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 = '205A1' 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 = '205A1' 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 CA001122033Clip · missing(CAN) CIRCLIP AT END OF PUMP, (SOME PARTS FOUND IN PUMP P/S CAVITY) WAS FOUND MISSING, AND ALLOWED THE DRIVE SHAFT TO DISENGAGE FROM PUMP AND MOVE INTO THE TRANSMISSION DRIVE QUILL. THE PUMP WAS REMOVED AND SENT FOR TEST AND INSPECTION WHICH CONFIRMED SUSPICIOSDR CA000905011Boot · torn(CAN) - LEAKAGE OF GREASE WAS DISCOVERED COMING FROM THE MAIN DRIVE SHAFT AFTER AIRCRAFT WAS SHUT DOWN . FURTHER INVESTIGATION REVEALED THAT THE BOOT WAS TORN THUS ALLOWING LEAKAGE OF GREASE FROM THE DRIVE SHAFT COUPLING.- NO INDICATION OF OVERHEATING.SDR CA000801009Bearing · failed(CAN) T/R BECAME UNBALANCED. INSPECTED HUB AND FOUND BEARING TEFLON LINER CAME OFF FROM OUTER RACE.SDR CA000801008Impeller · cracked(CAN) WHEN COMPLYING AD 95-10-04. FOUND CRACKS ON IMPELLER.SDR CA000719015Combustion Chamb · cracked(CAN) COMBUSTION CHAMBER CRACKED 1.5 INCH IN LENGTH ON BACKEND CONE.AT 3 O CLOCK POSITION FRONT OF V BAND.SDR CA000718019Tail Rotor · missing(CAN) WHILE IN FLIGHT,TAIL ROTOR TIP CLOSURE FROM BLADE S/N A-9612 DEPARTED BLADE. ENSUING, EXTREME VIBRATION, CAUSED PILOT TO LAND IMMEDIATELY, WITHOUT FURTHER DAMAGE TO A/C. INSPECTION OF T/R SHOWED TIP CLOSURE OF BLADE S/N A-9612 TO BE GONE IN ITS ENTIRETYSDR CA000712003Fitting · cracked(CAN) A CRACK WAS FOUND AROUND THE HANGER BOLT HOLES. REPLACED SERVICEABLE PARTS.SDR CA001206002Blade · damaged(CAN) BOTTOM 1 INCH OF TAIL ROTOR SKIN PEELED OFF AND DEPARTED IN-FLIGHT. (X)SDR CA000614015Housing · cracked(CAN) PART WAS SUSPECTED TO BE CRACKED DURING A DAILY INSPECTION OF THE AIRCRAFT. THE PART WAS MOVED FOR INVESTIGATION AND THE CRACK FAILED. IF THE PART HAD FAILED IN FLIGHT IT WOULD HAVE CAUSED SEVERE COMPRESSOR STALLING OF THE ENGINE.SDR CA000926012Switch · failed(CAN) FUEL PUMP CAUTION LIGHT ILLUMINATED AFTER REPLACING FUEL REGULATOR. REPLACED PRESS SWITCH. CHECKED THIS SWITCH. CIRCUIT WAS CLOSED WITH PRESSURE. (X)SDR CA000926011Regulator · failed(CAN) - BLEED BAND OPENED WITH COLLECTIVE PITCH UP AND TORQUE INDICATOR SPIKED AND N1 SPOOL UP. BLEED BAND WOULD NOT CLOSE. N1 TOPPED UP AND TORQUE STAYS LOW. REPLACED BLEED BAND ACTUATOR WOULD NOT SOLVE PROBLEM. PROBLEM WAS FIXED WITH REPLACEMENT OF FUESDR CA000419005Sun Gear · broken(CAN) UPON FURTHER INVESTIGATION INTO WHY ENGINE WAS MAKING METAL, IT WAS FOUND THAT TWO TEETH HAD FRAGMENTED OFF THE GEAR. THE TEETH FRAGMENTS WERE .6250 INCH LONG AND WERE FOUND TRAPPED IN THE INTERNAL OIL SCREEN. THE CAUSE FOR THE GEAR FAILURE WAS NOT EVISDR CA000306002Coupling · cracked(CAN) CRACKS WERE FOUND IN THE ROOT AREA OF THE END COUPLINGS DURING LUBRICATION SCHEDULE AT 600 HRS/6 MONTHS. CRACKS CONFIRMED BY NDT TESTING. OVERHAUL SCHEDULE IS 1000 HRS.SDR CA000128014Gear · spalled(CAN) SPALLED GEAR TEETH ON BOTH THE PINION SHAFT GEAR AND THE STARTER SERVO GEAR. N1 GEARBOX REMOVED.SDR CA991229030Bearing · noisy(CAN) DURING ROUTINE INSPECTION, THE AME ROTATED THE MAIN INPUT SHAFT TO ENSURE PROPER FUNCTION ON FREEWHEEL UNIT AND HEARD UNUSUAL NOISES. FREEWHEEL UNIT WAS REMOVED AND THE INNER RACE OF THE BEARING WAS FOUND DAMAGED. NO OIL LEAK, DISCOLORATION OR METAL WAS SDR 99ZZZX4665Bearing · failedDURING OPERATION, PILOT EXPERIENCED AN ENGINE CHIP. OIL SYSTEM PRELIMINARY INVESTIGATION SUGGESTED NR 2 BEARING FAILURESDR CA991208087Bellcrank · broken(CAN) BELLCRANK FAILED ON POWER LEVER.SDR CA991027077Bearing · failed(CAN) DURING DAILY INSPECTION, THE BEARING WAS FOUND UNSERVICEABLE. THE BEARING IS HELD IN THE ROD END BY SWAGING AND FAILED ALLOWING THE BEARING TO SLIDE OUT OF THE ROD END. REPLACED.SDR CA991027075Bracket · cracked(CAN) DURING DOOR PANEL REPLACEMENT, THE DOOR POST SUPPORT WAS FOUND CRACKED WHICH HOLDS THE MAIN LATCH FOR THE CREW DOOR. FURTHER INVESTIGATION REVEALED THAT THE LT DOOR SUPPORT WAS ALSO CRACKED. SUBMITTER STATED IF LEFT LONGER, THE SUPPORTS WOULD HAVE FAILSDR CA990812004Bearing · damaged(CAN) DURING SCHEDULED MAINTENANCE, IT WAS DISCOVERED THAT THE BALL LINER WAS MOVING ALLOWING THE BALL TO CONTACT METAL THEREBY CAUSING DAMAGE TO BALL.SDR CA990812002Turbine Vanes · bent(CAN) THE ENGINE WAS ON ITS SECOND TBO EXTENSION WHEN IT EXPERIENCED A TURBINE FAILURE AT 240 HOURS TIME REMAINING.SDR CA990614020Transmision · making metal(CAN) MAIN TRANSMISSION MAKING ROARING NOISE. AFTER SHUTDOWN THE TRANSMISSION WAS MAKING A CLICKING NOISE. INSPECTION FOUND METAL IN THE FILTERS AND CHIP DETECTORS. TRANSMISSION AND MAST ASSEMBLY WERE REPLACED. TRANSMISSION GEAR SENT TO TSB LABS FOR ANALYSSDR CA990603006Pump · failed(CAN) PILOT HEARD NOISE FROM PYLON AREA,THEN NR 2 HYDRAULIC PRESSURE WARNING LIGHT ILLUMINATED. PILOT RESET CIRCUIT BREAKER, BUT PROBLEM STILL PRESENT. DEFECTIVE HYDRAULIC PUMP REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR CA990531002Switch · failed(CAN) DURING EXTERNAL HOISTING OPERATIONS, THE HOIST FAILED NEAR THE FULL-UP POSITION. A VISUAL INSPECTION FOUND THE PLUNGER FOR THE FULL-IN LIMIT SWITCH JAMMED IN THE CABLE GUIDE HOUSING OF THE HOIST THEREBY CUTTING POWER TO THE HOIST MOTOR NOT ALLOWING THE SDR CA990531007Generator · failed(CAN) GENERATOR WARNING LIGHT FLASHED SEVERAL TIMES AND WOULD NOT PRODUCE ANY OUTPUT. GENERATOR REPLACED, BUT PROBLEM REMAINED. VOLTAGE REGULATOR CHANGED AND SYSTEM IS NOW SERVICEABLE.SDR CA990430008Shield · failed(CAN) ON SHUTDOWN, FOLLOWING A ONE HOUR LEG OF A 3.5 HOUR FLIGHT, A RUBBING NOISE WAS HEARD FOLLOWING SHUTDOWN WHILE DYNAMIC COMPONENTS WERE STILL ROTATING. ON FURTHER INSPECTION, IT WAS NOTED THAT THE TAILPIPE SHIELD HAD DROPPED OUT OF POSITION AND HAD CONTASDR CA990401006Bearing · loose(CAN) DURING INSPECTION, GREASE SHIELD WAS FOUND MOVED/TURNED BY THE SLIP MARK. BEARING REPLACED.SDR CA990318016Liner · loose(CAN) AFTER REPLACING THE OIL COOLER BLOWER BEARING, THE BLOWER ASSEMBLY CAUSED HIGH FREQUENCY VIBRATION WHEN GROUND RUN. TROUBLESHOOTING REVEALED BEARING LINER, WHICH IS PRESSURE FITTED INTO THE BLOWER HOUSING, WAS LOOSE AND TURNING. THIS CAUSED MISALIGNMENSDR CA990308006Bearing · lack of lube(CAN) NOTICEABLE NOISE COMING FROM ENGINE OIL COOLER BLOWER. BEARINGS INSPECTED AND FOUND DRY. INSTALLATION OF NEW BEARINGS ELIMINATED EXCESS NOISE.SDR CA990224006Gearbox · malfunctioned(CAN) ENGINE VIBRATION AROUND N2 GEARBOX AREA. THE GEARBOX WAS REPLACED AND THE PROBLEM WAS CURED.SDR CA990223008Bearing · failed(CAN) HAND TURNING OF ENGINE OIL COOLER DURING INSPECTION REVEALED SOMETHING LOOSE AND NOISEY. BEARINGS REPLACED THEREBY RECTIFYING PROBLEM.SDR CA990223003Nut · cracked(CAN) DURING ROUTINE INSPECTION OF THE MAIN ROTOR HEAD, THE DRAG BRACE NUT WAS FOUND CRACKED. NUT WAS REPLACED.SDR CA990203004Mount · cracked(CAN) ENGINE MOUNT CRACKED ALONG WELD BEAD. REPLACED.SDR CA981230012Pivot Pin · broken(CAN) PILOT REPORTED THAT THE ENGINE WOULD NOT SPOOL DOWN WHEN HE TRIED TO CLOSE THE TWIST GRIP. FOUND THE PIVOT PIN ON THE TORQUE TUBE ASSY BROKEN OFF ON THE RT END. REPLACED.SDR CA981027003Nut · cracked(CAN) ON DAILY INSPECTION, ONE SCISSOR ASSY HAD TOO MUCH PLAY AT THE PIVOT. PIVOT BOLT CASTELLATED NUT CRACKED AND TORQUE LOST. NUT HELD IN PLACE BY SPLIT PIN.SDR CA981030018Support · loose(CAN) SUPPORT SLIPPING TO THE RIGHT ON BOTH FRONT AND AFT CROSSTUBES. ADHESIVE (PRC) PEELING FROM SUPPORT.SDR CA981022006Support · loose(CAN) SUPPORT SLIP TO THE RIGHT ON BOTH FRONT AND REAR CROSSTUBE. ADHESIVE (PRC) PEELING OFF SUPPORT. P/N ARE STC-AERONAUTICAL ACCESSORIES INC.SDR CA980930001Bearing · worn(CAN) ON PURGING GREASE FROM MAIN ROTOR GRIPS, OUTGOING GREASE WAS BROWNISH IN COLOR. ON DISASSEMBLY, BEARING CAGE WEARING ON THE INNER RACE. BEARING REPLACED.SDR CA980930006Bearing · broken(CAN) DURING INSPECTION, A COUPLE OF PIECES OF METAL WERE FOUND IN THE ENGINE EXTERNAL OIL FILTER. THE ENGINE WAS OPENED AND INSPECTION FOUND THE NR 2 BEARING CAGE WAS BROKEN.SDR CA980922004Driveshaft · sheared(CAN) ON START-UP, ENGINEER NOTICED THAT TAIL ROTOR WAS NOT ACCELLERATING LIKE THE M/R. SECOND DRIVESHAFT AHEAD OF THE 42 DEGREES GEARBOX HAD SHEARED AT ABOUT MID-SPAN.SDR CA980922002Chip Detector · illuminated(CAN) DURING FIREFIGHTING OPERATIONS, THE CHIP LIGHT ILLUMINATED. AFTER INSPECTION, THE AIRCRAFT WAS RETURNED TO SERVICE. ONE HOUR INTO OPERATIONS, THE CHIP LIGHT AGAIN ILLUMINATED AND THE AIRCRAFT WAS REMOVED FROM SERVICE. A FURTHER REPORT WILL BE SUBMITTESDR CA980922009Blade · cracked(CAN) DURING A FUEL STOP, ENGINEER FOUND CRACK IN BLADE. NO ABNORMAL FLIGHT CHARACTERISTICS. CRACK RUNS FROM THE INBOARD CORNER OF THE TRIM TAB, FORWARD TO THE SPAR AND THEN INBOARD ALONG THE SPAR FOR 6 INCHES. BELL ASB 205-96-67 IS BEING DONE DAILY, BUT THISDR CA980915001Cap · debonded(CAN) CAPS COMING OFF ON BOTH LT AND RT SKID TUBES. ADHESIVE PEELING OFF FROM CAP AND ADHESIVE WAS APPLIED OVER THE PAINTED TUBE.SDR CA980908010Governor · failed(CAN) ROTOR RPM DROPS AND OVERSPEEDS WITH COLLECTIVE LEVER MOVEMENT. ADJUSTMENT OF DROOP COMPENSATOR TO MAXIMUM DID NOT SOLVE THE PROBLEM. GOVERNOR WAS REPLACED AND PROBLEM SOLVED.SDR 98ZZZX2539Pitch Link · brokenPITCH LINK FAILED WHILE IN HOVER FLIGHT. PILOT EXECUTED HOVERING AUTOROTATION SUCCESSFULLY. TAIL ROTOR ASSY COMPLETE, 90 DEGREE GEARBOX, AND 42 DEGREE GEARBOX WERE REPLACED AS A PRECAUTION, FOR INSPECTION.SDR CA980629002Cross Tube · broken(CAN) WHILE DISEMBARKING PASSENGER AFTER LANDING WITH THE ROTOR STILL TURNING, A LOUD SNAP WAS HEARD ACCOMPANIED WITH A SUDDEN ROLLING OF THE HELO TO THE RIGHT. PILOT PREVENTED ANY FURTHER ROLL BY APPLYING CYCLIC AND AC FLOWN BACK TO BASE WHERE IT WAS SAFELY SDR CA980616003Rod · broken(CAN) ROD END OUTER RACE FRACTURED LOSING 1/3 OF CIRCUMFERENCE AND RELEASING THE BALL. LOSS OF CONTROL OF ONE BLADE AND TAIL ROTOR AUTHORITY.SDR CA980616002Crosstube · broken(CAN) ON LIFTING 6 FUEL DRUMS ON A SHORT LANYARD, PILOT SAW IN THE SLING MIRROR THAT THE LANYARD HAD CAUGHT ON THE RT SKID TUBE. ON ATTEMPT TO LAND, IT BECAME EVIDENT THAT THE REAR CROSSTUBE HAD BROKEN AND THE LANDING WAS ABORTED, THE LOAD RELEASED AND HELO RSDR CA980602031Bevel Gear · broken(CAN) ON FIRE FIGHTING MISSION, 90 DEGREE CHIP LIGHT ON. AFTER LANDING, CHIP PLUG WAS HEAVILY CONTAMINATED. INPUT GEAR 212-040-450-001 S/N A13-02363 HAD BROKEN TEETH, BEVEL GEAR 212-040-451-001 S/N A13-03609 HAD BROKEN TEETH, G/B HOUSING 212-040-468-001 S/N ASDR CA980602030Bearing · broken(CAN) CHIP DETECTOR WARNING LIGHT ILLUMINATED IN FLIGHT. AFTER LANDING INSPECTION OF THE CHIP DETECTOR SHOWED EXCESSIVE METAL CONTAMINATION. A MORE DETAILED INSPECTION FOUND THE NR 21 BEARING HAD A BROKEN BEARING CAGE. NO OTHER DAMAGE WAS FOUND.
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