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 = '407' 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 = '407' 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 QMLA2013102413149Engine · making metalPILOT REPORTED ENGINE CHIP LIGHT ILLUMINATED. REMOVED UPPER AND LOWER CHIP PLUGS AND REMOVED A SMALL AMOUNT OF FLAKES. CLEANED THE PLUGS AND REINSTALLED. THE ENGINE WAS RUN AT 100 PERCENT FOR 30 MINUTES WITH NO ADDITIONAL WARNING LIGHTS. THE ACFT WAS RETURSDR QMLA2013101513145Longeron · crackedFOUND A CRACK IN LONGERON ON TAILBOOM.SDR CA131010011Bearing · loose(CAN) ON THE ACFT, THE DUAL CYCLIC CONTROL WAS MAKING NOISE WHILE MOVING IT LATERALLY, A CLICKING SOUND. AFTER INVESTIGATION, IT WAS FOUND THAT THE LOWER BEARING OF THE PIVOT ASSY WAS SLIGHTLY MOVING AXIALLY INSIDE OF ITS HOUSING. IT APPEARS THAT THE BEARINGSDR EOPA20131010847Skin · crackedDURING A ASB CHECK DISCOVERED SKIN CRACKED.SDR EOPA201309270415Fuel Filter · leakingAIRFRAME FUEL FILTER FOUND LEAKING FROM DRAIN VALVE.SDR QMLA2013090513127Gearbox · making metalENGINE CHIP LIGHT ILLUMINATED DURING FLIGHT. PERFORMED A PRECAUTIONARY LANDING. MECHANIC ARRIVED, PULLED AND INSPECTED ALL ENGINE CHIP DETECTORS AND FOUND CHIPS/FLAKES ON THE LOWER ENGINE CHIP PLUG. CLEANED CHIP PLUG, PERFORMED 30 MINUTE PENALTY RUN. NO LIGHTSDR M3XA201309030001Longeron · crackedFOUND CRACKED LONGERON WHILE PERFORMING ASB 407-11-95.SDR CA130903005Engine · making metal(CAN) ENGINE CHIP LIGHT ILLUMINATED DURING DESCENT FORM SIGHTSEEING FLIGHT. ACFT LANDED NORMALLY AT BASE WITHIN 5 MINUTES OF CAUTION LIGHT ACTIVATION. METAL FOUND ON BOTH ENGINE CHIP DETECTORS. ENGINE REMOVED FOR INSPECTION.SDR 2013F00176Chip Detector · activatedENGINE CHIP LIGHT.SDR QMLA2013082913125Stringer · crackedDURING DAILY INSPECTION, FOUND TAIL SKID STRINGER, EXCESSIVELY LOOSE. FOUND CRACK AT BASE OF STRINGER AROUND MOUNTING HOLE.SDR CA130930008Disc Pack · cracked(CAN) UPON INSPECTION THE ENGINEER FOUND 1 OF THE DISCS IN THE DISC PACK CRACKED AND CORRODED. THE DISC PACK WAS REPLACED. THIS ACFT HAD A DISC CRACKED IN 2009 AND HAS FLOWN OVER 3300 HOURS SINCE THE LAST INCIDENT.SDR QMLA2013081513117Engine · making metalWHILE PERFORMING 25 HOUR INSPECTION OF ENGINE MAGNETIC CHIP DETECTORS IAW EO 13-7900-EO-432 IAW CEB-A-72-6075, REV 1. METAL FLAKES CONSISTING OF MORE THAN 10 PIECES EACH WERE DISCOVERED ON BOTH UPPER AND LOWER CHIP DETECTORS. ACFT WAS GROUNDED AT THAT TIME ASDR ALGA201308167605Bearing · galledENGINE HOT START. NR 2 BEARING GALLED.SDR CA130812008Bolt · sheared(CAN) WHILE PERFORMING INSPECTION, ACCORDING WITH BHT-407-MM1, CH 5-00-00, PARA 5-20 & DOC B0223-OM4, PARA 1.2. ROTOR BRAKE GUIDE BOLTS FOUND SHEARED, ROTOR BRAKE PADS WORN EXCESSIVELY AND CAUSED CALIPER WEAR.SDR QMLA2013080913114Gearbox · making metalON LANDING, ENGINE CHIP LIGHT ILLUMINATED. NUMEROUS SLIVERS AND CHIPS FOUND ON BOTH THE TOP AND BOTTOM GEARBOX CHIP DETECTORS. ACFT WAS REMOVED FROM SERVICE. ENGINE CHANGED.SDR EOPA20130806637Servo · ratchetingCOLLECTIVE MOVEMENT WAS NOT SMOOTH. A RATCHETY FEELING IN THE COLLECTIVE LEVER. SERVO'S WERE SWAPPED TO THE CYCLIC CONTROLS. PROBLEM FOLLOWED THE SERVO.SDR ALGA201308017561Bearing · failedTRANSMISSION CHIP PLUG INDICATED METAL WAS BEING MADE. ON TEARDOWN OF TRASMISSION, FOUND THAT THE DUPLEX BEARINGS WERE BREAKING DOWN.SDR M3XA2013073000003Bearing · delaminatedDURING FLIGHT, EXPERIANCED A MAIN ROTOR VIBRATION, PRECAUTIONARY LANDING MADE. NORMAL SHUTDOWN. MX INSPECTED AND FOUND SHEAR BEARING ON MAIN ROTOR HEAD DELAMINATING.SDR CA130730001Blade · damaged(CAN) MFG DISCOVERED T/R BLADE ABRASION STRIP BONDING VOIDS AROUND AND EXTENDING AT PROXIMITY OF THE BLADES` DRAIN HOLE.SDR CA130923006Pinion Gear · broken(CAN) PILOT EXPERIENCED ENGINE CHIP LIGHT IN FLIGHT. ACFT LANDED, CHIP PLUGS INSPECTED. NOTHING APPARENT FOUND ON SELF SEALING QUICK DISCONNECT PLUG. PLUG REINSTALLED LIGHT STILL ON. MAINTENACE WENT TO SITE, REMOVED CHIP PLUG BOSS, FOUND GEAR TOOTH. ACFT GSDR ALGA071220137529Duplex Bearing · galledRECURRING CHIP LIGHT. DISCOVERED DUPLEX BEARING IN TRANSMISSION BREAKING DOWN.SDR QMLA2013070213090Engine · power lossACFT DEPARTED. 7 MINUTES INTO FLIGHT, 1600 FT MSL, CLIMBING TO 2000 FT, FADEC FAULT CAUTION ILLUMINATED. BETWEEN 10 & 15 SECONDS LATER ACFT EXPERIENCED A VIOLENT LEFT YAW OF APPROX 45 DEGREES. AN AUTOROTATIVE DESCENT IMMEDIATELY INITIATED. DURING DESCENTSDR CA130709003Tip Cap · detached(CAN) TIP CAP DEPARTED TAIL ROTOR BLADE. BLADE HAD BEEN RECENTLY REPAIRED.SDR QMLA2013063013086Hydraulic System · malfunctionedAFTER DECENT AND LEVELING AT 2500 FEET THE HYD PRESS AND CYCLIC CENTER LIGHTS ILLUMINATED ALONG WITH THE LOSS OF NORMAL CONTROL FORCES AND THE ACFT BECAME VERY SLOPPY AND HEAVY. ALL INDICATIONS ARE THAT THE HYD FAILED, DECLARED AN EMERGENCY AND DIVERTED. TURSDR CA130702010Relay · failed(CAN) THE MAIN STARTER RELAY HAS THREE SETS OF CONTACTS INSIDE. THE MAIN CONTACTS AND 2 MICROSWITCHES FOR THE IGNITION SYSTEM. THE MICROSWITCH FOR THE IGNITION RELAY HAS FAILED AND THIS SEEMS TO BE A RECURRING PROBLEM. THESE MICROSWITCHES DON`T SEEM TO LAST ASDR ALGA0620201330374Warning Light · illuminatedFUEL FILTER CAUTION LIGHT ILLUMINATED DIMLY.SDR ALGA201306187448Blade · cracked3 EA MAIN ROTOR BLADES HAVE CRACKED ABRASION STRIPS. SNS A-179, A-629, A-1960.SDR CA130618009Cable · corroded(CAN) REPAIR FACILITY WAS TROUBLESHOOTING INSTRUMENT INDICATIONS/ FAILURES WHEN THE CABLE BACK SHELL AREA WAS FOUND TO BE COMPLETELY CORRODED.SDR ALGA060720137435Beam · corrodedCORROSION FOUND ON ROCKER BEAM AROUND PIVOT BUSHING.SDR CA130612006Ecu · failed(CAN) 11 PM LOCAL TIME. THE PILOT MADE A NORMAL OUTBOUND FLIGHT AND SHUTDOWN AT A TRAUMA SCENE. 5 MINUTES INTO A 10 MINUTE RETURN FLIGHT THE FADEC DEGRADE LIGHT, AUTO RELIGHT LIGHT CAME ON WITH ALL OTHER INDICATIONS NORMAL FADEC REMAINED IN AUTO MODE. THE PISDR CA130611005Engine · making metal(CAN) ACFT WAS ENROUTE TO DROP THE OWNER OFF FOR VACATION. ENGINE CHIP LIGHT ILLUMINATED. ACFT LANDED, REMOVED THE UPPER AND LOWER CHIP PLUGS AND FOUND CHIPS ON UPPER AND LOWER PLUGS BUT THE UPPER PLUG HAD A 1.93 MM "CHUNK" THAT ILLUMINATED THE LIGHT IAW THESDR CA130611009Engine · making metal(CAN) SUBJECT HELICOPTER, ROUTINE ANNUAL INSPECTION, WHEN TECHS CHECKED THE ENGINE CHIP PLUGS IAW ASB 407-13-99 AND CEB A-72-6075 AND FOUND SIGNIFICANT AMOUNTS OF METAL FLAKES ON BOTH PLUGS. AT LEAST 1 OF THE CHIPS EXCEEDS THE R & R OPS & MM 72-00-00, PAGE 33SDR CA130612003Mount · damaged(CAN) PILOT REPORTED A STRANGE INTERMITTENT VIBRATION. DURING A VISUAL INSPECTION, THERE WERE CONTACT MARKS ON THE LT AFT CORNER MOUNT UP STOP/SAFETY WASHER. UPON INSPECTION WITH THE CORNER MOUNT LIFT TOOL, THE LT AFT CORNER MOUNT WAS FOUND SEPARATED. ALL 4SDR CA130515011Hmu · malfunctioned(CAN) DURING CRUISE FLIGHT AND APPROXIMATELY 30 TO 45 MINUTES AFTER TAKEOFF THE PILOT HEARD A PING AND NOTED THE FADEC DEGRADE AND RESTART LIGHTS ON. UPON LANDING THE THROTTLE WAS SELECTED TO IDLE BUT THE ENGINE REMAINED AT 100 PERCENT NR. WITH THE THROTTLESDR CA130509008Scroll · cracked(CAN) CRACK IN SCROLL FOUND BY AME AFTER COMPRESSOR ASSY WAS REMOVED FOR LOOSE PERCUSSION WELDED ATTACHMENT STUDS. COMPRESSOR ASSY BEING SHIPPED FOR REPAIR. SCROLL, SN FU40784. SCROLL TSN TO FOLLOW.SDR QMLA2013050613063Sump · making metalDURING THE 20 HOUR INSPECTION OF THE CHIP DETECTORS IAW 13-7900-E0-432 FOUND METAL CHIP ON THE SUMP CHIP PLUG THAT EXCEDED THE LIMITS CALLED OUT IN MM.SDR CA130515012Ecu · malfunctioned(CAN) FADEC DEGRADED, FADEC FAULT, AUTO RELIGHT AND RESTART CAUTION LIGHTS ILLUMINATED DURING LEVEL FLIGHT, SHORTLY AFTER TAKEOFF FROM THE MEXICO CITY AIRPORT. A NORMAL LANDING WAS COMPLETED 6 MINUTES AFTER TAKEOFF. THE THROTTLE WAS MOVED TO THE FLIGHT IDLE PSDR CA130507003Line · collapsed(CAN) UPON INSTALLATION OF NEW LINE INTERFACING THE AIRFRAME FUEL FILTER WITH THE HMU TECH NOTED THE LINE COLLAPSED INTERNALLY WHEN APPLYING THE NECESSARY TORSION.SDR QMLA2013042413061Warning Light · illuminatedON APPROACH, PILOT ENCOUNTERED FLYING DEBRIS, PULLED IN COLLECTIVE AND ENCOUNTERED A FLASHING TORQUE DISPLAY AND SUBSEQUENT ERROR MESSAGE ON THE INDICATOR. AFTER RETURNING TO BASE, MECHANIC DOWNLOADED THE TORQUE INDICATOR RECORDED EXCEEDANCE, WHICH WAS 119 PESDR QMLA2013042213057Disc Pack · crackedAIRWORTHINESS INSPECTION FOUND TAIL ROTOR AFT SHORT SHAFT COUPLING DISC PACK CRACKED.SDR CA130502009Stud · broken(CAN) FOUND STUD BROKEN DURING DAILY INSPECTION.SDR JBZA20130430002Panel · corrodedDURING 60 MONTH INSPECTION, FOUND CORROSION ON THE RT AND LT TRANSMISSION MOUNTS AFT. ATTACHING SURFACE OF THE ROOF PANEL ASSY. REPAIRED IAW THE PSE FIELD REPAIR NR 13RL-045.SDR QMLA2013041513053Clock · burnedDURING FLIGHT, PILOT NOTICED AND SMELLED SMOKE IN COCKPIT WHICH APPEARED TO BE COMING FROM THE CLOCK AREA. PILOT PERFORMED A SAFE PRECAUTIONARY OFF SITE LANDING. PILOT ALSO MENTIONED THAT THE NVG LIGHTING ON OTHER INSTRUMENTS WENT OUT THEN RETURNED AFTER LANSDR ALGA0409201329919Cartridge · cloggedABOUT 10 MILES OFF OF BEACH LINE, THE BOOST PUMP CAME ON. PILOT TURNED ACFT AROUND AND RETURNED TO BASE. REPLACED LT BOOST PUMP CARTRIDGE.SDR QMLA2013032113043Panel · deformedCREW REPORTED BURNING PLASTIC ODOR IMMEDIATELY AFTER TURNING OFF HEATER SYS. ODOR LASTED ABOUT 30 SECONDS AND WAS GONE. ON INSPECTION OF HEATER SYS, FOUND THE INTERIOR TRIM PANEL AT THE OUTLET OF THE AIR COMM HEATER IN THE CABIN AT THE RT SIDE AFT FACING SEATSDR CA130311025Nut · loose(CAN) HYDRAULIC SERVO, WAS FOUND TO HAVE A LOOSE ROD END JAM NUT ON THE FORWARD END OF THE SERVO. THE NUT LOCKS THE ROD END FROM SPINNING IN OR OUT OF THE SERVO SHAFT. THIS ROD END IS NOT FIELD ADJUSTABLE AND THE LENGTH IS SET UP AT O/H/FACTORY. THE LOCK NOSDR COZR20130311003Pump · failedINSTALLED FOUR O/H FUEL BOOST PUMPS, IN SAME POSITION. EACH BOOST PUMP WOULD OPERATE WHEN INITIALLY POWERED UP, THEN FAIL TO OPERATE ON SUBSEQUENT ATTEMPTS. INSTALLATION OF FIFTH OVER HAULED UNIT OPS CHECKED NORMAL WITH NO SUBSEQUENT FAILURES.SDR CA130222007Wire · cracked(CAN) LOW LEVEL FUEL SWITCH, PN 407-362-005-103, S/N 301 WAS DISCOVERED TO HAVE CRACKED AND MISSING INSULATION ON BOTH THE WIRES ENTERING AND EXITING THE SWITCH. THE WIRES ARE BONDED INTO THE BASE OF THE SWITCH AND THE WIRES ARE NON REMOVABLE. THE CRACKED INSDR QMLA2013021613025Engine · making metalPILOT REPORTED ENGINE CHIP LIGHT ILLUMIINATED JUST AFTER LANDING AND RETURNING TROTTLE TO IDLE. MX WAS CALLED AND A LARGE AMOUNT OF FLAKES WERE FOUND ON BOTH THE UPPER AND LOWER ENGINE CHIP DETECTORS. SOME FLAKES EXCEEDED THE MAXIMUM ALLOWABLE IAW MM 72, PARA SDR CA130208007Blades · damaged(CAN) PILOT HAD JUST COMPLETED POWER CHECK FOLOWING DAY OF HELISKI OPS AND WHEN MECHANIC EXITED THE AIRCRAFT DURING ENGINE COOL DOWN HE HEARD A LOUD BANG FOLLOWED BY A GRINDING NOISE. SHUT ENGINE DOWN AND DISCOVERED A PROBLEM NEAR THE FRONT OF THE ENGINE. BO
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