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 = 'B36TC' 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 = 'B36TC' 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 2025FA0000681Oxygen Bottle · leakingTIMED OUT OXYGEN BOTTLE WITH SERVICEABLE OXYGEN REGULATOR WERE SENT TO AEROSPACE TURBINE ROTABLES FAA CRS NV2R045L UNDER WO: WO218149. THE SERVICEABLE REGULATOR WAS REMOVED AND INSTALLED ON A NEW BOTTLE. WHEN WE RECEIVED THE "INSPECTED/TESTED" BOTTLE AND REGSDR FAA2017113000001Strut · separatedON TAKE OFF ROTATION, LOWER NOSE GEAR STRUT AND AXLE ASSEMBLY SEPARATED FROM THE UPPER STRUT AND DEPARTED THE AIRCRAFT. INVESTIGATION REVEALED THE UPPER TORQUE LINK TO BE DESTROYED DURING CONTACT WITH THE RUNWAY ON LANDING. LOWER TORQUE LINK REMAINED ATTACHEDSDR 2014FA0000700Cylinder Head · crackedDURING AN INSPECTION, IT WAS NOTICED ON THE TOP COWL BLACK SOOT NEAR CYLINDER NR 5. COMPRESSION TEST DONE AND CYLINDER SPRAYED WITH SOAP SOLUTION. BUBBLES WERE SEEN WHERE THE CYLINDER HEAD AND BARREL ATTACH. CYLINDER REMOVED AND CRACK FOUND. THIS IS CYLINDSDR 2014FA0000001Plate · crackedENGINE WAS IN OVERHAUL, A REBUILT TURBOCHARGER WAS INSTALLED ON THE ENGINE AT THAT TIME. THE ENGINE WAS INSTALLED, THE TURBOCHARGER WAS REMOVED DUE TO AN OIL LEAK AND RETURNED. TURBOCHARGER WAS REPAIRED AND REINSTALLED ON THE ENGINE. THE TURBOCHARGER WAS RESDR 2012FA0000483Intake Valve · crackedTROUBLESHOT ROUGH RUNNING ENGINE. FOUND NR 4 CYLINDER HAS NO COMPRESSION. REMOVED CYLINDER AND FOUND DAMAGED INTAKE VALVE. THIS O/H CYLINDER ASSY WAS INSTALLED 10/14/06. TSI 271.0. THIS CYLINDER ASSY, PN EC636122, VALVE, PN AEC539988W. FOR INSTALL INFO: SDR 2010FA0001199Camshaft · spalledDURING CYLINDER REPLACEMENT DUE TO LOW COMPRESSION FOUND NR3 & NR4 INTAKE LOBE ON CAM WORN AND SPALLING. ENGINE REMOVED FOR CAM REPLACEMENT OR ENGINE O/H. SPALLING OF LIFTER FACES ALSO NOTED.SDR 2009FA0000333Support · arcedDURING FLIGHT THE PILOT NOTICED THE INSTRUMENT SUBPANEL LIGHTING FLICKERING. UPON INSP THE WIRE BUNDLE THAT CROSSES OVER THE CENTER SUPPORT FWD OF THE INSTRUMENT PANEL HAD (2) WIRES CHAFED AND ARCING ON THE SUPPORT. DAMAGED SECTION OF THE WIRING WAS REPLACED ASDR 2006FA0000908Switch · fouledLANDING GEAR WOULD NOT EXTEND ELECTRICALLY UPON APPROACH TO RFD. MANUAL EXTENSION OPERATIONS NORMAL. TROUBLESHOT LANDING GEAR ELECTRICAL SYS. FOUND S45 LANDING GEAR ACTUATOR DYNAMIC BRAKE DOWNLIMIT SWITCH OIL SOAKED AND FOULED BY LINT, FUZZ, ETC. CLEANED DSDR 2006FA0000465Bolt · crackedMAG PART INSP FOUND FWD WING ATTACH POINTS BOLT P/N 130909B103 AND 131790-3 CRACKED. BOLTS INSTALLED NEW IN FWD WING BOLT FITTINGS ON BEECH MODEL 36 SER A/C S/N EA-455 ON 1/25/2002. THE LT UPPER BOLT (P/N 130909B103) REMOVED FOR FIRST 5 YEAR NDT INSPECTION ANSDR 2006FA0000464Bolt · crackedMAG PART INSP FOUND FWD WING ATTACH POINTS BOLT P/N 130909B103 AND 131790-3 WITH CRACKS. THE BOLTS WERE INSTALLED NEW IN FWD WING BOLT FITTINGS ON BEECH MODEL 36 SERIES AIRCRAFT S/N EA-455 ON 1/25/2002. THE LH UPPER BOLT (P/N 130909B103) WAS REMOVED FOR IT'S SDR 2005FA0001080Alternator · failedAIRCRAFT ENGINE RUNNING AND ALTERNATOR SWITCH SELECTED TO (ON) POSITION, ALTERNATOR RED ANNUCIATOR LIGHT (ON) AND LOAD METER SHOWING ZERO LOAD BEING CARRIED BY ALTERANTOR. AC OIL TEMP AND OIL PRESSURE INDICATIONS DROPPED TO ZERO IN FLIGHT AS BATTERY VOLTAGE DSDR Q532004F00000Connecting Rod · bentROUGH RUNNING ENGINE, PULLED NR 4 CYLINDER FOUND CONNECTING ROD HAD SLIGHT BEND. CAM SHAFT LOBES FORWARD OF CYL 4, WORN OUT.SDR QCW2004F00000Heat Shield · chafedTHE TURBO HEAT SHIELD CHAFED 30 PERCENT THROUGH THE LT INDUCTION ELBOW DUE TO ENGINE VIBRATION. STRICT ATTENTION SHOULD BE PAID TO THE AFT IB SIDE OF HEAT SHIELD. THE HEAT SHIELD HAD TO BE ALTERED TO PREVENT FURTHER REOCCURRENCE OF THIS SITUATION.SDR AKG2004F00006Nut · looseWHILE COMPLETING AN ANNUAL INSPECTION. ONE OF THE CYLINDER RET BASE NUTS FOR THE NR 4 CYLINDER WAS MISSING. NUT WAS FOUND BETWEEN CYLINDER. TORQUE CHECK MADE OF THE OTHER NUTS FOUND 3 MORE LOOSE. WE CHECKED THE OTHER CYLINDER AND FOUND THEN TO BE OK. ALL SDR 2003FA0000857Rod End · wornAIRCRAFT WAS IN FOR ITS FIRST ANNUAL INSPECTION SINCE NEW. FOUND FORWARD PROP CONTROL ROD END WORN BEYOND SERVICEABLE LIMITS. PART MAY HAVE A MFG DEFECT.SDR PCP2003F00000Clamp · damagedOWNER REPORTED, UNABLE TO ACHIEVE GEAR DOWN AND LOCK ON APPROACH TO LANDING. GEARS WERE MANUALLY EXTENDED IAW POH EMERGENCY GEAR EXTENSION PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION BY TECH REVEALED A HEAT DUCT CLAMP (UNDER CSDR IL32003F00000Pitot Tube · brokenAIRCRAFT BROUGHT IN FOR 24 MONTH ALTIMETER/TRANSPONDER CERTIFICATION. WHILE TROUBLESHOOTING LEAKS, THE SOLID NUMBER 4 COPPER LINE FROM THE PITOT TUBE ASSEMBLY WAS FOUND TO BE BROKEN FLUSH WITH THE ASSEMBLY CASTING. THE LINE HAD BEEN EPOXIED BACK ON TO THE ASSDR CGO2002F00004Relief Valve · inoperativeVERIFIED COMPLAINT OF FUEL TANKS UNDER PRESSURE WHEN FILLED IN COLDER WEATHER THEN AIRCRAFT HANGARED IN WARMER TEMPERATURE AREA. FUEL SPRAYING OUT UNDER PRESSURE WHEN FILLER CAPS REMOVED. FOUND FUEL VENT SYSTEM LEFT, RIGHT PRESSURE RELIEF VALVES TO BE OPERASDR 2002FA0001270Clamp · disconnectedPILOT REPORTED HEARING A POP AT 11,000 FT AND IMMEDIATELY LOST MANIFOLD PRESSURE. PILOT MAKE PRECAUTIONARY LANDING WITHOUT INCIDENT. INSPECTION OF ENGINE REVEALED FORWARD CYLINDER INDUCTION MANIFOLD CROSSOVER TUBE HAD BECOME DISCONNECTED FROM NR 5 CYLINDER ISDR 2002FA0000293Turbocharger · leakingTURBOCHARGER WAS FOUND TO BE LEAKING OIL INTO INDUCTION SYSTEM. CHECKED SYSTEMS AS PER MFG AND MM. THIS IS NR 1 OF SEVERAL REPLACED ON THIS ENGINE.SDR 2002FA0000303Turbocharger · leakingTURBOCHARGER LEAKING OIL IN INDUCTION. THIS UNIT WAS REMOVED AND RETURNED DIRECTLY TO MFG FOR INVESTIGATION. THIS IS NR 3 FOR THIS ENGINE. NO WORD FROM MFG ON CAUSE OF PROBLEM. ENGINE IS TO BE REPLACED BY MFG.SDR 2002FA0000386Turbocharger · leakingTURBOCHARGER LEAKING OIL IN INDUCTION SYSTEM. RECHECKED SYSTEMS AS PER MFG. AND MM. THIS IS NR2 OF SEVERAL ON THIS ENGINE.SDR 20010511CW006Ring · crackedIN COMPLETING ANNUAL INSPECTION, CABIN HEATER ASSEMBLY WAS REMOVED FOR LEAK INSPECTION. FOUND ONE OF MUFF SUPPORT RINGS CRACKED HALF WAY AROUND. IF THIS WOULD HAVE CRACKED ALL THE WAY OFF THE EDGE WOULD HAVE CUT THROUGH EXHAUST PIPE PART OF MUFF, THIS WOULD SDR 20001218SH034Turbocharger · leakingTURBOCHARGER LEAKING OIL. (X)SDR 20001218SH015Cylinder · failedCYLINDER HAD LOW COMPRESSION. (X)SDR 20001120SH028Bracket · brokenTURBO CONTROLLER SUPPORT BRACKET BROKEN AT CASE ATTACHMENT POINT. (X)SDR 20001120SH027Baffle · crackedBAFFLE ABOVE OIL COOLER CRACKED OUT FROM PRESS FILTER HOLE. (X)SDR 20001214SH022Exhaust Valve · groovedDUE TO LOW COMPRESSION READING, CYLINDER WAS BORESECOPED. EXTREME OVERHEATING OF EXHAUST VALVE WAS NOTED. WEAR GROOVE WAS CUT INTO VALVE FACE BY SEAT. REMOVED CYLINDER. UPON INSPECTION, UNUSUAL WEAR WAS DUE TO MISALIGNMENT OF VALVE GUIDE OR VALVE SEAT. CYSDR 98ZZZX3281Drive Shaft · seizedENGINE DRIVEN FUEL PUMP SEIZED AND SHEARED THE DRIVE SHAFT. THE AIRCRAFT MADE A NORMAL LANDING AND ENGINE SHUT DOWN ON THE PARKING RAMP. UPON ENGINE START-UP, THE SHAFT APPARENTLY SHEARED BECAUSE IT WOULD NOT CONTINUE RUNNING WITHOUT THE ELECTRIC BOOST PUMP SDR 98ZZZX2983Inlet · crackedAD 89-24-03 CALLED FOR 100-HOUR INPSECTION OF TURBOCHARGER. THIS AIRCRAFT HAS NEW P/N PART AND WAS CRACKED 2 INCHES AT THE Y-TURBO INLET.SDR 98ZZZX1615Transmitter · wrong partFUEL STARVATION PROBLEM FOUND TO BE DUE TO INCORRECT FUEL QUANTITY TRANSMITTER HAD BEEN INSTALLED.SDR 98ZZZX1614Sight Gauge · stuckRIGHT FUEL TANK SIGHT GAUGE STUCK AT 35 GALLONS. REMOVED AND REPLACED SIGHT GAUGE. SUGGEST DURING ANNUAL INSPECTION, CHECK FOR CORRECT OPERATION OF SIGHT GAUGES.SDR 97ZZZX4638Turbocharger · seal leakFOUND OIL LEAKING FROM TURBOCHARGER ON COMPRESSOR SIDE AND EXHAUST SIDE OF TURBOCHARGER. SENT IN FOR OVERHAUL AND FOUND EXHAUST TURBINE WHEEL OUT OF BALANCE WHICH WORE OUT THE OIL SEALS ON THE HOT AND COLD SIDE OF TURBO. ESTIMATED TIME ON PART, 1,000 HOURS.SDR 97ZZZX968Line · leakingENGINE WOULD NOT IDLE ON FINAL. PRESSURE CHECKED HOSE AND FOUND SEVERAL LEAKS. (NOT VISIBLE WITH FIRE SLEEVE ON). HOSE DATE 4TH QUARTER '94. A/C AIRWORTHINESS 2-95.SDR 95ZZZX1590Torque Tube · crackedWHILE C/W AD 93-24-03, THE RUDDER TORQUE TUBE ASSY WAS FOUND CRACKED AT THE UPPER ATTACH POINT WELDS ON BOTH SIDES OF THE TUBE. THE UPPER ATTACH POINT OF THE TORQUE TUBE IS RIVETED TO THE RUDDER SKIN AND THESE RIVETS SHOWED SIGNS OF WORKING. SUGGEST TECHNICI
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