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 = '35A' 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 = '35A' 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 CA030618004Liner · bent(CAN) ONE OF TWO MS20427-4C7 RIVETS THAT HOLD THE KEYWAY LINER ON THE INNER WHEEL HALF FAILED ALLOWING THE CENTRIFUGAL FORCE OF THE SPINNING WHEEL TO BEND THE LINER OUTWARD UNTIL IT CONTACTED THE LOWER TORQUE LINK, DAMAGING IT AND ALSO CUTTING THE SIDEWALL OF SDR 852186Valve · failedDE-OIL VALVE FAILED TO OPEN AND ALLOW OIL TO THE 4/5 CAVITY. THEREBY CAUSING THE NR 4 AND NR 5 BEARINGS TO SEIZE, AND THE ENGINE TO LOCK UP AFTER 17 MIN OF OPERATION.SDR BSY2003F00015Fire Loop · inoperativeLEFT ENGINE HAD A FIRE LIGHT COME ON IN FLIGHT, SHUT ENGINE DOWN, BLEW BOTH FIRE BOTTLES AND RETURNED TO AIRPORT. INSPECTED ENGINE FOR FIRE, NONE NOTED. REMOVED ENGINE TAILCONE AND CHECKED FOR EXHAUST LEAKS NONE FOUND. REMOVED AND REPLACED LOWER MIDDLE AND SDR CA030605015Fuel Control · inoperative(CAN) WHEN TESTING MANUAL MODE (COMPUTER OFF) THERE WAS NO ENGINE POWER RESPONSE TO POWER LEVER INPUTS. FCU REPLACED, PROBLEM SOLVED.SDR CA030605009Tube · leaking(CAN) ON FINAL, CREW SELECTED GEAR DOWN, GEAR UNLOCKED AND FAILED TO EXTEND, NO HYDRAULIC PRESSURE, AIRCRAFT DIVERTED TO QUEBEC AIRPORT, GEAR EMERGENCY EXTENDED, AIRCRAFT LANDED WITH NO FURTHER PROBLEM.FOUND LT ENGINE HYDRAULIC PUMP FUSELAGE LINE HAD A CHAFED SDR L35SDR0301Motor · burned outDURING APPROACH INTO CVG, CREW EXPERIENCED SMOKE AND ELECTRICAL FUMES IN THE CABIN WHICH SEEMED TO ORIGINATE IN VICINITY OF BAGGAGE COMPARTMENT. FOUND COCKPIT BLOWER MOTOR BURNED OUT. NO FIRE OR FIRE DAMAGE. AICRAFT LANDED WITHOUT FURTHER INCIDENT.SDR BAQA086292Switch · inoperativeSTAB ON/OFF SWITCH INOPERATIVE. SPEX FILE NR 00118196. REPLACED WITH SERVICEABLE UNIT.SDR 042703Brake Assy · failedWHILE TAXING ON THE RAMP, BOTH BRAKES AND STEERING FAILED. CREW USED EMERGANCY BRAKES TO STOP THE AIRCRAFT. NOSE OF AIRCRAFT BUMP INTO THE RAILING. MAINTENANCE SUSPECTS ANTI-SKID SYSTEM.SDR EAE00103Line · crackedLOST HYDRAULIC PRESSURE WHEN LANDING GEAR WAS EXTENDED. NO BRAKES AVAILABLE UPON LANDING. DRAG CHUTE DEPLOYED TO STOP AIRCRAFT.SDR 041103Computer · failedRIGHT FUEL COMPUTER FAILED, OPERATED ENGINE IN MANUAL MODE, OIL PSI NORMAL, NR 2 N2 FLUCTUATED, NR 2 ITT GAUGE FAILED MOMENTARILY, ABOUT 20 MINUTES LATER ENGINE FLAMED OUT AT FL390. AIRCRAFT LANDED WITHOUT INCIDENT. STAGE OF OPERATION PART 91, EMPTY. GARRETSDR BSY2004F00002Bulb · inoperativeNO NOSE GEAR DOWN AND LOCK LIGHT. REMOVED AND REPLACED BULB, OPS CHECK GOOD.SDR CA030225001Pump · failed(CAN) AIRCRAFT WAS AT 70 KNOTS ON TAKE-OFF ROLL WHEN LT ENGINE FLAMED OUT. CREW REJECTED TAKE OFF. TROUBLESHOOTING FOUND LT ENGINE DRIVEN PUMP AT 30 PSI. AMM STATE MINIMUM 300 PSI. PUMP REPLACED. AIRCRAFT RETURN TO SERVICE.SDR BSY2003F00009Module · inoperativeLOST PRESSURIZATION AT 35,000 FT, RETURNED TO (NEW) REMOVED AND REPLACED PRESURIZATION MODULE OPS CHECKED GOOD.SDR 1387SMount · crackedDICOVERED DURING INSPECTION FOUND A CRACK IN THE RT TIP TANK MOUNTING FLANGE. REPAIRED PER MFG. DRAWING.SDR 0019Seal · tornDURING CLIMB TO ASSIGNED ALTITUDE, PILOT HEARD AN AUDIBLE AIR LEAK FROM AROUND ENTRY DOOR AT APPROXIMATELY 4.5 CABIN PSI. THE CABIN WOULD NOT PRESSURIZE BEYOND 5.5 CABIN PSI. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. CABIN DID NOT DEPRESSURIZE. LOWER SDR CJP2003F00001Gasket · failedFLIGHT CREW AND PASSENGER NOTED BURNING ODOR AND HAZE IN CABIN. AIRCRAFT DIVERTED TO AN ALTERNATE AIRPORT FOR MAINTENANCE. A LEAK WAS FOUND IN BLEED AIR CROSS-OVER DUCT FOR LT WING AND STABILIZER HEAT. A GASKET HAD FAILED ON THE CROSSOVER DUCT CONNECTION TOSDR CJP2003F00000Gasket · failedFLIGHT CREW AND PASSENGER NOTED BURNING ODOR AND HAZE IN CABIN. AIRCRAFT DIVERTED TO ALTERNATE AIRPORT FOR MAINTENANCE. A LEAK WAS FOUND IN BLEED AIR CROSS OVER DUCT FOR LEFT WING AND STABILIZER HEAT. A GASKET HAD FAILED ON THE CROSSOVER DUCT CONNECTION TO SDR 2003F00161Bleed Valve · stickingRIGHT ENGINE DEVELOPED ITT SPLIT 60 DEGREES HOTTER THAN NR 1. EXTENSIVE MAINTENANCE TROUBLESHOOTING WITH NUMEROUS GROUND RUNS COULD NOT DUPLICATE THIS PROBLEM. ENGINE WAS ACCESSED TO SURGE BLEED VALVE DUE TO SUPPOSED INTERMITTENT STICKING. REPLACED SURGE BLESDR BSY2003F00001Bulb · inoperativeLT MAIN GEAR DOWN AND LOCK LIGHT INOPERATIVE. CHECKED WITH TOWER FOR LANDING LIGHTS BEING ON. LANDED NO PROBLEM. REMOVED AND REPLACED BULB, OPS CHECK GOOD.SDR DBCA1220Ignition Lead · failedNR 2 ENGINE START ATTEMPTED. ENGINE WOULD SPOOL, BUT NOT LIGHT-OFF. PILOT ABORTED START ATTEMPT AND CONTACTED MAINTENANCE. TROUBLESHOT AND FOUND ONE IGNITION LEAD BAD. REPLACED DEFECTIVE LEAD AND BOTH IGNITORS. OPS CHECKED GOOD.SDR I122003F00000Switch · failedMACH OVERSPEED SWITCH FAILED DURING FUNCTIONAL TEST.SDR DBCA1222D1Relay · failedDURING PRE-TAKEOFF CHECKS, LT HAND PRESSURIZATION WENT INTO EMERGENCY PRESSURIZATION MODE AND WOULD NOT RESET TO NORMAL. PILOT RETURNED TO DEPARTURE AREA AND ABORTED TRIP. TROUBLESHOT TO FAILED RELAY IN MODULATING VALVE CONTROL BOX. FAILED RELAY INTERRUPTESDR 103102Torque Link · crackedDURING EDDY CURRENT OF LOWER TORQUE LINK ON THE LT MLG, A CRACK WAS DISCOVERED. THE PART WAS REPLACED.SDR ESUA119026Squat Switch · intermittentAFTER LANDING, DURING TAXI, SECOND TURN DURING TAXI OPERATION, THE AIRCRAFT DID NOT RESPOND TO BRAKING OR STEERING. AFTER REALIZING THAT THE AIRCRAFT WAS NOT RESPONDING DURING TAXI OPERATIONS, THE CREW ENGAGED THE EMERGENCY BRAKES TO STOP THE AIRCRAFT. AT THSDR 101502Squat Switch · intermittentAFTER LANDING, DURING TAXI, SECOND TURN DURING TAXI OPERATION, THE AIRCRAFT DID NOT RESPOND TO BRAKING OR STEERING. AFTER RELIZING THAT THE AIRCRAFT WAS NOT RESPONING DURING TAXI OPERATIONS, THE CREW ENGAGED THE EMERGANCY BRAKES TO STOP THE AIRCRAFT. AT THIS TSDR 2002FA0001181Computer · malfunctionedNOSE WHEEL STEERING WILL NOT ARM. FOUND NO OUTPUT VOLTAGE ON P224 PIN A. 1.0 VAC REQUIRED FROM THIS PIN.SDR ROSA200200001Elbow · looseLOST ALL HYDRUALIC PRESSURE IN FLIGHT, AUX PRESSURE WORKED OK. FOUND HYDRUALIC LEAK IN LEFT MAIN GEAR WELL AIRFRAME FITTING TO RETRACT SIDE OF MAIN GEAR ACTUATOR. TIGHTENED FITTING TO RETRACT ACTUATOR PER LEARJET MAINTENANCE MANUAL 20-30-00, SERVICED RESERVIOSDR BSY2002F00018Drag Chute · deployedON CLIMB OUT, AT 15,000 FEET, DRAG CHUTE DEPLOYED AND SEPARATED FROM AIRCRAFT. INSTALLED DOOR AND DRAG CHUTE. OPS CHECKED GOOD. CAUSE FOR DEPLOYMENT UNKNOWN AT THIS TIME.SDR CA020731007Bolt · loose(CAN) DURING HUMP INSPECTION THE RT ELEVATOR BELLCRANK ATTACHMENT BOLT HAD VERTICAL FREE PLAY BETWEEN THE BELLCRANK AND THE ELEVATOR INPUT SHAFT. THE RT ELEVATOR TORQUE TUBE AND BELLCRANK ATTACHMENT HOLES WERE ELONGATED.AS PER LEARJET ENGINEERING REPORT. THSDR CA020731005Fitting · loose(CAN) DURING HUMP INSPECTION THE FOLLOWING DISCREPANCY WERE FOUND. THE HORIZONTAL STAB CENTER HINGE FITTING HAD LOOSE AND MISSING RIVETS. A TOTAL OF 14 RIVETS WERE AFFECTED AND CONSEQUENTLY REPLACED BY HI-LOK AS PER STRUCTURAL REPAIR MANUAL.SDR CA020711001Rheostat · damaged(CAN) WITH THE AIRCRAFT POWERED UP AND AC INVERTER ON, FLIGHT CREW NOTICE SMOKE RISING FROM LT SIDEWALL PANEL. UPON FUTHER INSPECTION WITH SIDEWALL REMOVED. THREE WIRE BUNDLES THAT GO TO THREE DIFFERENT REHOSTAT WERE FOUND WITH SPIRAL WRAP AROUND THEN AND MELSDR CJP2002F00000Selector Valve · failedLANDING GEAR WOULD NOT EXTEND WHEN GEAR HANDLE WAS SELECTED TO DOWN POSITION. FLIGHT CREW COMPLETED AN EMERGENCY LANDING GEAR EXENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE JACKED AIRCRAFT AND DUPLICATED PROBLEM. LANDING GEAR TROUBLESHOOTING DETERMINED LSDR MXI2002F00000Actuator · leakingRIGHT MAIN LANDING GEAR ACTUATOR LEAKING HYDRAULIC FLUID. PLUNGER O-RING PART NUMBER M83461/1-146 FAILED BY ROLLING IN THE ACTUATOR. INSTALLED ACTUATOR REPAIR KIT WHICH CONTAINED AN IMPROVED SEAL.SDR CWUA072DComputer · intermittentAIRCRAFT EXPERIENCED RIGHT ENGINE FIRE WARNING SHORTLY AFTER TAKEOFF. CREW FOLLOWED CHECKLIST, DECLARED AN IFE, AND LANDED WITHOUT INCIDENT. AFTER HOURS OF TROUBLESHOOTING, MAINTENANCE DETERMINED THEY COULD TURN ON AND OFF THE RIGHT ENGINE FIRE LIGHT BY LIGHSDR 0018Actuator · out of adjustAFTER TAKEOFF, THE GEAR RETRACTED NORMAL BUT RT MAIN GEAR SHOWED AN UNSAFE INDICATION. THE INBOARD GEAR DOOR DID NOT CLOSE ENOUGH TO COMPRESS THE INBOARD GEAR DOOR SWITCH. INBOARD GEAR DOOR ACTUATOR HAD BEEN RESEALED DURING A 600 HR INSPECTION PRIOR TO TAKEOSDR CA020508002Rod · corroded(CAN) DURING 12 YEARS MAJOR AIRFRAME INSPECTION, RT WING SPOILER ACTUATOR WAS REMOVED TO GAIN ACCESS TO INSPECT THE RT FLAP ACTUATOR ATACHMENT FITTING. WHEN HANDLING THE SPOILER ACTUATOR FOUND PITTING COROSION ON THE PISTON-ROD (CHROME SURFACE). NEW PART ORDERSDR CA020506001Bulb · burned out(CAN) ON APPROACH, PILOT SELECTED GEAR DOWN, ALL GEAR GREEN LIGHTS ILLUMINATED, EXCEPT THE LT MAIN GEAR LIGHT. THE BULB WAS CONFIRMED BURNED AFTER BULB TEST, BUT PILOT AS PRECAUTIONARY MEASURE, ACTIVATED THE GEAR BLOW DOWN. AIRCRAFT LANDED WITH NO ADDITIONAL SDR O9I2002F00003Hinge · crackedLOWER ENTRY DOOR FORWARD CORNER AT HINGE WAS FOUND CRACKED. DOOR WAS REPAIRED WITH MANUFACTURER SUPPLIED PARTS. THE PROBABLE CAUSE MAY HAVE BEEN WORN DOOR CABLES FOR AN EXTENDED TIME. MFG RECOMMENDS USING DOOR SUPPORT RODS DURING ROUTINE MAINTENANCE TO PREVSDR 2002F00408Connector · meltedCONNECTOR ON AUX DEFOG BLOWER MELTED AND INSULATION ON WIRE AT CONNECTOR MELTED. THIS DEFOG BLOWER WAS INSTALLED UNDER STC SA1482SO REV B. THIS IS THE 4TH BLOWER ASSY WHERE THE CONNECTOR HAS MELTED. MANUFACTURED BY FLIGHT ENGINEERING AND DEVELOPMENT.SDR CA020417003Actuator · leaking(CAN) ON GEAR EXTENSION, 3 GREENS, 1 UNSAFE ON RT SIDE. ON RETRACTION, NO GREENS LIGHTS, THREE UNSAFE. TWO MORE EXTENSIONS CARRIED OUT WITH SAME RESULT. GEAR EXTENDED AS PER EMERGENCY CHECK LIST(BLOWN DOWN). GEAR SWING CARRIED OUT ON JACKS, FOUND RT GEAR ACTSDR KOS2002F00001Pressure Switch · inoperativeFUEL PRESSURE SWITCH, INOPERATIVE.SDR KOS2002F00000Battery · inoperativeBATTERY INOPERATIVE.SDR DRU2002F00000Hose · leakingWHILE TROUBLESHOOTING THE BLEED AIR HEATING SYSTEM, WHICH WAS INOPERATIVE, SOME LEAK CHECK SOLUTION HAD GOTTEN ON HEATING SENSOR AND CONTROL HOSES. HOSES WERE LEAKING. REMOVED OLD SENSOR AND CONTROL HOSES, AND INSTALLED NEW HOSES. LEAK CHECK WAS GOOD, AND SSDR 35A501Engine · malfunctionedENGINE START, TAXI, AND CLIMB UNEVENTFUL. CLIMB FROM 5000 FT TO 15000 FT, TURNED ON ANTI-ICE SYSTEMS, PRIOR TO ENTERING CLOUDS AT APPROX 6000 FT, LT ENGINE FLUCTUATED AND ROLLED BACK SHORTLY AFTER ENTERING CLOUDS. ENCOUNTERED ICING SHORTLY AFTER ENTERING CLOSDR QH52002F00000Mount · crackedMOUNT HAS A .500 INCH CRACK AS MARKED ON PART.SDR CA020227001Fuel Control · defective(CAN) LT ENGINE HOT START ON MANUAL AND COMPUTER MODE. LT FCU REPLACED, GROUND RUNS C/O, GROUD CHECK SERVICEABLE.SDR FCP2002F00000Frame · wornMAINTENANCE DISCOVERED WHILE TROUBLESHOOTING PITCH TRIM DISCREPANCY. ELEVATOR PITCH SPRING FRAME ASSEMBLY (PN 2631507-13). DURING INSPECTION OF SPRING AND FRAME ASSEMBLY, UPPER ATTACH POINT FOR SPRING WAS FOUND WORN BEYOND LIMITS. SPRING ATTACH BOLT WAS WORSDR JGV2002F00000Connector · crackedPLASTIC CONNECTION THAT CONNECTS TO THE HOSE UNION CRACKED TO THE POINT THAT THE THREADED UNION WILL NOT STAY CONNECTED TO THE OUTFLOW VALVE.SDR BSY2002F00000Bulb · burned outMIR LEFT MAIN GEAR, NO DOWN AND LOCK INDICTATION. REMOVED AND REPLACED BULB, OPS CHECK GOOD.SDR DIN2002F00000Plate · wornCARBON DUST NOTICED COMING FROM A BRUSHLESS GENERATOR. TSO GENERATOR 445 HRS. LOANER UNIT WAS INSTALLED. TEARDOWN INSP FOUND DRIVESHAFTS FRICTION CLUTCH PLATE TO BE WORN REQUIRING REPLACEMENT. THE OVERHAUL SHOP SAID THE FANUFACTURE HAD CHANGED MATERIALS FRO
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