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 CA120912006Blade · delaminated(CAN) ON A DAILY INSPECTION, THE PILOT NOTICED ONE OF THE TAIL ROTOR BLADES WAS DELAMINATING/SKIN SEPARATING ON THE T/E NEAR THE TIP. A REPLACEMENT WAS ORDERED.SDR CA120712007Servo · worn(CAN) INTERMITTENT VIBRATIONS WERE FELT THROUGH AIRFRAME DURING A FUNCTION CHECK OF THE HYDRAULICS. UPON INSPECTION OF THE T/R SERVO THE HARDWARE AND BUSHING WERE FOUND TO BE WORN. THIS CAUSED A FLUTTERING OF THE INPUT VALVE WHICH WAS FELT THROUGH THE AIRFRASDR HEEA20120629172Bearing · spalledNR 5 BEARING EXHIBITED SPALLING AT OUTER RACE SPLIT. REPLACED WITH NEW BEARING.SDR CA120724003Audio Control · shorted(CAN) AUDIO ALERT SYS, AN INTERMITTENT CONDITION OCCURRED WHEN THE MASTER CAUTION PANEL DID NOT PROVIDE A SOLID GROUND BUT A GROUND SIGNAL FLOATING A FEW VOLTS ABOVE GROUND DUE TO LEAKING VOLTAGE THROUGH THE INCANDESCENT LIGHTING IN THE CAUTION PANEL. THIS RESDR QMLA2012062612107Engine · making metalDURING CRUISE, ENGINE CHIP CAUTION WARNING LIGHT ILLUMINATED, NO OTHER INDICATORS WERE EVIDENT OF ENGINE DAMAGE, ACFT LANDED. MECHANIC FOUND CHIPS ON BOTH CHIP DETECTORS AND IS EVALUATING CORRECTIVE ACTIONS.SDR HEEA20120623174Bearing · spalledNR 5 BEARING EXHIBITED SPALLING OF OUTER RACE. INSTALLED NEW BEARING.SDR CA120907008Signal Cond Unit · malfunctioned(CAN) BELL HAS RECEIVED A REPORT FROM OUR CSE OF A PRIMARY TORQUE SOURCE FAILURE. EXTENSIVE TROUBLESHOOTING WITH THE ONSITE CSE HAS LED TO THE ROOT CAUSE BEING THE ENGINE SIGNAL CONDITIONER THAT CONVERTS ANALOG DATA SIGNALS TO DIGITAL TO BE ABLE TO BE SEEN BY SDR HEEA20120619118Bearing · spalledENGINE REMOVED FOR TURBINE OVERHAUL. NR 5 BEARING EXHIBITED SPALLING OUTER RACE AT SPLIT. REPLACED WITH NEW BEARING.SDR ALGA2012061901Fitting · leakingDURING ENGINE FUNCTIONAL CHECK ON ENGINE TEST CELL, ENGINE LEAKING OIL AT FITTING.SDR ALGA2012061803Bearing · failedENGINE CHIP LIGHT CAUSED BY PTO AFT BEARING FAILURE.SDR CA120911001Throttle Cable · disconnected(CAN) AFTER LANDING, THE ENGINE WOULD NOT RETURN TO IDLE. IT WAS SHUTDOWN USING THE FUEL VALVE. FOUND THAT THE CONTROL ASSY, THROTTLE CABLE, HAD DISCONNECTED INTERNALLY.SDR ALGA2012061412Step · corrodedFLOAT STEP, CORROSION BEYOND REPAIRABLE LIMITS.SDR ALGA2012061411Step · corrodedFLOAT STEP, CORROSION BEYOND REPAIRABLE LIMITS.SDR HEEA20120613173Bearing Race · spalledENGINE REMOVED DUE TO, RAN WITHOUT OIL PRESSURE. NR 5 BEARING EXHIBITED SPALLING OF OUTER RACE. INSTALLED NEW BEARING.SDR ALGA2012061201Rotor · damagedONE TRUNNION, PN 407-312-100-101, SN LKFS3425, HAS ELASTOMERIC EXTRUSION, FOUR WORN BEARINGS, PN 406-312-100-101 AND TWO PITCH HORNS PN 406-012-108-107, PITTING. CORROSION BEYOND LIMITS.SDR CA120906010Clamp · missing(CAN) CUSTOMER TOOK THE ENGINE TO REPAIR STATION TO HAVE THE NR 2 BEARING UPGRADED TO THE LATEST PN. UPON ENGINE DISASSEMBLY THEY FOUND THE CIRCLIP HOLDING THE SPUR ADAPTOR GEARSHAFT INTO THE COUPLING WAS MISSING. THE TEFLON RING WAS THE ONLY ITEM KEEPING THE SDR ALGA2012060501Wire · chafedPRIOR TO DEPARTURE, EMERGENCY FLOAT SYS WAS ARMED. AFTER DEPARTURE PILOT CLIMBED TO 500FT AND EMERGENCY FLOAT SYS UNEXPECTEDLY DEPLOYED, CONTINUED FLIGHT TO LOOP TERMINAL, AT 60 KTS AND LANDED. UPON INSPECTION BY MX PERSONNEL, POWER WIRE FOR FLOAT SYS WAS FOUSDR CA120907006Governor · malfunctioned(CAN) RECEIVED A REPORT FROM A PRIVATE OPERATOR THAT AN ACFT HAD AN UNCOMMANDED REVERSION TO MANUAL MODE FOLLOWED BY AN ENGINE OVERSPEED. FOLLOWING A DOWNLOAD OF THE ECU INCIDENT RECORDER IT WAS NOTED THAT THE REVERSIONARY GOVERNOR HAD FAILED AND WITHIN 5 SESDR CA120620010Seal · leaking(CAN) CUSTOMER REPORTED AN INCREASE IN ENG OIL LEVEL & A DECREASE IN HELICOPTER FREEWHEELING UNIT OIL LEVEL DURING OPERATION, OIL TRANSFER FROM ONE UNIT INTO THE OTHER. THE PROBLEM WAS IDENTIFIED BY ROUTINE PRE-FLIGHT OIL LEVEL CHECKS SHORTLY AFTER INSTALLATISDR ALGA2012052401Bearing · corrodedMAIN ROTOR MAST HAS BEARING CORROSION BEYOND LIMITS.SDR ALGA2012052214Panel · corrodedPANEL CORRODED BEYOND LIMITS.SDR ALGA2012052213Channel · corrodedCHANNEL CORRODED BEYOND LIMITS.SDR ALGA2012052212Frame · crackedFRAME CRACKED BEYOND REPAIRABLE LIMITS.SDR ALGA2012052211Skin · corrodedSKIN CORRODED BEYOND LIMITS.SDR ALGA2012052210Shelf · corrodedSHELF CORRODED BEYOND LIMITS.SDR ALGA2012052209Support · corrodedSUPPORT CORRODED BEYOND LIMITS.SDR ALGA2012052208Angle · corrodedANGLE CORRODED BEYOND LIMITS.SDR ALGA2012052207Skin · corrodedSKIN CORRODED BEYOND LIMITS.SDR ALGA2012052206Angle · corrodedANGLE CORRODED BEYOND LIMITS.SDR ALGA2012052205Angle · corrodedANGLE CORRODED BEYOND LIMITS.SDR CA120524014Scroll · cracked(CAN) 1" CRACK FOUND ON PRE-FLIGHT DAILY INSPECTION BY AME APPRENTICE ON LOWER LT SIDE OF COMPRESSOR SCROLL ADJACENT TO A WELD. HELICOPTER WAS GROUND RUN TO CONFIRM AND AIR WAS NOTED BLOWING FROM CRACKED AREA. COMPRESSOR ASSY WAS REMOVED FROM ENGINE AND SENTSDR CA120906012Wire · damaged(CAN) THE FUEL PRESSURE INDICATION WOULD GO TO 1 OR NO BARS INDICATED. THIS REQUIRED A TERMINATION OF ANY PATIENT FLIGHTS AND RETURN TO BASE MULTIPLE TIMES. THE SYSTEM SEEMED TO CHECK OUT PROPERLY WHEN MAINTENANCE SHOWED UP. EVENTUALLY, PN 407-375-007-107 INSDR ALGA2012051803Adapter · corrodedADAPTER CORRODED BEYOND LIMITS.SDR ALGA2012051802Adapter · corrodedADAPTER CORRODED BEYOND LIMITS.SDR HEEA20120517921Skin · corrodedFWD ROOF SKIN FOUND CORRODED COMMON TO THE SERVO COWLING HINGE AND NUTPLATE INSTALLATION. THE REPAIR DOCUMENTATION WILL BE SUBMITTED TO A STRUCTURAL FAA-DER FOR APPROVAL. THE FORWARD ROOF SKIN WILL THEN BE REPAIRED IAW THE FAA-APPROVED REPAIR DATA.SDR ALGA2012051601Hub · damagedONE SHEAR BEARING PN 407-310-101-101, SN LK13178 ELASTOMERIC SEPARATED FOUR FEATHER BEARINGS PN 407-310-102-101, SN'S LK3060, LK3654, LK5682, LK5644 WITH ELASTOMERIC EXTRUSION, AND ONE PITCH HORN PN 407-010-103-113, SN AZ1694. PITTING CORROSION BEYOND LIMITS.SDR HEEA20120514913B-Nut · looseAFTER TAKEOFF, ENGAGED AIR CONDITIONER. ABOUT 2 MINUTES LATER CREW INFORMED ABOUT A LARGE AMOUNT OF SMOKE ON LT SIDE OF ACFT AND IN REAR CABIN. DISENGAGED AIR CONDITIONER, OPENED WINDOWS AND LANDED. SHUTDOWN ELECTRICAL POWER AND THROTTLE. NO DAMAGE OR EVISDR QMLA2012050912075Engine · making metalWHILE ON A POST MX CHECK FLIGHT, ENGINE CHIP LIGHT ILLUMINATED IN FLIGHT. PILOT MADE A PRECAUTIONARY LANDING AT A REMOTE LZ, MX FOUND A SUBSTANSIAL AMOUNT OF METAL ON THE ENGINE ACCESSORY GEARBOX CHIP DETECTOR. ACFT REMOVED FROM SERVICE.SDR ALGA2012050701O-Ring · leakingPERFORM FUNCTIONAL CHECK, FOUND O-RING ON DIFFERENTIAL VALVE FAILED, CAUSING INTERNAL FLUID BYPASS. REPLACED O-RING.SDR HEEA201205033750Panel · corrodedUPPER SKIN ON OIL COOLER PANEL ASSY WAS FOUND TO BE CORRODED.SDR HEEA20120501940Bearing · spalledNR 5 BEARING EXHIBITS SPALLING ON OUTER RACE IN TURBINE. INSTALLED NEW NR 5 BEARING.SDR QMLA2012042712070Chip Detector · contaminatedREMOVED LOWER & MAST TRANSMISSION AND FREEWHEEL CHIP DETECTORS. ONLY THE TRANSMISSION LOWER DETECTOR HAD A SMALL AMOUNT OF FUZZ. CLEANED DETECTORS AND REINSTALLED, RAN UNIT AND REINSPECTED AFTER RUN AND RETURNED TO SERVICE IAW MM 63-14 & FIG 63-2.SDR CA120501005Skid · cracked(CAN) THE ENGINEER WAS CARRYING OUT A DI AND FOUND THE STINGER, TAIL SKID, LOOSE AND UPON FURTHER INSPECTION FOUND THE STINGER CRACKED AT THE BOLT HOLE. THERE WAS CORROSION IN THE AREA OF THE CRACK.SDR HEEA2012042933771Bearing · spalledTURBINE REMOVED TO INSPECT FOR METAL IN OIL. ON INSPECTION OF NR 5 BEARING, FOUND SPALLING AT OUTER RACE SPLIT. SCRAP PART AND REPLACE WITH NEW.SDR ALGA2012042702Frahm · multiple failDURING COURSE OF REPAIR TO FRAHM DAMPER FOUND STOP ASSY, (407-010-165-103), & HOUSING, (407-010-152-109) DESTROYED. SEVEN SPRINGS (407-310-104-105) GOUGED. ONE SPRING (407-310-104-105) BROKEN. ONE PLUG (407-010-155-109) GOUGED. TWO SPRING SEATS, (407-010-173SDR ALGA2012042604Structure · crackedCRACKED BEARING BORE GOING OUTWARD.SDR ALGA2012042603Blower · damagedDURING COURSE OF REPAIR TO OIL COOLER BLOWER ASSY, FOUND AND REPLACED ONE SHAFT (407-040-320-103, SN A-3283), BEARING JOURNAL WORN BEYOND LIMITS. TWO NUTS (90-118-4) DAMAGED BEYOND LIMITS. ONE SHIELD (407-040-328-101) DAMAGED BEYOND LIMITS, ONE BEARING (407-SDR CA120906007Blades · broken(CAN) DURING RECEIVING INSPECTION, IT WAS REPORTED THAT 1 OF THE COMPRESSOR BLADES WAS FOUND BROKEN. DUE TO THE EXTENT OF DAMAGE FOUND ON COMPRESSOR IMPELLER, COMPRESSOR ASSY WAS DISASSEMBLED COMPLETELY. MOREOVER, THE GP SECTION WAS SEPARATED FROM THE REST OSDR K2DA201205310001Turbine Wheel · failedTURBINE RUBBING SOUND DETECTED ON SHUTDOWN. TURBINE SECTION REMOVED FROM SERVICE FOR INSPECTION. INSPECTION FOUND NR 1 AND NR 2 TURBINE WHEELS RUBBING DUE TO NR 2 NOZZLE WARPING. BOTH TURBINE WHEELS AND NR 2 NOZZLE UNSERVICEABLE.SDR ALGA2012042501Structure · corrodedSLAT ASSY CORRODED BEYOND REPAIR LIMITS.
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