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 = '58P' 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 = '58P' 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 2000ZZZX260Bladder · leakingRIGHT WING BOX SECTION FUEL CELL (BLADDER) P/N 58-380003-6, LEAKING FUEL. ONCE OLD BLADDER WAS REMOVED, FOUND FUEL STAINS AT 2 INTERCONNECT HOSES. THE CLAMPS THAT ARE ACCESSED FROM INSIDE THE TANK WERE FINGER TIGHT. THERE IS NO MEANS FOR SAFETY WIRE OR INTESDR 99ZZZX4381Capacitor · failedCOMPONENT FAILURE CAUSES RECEIVER TO LOSE STORED FREQUENCY AND TIMER INFORMATION. THIS FACILITY HAS SEEN TWO IDENTICAL FAILURES IN PAST YEAR.SDR 2000ZZZX40Arm · brokenINSPECTION OF THE LANDING GEAR SYSTEM ON THE SUBJECT AIRCRAFT REVEALED THE FOLLOWING. THE LANDING GEAR GEARBOX IS IN THE FULL DOWN POSITION. THE NOSE GEAR RETRACT ARM P/N 35-825172-2 IS BROKEN. THIS RELEASED THE OVERCENTER TENSION ON THE NOSE GEAR DOWNLOCK SDR 99ZZZX4487Bolt · shearedNOSE GEAR RETRACT ARM FORWARD BOLT THAT ATTACHES THE ARM TO NOSE GEAR DRAG LEG RETRACT MECHANISM SHEARED CAUSING THE GEAR TO ONLY RETRACT PARTIALLY. THIS ALSO CAUSED THE UP AND DOWN SWITCH ARM TO BREAK AT ITS PIVOT POINT AS IT WAS ATTEMPTING TO RETRACT THE GESDR 99ZZZX2291Tire · failedTREAD SEPARATING, SPLITTING, AND BUMPS AT TOP OF SIDE WALL.SDR 99ZZZX1433Boot · looseTHE INDUCTION BOOT SLIPPED OFF THE INDUCTION TUBE AT THE INNER COOLER OUTLET CONNECTION. THE WORM CLAMP SECURING THE BOOT WAS APPARENTLY NOT FULLY OVER THE RIDGE ON THE INDUCTION TUBE CAUSING THE BOOT TO EVENTUALLY SLIP OFF THE TUBE AT HIGH MANIFOLD PRESSURE.SDR 98ZZZX3670Seat Belt · malfunctionedSEAT BELT LATCHES INTERMITTENTLY.SDR 98ZZZX4048Magneto · failedLEFT MAG FAILED. RIGHT ENGINE FAILED AT LIFT-OFF. LEFT MAG REMOVED AND DISASSEMBLED. FOUND DISTRIBUTOR BLOCK BUSHING LOOSE IN BLOCK P/N 10-391586. REPLACED BLOCK AND GEAR OPS CHECK OK.SDR 98ZZZX3580Line · chafedON REMOVING INBOARD SECTION OF LEADING EDGE TO REPLACE MIXTURE CONTROL CABLE ON LEFT SIDE, FOUND OIL PRESSURE LINE WORN OVER HALF WAY THROUGH WHERE LINE WAS RUBBING ON NOSE RIB FLANGE ON LEADING EDGE. REMOVED RT SIDE AND FOUND OIL LINE ON THAT SIDE RUBBING ALSDR 98ZZZX3010Transmitter · leakingDURING ANNUAL INSPECTION, FUEL WAS NOTED LEAKING PAST RIGHT WING LEADING EDGE. FUEL TANK UPPER TRANSMITTER, NEW UNIT INSTALLED.SDR 98ZZZX3009Manifold · leakingDURING ENGINE STARTS, PNEUMATIC GAUGE SHOWED 2 BUTTONS WITH RIGHT ENGINE OFF AND ZERO PRESSURE. BOTH BUTTONS PULLED WHEN RIGHT ENGINE STARTED AND GAUGE INDICATED 5.25 INCHES. TROUBLESHOOTING REVEALED CHECK VALVES IN MANIFOLD LEAKING. VALVE HAD BEEEN INSTALLSDR 98ZZZX2665Channel · crackedUPON INPSECTION, THE HORIZONTAL STABILIZER LEFT SUPPORT AFT CHANNEL WAS FOUND CRACKED IN THE UPPER AND LOWER BEND RADII. THE CHANNEL HAD A LARGE BOW FROM TOP TO BOTTOM AND WAS NOT RESTING AGAINST THE SPAR. POORLY FIT. (FROM MFG).SDR 98ZZZX2664Spar · cracksUPON INSPECTION OF LEFT SUPPORT CHANNEL, THE CHANNEL HAD CRACKS IN UPPER AND LOWER RADII. THE CRACKS WERE STOP DRILLED AND THE DRILL PENETRATED THE SPAR. THE SPAR AND CHANNEL WERE REPLACED, THE CHANNEL APPARENTLY HAD A LARGE BOW IN IT AND CAUSED THE UPPER ANSDR 98ZZZX2666Pin · failedUPON RETRACTING GEAR, NOSE GEAR DOORS STAYED OPEN. GEAR WAS EXTENDED, SAFE LANDING WAS MADE. INSPECTION REVEALED NOSE GEAR DOOR PIN ASSY BROKE PIN OFF. POSSIBLY NOT RIGGED PROPERLY. INSTALLED NEW PIN ASSY AND RIGGED.SDR 98ZZZX1918Tubing · collapsedAT ANNUAL INSPECTION, THE BLUE PNEUMATIC LINE FOR RT WING DE-ICE BOOTS WAS FOUND COLLAPSED IN THE AREA JUST BELOW THE RT CABIN HEAT VENT LOCATED AFT OF THE CO-PILOT'S SEAT. THE VENT DUCTING APPEARED TO HAVE BECOME DISCONNECTED AND HAD HEATED THE TUBING ENOUGHSDR 98ZZZX1025Bracket · crackedDURING REPLACEMENT OF ELEVATOR INBOARD BEARINGS (WHICH WERE BOTH UNSERVICEABLE), THE UPPER RT CORNER OF BRACKET WAS FOUND CRACKED. A DYE-PENN INSP WAS PERFORMED AND TWO OTHER CRACKS WERE NOTED. WHEN BRACKET/HINGE WAS REMOVED AND CLEANED, THE BACK SIDE SHOWEDSDR 99ZZZX1978Brace · failedREF: ALERT NR 232, 11-97, PG 3, NOSE LANDING GEAR DOOR FAILURE. DURING ANNUAL INSPECTION, FOUND NOSE GEAR DOORS REMAINED OPEN DURING A RETRACTION TEST. INSPECTION OF THE SYSTEM FOUND P/N 002-410038-1 BROKEN. AFTER INSTALLING A NEW PART, THE NOSE GEAR DOORSSDR 97ZZZX4816Step · crackedUPON INSPECTION OF AIRCRAFT, FOUND RIGHT SIDE ASSIST STEP CRACKED WHERE IT HAD BEEN WELDED 7.5 HOURS AGO.SDR 97ZZZX4815Bulkhead · misinstalledUPON INSPECTION OF AIRCRAFT, FOUND AFT FUSELAGE BULKHEAD IMPROPERLY RIVETED. RIVET HEADS CLEARLY HAVE DENTS ALMOST LOOKING LIKE WRONG SET WAS USED TO DRIVE RIVETS. MOST OF THE UPSET ENDS WERE NOT PROPERLY BURRED. ALL RIVETS WERE REMOVED AND REPLACED AND PROSDR 97ZZZX4814Crush Washer · deformedUPON INSPECTION OF AIRCRAFT, FOUND LEFT WING SETTING AT A HIGHER ANGLE OF INCIDENCE. FURTHER INSPECTION REVEALED THE UPPER AFT CRUSH WASHER AND BOLT HAD SLIPPED DOWN APPROXIMATELY .25 INCH CAUSING LEFT WING TO HAVE MORE LIFT. AIRCRAFT HAD JUST FINISHED WITH SDR 97ZZZX4795Gearbox · out of rigUPON INSPECTION OF AIRCRAFT, THE LANDING GEAR HAD NO INTERNAL GEAR CLEARANCE IN ACTUATOR GEARBOX. AIRCRAFT HAD BEEN RIGGED 7.5 HOURS PRIOR AFTER THE NOSE GEAR FORWARD ROD END HAD BEEN REPLACED.SDR 97ZZZX4794Fairing · deformedUPON INSPECTION OF AIRCRAFT, NOTED LT WING INBOARD FAIRING DENTED AND DEFORMED. WING HAD JUST BEEN REMOVED AND REINSTALLED FOR A STRUCTURAL INSPECTION 7.5 HOURS PRIOR.SDR 97ZZZX3895Cylinder · scoredDURING COMPLETION OF CONTINENTAL CRITICAL SB CSB 97-10A, FOUND NR 2 CYLINDER SEVERELY SCORED DURING A BORESCOPE INSPECTION. DAMAGE COVERS 50 PERCENT OF TOTAL CYLINDER WALL AND IS BEYOND PISTON PIN WEAR AREA. HIGH AMOUNT OF ALUMINUM SHAVINGS FOUND IN OIL FILTSDR 97ZZZX3745Separator Tank · leakWHILE TROUBLESHOOTING AN OIL LEAK, SUBMITTER FOUND AIR OIL SEPARATOR TANK CRACKED AROUND THE INLET TUBE COMING FROM THE TURBOCHARGER. TWO CRACKS WERE RUNNING PARALLEL ALMOST 350 DEGREES AROUND THE TUBE. CRACKS HAD BEEN MASKED BECAUSE SOMEONE PREVIOUSLY COVERSDR 97ZZZX3419Valve · wrong partDURING AN ANNUAL INSPECTION, FOUND LEAKING EXHAUST VALVES ON NR 2, NR 4, AND NR 6 CYLINDERS, ON LT ENGINE. SINCE TOTAL TIME OF THIS ENGINE WAS ONLY 177.3 HOURS SINCE REBUILT, THE CUSTOMER DECIDED TO REMOVE ALL CYL'S FOR INSP AND/OR REPAIR. CYL'S DISASSEMBLEDSDR 97ZZZX3150Pump · leakINSPECTION OF LEFT FUEL BOOST PUMP REVEALED FUEL LEAKING FROM B PLUS INSULATOR. REF: BSL 1255 R1. PUMP WAS OVERHAULED 3-91.SDR 97ZZZX1173Pump · inoperativePILOT REPORTED GYRO WAS OUT. (IFR) A/C DIVERTED TO RFD. BOTH INSTRUMENT VACUUM PUMPS FAILED, LT AND RT. NO FAULT COULD BE FOUND THAT WOULD CAUSE BOTH PUMPS TO FAIL SIMULTANEOUSLY. TOTAL TIME OF PUMPS UNKNOWN. RECOMMEND LOG BOOK ENTRIES BE MADE WHEN VACUUMSDR 97ZZZX356Elbow · crackedPILOT REPORTED RIGHT MAIN STRUT BOTTOMED ON LANDING AND RIGHT BRAKE FAILED. ON INSPECTION, THE FITTING ON THE WHEEL CYLINDER WAS FOUND CRACKED. FURTHER INVESTIGATION FOUND WHEN STRUT WAS FULLY COMPRESSED, BRAKE LINE CONTACTED GEAR DOOR LINK ASSY. PN 35-8150SDR 96ZZZX5996Air Filter · rivets pulledNEW ENGINE AIR FILTERS WERE ORDERED FROM BEECH. WHILE INSTALLING A FILTER, IT WAS DISCOVERED THAT THE FRAME WAS ASSEMBLED WITH A PULLED 'POP' RIVET. THE RIVET STEM WAS NOT REMOVED FROM THE RIVET AFTER IT WAS PULLED. ONE STEM FELL TO THE FLOOR. FURTHER INVESDR 96ZZZX6154Truss · looseON ANNUAL INSPECTION, RIGHT TRUSS WAS FOUND LOOSE AT FORWARD END ATTACHMENT TO MOUNT. NUT ON HILOCK WAS FINGER TIGHT ONLY AND REMOVED BY HAND. REMOVAL OF HILOCK REVEALED .031 INCH DEEP SLOT WORN IN SHANK. WEAR IS IN AREA THAT CONTACTS MOUNTS. NO WEAR IN ARSDR 96ZZZX5442Pump · failedVACUUM SYSTEM FAILED PER PILOT REPORT. GAINED ACCESS TO VACUUM PUMPS, FOUND DRIVE SHAFTS SHEARED. REPLACED BOTH PUMPS, FILTERS, AND EVACUATED LINES AS REQUIRED. (NOTE: IT WOULD BE POSSIBLE THAT ONE PUMP HAD BEEN INOPERABLE FOR SOME TIME.)SDR 96ZZZX5441Pump · failedVACUUM SYSTEM FAILED PER PILOT REPORT. GAINED ACCESS TO VACUUM PUMPS, FOUND DRIVE SHAFTS SHEARED. REPLACED BOTH PUMPS, FILTERS, AND EVACUATED LINES AS REQUIRED. (NOTE: IT WOULD BE POSSIBLE THAT ONE PUMP HAD BEEN INOPERABLE FOR SOME TIME.)SDR 96ZZZX4088Gear Handle · not functionalDURING ANNUAL INSPECTION, FOUND EMERGENCY GEAR HANDLE TRAPPED UNDER FORWARD SPAR COVER. EMERGENCY EXTENSION WOULD HAVE BEEN IMPOSSIBLE. SUBMITTER STATED SPAR COVER INSTALLED INCORRECTLY BY PERSONS UNKNOWN.SDR 96ZZZX4399Spring Retainer · failedWHILE CHANGING VALVE COVER GASKET ON NR 3 CYLINDER, MECHANIC FOUND TWO SMALL PIECES OF METAL IN VALVE COVER. INVESTIGATED AND DETERMINED PIECES CAME FROM THE EXHAUST VALVE INNER VALVE SPRING RETAINER TCM. PERFORMED HIDDEN DAMAGE INSPECTION. INSPECTED AND CHSDR 96ZZZX3702Filter · defectiveOIL FILTER CUT OPEN AT OIL CHANGE. NOTICED INSIDE GASKET WAS CUT AND SLIGHTLY MISALIGNED. CLOSER LOOK REVEALED METAL PORTION WAS CUT APPROXIMATELY ONE INCH AND ONE INCH SLIVER ABOUT .0625 INCH THICK WAS STICKING INTO OIL OUTLET PATH. HAD THIS SLIVER COME LOSDR 96ZZZX3366Retract Arm · crackedDURING THE ANNUAL INSPECTION LANDING GEAR RETRACTION TEST, THE NOSE GEAR DOORS WERE OPEN 1.50 INCHES AND NOSE GEAR TIRE WAS MAKING CONTACT WITH THE RT GEAR DOOR. WITH A SLIGHT BIT OF HAND PRESSURE, THE NOSE GEAR RETRACTED AND DOORS CLOSED. A THOROUGH INVESTIGSDR 96ZZZX3374Pump · drive shearedPILOT REPORTED LEFT GYRO PRESSURE INOPERATIVE. INSPECTED AND FOUND SHEARED LEFT PUMP. WHILE REPLACING SYSTEM FILTERS, FOUND IN-LINE FILTER INSTALLED BACKWARDS. THIS IS BELIEVED TO HAVE CAUSED FAILURE.SDR EY2R9600691Split Bearing · corrodedCORROSION FOUND ON SPLIT BEARING.SDR EY2R9600690Split Bearing · corrodedCORROSION FOUND ON SPLIT BEARING.SDR EY2R9600689Low Stop Collar · corrodedCORROSION FOUND ON LOW STOP COLLAR.SDR EY2R9600688Low Stop Collar · corrodedCORROSION FOUND ON LOW STOP COLLAR.SDR EY2R9600068Propeller · crackedPROPELLER ASSY P/N 5244 IS CRACKEDSDR EY2R9600067Propeller · crackedPROP ASSY P/N 5244 IS CRACKEDSDR EY2R9600053Pitch Change Blk · crackedPROP ASSY HAS A PITCH CHANGE BLOCK CRACKEDSDR EY2R9600052Spring Retainer · crackedPROP ASSY HAS A CRACKED SPRING RETAINERSDR 96ZZZX2771Coupling · crackedCLAMP WAS FOUND CRACKED WHEN REMOVED FOR OTHER MAINTENANCE ON THE EXHAUST SYSTEM. SUBMITTER SUSPECTS CLAMP WAS OVERTORQUED AT PRIOR INSTALLATION. FAILURE OF THIS CLAMP COULD ALLOW HOT EXHAUST GASES TO BE RELEASED IN THE ENGINE COMPARTMENT. SUBMITTER RECOMMESDR 96ZZZX2770Shaft Assy · failedPILOT NOTICED ODD NOISE DURING GEAR RETRACTION AND SUBSEQUENT EXTENSION. INSPECTION ON GROUND REVEALED PART OF SHAFT ASSY THAT CLOSES GEAR DOORS BROKEN ALLOWING DOORS TO FLAP IN FLIGHT. SUBMITTER SUSPECTS NOISE HEARD BY PILOT WAS NOSE GEAR FORCING ITS WAY THSDR EY2R9600487Hub · corrodedCORROSION FOUND ON HUB.SDR 96ZZZX4723Rod End · fracturedROD END FAILED (FRACTURED) WHILE RETRACTING LANDING GEAR. PILOT HAD AN UNSAFE NOSE GEAR LIGHT, PILOT REPOSITIONED GEAR HANDLE TO THE DOWN POSITION. PUSH ROD TRAVELLED FORWARD PUSHING AGAINST NOSE GEAR EXTENDING AND LOCKING GEAR IN THE DOWN POSITION. CAUSE OSDR 96ZZZX681Starter Adapter · failedLOST OIL PRESSURE ON LT ENGINE DUE TO LOSS OF OIL VIA BROKEN STARTER ADAPTER. AIR CONDITIONER DRIVEN PULLEY AND DRIVE SHAFT HAD BROKEN LOOSE FROM STARTER/ADAPTER ALLOWING OIL TO ESCAPE OUT DRIVE AREA. WRONG TYPE BELT INSTALLED FOR THE TYPE DRIVE PULLEYS USED
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