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 = 'A185F' 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 = 'A185F' 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 20001120SH040Drive Shaft · defectiveSTARTER DRIVE STARTED MAKING NOISE WHEN CRANKING ENGINE. WHEN STARTER WAS REMOVED, LOWER FLANGE OF STARTER DRIVE WAS FOUND TO BE BROKEN. WHEN ''STARTER DRIVE'' SHAFT WAS TURNED AFTER REMOVAL FROM ENGINE, IT WAS VERY NOISY LIKE A VERY BAD BEARING OR SOMETHINGSDR CA000803002Cylinder · cracked(CAN) HEAD CRACKED TWO/THIRDS AROUND AT 3RD FIN FROM BOTTOM OF HEAD. HEARD BY MAINTENANCE WHEN AIRCRAFT WAS TAXIING TO DOCK, PILOT REPORTED NO INDICATION OF PROBLEM. NO CAUSE FOUND. CYLINDER REPLACED.SDR 20000724SH019Muffler · separatedMUFFLER OUTLET PIPE FELL OFF AFTER TAKEOFF. AIRCRAFT RETURNED. MUFFLER AND SHROUD WERE REPLACED. AIRCRAFT RELEASED TO SERVICE. (X)SDR CA010507002Hub · cracked(CAN) A ROUTINE MAINTENANCE INSPECTION RED DYE LEAKAGE WAS OBSERVED ON PROP BLADES. PROP WAS REMOVED AND SHIPPED TO PROPELLER SHOP AND HUB WAS FOUND CRACKED. 2001-05-09 TC: FAA AD PERTAINS.SDR 20001218SH036Bushing · crackedON INSPECTION OF TAILWHEEL SUPPORT BUSHINGS, FOUND NEWLY INSTALLED BUSHINGS SEVERELY WORN, EXTRUDED AND CRACKED. THESE BUSHINGS, OBTAINED FROM CESSNA, ARE MADE OF INFERIOR MATERIALS. (X)SDR 20001218SH035Bushing · wornTAILWHEEL TO AFT BULKHEAD SUPPORT BUSHINGS FOUND SEVERELY WORN. SUBMITTER STATED NEW PARTS OBTAINED FROM CESSNA APPEAR TO BE MADE FROM INFERIOR MATERIALS. (X)SDR CA000614025Cylinder · cracked(CAN) CRACK BETWEEN SPARK PLUG AND EXHAUST PORT.SDR AU000401Capacitor · faulty(AUS) RIGHT MAGNETO CAPACITOR FAULTY. CAPACITOR WAS A NEWLY FITTED ITEM.SDR 20000719SH014Crankshaft · failedPER TCM MSB 00-5, CRANKSHAFT WAS REJECTED BY TELEDYNE CONTINENTAL MOTORS. (X)SDR 20000602SH006Crankshaft · unserviceablePER TCM MSB 00-5, CRANKSHAFT WAS REJECTED BY TELEDYNE CONTINENTAL MOTORS. (X)SDR CA000404022Blade · cracked(CAN) BLADE THREADS CRACKED S/N K67168YSSDR 2003FA0001214Mount · crackedDURING AN ANNUAL, FOUND THE RT MAIN GEAR BOX STRUCTURE TO BE CRACKED. ALSO NOTED THAT THE RT GEAR WAS LOOSE IN CASTING.SDR 2000ZZZX843Bracket · brokenRIGHT FLAP RETRACTED AFTER PILOT SELECTED FIRST NOTCH OF FLAPS. FOUND INBOARD MOUNTING EARS BROKEN AWAY FROM PULLEY BRACKET LOCATED JUST AFT OF FLAP HANDLE. SUBMITTER STATED THIS IS THIRD BRACKET REPLACED IN FLEET OF THREE A185F'S.SDR 2000ZZZX642Muffler · damagedMUFFLER TAILPIPE BROKEN LOSE FROM BODY. DEFECT NOTED TO BE CRACKS IN A VERY UNUSUAL AREA. NOT A WELD OF BODY AND TAILPIPE. SUSPECT MUFFLER SHELL/BODY MATERIAL PROBLEM PART WAS NEW MANUFACTURE WITH 131 HOURS TOTAL TIME. SHOWED NO SIGN OF ADVERSE STRESS. (XSDR 2000ZZZX637Line · crackedFUEL PRESSURE LINE BROKEN AT FITTING (FIREWALL TO ENGINE).SDR 2000ZZZX650Line · brokenFUEL PRESSURE LINE BETWEEN ENGINE AND FIREWALL BROKEN AT SILVER SOLDER JOINT. (X)SDR 2000ZZZX649Line · brokenFUEL PRESSURE LINE BETWEEN ENGINE (BAFFLE) AND FFIREWAL BROKEN AT SILVER SOLDER JOINT. (X)SDR 20000404SH016Hose · disintegratedFOUND HOSE .3750 INCH AND .25 INCH (AS REQUIRED BY SUCTION SYSTEM/INSTRUMENTS) TO HAVE ITS RED INNER SLEEVE COMPONENT DISINTEGRATED AND HOSE BLOCKED. SECTIONS OF BLACK OUTER SLEEVE WOULD ALSO DISINTEGRATE ON CONTACT. ORIG CAUSE FOR INVEST WAS VARIOUS SUCTIONSDR CA991208062Cylinder · separated(CAN) ROUGH ENGINE ON TAKEOFF EXPERIENCED. INSPECTION REVEALED NR 2 CYLINDER SEPARATED AND CRACKED FROM EXHAUST PORT THROUGH BOTH SPARK PLUGS AND COOLING FINS.SDR CA990927024Housing · corroded(CAN) THE POLE SHOES IN THE MAGNETO HOUSING WERE FOUND RUSTED AND WERE RUBBED BY THE ARMATURE (ROTATING MAGNET). PARTICLES WERE FOUND SCATTERED IN THE DISTRIBUTOR CAP CAUSING MISFIRING TO GROUND AND OTHER CYLINDERS. THE SUBMITTER SUGGESTS THE CORROSION WAS CSDR 99ZZZX3745Strut · failedDURING THE LANDING ROLL-OUT, THE LEFT GEAR LEG SHEARED OFF THROUGH THE TWO UPPER BOLT HOLES THAT ARE USED TO HOLD THE AXLE ON CAUSING THE AIRCRAFT TO NOSE OVER ON ITS BACK. THE AIRCRAFT IS USED IN THE WINTER ON WHEEL SKIS AND IN THE SUMMER ON TIRES. MOST OF SDR 20000622SH007Strut · crackedRIGHT MAIN LANDING GEAR LEG FOUND CRACKED IN UPPER AXLE ATTACH BOLT HOLE TO LEADING EDGE. AIRCRAFT OPERATED ON C4000 WHEEL SKIS. 1,032 HRS SINCE LAST INSPECTION (MAGNAFLUX) OF GEAR LEG. (X)SDR CA991007085Rocker Boss · broken(CAN) BROKEN EXHAUST ROCKER BOSS ON NR 1 CYLINDER.SDR CA990907019Cylinder · cracked(CAN) NR 6 CYLINDER CRACKED NEAR EXHAUST VALVE.SDR CA990728079Connecting Rod · failed(CAN) NR 1 CONNECTING ROD FAILURE, ENGINE DAMAGE SEVERE. FURTHER INVESTIGATION AT TEAR-DOWN.SDR 99ZZZX2807Adapter · brokenFAILURE OF BEARING DUE TO CORROSION CAUSING SHAFT TO SHIFT AND DAMAGE CRANKCASE. BEARING VERY ROUGH AND NEAR FAILURE DUE TO CORROSION AND RUST. TELEPHONE CONVERSATION WITH MFG, CONTINENTAL, SAYS THAT AFTER MARKET ENGINE HEATERS MAY CONTRIBUTE TO MOISTURE IN SDR CA990719001Capacitor · failed(CAN) RIGHT MAGNETO CAPACITOR FAILURE. ENGINE WOULD NOT SHUT DOWN WITH MAGNETO SWITCH.SDR 99ZZZX2541Head · crackedCRACK DEVELOPED FROM SPARK PLUG HOLE TOWARD INTAKE VALVE. COMPRESSION CHECK WAS GOOD BECAUSE CRACK WAS ABOVE COMBUSTION CHAMBER.SDR 20000713SH007Throttle Cable · brokenTHROTTLE CABLE OUTER HOUSING SEPARATED AT THE THROTTLE HORN END CAUSING SLOPPY OPERATION OF THROTTLE CONTROL. (X)SDR 99ZZZX2376Axle · damagedAIRCRAFT ON WHEEL SKIS. TURNING AIRCRAFT BY HAND APPLIED TORQUE LOAD TO LANDING GEAR.SDR 99ZZZX2051Support · wornPILOT REPORTED MIXTURE SETTING CONSISTANCY WAS ERRATIC. INVESTIGATION INTO THE CONTROL MOUNT IN THE ENGINE COMPARTMENT REVEALED THE U-CHANNEL THAT SUPPORTS THE MIXTURE CONTROL HAD WORN TO AN EXTENT THAT THE CABLE HOUSING WAS SLIDING IN THE MOUNT. THE OUTER CSDR 99ZZZX2038Bellcrank · wornDURING INSTALLATION OF TAILCONE ACCESS PANELS AT STA 198, DISCOVERED THE BELLCRANKS FOR TAIL WHEEL STEERING (WHERE THE SPRING ATTACHES) WERE WORN EXTENSIVELY. FURTHER INVESTIGATION REVEALED THE STEEL BUSHING WAS MISSING ON BOTH BELLCRANKS RESULTING IN EXCESSISDR 99ZZZX1214Line · chafedFUEL LINE DAMAGED DURING PRIOR REPAIR, NOT LEAKING, BUT NICKED BY DRILLING AND INSTALLATION ALIGNMENT CAUSING CHAFING.SDR 99ZZZX1213Line · chafedAILERON CABLE CHAFED FUEL LINE. RUBBED THROUGH PLASTIC PROTECTOR AND INTO ALUMINUM LINE. CAUSED BY MISALIGNED FUEL LINE.SDR 99ZZZX1114Line · chafedDURING AN ANNUAL INSPECTION, FUEL FUMES WERE DETECTED UNDER THE INSTRUMENT PANEL, NEAR THE COPILOT RUDDER PEDALS FUEL STAINS WERE FOUND ON THE CABIN FLOOR MAT. INVESTIGATION REVEALED THE FUEL LINE HAD BEEN CHAFED THROUGH BY THE CABIN AIR CONTROL CABLE. SUBMISDR 99ZZZX1060Line · chafedFLAP CABLE CHAFING FUEL LINE 7 INCHES FROM UPPER END. CABLE RUBBED THROUGH PLASTIC SHIELDING AND .020 INCH DEEP INTO FUEL LINE.SDR CA990224019Mount · broken(CAN) AFTER REMOVING THE ENGINE COWLING, THE ENGINE SUPPORT WAS FOUND BROKEN.SDR CA990210005Bracket · cracked(CAN) INBOARD FLAP TRACK BRACKET IN THE LEFT AND RIGHT WINGS FOUND CRACKED.SDR 99ZZZX1407Bracket · corrodedBRACKET HAD INTERGRANULAR CORROSION ON THE BOTTOM OF THE MAIN LANDING GEAR CUT.SDR CA981125055Engine · failed(CAN) AIRCRAFT PRE-HEATED FOR 4 HRS PRIOR TO START DUE TO -19 CELSIUS OVERNIGHT TEMP. 100 LL FUEL WAS OBTAINED FROM SEALED DRUMS. ENG RUN-UP WAS GOOD. TAKEOFF WAS GOOD WITH ENG PRODUCING FULL POWER AND RPM. ALL ENG PARAMETERS WERE NORMAL. ACFT CLIMBED TO SDR 98ZZZX4790Collector · brokenNR 6 EXHAUST FLANGE BROKEN OFF EXHAUST COLLECTOR.SDR 98ZZZX4789Control Cable · damagedELEVATOR LOWER CABLE FRAYED AT FS 140.0, RUBBING ON WEAR BLOCK. INSPECTED ALL CABLES THAT MAKE CONTACT WITH ANOTHER SURFACE, PULLEYS, RUB BLOCKS.SDR CA981207002Crankcase · cracked(CAN) INSPECTION FOUND ENGINE CASE CRACKED AT A NON-CRITICAL AREA, RADIATING OUT FROM CYLINDER HOLD-DOWN STUD.SDR 98ZZZX4541Bulkhead · crackedPARTS ARE THE COMPONENTS OF STA 90.00. THEY RIVET TOGETHER. THIS AREA IS WHERE THE FLOAT KIT IS INSTALLED. RIGHT AND LEFT FLOAT ATTACH AREA WAS CRACKED IN MANY PLACES. THIS AIRCRAFT HAS BEEN ON FLOATS MOST OF ITS LIFE. SUBMITTER SUGGESTED INSPECTION OF THSDR 98ZZZX4490Brake Disk · failedSUBJECT BRAKE DISK INSTALLED ON EDO 3500 AMPHIBIOUS FLOATS. FLANGE FAILURE AT EACH OF THREE MOUNTING HOLES TO WHEEL RESULTING IN LOCKED BRAKE. DISK IS EXCESSIVELY LOADED IN THIS INSTALLATION DUE TO GROSS WINDS OF AIRCRAFT, SPEEDS, AND NECESSITY OF OVERUSE OFSDR CA981007004Channel · cracked(CAN) ON 100-HOUR INSPECTION, THE LEFT REAR REINFORCEMENT BOX ON THE HORIZONTAL STABILIZER WAS FOUND CRACKED FROM THE BOLT HOLE. THE SPAR REINFORCEMENT CHANNEL WAS ALSO FOUND CRACKED. CRACK ABOUT 2 INCHES LONG. P/N OF CHANNEL 0732603.SDR 99ZZZX102Fuel System · contaminatedCONTAMINATED FUEL RECEIVED AT AIRPORT DURING JULY, AUG, 1998, IS BELIEVED RESPONSIBLE FOR: INCREASED OIL CONSUMPTION, CYLINDER COMPRESSIONS RAPIDLY DETERIORATING, INJECTORS PLUGGING, SPARKPLUGS FOULING, FUEL SYSTEM COMPONENTENTS FAILING. AIRCRAFT ARRIVED WITHSDR CA980915014Nose Gear · out of adjust(CAN) LEFT FLOAT MAIN GEAR WOULD NOT LOCK UP ALL THE TIME. MAIN SLIDE FITTING IN UP POSITION, BUT NOT LOCKED. PUMP WOULD CONTINUE TO OPERATE TO FORCE GEAR TO LOCK. NEITHER CABLE ADJUST, NOR TENSION CYLINDER O-RING REPLACEMENT DID ANY GOOD. LEFT NOSE STRUT SDR 98ZZZX3076Regulator · failedOVERVOLTAGE LIGHT CAME ON IN-FLIGHT. REPLACED VOLTAGE REGULATOR.SDR 98ZZZX2656Duct · detachedTHE ENGINE LOST POWER SHORTLY AFTER TAKEOFF. FOUND ENGINE AIR INTAKE DUCT DISCONNECTED FROM DUCT ADAPTER P/N 1652021-10. CLAMP WAS STILL ON THE ADAPTER. THIS DUCT IS MADE OF SILICON IMPREGNATED CLOTH AND BECOMES VERY FLEXIBLE WITH EXTENDED USE AND VERY SLIP
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