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 = 'A36' 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 = 'A36' 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 2013FA0000015Bearing · failedPILOT REPORTED ELECTRICAL FAILURE. INSPECTED ACFT, FOUND A/C IDLER PULLEY BEARING SEIZED, CAUSING PULLEY TO COME OFF AND CUT THROUGH SENSOR ALTERNATOR-OUT CONTROL BOX WIRING BUNDLE, CAUSING A/C AND ELECTRICAL POWER TO FAIL.SDR 2012FA0000752Control Switch · failedUPON TAKEOFF, THE LANDING GEAR RETRACTED WITH THE LANDING GEAR CONTROL SWITCH IN THE DOWN AND LOCKED POSITION. THE LANDING GEAR RETRACTED UNCOMMENDED AND UNKNOWN BY THE PILOT AS SOON AS THE ACFT ACHIEVED A WEIGHT-OFF-WHEELS CONFIGURATION DURING TAKEOFF ROLL. SDR 2013FA0000125Engine · malfunctionedACFT ENGINE WAS BEING RUN AFTER LT MAGNETO CHECKS. ACFT WENT INTO FULL POWER AND ROLLED ON ITS WHEELS UNCONTROLLABLY TOWARDS THE DIRECTION OF A MAJOR AIRPORT CONSTRUCTION SITE CAUSING SEVERE UNREPAIRABLE DAMAGE TO BOTH WINGS. THE NOSE GEAR AND BOTH MAIN GEARSSDR 2012FA0000671Cylinder Head · separatedDURING CLIMB OUT, PILOT HEARD A BANG/POP SOUND FORWARD OF COCKPIT. LOST SOME POWER AND RPM. NOTICED DROP IN NR 1 CYLINDER TEMP ON ENGINE INDICATING SYS. RETURN TO FIELD, NORMAL LANDING. ACFT SHUTDOWN. POST FLIGHT INSPECTION REVEALED A HEAD TO BARREL SEPARASDR 2012FA0000640Check Valve · obstructedAT 15,000 FT IN CRUISE, PILOT EXPERIENCED DROP IN ENGINE OIL PRESSURE AND DROP IN MANIFOLD PRESSURE. ON LANDING, FOUND ENGINE EXHAUST COATED WITH ENGINE OIL AND DRIPPING FROM TAIL PIPE. INSPECTION OF TURBOCHARGER INSTALLATION REVEALED LOWEST CHECK VALVE TO HSDR 2012FA0000586Gear · making metalCHANGING OIL DURING ANNUAL INSPECTION, FOUND STEEL AND RED RUBBERY PIECES IN FILTER. REMOVE ALTERNATOR, METAL COMING FROM DRIVING GEAR ON CRANKSHAFT AND ALTERNATOR DRIVEN GEAR. RUBBER COMING FROM ALTERNATOR DRIVE COUPLER. FOUR BOLTS HOLDING CRANKSHAFT GEAR SDR 2012FA0000510Brushes · wornINSPECTED ALTERNATOR AND FOUND ONE BRUSH WAS WORN PAST LIMITS, THE OTHER EXHIBITED IMMINENT FAILURE.SDR 2012FA0000497Impulse Coupling · crackedDURING A ROUTINE 500 HR MAGNETO AND IMPULSE COUPLING INSPECTION, THE LT MAGNETO IMPULSE COUPLING PAWL WAS FOUND CRACKED FROM THE RIVET HOLE TO OUTER EDGE OF PAWL. A NEW IMPULSE COUPLING WAS INSTALLED AND ACFT RETURNED TO SERVICE. CAUSE OF CRACK MAY BE IMPROPSDR 2012FA0000695Wire · failedDURING A ROUTINE INSPECTION, IT WAS NOTED THAT THE STROBE LIGHTS WOULD REMAIN ON AFTER THE SWITCH WAS SELECTED OFF, TROUBLESHOOTING REVEALED THE SWITCH TO BE DEFECTIVE. REPLACED THE SWITCH AND DISASSEMBLED AND FOUND THAT THE SOLDER JOINT HOLDING THE BRAIDED WSDR 2012FA0000681Wire · detachedDURING A ROUTINE INSPECTION, NOTED THAT THE STROBE LIGHTS WOULD REMAIN ON AFTER THE SWITCH WAS SELECTED OFF. TROUBLESHOOTING REVEALED THE SWITCH TO BE DEFECTIVE. REMOVED SWITCH AND DISASSEMBLED AND IT WAS FOUND THAT THE SOLDIER JOINT HOLDING THE BRAIDED WIRESDR 2012FA0000363Blade · gougedNOTICED OIL ON NOSE COWL. PROP REMOVED TO REPLACE CRANKSHAFT O-RING. BUT DURING REMOVAL, IT WAS DISCOVERED THAT THE SEEPAGE WAS ACTUALLY COMING FROM A BLADE. SEEPAGE WAS CONSIDERED MINOR AND PROPELLER OPERATION APPEARED NORMAL. REPAIR SHOP DISCOVERED DURINSDR 2012FA0000265Spring · brokenDURING FLIGHT, THE PILOT NOTICED THE AILERON CONTROL WAS PULLING TO THE RT. ACFT RETURNED TO BASE WITHOUT INCIDENT. UPON INSP OF AILERON CONTROL SYS THE UPPER AILERON/RUDDER INTERCONNECT SPRING PN 35-5524664 WAS FOUND BROKEN AT THE BELLCRANK ARM, PN 002-5240SDR 2012FA0000257Contact · missingENGINE WAS RUNNING ROUGH AND WHEN THE MAG SWITCH WAS MOVED TO THE RT MAGNETO POSITION, THE ENGINE WOULD STALL. PERFORMED RUN UP TO VERIFY DISCREPANCY. REMOVED MAG FROM ENGINE AND DISASSEMBLED FAR ENOUGH TO FIND THAT THE CONTACT ASSY PN M3081 HAD THE ARM CONTSDR 2012FA0000005Adapter · brokenENGINE FAILS TO START, PROP WAS LOCKED SOLID. STARTER ADAPTER REMOVED TO FIND 2 GEAR TEETH MISSING. EMERGENCY AD 2011-25-51 SEEMS TO BE RELEVANT TO THIS FAILURE BUT DOES NOT COVER THIS ENGINE TYPE AND STARTER PN. UNABLE TO ASCERTAIN ENGINE HOURS, BUT BELIEVSDR C41R201110060105Circuit Breaker · shortedACFT IN ANNUAL INSPECTION. ELECTROLUMINESCENT PANEL LIGHTING INOPERATIVE. TROUBLESHOT SYS AND FOUND MAIN CIRCUIT BREAKER PANEL, CENTER ROW STRIP PANEL TO BE INTERNALLY SHORTED. REMOVED PANEL FROM CIRCUIT AND ALL OTHER STRIP PANELS LIGHT OK. SENT OUT BAD PANESDR C41R201110030104Annunciator · burned outDURING PRE-INSPECTION RUN-UP, TECH FOUND "FD" LIGHT INOP ON AUTOPILOT ANNUNCIATOR. UNIT REMOVED FOR REPAIR.SDR C41R201110030103Indicator · intermittentDURING PRE-INSPECTION RUN-UP, TECH FOUND OIL TEMPERATURE AND OIL PRESSURE NEEDLES (DUAL GAUGE) INTERMITTENTLY PEG FULL SCALE. REMOVED GAUGE AND FOUND SMALL PIECES/PARTS RATTLING AROUND INSIDE UNIT. ALSO, GAUGE CORE MOVES FORE AND AFT (REAR SCREWS MISSING). SSDR 2011FA0000441Cylinder · crackedON INITIAL CLIMB OUT PILOT NOTICED A VIBRATION AND ELECTED TO RETURN FOR LANDING. THE NR2 CYLINDER WAS FOUND CRACKED FROM THE SPARK PLUG, PAST THE EXHAUST VALVE AND APPROXIMATELY 75 PERCENT AROUND THE HEAD / CYLINDER. THE CYLINDER HAD GOOD COMPRESSION (72/80) SDR XGN2011F00009Wire · disconnectedALTERNATOR FAILED IN FLIGHT. WIRES TO THE BRUSH BLOCK HAD BECOME DISCONNECTED INSIDE THE ALTERNATOR.SDR 2011FA0000044Oil Cooler · crackedAFTER AN OIL CHANGE, THE CUSTOMER COMPLAINED OF OIL ON TOP OF THE NOSE GEAR WELL AREA BEHIND & BELOW ENGINE. ENGINE COMPARTMENT CLEANED, GROUND RUN & ENGINE COMPARTMENT INSPECTED FOR LEAKS. NONE NOTED. CUSTOMER CONTACTED SHOP THE FOLLOWING WEEK AFTER FLYING OVSDR 2010FA0001188Pulley · loose(OY1R) AFTER LANDING, PILOT NOTICED OIL DRIPPING FROM BELLY OF ACFT. FURTHER INSP REVEALED AC DRIVE PULLEY MOUNTED AT AFT SIDE OF STARTER ADAPTER HOUSING LOOSE WHEN MOVED SIDE TO SIDE BY HAND. DURING REMOVAL OF STARTER ADAPTER HSG , IT WAS NOTED THAT THE SHASDR 2010FA0001152Baffle · chafedTHE FRONT 2 PRODUCTS CENTER AND LT BAFFLES WERE FOUND CHAFED THROUGH THE INNER NOSE BOWL AND CAUSED A HOLE APPROX 7 INCHES LONG AND .2500 INCH WIDE. THE BAFFLES ENDED UP TOO LONG OVER TIME AS THE ENGINE MOUNTS STARTED TO SAG. HAVE HEARD OF SEVERAL OTHER REPOSDR 2010FA0001151Baffle · chafedTHE FRONT 2 PRODUCTS CENTER AND LT BAFFLES WERE FOUND CHAFED THROUGH THE INNER NOSE BOWL AND CAUSED A HOLE APPROX 7 INCHES LONG AND .2500 INCH WIDE. THE BAFFLES ENDED UP TOO LONG OVER TIME AS THE ENGINE MOUNTS STARTED TO SAG.SDR 2010FA0000785Camshaft · wornDURING REMOVAL OF CYLINDER ASSEMBLIES FOR TOP O/H, FOUND SEVERAL LIFTERS SPALLED AND EXCESSIVE CAM LOBE WEAR. RECOMMEND THAT AD 2010-11-04 AND TCM MSB098A BE REVISED TO INCLUDE ENGINE MFG EARLIER THAN SPECIFIED IN THE AD. THIS ENGINE WAS BUILT IN 2005.SDR 2010FA0000746Bevel Gear · chippedALTERNATOR FAILURE IN FLIGHT. NORMAL LANDING. UPON REMOVAL OF ALTERNATOR BY MX, (FRT MOUNT, DIRECT DRIVE ALTERNATOR) FOUND ALTERNATOR DRIVE GEAR INSIDE ENGINE TO BE DAMAGED (GEAR TEETH CHIPPED, AND "ARC'ED LOOKING") NO SIGNS OF DAMAGE TO THE "DRIVEN" (ALTERNASDR 2010FA0000637Hose · leakingDURING ANNUAL INSPECTION, NOTICED A POSSIBLE FLASH FIRE IN ENGINE COMPARTMENT. AFTER FURTHER INSP, FOUND FUEL HOSE (330995F-0060 FROM FUEL FLOW SENSOR TO FUEL SPIDER HAD BEEN LEAKING. REMOVED FUEL HOSE AND PRESSURIZED LINE WITH AIR AND FOUND HOSE LEAKING THRSDR 2010FA0000715Cylinder · leakingDURING A ROUTINE 100 HR INSP, A CYLINDER COMPRESSION TEST WAS PERFORMED ON THE ENGINE USING SOAP SOLUTION FOR VISUAL INSPECTION AND DURING THAT CHECK IT WAS FOUND THAT THE NR 4 CYLINDER (SN 4857) AND NR 6 CYLINDER (SN 4864) WERE LEAKING OUT OF THE SIDES OF THESDR 2010FA0000582Rib · cracked((OF1R)) DURING AN ANNUAL INSP, THE RT FLAP RIB WAS FOUND CRACKED THROUGH THE L/E RELIEF CUTOUT, IN THE UPPER FANGE BEND RADIUS, AND THROUGH THE ACTUATOR ATTACH BRACKET NUTPLATE RIVET HOLES. THIS COULD ONLY BE VIEWED THROUGH THE INBD ROLLER BOLT ACCESS HOLE. SDR 2010FA0000580Rib · cracked((OF1R)) DURING AN ANNUAL INSP, 1 RT FLAP NOSE RIB WAS FOUND CRACKED. IT IS THE RIB LOCATED DIRECTLY BENEATH THE ACTUATOR ATTACH BRACKET. IT WAS CRACKED IN THE RELIEF CUTOUT FOR THE FLANGES AND THROUGH THE MOST FWD NUTPLATE RIVET HOLES. VERY INACCESSABLE ASDR 2010FA0000538Rib · crackedDURING AN ANNUAL INSP, (1) NOSE RIB WAS FOUND CRACKED IN THE RT FLAP. IT IS THE RIB LOCATED DIRECTLY BENEATH THE ATTACH BRACKET MOUNTED ON THE SKIN.SDR 2010FA0000419Exhaust Valve · brokenACFT EXPERIENCED POWER LOSS, VIBRATION, AND LOW NR EGT ON INSP THE NR 2 CYLINDER EXHAUST VALVE WAS FOUND TO BE MISSING ABOUT HALF OF IT'S FACE.SDR 2010FA0000418Exhaust Valve · brokenAIRCRAFT EXPERIENCED POWER LOSS, VIBRATION, AND LOW NR 2 EGT. ON INSPECTION THE NR 2 CYLINDER EXHAUST VALVE WAS FOUND TO BE MISSING ABOUT HALF OF IT'S FACESDR 2010FA0000243Cylinder · crackedTHIS IS THE LATEST OF SEVERAL CYLINDERS PN SA52006A-1 WE HAVE HAD DEVELOP CRACKS BETWEEN HEAD AND BARREL ON EXHAUST SIDE. THE COMPRESSION WAS NORMAL AT 75/80 PSI, BUT WHEN A SOAP SOLUTION WAS APPLIED BETWEEN THE FINS A CRACK WAS FOUND.SDR 2010FA0000215Control Cable · frayedDURING A PRE-PURCHASE INSPECTION, FOUND CONTROL YOKE BINDING WHEN TURNED TO THE LT AT APPROX 45 DEGREES. INSPECTED AILERON CNTRL SYS AND FOUND SCREW LODGED IN PULLEY GROOVE AND DAMAGED CABLE. ACFT HAD FLOWN 2.0 HRS SINCE LAST ANNUAL INSPECTION. THE SCREW APSDR 2010FA0000281Fuel Nozzle · fod(HOQR) ENGINE WOULD NOT MAKE RATED POWER AND WAS ROUGH RUNNING ONCE ACFT WAS OF THE GROUND. TROUBLESHOT ISSUE AND FOUND IT TO BE FOREIGH OBJECTS ON THE AIR SIDE OF THE FUEL INJECTOR NOZZLES. THE FOREIGH OBJECTS APPEARED TO BE O-RING MATERIAL INTRODUCED THRU SDR 2010FA0000280Wastegate Valve · leakingOIL LEAKING FROM WASTEGATE ACTUATOR SHAFT. R & R WASTEGATE WITH A SECOND O/H UNIT. SECOND WASTEGATE ALSO LEAKED OUT THE ACTUATOR SHAFT. CHECKED INSTALLATION AND FOUND IT TO BE INSTALLED IAW STC NR SA 762NW INSTALLATION INSTRUCTION 68-1, DATED MAY 1, 1979, ASDR 2009FA0001013Clamp · brokenDURING ACCIDENT INVESTIGATION, FOUND TOP LT ENGINE COWLING WITH EVIDENCE OF FIRE AND BURNED HOLES, LT EXHAUST MANIFOLD PIPE WAS LAYING LOOSE, AND LT CLAMP TO TURBO COMPRESSOR BROKEN AND LAYING IN BOTTOM OF ENGINE COWL. AIRCAFT WAS DESTROYED IN FIRE WITH ONE FSDR 2009FA0001030Cylinder · leakingDURING A ROUTINE 100 HR INSPECTION A CYLINDER COMPRESSION TEST WAS PERFORMED ON THE ENGINE USING SOAP FOR VISUAL INSPECTION AND DURING THAT CHECK IT WAS FOUND THAT THE NR 3 CYLINDER (SN 4847) WAS LEAKING OUT OF THE TOP OF THE CYLINDER HEAD BETWEEN FINS ON THE SDR 2009FA0001029Cylinder · failedDURING LANDING PHASE OF AN INSTRUCTION FLIGHT, THE PILOT HEARD A LOUD "BANG" AND IMMEDIATE ENG VIBRATION. UPON LANDING THE ACFT SAFELY THE INSTRUCTOR AND STUDENT NOTICED THA THE RPM COULD NOT GBE BROUGHT BACK BELOW 1500 RPM. ONCE PARKED THEY OBSERVED A LARGESDR 2009FA0001011Circuit Breaker · failedUPON INSTALLATION OF NEW REPLACEMENT CIRCUIT BREAKERS TO COMPLY WITH AD 2008-13-7, IT WAS FOUND THAT TIGHTENING OF SWITCH RETAINER NUT ON THE INSTRUMENT PANEL CAUSED SWITCH SEPARATION AND FAILURE. AS THESE SWITCHES HAVE TO SUPPORT THE BUSS AND WIRE BUNDLE, IF SDR 2009FA0000512Clevis · separatedTHE NOSE GEAR RETRACT PLUNGER BRAZE ASSY CLEVIS SEPARATED FROM (PULLED OUT OF) THE PLUNGER ROD. CLEVIS IS BRAZED INTO THE ROD, EXCEPT IN THIS CASE, DURING THE MFG PROCESS, BRAZE DID NOT FLOW INTO THE AREA BETWEEN THE CLEVIS AND THE ROD. THERE WAS A BEAD OF BSDR 2009FA0000648Impulse Coupling · failedMAGNETO, HAVING RT ROTATION AND IMPULSE COUPLING. INSTALLED ON ENG. ONE OF THE FLYWEIGHTS SEPARATED FROM THE IMPULSE COUPLING BODY AND BECAME JAMMED BETWEEN THE COUPLING AND THE MAGNETO HSG. THE DRIVE GEAR FORCE BROKE THE FLANGE OF THE MAGNETO CAUSING IT TOSDR 2009FA0000460Bolt · brokenPILOT FLEW A NORMAL FLIGHT OF 1.5 HOURS, FOUND OIL CONSUMPTION AT 5.0 QTS. INVESTIGATION FOUND A FOREIGN OBJECT BLOCKING THE TURBO OIL SCAVENGE LINE CHECK VALVE. WHEN AN ATTEMPT WAS MADE TO START THE ENGINE AFTER REPAIR OF THE CHECK VALVE, THE STARTER SPUN FSDR 2009FA0000255Wire · arcedTHIS IS ACTUALLY A G-36. THE ENGINE LOST POWER ON CLIMBOUT. TROUBLESHOOTING REVEALED THAT THE FUEL DELIVERY LINE 36-920001-13 HAD A HOLE ARCED IN IT FROM AN ELECTRICAL WIRE, P6 PIN 14 WIRE H21A20. THE WIRE BUNDLE HAD BEEN RUBBING AGAINST THE FUEL LINE AND HASDR 2009FA0000208Bellcrank · corrodedWHILE PERFORMING SB 27-3935 ELEVATOR BELLCRANK BRG REPLACEMENT, CORROSION WAS FOUND INSIDE THE BELLCRANK BEARING BOSS. THIS CORROSION IS BETWEEN THE 2 BEARING SEAT AREAS. (K)SDR 2009FA0000145Bolt · wrong partDURING THE COMPLIANCE WITH RECOMMENDED SB 27-3929, BOTH ELEVATOR TORQUE TUBES MOUNT BOLTS (8 TOTAL, 4 PER SIDE) WERE SHANKED OUT AND NOT TIGHT AT THE ATTACH POINTS. THE IPC CALLS FOR BOLTS AN-23-10, AND THE REPLACEMENT BOLTS ARE AN23-9. THIS SHOULD BE A MANDASDR 2009FA0000009Fairing · crackedAIR CONDITIONER CONDENSER L/E FAIRING WAS CRACKED ALL THE WAY ACROSS. THE CRACK RAN THE ENTIRE WIDTH OF THE FAIRING THROUGH THE MOUNTING SCREW HOLES. THE ONLY THING HOLDING IT ON WAS THE CONDENSER ACTUATOR ROD.SDR 2008FA0000681Cylinder · crackedAIRCRAFT OWNER REPORTED SEVERE VIBRATION. AFTER INSPECTION IT WAS FOUND THAT SPINNER BULKHEAD WAS SEVERELY CRACKED. AFTER FURTHER INSPECTION NR 1 CYLINDER WAS FOUND TO BE CRACKED ALL AROUND THE CIRCUMFERENCE OF THE CYLINDER DIAMETER. THE CRACK WAS RIGHT AT THSDR WS9R030608001Cylinder · crackedCRACK BETWEEN 3RD AND 4TH CYLINDER HEAD, COOLING FIN.SDR 2007FA0001086Nose Rib · crackedAT ANNUAL INSPECTION FOUND BOTH LT AND RT FLAP ATTACH POINT RIBS CRACKED. (K)
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