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 = 'TU206G' 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 = 'TU206G' 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 CA040805002Gear · broken(CAN) THE AIRCRAFT COMPLETED ITS FIRST FLIGHT OF THE DAY WITHOUT INCIDENT. ON THE SECOND START OF THE DAY THE PILOT HEARD THE STARTER MOTOR RUNNING BUT THE ENGINE WAS NOT ROTATING. INSPECTION AND TROUBLESHOOTING PROCEDURES WERE CARRIED OUT. THE MECHANIC FOUNSDR RDD2004F00000Contactor · failedSTARTER CONTACTOR REMAINED ENERGIZED AFTER START. AIRCRAFT WAS FLOWN THROUGH ONE ABBREVIATED CYCLE OF TAKE-OFF, PATTERN AND LANDING. UPON INSPECTION THE STARTER MOTOR WAS FOUND COMPLETELY DESTROYED.SDR 2004FA0000532Spar · crackedLT SKIN CRACKED 6 INCHES AFT OF LOWER RUDDER HINGE POINT. RT SKIN WRINKLED 6 INCHES AFT OF LOWER HINGE POINT. LOWER RIB CRACKED 5 INCHES AFT OF SECURING POINT TO FORWARD RUDDER SPAR, CRACKED ON LT SIDE. PROBABLE CAUSE UNNECESSARY ROUGHNESS. (WP25200404045)SDR 2004FA0000531Spar · crackedLT SKIN CRACKED 6 INCHES AFT OF LOWER RUDDER HINGE POINT. RT SKIN WRINKLED 6 INCHES AFT OF LOWER HINGE POINT. LOWER RIB CRACKED 5 INCHES AFT OF SECURING POINT TO FORWARD RUDDER SPAR, CRACKED ON LT SIDE. PROBABLE CAUSE UNNECESSARY ROUGHNESS. (WP25200406045)SDR 2004FA0000530Spar · crackedLT SKIN CRACKED 6 INCHES AFT OF LOWER RUDDER HINGE POINT. RT SKIN WRINKLED 6 INCHES AFT OF LOWER HINGE POINT. LOWER RIB CRACKED 5 INCHES AFT OF SECURING POINT TO FORWARD RUDDER SPAR, CRACKED ON LT SIDE. PROBABLE CAUSE UNNECESSARY ROUGHNESS. (WP25200406045)SDR 2004FA0000343Brushes · misinstalledUPON COMPLETING THE FIRST 500 HOUR INSPECTION ON THE MAGNETO, IT WAS DISCOVERED THAT THE CARBON BRUSH AND SPRING ASSY (PN 10160844) WERE NOT INSTALLED. THE BUSHING IN THE DISTRIBUTOR GEAR HAD BEEN MAKING CONTACT WITH THE TAB ON THE COIL SO THE MAGNETO APPEARESDR MAFPAPUADrain · failedWHILE INSTALLING THE WING FUEL TANK SUMP DRAIN AT THE MFG RECOMMENDED TORQUE VALUE OF 90 IN-LBS, THE DRAIN ITSELF FAILED, SEPARATING AT THE DRILLED HOLES JUST ABOVE THE FITTING HEAD.SDR 2004FA0000032Plug · looseSENT CRANKSHAFT FOR ULTRASONIC AND MAGNAFLUX INSP. REMOVED OIL TRANSFER PLUG FROM CRANKSHAFT AS PART OF INSP. PLUG WAS REINSTALLED INTO CRANKSHAFT BEFORE RETURNING. APPROX. 70 HRS AFTER REPAIR, PROP WOULD NOT CYCLE AT NORMAL RUN-UP. WHEN PILOT APPLIED POWSDR 2003FA0001291Attach Fitting · crackedON SCHEDULED 200 HRS VISUAL INSPECTION, REVEALED ATTACHMENT FITTING MAIN LANDING GEAR OB CRACKED IN AREA OF FWD. LOWER RADIUS CLOSE THE BOLT HOLE HISTORY RECORD REVELEAD ITS THIRD CHANGE.SDR AK02003F00002Battery · inoperativeDURING AN ANNUAL INSPECTION OF THE ELT UNIT, THE ELT WAS FUNCTIONAL CHECKED BY THE REMOTE SWITCH ON THE PANEL. THERE WAS NO LED LIGHT INDICATION WHEN SWITCHED TO THE ON POSITION. THE ELT UNIT WAS REMOVED FROM THE AIRCRAFT AND TESTED AGAIN, THE UNIT WAS INOPESDR CA030606004Line · severed(CAN) DURING THE LAST OPS 4 INSPECTION, SEB 95-6, RUBBER FUEL HOSE INSPECTION AND REPLACEMENT WAS ACCOMPLISHED. SUBSEQUENT INSPECTION REVEILED THAT THE FUEL PRIMER LINE FROM THE MANIFOLD TO THE PRIMER T FITTING ROUTED NEAR THE ALTERNATOR PULLEY FOUND BROKEN INSDR CA030514016Door Frame · cracked(CAN) DURING A CESSNA CONTINUED AIRWORTHINESS PROGRAM INSPECTION 53-10-02 A 2 INCH CRACK WAS NOTED IN THE DOOR POST AT THE BOTTOM LEFT OF THE WINDOW. A REPAIR HAD TO BE COMPLETED IN ACCORDANCE WITH CESSNA SEB 93-4 BY INSTALLING THE DOORPOST MODIFICATION KIT SKSDR 2002FA0001030Gear · damagedDURING PRE-FLIGHT INSPECTION PROPELLER WAS ROTATED BACKWARDS BY HAND TO CHECK COMPRESSION OF CYLINDERS. PROPELLER PHYSICALLY STOPPED BY SOMETHING INTERNAL IN ENGINE. AFTER INSPECTION BY REMOVING THE STARTER ADAPTER ASSEMBLY, THE CRANKSHAFT GEAR WAS FOUND TO SDR CA020906001Link · severed(CAN) AMPHIB FLOATS SELECTED TO DOWN POSITION AND AIRCRAFT LANDED ON RUNWAY. THE PILOT FELT THE RT AFT FLOAT CONTACT PAVEMENT AND IMMEDIATELY INITIATED A GO-AROUND. SELECTED GEAR UP AND LANDED WITH NO INCIDENT ON THE WATER. INSPECTION FOUND THE RT MLG ACTUATSDR 2002FA0000125Distributor Blk · brokenTHE CENTER BUSHING IN THE DISTRIBUTOR BLOCK IS LOOSE AND SHOWS SIGNS OF OVERHEATING. AS A RESULT THE DISTRIBUTOR GEAR WOBBLED AND THE FINGER CONTACTED ALL THE HIGH TENSION CONTACT TOWERS AND GROUND THEM OFF.SDR 2002FA0000110Distributor · burnedMAGNETO WAS SUPPLIED AS PART OF A TCM FACTORY REBUILT ENGINE. IT FAILED AND UPON INSPECTION IT WAS DISCOVERED THAT THE DISTRIBUTOR GEAR SUPPORT WAS BADLY BURNED BY SPARKS GOING FROM THE COIL TERMINAL TO GROUND ON THE M3485 BEARING CAP BY ARCING ACROSS THE SHESDR 2001FA0000458Lifter · spalledDURING ROUTINE OIL CHANGE, METAL WAS FOUND IN FILTER. ENGINE WAS REMOVED AND DISASSEMBLED. CAUSE WAS FOUND TO BE LIFTER FACE AND CAM LOBE SPALLING ON CYLINDER CAM LOBES NR5 AND NR6 INTAKE. NO CORROSION NOTED. TWO OTHER INTAKE LIFTERS EXHIBIT PREMATURE WEARSDR 2001FA0000206Spring · brokenTHE MAGNETO IMPULSE COUPLING SPRING BROKE ABOUT 6 INCHES FROM THE OUTER END OF THE SPRING. THE FAILURE WAS DISCOVERED BECAUSE THE IMPULSE COUPLING WOULD NOT ENGAGE DURING THE ENGINE STARTING PROCESS.SDR CA010827004Distributor Blk · burned(CAN) BOTH MAGNETOS WERE REMOVED IN ERROR FOR 500 HR INSP ONLY LH WAS DUE WHEN RH MAGNETO WAS DISASSEMBLIED BY LEGGAT AVIATION. THE BEARING BAR P/N M3004 WAS BURNED THROUGH AT HIGH TENSION BRUSH AREA OF DISTRIBUTER BLOCK NO PROBLEM WAS EVER FOUND ON MAGNETO CHSDR 2001FA0000042Flap Track · looseTHE LEFT HAND INBOARD FLAP TRACK IS WORKING LOOSE. THIS WAS INDICATED BY CRACKED COVE SKIN ATTACH BRACKETS.SDR 2001F00014Flap Track · looseRIGHT INBOARD FLAPTRACK IS WORKING LOOSE. THIS WAS INDICATED BY A CRACKED COVE SKIN AT THE ATTACH BRACKET LOCATION.SDR 20010612CW018Bracket · brokenPILOT LOST LEFT BRAKE DURING TAXI. INSPECTION REVEALED MASTER CYLINDER LOWER ATTACH BRACKETS BROKEN. INSPECTION OF OTHER AIRCRAFT FOUND SAME PARTS BENT.SDR 20010612CW017Bracket · brokenPILOT LOST LEFT BRAKE DURING TAXI. INSPECTION REVEALED MASTER CYLINDER LOWER ATTACH BRACKETS BROKEN.SDR 2001FA0000159Wastegate Valve · undertorquedFOUND THE 7 ACTUATOR TO BYPASS VALVE MOUNTING BOLTS (REF. GARRETT MANUAL TP30-4001-1 PG. 10-11 ITMES NR 7 AND 10) WITH LITTLE TO NIL MEASURABLE TORQUE. THIS IS THE SECOND ACTUATOR ON WHICH WE HAVE DISCOVERED THIS PROBLEM. DURING INSTALLATION INSPECTION, A WSDR 2001F00031Rod End · failedDURING A DAILY AND PREFLIGHT INSPECTION THE RUDDER TRIM AND NOSE STEERING WERE FOUND INOPERATIVE. AT CLOSER INSPECTION THE ROD END (PN 12606311) FOR THE NOSE STEERING BUNGEE HAD FAILED AT THE (PN 12606323) RUDDER TRIM GEAR. THIS EFFECTUALLY DISCONNECTS NOT OSDR 20010416CW002Structure · damagedTHE 206 SEAPLANE RUDDER ASSEMBLY IS PRONE TO DAMAGE AFT OF PN 12310661, DOUBLER AT THE BOTTOM OF THE RUDDER. DAMAGE OF THIS NATURE IS EVIDENT BY A KINK AT THE BOTTOM OF THE RUDDER ON BOTH SIDES. THIS DAMAGE IS CAUSED BY THE WIND WHEN A RUDDER LOCK IS NOT USSDR 20010508CW009Coil · inoperativeMAGNETO INOPERATIVE BELOW 1,000 RPMS. OK AT 1,700 RPMS PER THE P.O.M. PILOTS HAD DONE A MAG CHECK AT IDLE WHICH LEAD TO THE DISCOVERY. OPENED MAGNETO FOR INSPECTION. TESTED COIL AND FOUND SECONDARY WINDING. RESISTANCE TOO HIGH BY FACTOR OF 10.SDR 20010508CW008Frame · crackedOBSERVED AN OIL LEAK FROM MAG BASE. FOUND MOUNTING FLANGE CRACKED AROUND LOWER CLAMPING WASHER. REMOVED MAG AND FOUND APPROX 2 INCH PIECE OF MOUNTING FLANGE BROKEN OFF.SDR 20010227SG002Pump · leakingENGINE DRIVEN FUEL PUMP BEGAN LEAKING FROM SHAFT SEAL.SDR 20010227SG004Pump · leakingFUEL LEAK FROM PUMP DRAINSDR AU001270Bolt · broken(AUS) UPPER THROUGH BOLT LOCATED BETWEEN NR 2 AND NR 3 CYLINDERS BROKEN.FAILURE OCCURRED APPROXIMATELY 76.2MM (3IN) FROM THE LEFT END OF THE BOLT.SDR 20000417SH014Alternator · failedALTERNATOR FAILED DURING FLIGHT. TROUBLESHOOTING WITH ALTERNATOR TEST BOX SHOWED NO OUTPUT. CHECKING FIELD WINDING RESISTANCE PER CESSNA MM SHOWED EXCESSIVELY HIGH RESISTANCE. ALTERNATOR REPLACED. (X)SDR 20000515SH003Pump · leakingENGINE DRIVEN FUEL PUMP WAS LEAKING FUEL FROM THE PUMP DRAIN LINE. (X)SDR 20000515SH002Pump · leakingENGINE DRIVEN FUEL PUMP WAS LEAKING FUEL OUT OF THE PUMP DRAIN LINE. (X)SDR CA991004050Actuator · cracked(CAN) THE FORWARD WHEEL GEAR ACTUATOR ON THE LEFT FLOAT WAS FOUND CRACKED AND LEAKING. TWO LONGITUDINAL CRACKS WERE LOCATED IN THE ACTUATOR CYLINDER.SDR 99ZZZX2394Heat Exchanger · crackedHEAT EXCHANGER IS PART OF COMPLETE KINLEY WELDING, INC., EXHAUST SYSTEM INSTALLED UNDER STC SA5010NM AND STC SE5009NM. THE HEAT EXCHANGER HAS HEAT TRANSFER STUBS WELDED TO ITS OUTER SURFACE FOR WARMING AIR FOR CABIN HEAT. TWO OF THESE STUDS WERE FOUND CRACKEDSDR 20000714SH016Bracket · crackedTHIS AIRCRAFT IS EQUIPPED WITH A ROBERTSON STOL KIT. BOTH OUTBOARD AILERON ATTACH BRACKETS WERE FOUND CRACKED AND BROKEN. THE ADDITIONAL STRESSES RELATED TO THE ROBERTSON CAUSED THIS CONDITON. ALL ROBERTSON STOL EQUIPPED AIRCRAFT SHOULD HAVE THIS BRACKET INSDR 20000714SH015Bracket · crackedTHIS AIRCRAFT IS EQUIPPED WITH A ROBERTSON STOL KIT. BOTH OUTBOARD AILERON ATTACH BRACKETS WERE FOUND CRACKED AND BROKEN. THE ADDITIONAL STRESSES RELATED TO THE ROTATION CAUSED THIS CONDITION. THESE PARTS SHOULD BE INSPECTED ON ALL ROBERTSON EQUPPED AIRCRAFSDR AU990056Frame · cracked(AUS) LEFT FRONT DOOR POST FRAME CRACKED THROUGH. DOUBLER ALSO CRACKED. AIRCRAFT OPERATES AS A FLOAT PLANE.SDR 99ZZZX118Switch · inoperativeDURING ANNUAL INSPECTION, FOUND STALL WARNING LIFT DETECTOR INOPERABLE DUE TO HIGH RESISTANCE. ALSO DISCOVERED THE WRONG LIFT SWITCH WAS INSTALLED PER CONVERSATION WITH SAFE FLIGHT. REPLACED P/N 146 WITH CORRECT P/N 150.SDR 98ZZZX4528Switch · wornDURING ANNUAL, DISCOVERED AD 93-05-06 NOT C/W. INSPECTED IGNITION SWITCH AND FOUND SIGNS OF MODIFIED STARTER RELAY IAW CESSNA SEB 91-5- R1. NOTE: AD IS RECURRING EVERY 2,000 HOURS AFTER INITIAL COMPLIANCE.SDR CA980908003Fitting · corroded(CAN) AIRCRAFT RECENTLY PURCHASED, FOUND LEFT AND RIGHT UPPER MAIN STRUT FITTINGS BADLY EXFOLIATED. AIRCRAFT HAD BEEN USED IN SALT WATER ENVIRONMENT. WATER CAN GET TRAPPED IN UPPER FITTINGS. LOWER FITTINGS ALL GOOD.SDR 98ZZZX1454Gasket · leaksA SMALL OIL LEAK ON NR 3 CYLINDER WAS REPAIRED BY INSTALLING A NEW P/N 653191 ROCKER COVER GASKET. NINE HOURS LATER, A LARGE OIL LEAK WAS EVIDENT, CYLINDER NR 3. UPON PULLING COVER, FOUND GASKET HAD SHRUNK CAUSING OIL LEAK WHERE THE GASKET WENT STRAIGHT BETSDR 98ZZZX186Trim Tab · corrodedIN THE PROCESS OF ANNUAL INSPECTION, TECHNICIAN NOTICED WHAT APPEARED TO BE CORROSION STARTING UNDER THE PAINT AROUND THE RIVET HEADS ON THE UPPER SURFACE OF THE BRACKET FOR THE ELEV TAB CONTROL ROD. WHEN PICKED AT THE RIVET HEADS WITH FINGERNAIL, SIX OF THE SDR 97ZZZX4880Mount · failedFORWARD ENGINE SHOCK MOUNTS FLATTENED CAUSING OIL TEMPERATURES TO INCREASE. INSTALLED NEW ENGINE SHOCK MOUNTS WHICH RAISED OIL COOLER INTO PROPER AIR STREAM FOR BETTER COOLING.SDR 97ZZZX4556Torque Link · crackedINSPECTION FOUND NLG UPPER TORQUE LINK ASSY CRACKED.SDR 97ZZZX3977Crankshaft · brokePILOT REPORTED A STRONG VIBRATION FOLLOWED BY A LOUD MECHANICAL BANG IN THE ENGINE DURING FLIGHT. SECONDS LATER THE ENGINE ABRUPTLY STOPPED. AN ENGINE 'TEAR DOWN' INSPECTION WAS PERFORMED AND REVEALED THE CRANKSHAFT BROKE AT THE NR 4 'CRANKSHAFT MAIN BEARINGSDR CA970922011Snap Ring · missing(CAN) A PROPELLER BLADE SNAP RING DEPARTED THE BLADE DURING FLIGHT. POST FLIGHT INSPECTION REVEALED A LOOSE PROPELLER BLADE AND A BROKEN PITCH LINK.SDR CA970612002Cylinder · cracked(CAN) CYLINDER HEAD CRACKED FROM UPPER SPARK PLUG HOLE TO INSPECTION HOLE.SDR CA970610003Lock Nut · cracked(CAN) THE NUT WHICH HOLDS THE LOWER WING STRUT TO THE WING STRUT FITTING WAS FOUND TO BE CRACKED. NUT REPLACED
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