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 = 'U206F' 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 = 'U206F' 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 AUS20030598Spar Cap · corroded(AUS) RT WING SPAR CAP RIVET HEADS MISSING. INVESTIGATION FOUND THE SPAR CAP EXTENSIVELY CORRODED.SDR AUS20030617Line · chafed(AUS) FUEL LINE CHAFED BY AILERON CABLE.SDR CA030726006Rivet · loose(CAN) LOOSE RIVETS ON BOTH WINGS AT AILERON HINGE BRACKET REPLACED.SDR AUS20030079Filter · contaminated(AUS) ENGINE FUEL FILTER CONTAMINATED WITH WATER.SDR CA030726005Alternator · failed(CAN) LOSS OF ALTERNATOR POWER. ALTERNATOR OVERHAULED.SDR 2002FA0001249Cylinder · crackedPILOT NOTED ROUGH RUNNING ENGINE AND MADE PRECAUTIONARY LANDING. LATER INSPECTION REVEALED NR 1 CYLINDER CRACKED AND A HOLE BLOWN THROUGH THE EXHAUST SIDE.SDR FMAA2002003Wheel · crackedTHE NOSE WHEEL IS MADE UP OF 3 MAJOR COMPONENTS, THE 2 WHEEL FLANGES AND THE HUB. THE SCREWS HAVE NO LOCKING DEVICE, AND AFTER MANY HOURS OF USE THE SCREWS BACK OUT OF THE HUB AND OR THE SCREW HOLES IN THE HUB CRACK AND ALLOW THE THREADED HOLE TO GET LARGER ASDR AUS20020858Bolt · loose(AUS) ALTERNATOR THROUGH BOLTS LOOSE. ROTOR RUBBING ON FIELD WINDINGS CAUSING DAMAGE TO STATOR. SUSPECT CAUSED BY FAILURE TO RETORQUE BOLTS AFTER FIFTEEN HOURS OPERATION.SDR CA030726003Throttle · malfunctioned(CAN) NEW THROTTLE INSTALLED DUE TO MALFUNCTION.SDR AUS20020631Pump · cracked(AUS) ENGINE OIL PUMP HOUSING CRACKED. CRACK APPEARS TO ORIGINATE FROMA CASTING MARK. FOUND WHEN OIL FILTER ADAPTER WAS REMOVED FOR RECTIFICATION OF AN OIL LEAK.SDR CA020529003Hinge · cracked(CAN) CRACK FOUND IN LOWER ATTACH FLANGE DURING SPECIAL INSPECTION PER CESSNA CONTINUED AIRWORTHINESS PROGRAM.THIS WAS LEFT HAND INBOARD HINGE. ALSO FOUND RIGHT HAND INBOARD HINGE CRACKED. OUTBOARD LEFT HAND HINGE HAD BEEN RECENTLY REPLACED.SDR CHI2002F00003Rod End · shearedNOSE GEAR WAS PROBABLY TURNED BEYOND LIMITS REPEATEDLY OVERTIME PUT STRESS ON THREADED PORTION OF THE ROD END.SDR 2002FA0000413Impulse Coupling · defectiveTHE WOODRUFF KEY (M2536) THAT LOCKS THE IMPULSE COUPLING ON THE SHAFT WAS FOUND LODGED UNDERNEATH THE IMPULSE COUPLING PAWL, RENDERING ONE OF THE TWO PAWLS IMMOBILE. THE PIN ATTACHING THE PAWL WAS BENT AND THE GAP BETWEEN THE PAWL BOSS AND PLATE WAS NEAR LIMISDR CA020226008Roll Pin · sheared(CAN) FUEL SELECTOR WOULD NOT ROTATE VALVE. DISASSEMBLED AND FOUND PIN SECTION MISSING ALLOWING HOUSING YOKE TO ROTATE ON SHAFT. PIN REPLACED.SDR AUS20020111Filter · burned(AUS) ENGINE AIR FILTER BURNT.SDR 2002FA0000109Distributor · burnedMAGNETO HAD FAILED 9.3 HOURS AFTER BEING SUPPLIED AS A PART OF A FACTORY REBUILT ENGINE. IT WAS DISASSEMBLED AND THE DISTRIBUTOR, COIL, CAPACITOR AND BREAKER WERE REPLACED. MAGNETO WAS CHECKED OK. 2.5 HOURS AFTER THIS REPAIR THE MAGNETO FAILED AGAIN. THE DSDR AUS20011403Mount · cracked(AUS) LT AND RT REAR ENGINE MOUNT SUPPORT BRACKETS CRACKED FROM REAR INBOARD BEND RADIUS. NUMEROUS RIVETS IN SURROUNDING STRUCTURE FRETTING.SDR AUS20011010Distributor · burned(AUS) MAGNETO DISTRIBUTOR BLOCK BADLY BURNT DUE TO TRACKING FROM DISTRIBUTOR WHEEL SPRING TO MAGNETO HOUSING.SDR CA010523006Placard · reversed(CAN) THE DECAL ON THE ELEVATOR TRIM WHEEL APPEARS TO HAVE BEEN FABRICATED. WHEN IT WAS INSTALLED, THE "NOSE UP" AND "NOSE DOWN" DECALS WERE REVERSED. WHEN THE PILOT THOUGHT HE WAS TRIMMING THE NOSE DOWN, HE WAS ACTUALLY TRIMMING IT UP. THE LOCATION OF THE DECSDR AUS20010426Fitting · cracked(AUS) LT AFT TAILPLANE ATTACHMENT REINFORCEMENT CRACKED.SDR 20010423CW016Line · leakingFOUND FUEL RETURN LINE LEAKING THROUGH THE STEEL BRAID. HOSE IS LESS THAN 3 YEARS OLD, WITH NO VISIBLE DAMAGE. EVEN THOUGH THIS TYPE HOSE IS APPROVED FOR FUEL, AVIATION FUEL SEEMS TO DETERIOATE IT. HOSE HAS STEEL BRAID EXTERIOR.SDR AU010132Exhaust Valve · leaking(AUS) ENGINE EXHAUST VALVE LEAKING.SDR AUS20010433Flap Track · corroded(AUS) FLAP TRACKS CONTAINED EXFOLIATION AND INTERGRANNULAR CORROSIONLOCATED IN THE FORWARD END OF THE LOWER SLOT.SDR AUS20010432Bulkhead · cracked(AUS) HORIZONTAL STABILISER ATTACHMENT BULKHEAD CRACKED THROUGH TOP RIVET HOLE. CRACK LENGTH 19.05MM (0.75IN).SDR AUS20010431Seat Track · cracked(AUS) SEAT TRACKS CRACKED THROUGH STOP PIN HOLES.SDR AU001071Engine · overspeed(AUS) ENGINE OVERSPED IN EXCESS OF 3,300 RPM. (X)SDR AU001050Switch · failed(AUS) LANDING GEAR LIMIT MICROSWITCHES PN 1SE1-3 FAILED. THE RUBBER INSERT HOLDING THE PLUNGER AND SEALING THE SWITCH HAD EXPANDED AND DISINTEGRATED APPROXIMATELY EIGHT TO TWELVE HOURS AFTER LUBRICATION WITH LPS1 LUBRICANT AS SPECIFIED IN THE 3500A FLOAT SERVISDR 20001120SH061Casting · brokenCASTING BROKE BETWEEN MOUNTING PAD AND BARREL. (X)SDR AU000947Bulkhead · cracked(AUS) FORWARD TAIL BULKHEAD CRACKED IN THE AREA OF THE HORIZONTAL STABILIZER ATTACHMENT POINT. (X)SDR AU000821Torque Tube · corroded(AUS) ELEVATOR TORQUE TUBE CRACKED ON INBOARD END. DISASSEMBLY FOUND SIGNIFICANT CORROSION BETWEEN THE TORQUE TUBE AND THE SPAR MOUNTING BRACKET. (X)SDR 20001109SH010Ferrule · crackedPROPELLER SENT FOR REPAIR OF OIL LEAK. AFTER INVESTIGATION OF THE PROPELLER AND DISASSEMBLY, FOUND THE OIL LEAK OCCURRED BECAUSE ONE BLADE FERRULE HAD BEEN CRACKED IN THE BEARING AREA. (X)SDR AU000743Control Cable · separated(AUS) PROPELLER CONTROL CABLE ROD END NOT CONNECTED TO CSU. BOLT MISSING. (X)SDR AU000678Spring · broken(AUS) ENGINE STARTER/ ADAPTER CLUTCH SPRING BROKEN EIGHT COILS FROM THE ATTACHMENT POINT TO THE CLUTCH DRUM. (X)SDR 20000817SH016Camshaft · making metalFERROUS MATERIAL FOUND IN OIL FILTER. ENGINE DIS-ASSEMBLED, PROBLEM FOUND TO BE FAILED CAMSHAFT AND LIFTER BODIES. (X)SDR CA000906008Engine · failed(CAN) PILOT REPORTED DURING CRUISE HE HAD BRIEF VIBRATION FOLLOWED BY A LOSS OF OIL PRESSURE AND IMMEDIATE ENGINE FAILURE. AN UNEVENTFUL FORCED LANDING WAS CONDUCTED ON A LAKE 40 NAUTICAL MILES NORTHWEST OF RANKIN INLET, NUNAVUT. MAINTENANCE FOUND THE FRONT SDR CA001122020Throttle Cable · seized(CAN) A NEW THROTTLE CABLE RECEIVED FROM CESSNA WAS INSTALLED ON THE AIRCRAFT BUT SEIZED UP WHEN THE CABLE WAS FLEXED TO ALLOW HOOKUP TO THE THROTTLE CABLE. ANOTHER NEW CABLE FROM CESSNA WAS TRIED WITH THE SAME RESULT.A THROTTLE CABLE MADE BY MCFARLANE MCC2995SDR 20000817SH020Crankshaft · inadequatePER TCM MSB 00-5B, CRANKSHAFT WAS REJECTED BY TELEDYNE CONTINENTAL MOTORS. (X)SDR AU000423Trim Tab · distorted(AUS) RIGHT ELEVATOR TRIM TAB DISTORTED, SPLIT AND BULGED. INVESTIGATION FOUND THAT THE CORE HAD BEEN FILLED WITH EXPANDABLE FOAM WHICH HAD CONTINUED TO EXPAND AFTER FILLING THE AVAILABLE SPACE. UNAPPROVED PART.SDR AU000403Wire · shorted(AUS) FIRE UNDER FUSELAGE FLOOR IN RT FUEL COLLECTOR TANK COMPARTMENT. EXTENSIVE DAMAGE CAUSED TO WIRING LOOM LOCATED BETWEEN THE COLLECTOR TANK AND THE FLOOR PANEL. SUSPECT CAUSED BY SPARKS FROM THE RIGHT EXHAUST TAILPIPE IGNITING LEAKING BOOST PUMP FUEL ANSDR CA000614024Handle · damaged(CAN) PILOT CLOSED DOOR WITH HANDLE SELECTED TO THE CLOSED POSITION, HOWEVER, HANDLE WAS PARTIAL STRIP ON INSIDE GEARING, AND DOOR WAS NOT FULLY LOCKED. MAINTENANCE REPLACED DOOR HANDLE WITH SERVICEABLE HANDLE AND RETURNED THE AIRCRAFT TO SERVICE.SDR AU000356Bulkhead · cracked(AUS) FORWARD DOORPOST BULKHEAD CRACKED IN RELIEF HOLE. CRACK LENGTH 12.7 MM (0.5 INCH). FOUND DURING INSPECTION IAW AD/C206/48.SDR CA000306020Cylinder · cracked(CAN) CYLINDER CRACKED AT INTAKE PORT NR 5 CYLINDER.SDR CA000306012Cylinder · cracked(CAN) EXHAUST PORT CRACK VISIBLE ON OUTSIDE OF CYLINDER.SDR 2000ZZZX831Impulse Coupling · failedTHE IMPULSE COUPLING ENGAGES ONLY 1 OUT OF 5 TIMES WHEN PROPELLER IS TURNED BY HAND. THE SPRING WHICH HOLDS THE PAWL OUT TO ENGAGE IMPULSE COUPLING HAS NOT BROKEN BUT HAS TOTALY LOST ITS SPRING EFFECT.SDR CA991230012Plug · missing(CAN) TWO LOCKING EXPANSION PLUGS FOR EACH BLADE ALL WERE FOUND NOT INSTALLED. LOCKING EXPANSION PLUGS ARE USED TO LOCK THE BLADES TO THE HUB . THIS IS AN O/H OVERSIGHT AND A MAINTENANCE ISSUE.SDR CA991230009Hub · cracked(CAN) FOUND CRACK IN DICATION USING EDDY CURRENT ON HUB SOCKET. NR 1 AND NR 2 HUB REPLACED.SDR CA991230008Pin · corroded(CAN) DEEP CORROSION PITS, ACTUATING PINS REPLACED.SDR 99ZZZX4546Camshaft · making metalFERROUS MATERIAL FOUND IN OIL FILTER. ENGINE DISASSEMBLED, PROBLEM FOUND TO BE FAILED CAMSHAFT AND LIFTER BODIES.SDR CA991208079Impulse Coupling · worn(CAN) IMPULSE COUPLING WORN PAST LIMITS. DISTRIBUTOR DRIVE GEAR BUSHES WEAR WAS EXCESSIVE.SDR AU990933Seat Track · worn(AUS) LEFT SEAT RAIL WORN BEYOND LIMITS.
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