA420' 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 5OKA202609150082Cover · separatedHONDAJET N909BP, 42000099, TAXIED OUT ON SUNDAY, AUGUST 2, AND THE LINE SERVICE PERSONNEL FOUND A 7" X 2" CURVED STAINLESS-STEEL PLATE/PIECE WITH P/N - 4JQT4-13121-Q0A-0100 LAYING ON THE GROUND WHERE THE AIRCRAFT HAD PARKED. A SECUITY VIDEO SHOWED AN OBJECT BESDR 3EJA202603250001Outflow Valve · failedCABI ALT HIGH CAS/DEPRESSURIZATION AT FL290. R&R OUTFLOW VALVE.SDR 3EJA20260310326Outflow Valve · failedCABI ALT HIGH CAS/DEPRESSURIZATION AT FL290. EXECUTED EMERGENCY PROCEDURES AND DIVERTED TO FXE. /R & R OUTFLOW VALVE.SDR 2023F00305Actuator · defectiveAFTER TAKEOFF CREW OBSERVED PITCH TRIM FAULT CAS MESSAGE AND EXPERIENCED INCREASED BACK PRESSURE ON THE YOKE DURING CLIMB OUT. CREW PERFORMED QRH PROCEDURES, SWITCHING TO STBY TRIM AND EXECUTED DIVERT TO NEARBY AIRPORT. AIRCRAFT LANDED WITHOUT INCIDENT.SDR 2023F00165Compensator · failedLH BRAKE FAILSDR 2023FA0000202Windscreen · crackedAT APPROXIMATELY 1640 EST, N829DL WHILE REPOSITIONING FROM OPF TO PDK (ATLANTA) AT FLIGHT LEVEL 330, THE LEFT, FOREWORD WINDSCREEN BEGAN TO DELAMINATE AND EVENTUALLY CRACK. THIS WINDSCREEN IS CERTIFIED TO MAINTAIN CABIN PRESSURE WHILE WITHSTANDING AERODYNAMIC SDR 2023F00104Unknown · unknownON TUESDAY APRIL 4 2023, AT APPROXIMATELY 1200 EST N719SJ WAS DESCENDING OUT OF FL390 FOR FL370. THE AUTOPILOT DISENGAGED AND FLASHED THE AMBER WARNING LIGHT. WE RECEIVED THE “PITCH TRIM FAIL” CAS MESSAGE. MICHAEL RICKETTS WAS THE PF AND DENNIS LELAND THE PM. SDR 2023F00172Compensator · failedDURING SLOW TAXI IN, (LESS THAN 10 KNOTS), AFTER LANDING HAD TOTTAL RELEASE OF BRAKING EFFECTIVENESS FOR 1 SECOND ON BOTH SIDES.SDR 2023F00103Pdu · unknownTHE #1 POWER DISTRIBUTION UNIT (PDU) FAILURE CAUSED A NUMBER OF CREW ALERT SYSTEM (CAS) MESSAGE. THIS FAILURE TRIGGERED A SERIES OF CASCADING
ELECTRICAL SIGNAL FAILURES TO NUMEROUS AIRCRAFT SYSTEMS, CULMINATING IN THE HYDRAULIC SYSTEMS PRESSURIZATION SIGNALS SDR 2023FA0000063Flap · crackedDURING ROUTINE MX, NOTED THE RIGHT FLAP TRAILING EDGE UNDER THE ENGINE PYLON TO BE CRACKED AND SEPARATED ALONG THE TRAILING EDGE BEND RADIUS FOR APPROX 9" WITH 2 PROPAGATING CRACKS RUNNING FORWARD INTO THE AIRSTREAM.SDR 2023F00173Transducer · failedRH BRAKE GRABBINGSDR 2023F00159Compensator · failedRUNWAY EXCURSIONSDR EKGA2022121200510Vent · mechanic errorLEFT ENGINE BLEED LEAK CAS MESSAGE DURING CLIMB OUT AT 21,000 FT. PILOT DEVIATED TO KBRO WITH NO INCIDENT. DISCOVERED L ENGINE VENTILATION SLOTS WERE FOUND SEALED OVER. REMOVED EXCESS SEALANT FROM SLOTS PER HONDA TECH SUPPORT. GROUND IDLE AND POWER RUNS SUCCESSDR 2023F00174Brake · failedRH BRAKE LOCKED UP ON LANDINGSDR 2023F00161Compensator · failedNORMAL BRAKE FAIL CAS MESSAGESDR 2023F00150Compensator · failedRH BRAKE SPONGYSDR 2023F00158Compensator · failedLH BRAKE PEDAL SOFTER THAN RHSDR 2022F00148None · openON SUNDAY, MARCH 20TH, TMB420, A HONDA JET (HA-420) OPERATED BY FLYDREAMS, LLC (DBA VOLATO) ACC 4F1A515O DEPARTED KAPF (NAPLES, FL) FOR KEYW (KEY WEST, FL). UPON DEPARTURE THE AIRCRAFT EXPERIENCED A CONTROLLABILITY ISSUE. SPECIFICALLY, THE TRIM SYSTEM FOR AISDR 2023F00151Compensator · failedBRAKES FAIL / RUNWAY DEPARTURESDR 2023F00162Compensator · failedLH BRAKE FAILSDR 2023FA0000269Compensator · failedLH BRAKE FAILSDR 2023F00170Compensator · failedRH BRAKE FADESDR 2023F00166Compensator · failedRH BRAKE FADESDR 2023F00171Compensator · failedLH BRAKE 0% BRAKING POWERSDR 2023F00168Compensator · failedLH BRAKE 0% BRAKING POWERSDR 2023F00167Compensator · failedSPONGY BRAKE / BRAKES FAILEDSDR 2023F00169Compensator · failedLH BRAKE PEDAL SOFTER THAN RH. SPONGYSDR 2023F00160Compensator · failedNORMAL BRAKE FAIL CAS MESSAGESDR 2023F00156Compensator · failedNORMAL BRAKE FAIL CAS MESSAGE ILLUMINATEDSDR 2023F00164Compensator · failedLH BRAKE FAILSDR 2021F00143Brake Sys · failedUPON LANDING AT KRYY ON RUNWAY 27, THE CREW REPORTED THEY HAD NO BRAKE ACTUATION AT TOUCH DOWN. THEY THEN DEPLOYED THE EMERGENCY BRAKES WHICH DOES NOT TIE INTO THE ANTISKID SYSTEM WHICH CAUSED BOTH MAIN TIRES TO FLAT SPOT THUS CAUSING THEM TO BLOW. THE LH TIRESDR 2023F00163Compensator · failedNORMAL BRAKE FAIL CAS MESSAGE ILLUMINATEDSDR K5SR202008103599Controller · malfunctionedCUSTOMER SQUAWK OF NO HEAT IN CABIN AREA. INSTALLED MODIFIED VCSC CONTROLLER FROM ENVIRO SYSTEMS INC P/N 1300640-10 S/N 00216. OPERATION CHECKED SATISFACTORY. AIRCRAFT FLEW ABOUT 2 HOURS AND CUSTOMER SQUAWKED THAT THERE WAS NOW NO COCKPIT HEAT AND WINDSHIELDSDR 2023F00153Compensator · failedAIRCRAFT PULLS TO THE LEFT ON LANDINGSDR 3HDR2019102800001Windscreen · delaminatedTHE AIRCRAFT ARRIVED FOR THE INITIAL 600 FLIGHT HR. INSPECTION WITH A KNOWN LH WINDSHIELD DELAMINATION. THE DELAMINATION RAN FROM THE LH EDGE OF THE WINDSHIELD TO APPROXIMATELY 3” INBOARD ALONG THE FULL LENGTH (HEIGHT) OF WINDSHIELD. PRIOR TO WINDSHIELD REMOVASDR 2023F00152Compensator · failedRUNWAY EXCURSIONSDR 2023F00157Compensator · failedLHBRAKE PEDAL SOFTER THAN RHSDR 2023F00154Compensator · failedLH BRAKE PEDAL SOFTER THAN RHSDR 3HDR2018102300004Pump · leakingDURING PRELIMINARY INSPECTION DISCOVERED ACCUMULATION OF HYDRAULIC FLUID ON AFT FUSELAGE EXTERIOR. UPON FURTHER INVESTIGATION FOUND HYDRAULIC SYSTEM ECOLOGY BOTTLE FULL AND OVER FLOWING. FURTHER TROUBLE SHOOTING WAS PERFORMED AND FOUND MAIN HYDRAULIC PUMP ASSESDR 2018FA0000395Wheel · looseMAIN WHEELS UNDER TORQUE FROM PRODUCTION: WE HAVE NOW REPLACED FOUR MAIN WHEELS ASSY. FROM NEW AND ALL FOUR WHEEL NUTS HAVE BEEN LOOSE ON THE AXLE SINCE THE AIRCRAFT WENT INTO SERVICE. IT WAS NOT DISCOVERED UNTIL THE WHEEL WAS REPLACED. OEM HAS BEEN CONTACTEDSDR 3HDR2018040600003Pump · contaminatedFLT CREW REPORTED FUEL DRAINS BACK TO CENTER TANK APPROX. 100 LBS. IN 30 MINUTES. TROUBLESHOT FUEL SYSTEM AND FOUND 280 LBS. OF FUEL PER HOUR WOULD TRANSFER FROM RH WING TANK INTO CENTER TANK WHILE AIRCRAFT SAT STATICALLY. GAINED ACCESS FOR VISUAL INSPECTION OSDR EKGA20171201001Skin · dentedDURING A ROUTINE POST FLIGHT INSPECTION SEVERAL DENTS WERE NOTED ON THE HORIZONTAL STABILIZER LEADING EDGES. FURTHER INSPECTION OF THE AIRCRAFT SHOW NO OTHER DAMAGE TO ANY OTHER SURFACES. THE HORIZONTAL STABILIZER DAMAGE APPEARS SIMILAR TO WHAT YOU WOULD SEE FSDR 3HDR2017022000003Window · migratedDURING A PRELIMINARY INSPECTION OF THE FUSELAGE EXTERNAL AREAS A GASKET TYPE MATERIAL WAS FOUND MIGRATING OUT BETWEEN THE FORWARD RT PASSENGER CABIN WINDOW AND THE FUSELAGE SKIN. APPROXIMATELY 1.0 INCHES IN LENGTH AND 1/4 INCHES HIGH OF MATERIAL WAS NOTED STICSDR 3HDR2017022000002Cable · intermittentTHE FLIGHT CREW REPORTED TCAS II INTERMITTENT FAILURES. TROUBLESHOT SYSTEM BY DOWNLOADING ASSERT LOG DATA HISTORY AND PROVIDING TO GARMIN AVIONICS TECHNICAL SERVICES FOR ANALYSIS. GARMIN DETERMINED FAULTS WERE TRIGGERED BY FAULTY LOWER ANTENNA CABLES. GAINED ASDR 3HDR2017021500001Tube · leakingFUEL WAS REPORTED DRIPPING FROM THE LOWER CENTER FUSELAGE AREA. FURTHER INVESTIGATION FOUND THE LOWER FUEL ELECTRICAL ISOLATOR TUBE LEAKING BETWEEN THE BONDED AREA OF THE METAL FERRULE AND THE OUTER SURFACE OF THE TUBE. FOLLOWING THE REPLACEMENT OF THE ELECTR
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