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 = 'T337G' 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 = 'T337G' 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 2020F00109Epsu · warning messagePER WORK CARD 25-94-02 OPERATION TEST BITE OF EPSU FAULTS EMERGENCY EXIT R.SDR 2017FA0000258Wheel · failedNOSE WHEEL FAILED ON LANDING. THE ASSEMBLY APPEARED TO HAVE COME APART WITH THE HUB AND THE SIDE PIECES SEPARATED. A REVIEW OF THE LOGS SHOWED THAT THE WHEEL HAD BEEN ON THE AIRCRAFT SINCE NEW IN 1973.SDR 2017FA0000082Hydraulic Line · out of positionTHE HYDRAULIC TUBE TOUCHING RESERVOIR WHICH CAUSING CORROSION.SDR 2015FA0000439Engine · failedAFTER TAKEOFF, IN CRUISE FLIGHT AT 7,000' ASL, FRONT ENGINE OIL PRESSURE DROPPED TO LOWER RED-LINE LIMIT, OIL TEMPERATURE WAS NORMAL APPROXIMATELY 150F AND ENGINE RUNNING SMOOTHLY. WITHIN 10 SECONDS, ENGINE WENT FROM SMOOTH RUNNING CONDITION TO A LOSS OF 300-SDR 2010FA0000630Structure · damaged((Z4AR)) ACFT WAS BROUGHT IN FOR INSP IAW SAID CE10-20 AND ANNUAL INSP. ACFT IS EQUIPED WITH EXTENDED RANGE FUEL STC AND WING TIP STC. ACFT IS ALSO EQUIPED WITH STALL FENCES STC AND BOOM TO VERTICAL FAIRINGS. AN INSP IS IAW SAIB WAS PERFORMED. COMPRESSION SDR YYE2008F00000Pump · failedTHE PRIMARY ELECTRIC/ HYD LANDING GEAR PUMP FAILED. THE ATTEMPT TO LWR THE GEAR WITH THE MANUAL GEAR LEVER ALSO FAILED, RESULTING IN A GEAR UP LANDING. THE PRIMARY PUMP FAILURE MAY HAVE CAUSED THE MANUAL PUMP FAILURE. (K)SDR YYE2009F00001Actuator · crackedLANDING GEAR HANLE SELECTED DOWN, NOSE GEAR DOWN AND LOCKED, MAINS REMAIN IN TRANSIT. EMERGENCY HAND PUMP INOPERATIVE. ALL HYDRAULIC FLUID LEAKED FROM POWER PACK. RT MAIN GEAR RETRACT ACTUATOR FOUND CRACKED FULL LENGTH OF CYLINDER.SDR YYE2009F00000Powerpack · failedHYDR PUMP FAILED TO EXTEND LANDING GEAR. HAND PUMP FAILED TO EXTEND LANDING GEAR. HAND PUMP FAILURE PROBABLY CAUSED BY DEBRIS FROM PRIMARY PUMP - YET TO BE DETERMINED. WILL SEND FOLLOW UP REPORT. LATE REPORT IS BEING DELT WITH BY FSDO. (K)SDR JNE2008F00000Starter · failedINSTALLED TWO FACTORY ENGINES. AFTER SEVERAL TEST RUNS , THE FRONT STARTER SOLENOID FAILED ON. REPLACED THE SOLENOID WITH AN NEW MFG SOLENOID. ON A TEST FLIGHT ELECTRICAL FAILURE OCCURRED. IT HAPPENED BECAUSE OF AN OVERLOAD OF THE BATTERY AND ELECTRICALSYSTSDR UIEA200700462Skin · crackedNR 4 PYLON LT SKIN WAS FOUND CRACK AT 483AL ACCESS PANEL CUTOUT LOWER AFT CORNER.SDR 2005F00105Wheel · looseWHEEL ASSEMBLY RETURNED FOR LOOSE TIE BOLTS OF 18 INSTALLED 14 WERE FOUND LOOSE 2 MISSING. MESSIER HAS NOW RELEASE SERVICE LETTER F6137-32--843 IN HOPES THIS WILL RESOLVE.SDR 2005F00104Wheel · looseWHEEL ASSEMBLY RETURNED FOR LOOSE TIE BOLTS OF 18 INSTALLED 14 WERE FOUND LOOSE 2 MISSING. MFG HAS NOW RELEASE SERVICE LETTER F6137-32--843 IN HOPES THIS WILL RESOLVE.SDR 2005F00107Wheel · looseWHEEL ASSEMBLY RETURNED FOR LOOSE TIE BOLTS OF 18 INSTALLED 14 WERE FOUND LOOSE 2 MISSING. MESSIER HAS NOW RELEASE SERVICE LETTER F6137-32--843 IN HOPES THIS WILL RESOLVE.SDR 2005FA0001251Clamp · separatedEXHAUST PIPE TO TURBOCHARGER CLAMP FOR FRONT ENGINE CRACKED AT SPOT-WELD AND SEPARATED ON TAKEOFF. WHEN THIS HAPPENED, THE EXHAUST PIPE DEPARTED THE AIRCRAFT AND THE EXHAUST SCORCHED THE ENGINE COWLING AND FIREWALL. (K)SDR CA041108007Cable · frayed(CAN) AT INSPECTION THE AUTOPILOT ROLL SERVO BRIDLE CABLE WAS FOUND TO BE FRAYED WHERE IT RUNS OVER IT'S PULLEYS.SDR CA040930002Skin · cracked(CAN) DURING INSPECTION, CRACKS WERE DISCOVERED AT THE IB END OF THE LT AND RT UPPER OB WING SKINS WHERE THEY UNDERLAP THE FUEL TANK BAY COVERS. THE CRACKS ARE LOCATED IN THE RADIUS OF CUTOUT AREAS IN THE SKINS WHERE THE STINGERS JOIN AT WING STATION 150.0. TSDR 2004FA0000397Impulse Coupling · brokenPILOT REPORTED REAR ENGINE WAS HARD TO START. AFTER TROUBLESHOOTING, THE LT MAGNETO WAS REMOVED. UPON INSPECTION THE IMPULSE COUPLING WOULD NOT ROTATE IN THE CORRECT DIRECTION. THE MECH WAS NOT SURE IF WRONG IMPULSE COUPLING OR SPRING TURN BACKWARD. DUE TOSDR CA040122003Control Cable · frayed(CAN) DURING INSPECTION IT WAS DISCOVERED THAT THESE CABLES (2EA. 1 LEFT AND 1 RIGHT) WERE FRAYED WHERE THE CABLE BENDS AROUND THE FLAP CABLE QUADRANT LOCATED IN THE WING TRAILING EDGE.SDR CA040122002Control Cable · frayed(CAN) DURING INSPECTION IT WAS DICOVERED THAT THESE CABLES (2EA. 1 LT AND 1 RT) WERE FRAYED WHERE THE CABLE BENDS AROUND THE FLAP CABLE QUADRANT LOCATED IN THE WING TRAILING EDGE.SDR CA031119004Coupling · separated(CAN) COUPLING SEPARATED FROM TURBOCHARGER COMPRESSOR HOUSING CAUSING INDUCTION LEAK AND RESULTING POWER LOSS.SDR 2003FA0001113Clamp · brokenFRONT ENGINE TURBO EXHAUST STACK RETAINER CLAMP (TURBINE OUTLET LIP) BAND CLAMP PN S19212 STRAP PORTION FRACTURED AND EXHAUST STACK FELL OFF AIRCRAFT ON TAKEOFF. CLAMP MAY HAVE BEEN CRACKED, AND IT HAD NOT BEEN DETECTED BEFORE FAILURE OCCURRED. CLOSER VISUALSDR AUS20031143Control Cable · frayed(AUS) LT AND RT FLAP DOWN CABLES PN 1460100-7 AND PN 1460100-8 FRAYED WITH BROKEN STRANDS AROUND BELLCRANK ACTUATOR.SDR CH1A200393049Stringer · crackedSTRINGER 26R CRACKED AT BS 46.SDR AMTA200200921Actuator · malfunctionedIN TRANSIT DOOR AND FE'S LT GEAR DOOR LIGHTS CAME ON IN CLIMB.SDR 2002FA0000822Swivel · failedTHIS ITEM IS INSTALLED ON A CESSNA T337G THAT HAS HAD TCM TSIO-520 ENGINES INSTALLED AS AN STC MODIFICATION. THE PART IS A BALL-TYPE SWIVEL THAT CONNECTS THE MIXTURE CABLE TO THE MIXTURE CONTROL ARM. THE BALL HAS PULLED OUT OF ITS SWAGED HOUSING. THIS IS THE TSDR AUS20010737Capacitor · unserviceable(AUS) MAGNETO CAPACITOR FAULTY. CAPACITOR LEAD LOOSE.SDR 2001FA0000120Swivel · separatedINSTALLED BALL JOINT OR SWIVEL PN S2999-1 ON MIXTURE CONTROL CABLE FRONT AND REAR ENGINES AT TIME OF ENGINE INSTALLATION. A/C WAS TEST FLOWN AND FERRIED TO PAINT SHOP AND RETURNED. PREVIOUS TO ANY ADDITIONAL ADJUSTMENT AND WHILE IN THE COCKPIT PERFORMING A MSDR 20000426SH030Bolt · brokenTIE BOLT FAILURE, 3 EACH. UNDETERMINED WHEEL SENT TO MFG FOR ANALYSIS. BOLT HARD TIME IMPLEMENTED, AND TIE NUT CYCLE PLAN INPLEMENTED. (X)SDR 2000ZZZX364Crankshaft · crackedFOUND CRANKSHAFT FLANGE CRACKED (APPROXIMATELY 2.5 INCHES) ON BACK SIDE. ENGINE IS A FACTORY REBUILT WITH 48 HOURS AND NO RECORDED DAMAGE HISTORY. ENGINE INSTALLED IN REAR POSTION.SDR 96ZZZX5624Through-Bolt · brokenINSPECTION FOUND LOWER THROUGH-BOLT IN NR 2 CYLINDER BASE BROKEN.SDR 96ZZZX701Valve · excess wearFREQUENT FINDING OF LOW COMPRESSION ON EITHER FRONT OR REAR ENGINE WITH ONLY 808 HOURS TT. EACH TIME REPAIR WAS ACCOMPLISHED DUE TO THIS HISTORY, COMPLETE CYLINDER TEAR DOWN REVEALED EXCESS WEAR TO EXHAUST VALVES AND EXHAUST VALVE GUIDES. SUBMITTER SUSPECTS SDR 96ZZZX700Valve Guide · excess wearFREQUENT FINDING OF LOW COMPRESSION ON EITHER FRONT OR REAR ENGINE WITH ONLY 808 HOURS TT. EACH TIME REPAIR WAS ACCOMPLISHED DUE TO THIS HISTORY, COMPLETE CYLINDER TEAR DOWN REVEALED EXCESS WEAR TO EXHAUST VALVES AND EXHAUST VALVE GUIDES. SUBMITTER SUSPECTS SDR 95ZZZX5836Electric Sys · failedAIRCRAFT SUFFERED A SHORT-TERM, COMPLETE ELECTRICAL SYSTEM FAILURE WHILE IN IFR CONDITIONS ON A NIGHT FLIGHT. ELECTRICAL SYSTEM BEGAN FUNCTIONING NORMALLY AGAIN AFTER AIRCRAFT RETURNED TO NON-PRECIP. VFR. SUSPECT CAUSE IS MOISTURE ENTERING AVIONICS COMPARTME
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