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 = '401A' 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 = '401A' 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 CA150511004Engine · power loss(CAN) DURING TAKEOFF, THE PILOT ADVANCED BOTH PLAS TO TAKEOFF & NOTICED THAT THE NR 1 ENG DID NOT RESPOND FROM THE IDLE SPEED OF 28% N1. THE PILOT ABORTED THE MISSION & RETURNED TO THE GATE & TRIED AGAIN WITH NO ABILITY TO ADVANCE POWER ON THE SUSPECT ENG NR SDR EBTR20150309008Unknown · unknownSHORTLY AFTER TAKE-OFF AT APPROXIMATELY 200 FT AGL, PILOT NOTICED PARTIAL LEFT ENGINE POWER LOSS WITH ENGINE FUEL FLOW SURGING FROM MINIMUM TO MAXIMUM. DECLARED AN EMERGENCY RETURNED AND LANDED . NOTICED WHEN PULLING POWER BACK TO LAND PROBLEM LEFT. VISUALSDR EBTR20130305007Lug · failedAPPROXIMATELY 1.5 HRS INTO FLIGHT, PILOT NOTED RT ENGINE MANIFOLD PRESSURE DROPPED AFTER SWITCHING FUEL TANKS ADJUSTED POWER, ENGINE MANIFOLD PRESSURE DROPPED AND SURGED, PILOT NOTICED OIL ON TOP OF RT ENG COWL AND OIL PRESSURE LOW AND SURGING, REDUCED POWERSDR EBTR20120712006Control Cable · brokenON APPROACH PILOT SELECTED FULL FLAPS, HEARD LOUD POP AIRCRAFT WANTED TO ROLL RIGHT. CORRECTED WITH AILERON, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENCE. INSPECTED AIRCRAFT FOUND THAT A FLOOR PANEL CLIP NUT HAD BECOME CAUGHT IN FLAP DRIVE GEAR/CHAIN CAUSSDR CA090710007Screw · broken(CAN) RT MLG COLLAPSED DURING TURN TO LINE UP FOR TAKEOFF. PARTS FOUND FAILED AFTER COLLAPSE. ADJUSTING SCREW PN 0841113-3 FOUND SHEARED. BOLT ATTACHING BELLCRANK ASSY TO LANDING GEAR TRUNNION FOUND SHEARED. BOLT PN NAS464P4-26 FOUND SHEARED. MOUNTING LUGSDR EBT2009F00000Torque Tube · brokenDURING RETURN FLIGHT, PILOTS NOTICED SLOPPY RUDDER CONTROL, THEY INVESTIGATED AND FOUND VERY LITTLE RUDDER INPUT FROM LT PEDAL ON BOTH PILOT AND CO-PILOTS SIDE. USING RUDDER TRIM FOUND THEY COULD CONTROL RUDDER. THEY FOUND CLOSEST AIRPORT ENROUTE WITH WINDS SDR CA060112008Intercostal · damagedCAPTAINS OUTBOARD RUDDER PEDAL MOUNT BLOCK INTERCOSTAL AT STN 118.55, REPAIRED DUE TO CRACKED.SDR TZR2005F00029Cylinder · crackedCRACKED BETWEEN SPARK PLUG BOSS AND EXHAUST CYLINDER. TYPICAL OF THE CYLINDERS. (K)SDR TZR2005F00028Cylinder · crackedRT ENGINE NR 5 CYLINDER. LOW COMPRESSION. (K)SDR TZR2005F00026Cylinder · crackedCRACK IS TYPICAL FOR THESE CYLINDERS, RT ENGINE NR 6 CYLINDER. (SW05200509365) (K)SDR TZR2005F00023Cylinder · crackedCRACK IS TYPICAL FOR THESE CYLINDERS, RT ENGINE NR 3. (K)SDR TZR2005F00022Cylinder · crackedCRACK IS TYPICAL FOR THESE CYLINDERS. RT NR 4. (SW05200509363). (K)SDR TZR2005F00021Cylinder · crackedCRACK IS TYPICAL FOR THESE CYLINDERS, LT NR 3, (SW05200509362). (K)SDR CA050722006Rudder Pedal · crackedPILOT REPORTED THAT RT PARK BRAKE DOES NOT HOLD WHEN SET. UPON MAINTENANCE INSPECTION IT WAS DISCOVERED THAT CAPTAINS OB RUDDER PEDAL INTERCOSTAL MOUNT AT STATION 110.00 WAS CRACKED. IT WAS REPAIRED AS PER CESSNA SRM SECTION 16-38 FIGURE 16-25.SDR TZR2005F00017Cylinder · crackedCRACKED FROM EXHAUST VALVE TO TOP SPARK PLUG. ECI CYLINDER. (SW05200507950) (K)SDR TZR2005F00016Cylinder · crackedCRACKED FROM EXHAUST VALVE TO TOP OF SPARK PLUG. ECI CYLINDER. (SW05200507949) (K)SDR TZR2005F00027Torque Link · crackedTHE LT AND RT MLG HAD CRACKS ON THE BOSS AREA WHERE THE TORQUE LINKS ATTACH. THE CRACKS WERE ABOUT .2500 INCH LONG AND LOCATED NEXT TO WHERE THE BOSS CONNECTS TO THE TUBE. (K)SDR TZR2005F00001Attach Fitting · crackedTHE LT AND RT MAIN LANDING GEAR HAD CRACKS ON THE BOSS AREA WHERE THE TORQUE LINKS ATTACH. THE CRACKS WERE ABOUT .2500 INCH LONG AND LACATED NEXT TO WHERE THE BOSS CONNECTS TO THE TUBE. (SW05200506155) (K)SDR 2002FA0001217Hub · mismanufacturedBLADE RETENTION NUT TO HUB LOCK PLUG HOLE DRILLED TO IMPROPER DEPTH. HUB RETIRED FROM SERVICE.SDR 2002FA0001216Hub · mismanufacturedBLADE FERRULE ACTUATING PIN HOLE DRILLED IN WRONG LOCATION IAW MM. (MIN. EDGE DISTANCE BETWEEN HOLE 1 INCH) HUB RETIRED FROM SERVICE.SDR 2002FA0001215Hub · mismanufacturedBLADE RETENTION NUT TO HUB LOCK PLUG HOLE MACHINED IN WRONG LOCATION AT LAST OVERHAUL OR LAST ASSEMBLY. HUB RETIRED FROM SERVICE.SDR MHJ2002F00001Cylinder · brokenNR 2 CYLINDER ON LEFT ENGINE HAD A SMALL PIECE MISSING FROM AROUND EXHAUST VALVE AREA. ENGINE HAS BEEN REMOVED FROM SERVICE FOR OVERHAUL.SDR AUS20010504Bracket · cracked(AUS) RUDDER LOWER HINGE BRACKET CRACKED AT CORNERS.SDR AUS20010498Structure · corroded(AUS) EXTENSIVE SURFACE CORROSION THROUGHOUT THE FIN AND TAIL ASSEMBLY.SDR 20001218SH017Link · wornUPON C/W AD 76-13-07, REPLACEMENT OF FORK BOLTS, PLAY WAS NOTICED AT ADJUSTING SCREW/DOWNLOCK SWITCH LOCK LINK. UPON FURTHER INSPECTION, THREADS WERE SHOWN TO BE WORN AND PART WAS ALLOWED ABOUT 5 THOUSANDS OF AN INCH IN PLAY. THIS IS THE SECOND REPORT FILED SDR 20001018SH028Counterweight · crackedRELEVANT MAGNETIC PARTICLE INDICATION. (X)SDR 20001018SH027Blade · corrodedPROPELLER BLADE CORRODED. (X)SDR 20001018SH026Blade · corrodedPROPELLER BLADE CORRODED. (X)SDR 20000404SH025Hub · crackedPROPELLER HUB CRACKED IN THE BLADE SOCKET AREA.SDR 99ZZZX4605Exhaust Pipe · crackedLEFT EXHAUST TAIL PIPE WAS FOUND CRACKED AND A PIECE OF THE PIPE APPROXIMATELY 2 INCHES BY 2.50 INCHES WAS MISSING. IT APPEARED THE CRACKING WAS MOST LIKELY CAUSED BY VIBRATION. EXHAUST GAS LEAKING FROM THIS TAIL PIPE CAN CAUSE DAMAGE TO THE WING SPAR.SDR AU990733Wire · loose(AUS) LANDING GEAR MOTOR CONNECTION LOOSE.SDR CA980928016Manifold · damaged(CAN) NR 1 ENGINE RAN ROUGH IN CRUISE. INSPECTION FOUND ONE FUEL INJECTOR WAS PARTIALLY BLOCKED. THE FUEL MANIFOLD WAS DISASSEMBLED AND THE SCREEN WITHIN THE MANIFOLD WAS FOUND DISTORTED. THE FUEL MANIFOLD WAS REPLACED. THE ENGINE WAS GROUND RUN SERVICEABLSDR CA980706004Case · fractured(CAN) AFTER TAKEOFF WITH CRUISE POWER SELECTED, THERE WAS SEVERE VIBRATION FROM THE LEFT HAND ENGINE. SMOKE, FLAMES, AND OIL WERE SEEN COMING FROM THE ENGINE COWLING. THE ENGINE WAS SHUT DOWN. POST-FLIGHT INSPECTION FOUND THERE WERE TWO HOLES IN THE UPPER ESDR 98ZZZX115Lifter · galledLIFTER/CAMSHAFT GALLED. LIFTER BODY CHIP FOUND IN OIL FILTER. PRESSURE RELIEF VALVE CAUSING LOW OIL PRESSURE. ENGINE TORN DOWN, NEW PARTS INSTALLED.SDR 98ZZZX114Camshaft · galledLIFTER/CAMSHAFT GALLED. LIFTER BODY CHIP FOUND IN OIL FILTER. PRESSURE RELIEF VALVE CAUSING LOW OIL PRESSURE. ENGINE TORN DOWN, NEW PARTS INSTALLED.SDR 97ZZZX2920Alternator · lug crackedALTERNATOR MOUNT LUG FOUND CRACKED, AND OIL LEAKING AT GASKET. ALTERNATOR HAS ONLY 197 HRS SINCE OVERHAUL. ON DISASSEMBLY, ONE LUG FOUND CRACKED AND ONE LUG FELL OFF COMPLETELY.SDR 97ZZZX1952Torque Tube · failedRUDDER SYSTEM CEASED TO OPERATE. FOUND LEFT RUDDER TORQUE TUBE ASSY ARM BROKEN FREE OF TORQUE TUBE. THIS ARM IS CONNECTED TO RUDDER CABLE. REPLACED TORQUE TUBE WITH NEW PART.SDR 97ZZZX2081Torque Tube · brokenPILOT EXPERIENCED LANDING DIFFICULTIES. UPON INSPECTION OF FLIGHT CONTROLS, TECHNICIAN DISCOVERED RUDDER CABLE ATTACH FITTING BROKEN OFF OF THE LT CONTROL TORQUE TUBE ASSY. MAGNAFLUX INSPECTION OF THE RT TORQUE TUBE ASSY REVEALED IT CRACKED AT THE EDGE OF THSDR AU961096Bearing · loose(AUS) RH ENGINE DRIVEN ALTERNATOR SLIP RING END BEARING LOOSE IN END HOUSING - BEARING HOUSING SUPPORT WEBS CRACKED AND BROKENSDR CA970421093Control Cable · separated(CAN) THE AREA WHERE THIS FAILURE OCCURRED IS LOCATED BEHIND A PULLEY AND IS NOT EASILY INSPECTED WITHOUT THE USE OF A MIRROR LOOKING INBOARD. SOME WEAR AND FRAYING WAS ALSO NOTICED JUST OUTBOARD OF THE PULLEY. THERE WAS SOME CORROSION ON THE CABLE BUT NOT IN SDR CA960826062Control Cable · separated(CAN) THE AREA WHERE THIS FAILURE OCCURRED IS LOCATED BEHIND A PULLEY AND IS NOT EASILY INSPECTED WITHOUT THE USE OF A MIRROR LOOKING INBOARD. SOME WEAR AND FRAYING WAS ALSO NOTICED JUST OUTBOARD OF THE PULLEY. THERE WAS SOME CORROSION ON THE CABLE BUT NOT IN SDR AU960556Diode · faulty(AUS) LH ALTERNATOR DIODES LOOSE AND BROKENSDR AU960302Switch · broken wire(AUS) FLAP SELECTOR DOWN MICROSWITCH WIRE BROKENSDR EY2R9601405Retain Bearing · frettedPROP ASSY RETAIN BEARING RACES FRETTEDSDR EY2R9601404Ball Bearing · frettedPROP ASSY BALLS FRETTEDSDR 96ZZZX722Shaft · shearedINSTALLED REBUILT STARTER/ADAPTER AFTER PREVIOUS ONE FAILED AFTER 26 HOURS OF USE. THIS CURRENT ONE, SN 77371, FAILED AFTER 2.5 HOURS AND SIX STARTS DUE TO THE SAME PROBLEM - SHEARED GEAR.SDR CA951228003Bearing · failed(CAN)DURING FLIGHT THE OIL PRESSURE ON THE #2 ENGINE BEGAN TO DROP SO THE ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION OF THE ENGINE REVEALED THE OIL BREATHER LINE HAD FROZEN AND CREATED A PRESSURE BUILD THAT CAUSED ONE OF THE PUSH RODS SEAL TO BLOW OUT RESULTSDR 95ZZZX5209Transfer Pump · leakingAIRCRAFT LANDED AND DURING TAXI OUT, PILOT NOTICED GLOW NEAR RT NACELLE AREA. TOWER REPORTED SUSPECT FIRE. PILOT SHUT DOWN, EXITED AIRCRAFT. FIRE WAS EXTERNAL UNDER WING. FIRE EXTINGUISHED ON ITS OWN. NO DAMAGE TO AIRCRAFT FOUND ON FOLLOW-UP INSPECTION.
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