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 CA130215011Ecu · failed(CAN) CUSTOMER REPORTS FADEC DEGRADE IN FLIGHT, REMAINS IN AUTO MODE, HOWEVER AT THROTTLE ROLL-DOWN NO RESPONSE, WHICH WOULD BE INDICATIVE THAT IT HAS REVERTED TO THE REVISIONARY GOVERNOR. IN THE DOWNLOADED FILES PROVIDED THERE ARE NO FAULTS OR EXCEEDANCES RESDR QMLA2013013113019Skin · damagedTWO AREAS OF CONCERN FOUND ON RT OUTER FUSALAGE SKIN. FIRST IS A CRACK ABOUT .7500" AT BS 163 & SECOND IS A OUTER SKIN DEBONDING AT BS 198.SDR EOPA20130123407O-Ring · leakingFUEL VAPORS WERE NOTICED IN CABIN. AFT CELL FUEL PROBE O-RING WAS TORN.SDR CA130215008Control Unit · malfunctioned(CAN) PILOT REPORTED FADEC FAULT, FADEC DEGRADED, AND RESTART FAULT INDICATIONS DISPLAYED ON THE MFD SCREEN AFTER LANDING AT DESTINATION NEAR THE COAST. THROTTLE WAS ROLLED FROM FLY TO IDLE BUT ENGINE DID NOT RESPOND, REMAINED AT 100 PERCENT ROTOR & N2 RPM. PSDR CA130124016Control Unit · defective(CAN) PILOT REPORTED FADEC FAULT, FADEC DEGRADED, AND RESTART FAULT INDICATIONS DISPLAYED ON THE MULTI FUNCTION DISPLAY, MFD, SCREEN AFTER LANDING AT DESTINATION NEAR THE COAST. THROTTLE WAS ROLLED FROM FLY TO IDLE BUT ENGINE DID NOT RESPOND, REMAINED AT 100SDR ALGA20130103647Drive Shaft · crackedNR 3 TAIL ROTOR DRIVE SHAFT CRACKED NEXT TO BOLT HOLE.SDR ALGA20130103447Drive Shaft · crackedNR 3 TAIL ROTOR DRIVE SHAFT CRACKED AT DRIVE FLANGE NEXT TO BOLT HOLE.SDR ALGA20130103408Drive Shaft · crackedSEGMENTED TAIL ROTOR DRIVE SHAFT CRACKED AT DRIVE FLANGE NEXT TO BOLT HOLE.SDR CA121220005Erosion Shield · cracked(CAN) A CRACK APPROXIMATELY 6.0" LONG WAS FOUND ON THE OTBD MOST AREA OF THE L/E EROSION STRIP.SDR CA130124023Cable Assy · chafed(CAN) DURING FUEL SYSTEM MAINTENANCE, FOUND FUEL SYSTEM CABLE ASSEMBLY DAMAGED FROM CHAFING ON LINE.SDR CA121220012Drive Shaft · cracked(CAN) DURING AN INSPECTION ON 1 OF OUR 407 ACFT, A CRACK WAS DISCOVERED IN A FLANGE OF THE NR 3 TAIL ROTOR DRIVE SHAFT AT THE BOLT HOLE. THIS PROMPTED US TO IMPOSE AN INSPECTION FOR CRACKS ON THE REST OF OUR FLEET. THIS INSPECTION REVEALED 5 ADDITIONAL CRACKSDR CA121220011Drive Shaft · cracked(CAN) DURING AN INSPECTION ON ACFT, A CRACK WAS DISCOVERED IN A FLANGE OF THE NR 3 TAIL ROTOR DRIVE SHAFT AT THE BOLT HOLE. THIS PROMPTED US TO IMPOSE AN INSPECTION FOR CRACKS ON THE REST OF OUR FLEET. THIS INSPECTION REVEALED 5 ADDITIONAL CRACKS IN TAIL ROTSDR CA121220010Drive Shaft · cracked(CAN) DURING AN INSPECTION ON ACFT, A CRACK WAS DISCOVERED IN A FLANGE OF THE NR 3 TAIL ROTOR DRIVE SHAFT AT THE BOLT HOLE. THIS PROMPTED US TO IMPOSE AN INSPECTION FOR CRACKS ON THE REST OF OUR FLEET. THIS INSPECTION REVEALED 5 ADDITIONAL CRACKS IN TAIL ROTSDR CA121220009Drive Shaft · cracked(CAN) DURING AN INSPECTION ON ACFT, A CRACK WAS DISCOVERED IN A FLANGE OF THE NR 3 TAIL ROTOR DRIVE SHAFT AT THE BOLT HOLE. THIS PROMPTED US TO IMPOSE AN INSPECTION FOR CRACKS ON THE REST OF OUR FLEET. THIS INSPECTION REVEALED 5 ADDITIONAL CRACKS IN TAIL ROTSDR CA121220008Drive Shaft · cracked(CAN) DURING AN INSPECTION, A CRACK WAS DISCOVERED IN A FLANGE OF THE NR 3 TAIL ROTOR DRIVE SHAFT AT THE BOLT HOLE. THIS PROMPTED US TO IMPOSE AN INSPECTION FOR CRACKS ON THE REST OF OUR FLEET. THIS INSPECTION REVEALED 5 ADDITIONAL CRACKS IN TAIL ROTOR DRIVE SDR CA121220007Drive Shaft · cracked(CAN) DURING AN INSPECTION ON ACFT, A CRACK WAS DISCOVERED IN A FLANGE OF THE NR 3 TAIL ROTOR DRIVE SHAFT AT THE BOLT HOLE. THIS PROMPTED US TO IMPOSE AN INSPECTION FOR CRACKS ON THE REST OF OUR FLEET. THIS INSPECTION REVEALED 5 ADDITIONAL CRACKS IN TAIL ROTOSDR K2DA20121214Transmission · making metalTRANSMISSION CHIP LIGHT DURING FLIGHT. PRECAUTIONARY LANDING PREFORMED. MX DISPACHED WITH COMPANY ACFT AND PASSENGERS WERE FLOWN FOR CONTINUATION OF THE FLIGHT. FOUND SMALL METAL PARTICALS ON LOWER CHIP PLUG, CLEANED PLUG PERFORMED PENALTY RUN WITHOUT FURTHESDR QMLA2012111712184Warning Light · false activationDURING FLIGHT, ENGINE CHIP LIGHT ILLUMINATED. DRAINED, FLUSHED, CHANGED FILTER, GROUND RUN COMPLETE, NO CHIPS DETECTED.SDR QMLA2012111512183Engine · malfunctionedPILOT REPORTED A FADEC FAIL, FADEC RESTART FAULT AND FADEC DEGRADE LIGHT IN CRUISE FLIGHT. FADEC CONTROLS REVERTED TO REVERSIONARY GOVERNOR AND PILOT HAD NO RESPONSE FROM COLLECT THROTTLE CONTROL. ENGINE SPEED REMAINED CONSTANT AT 100 PERCENT. MADE A PRECUATIOSDR QMLA2012111312179Pump · crackedON POST FLIGHT, NOTICE FUEL ODOR, OPEN ENIGNE COWLING NOTICED FUEL LEAKING FROM HMU ASSY. THERE ARE TWO CRACKS ON FUEL PUMP HOUSING. LOCATED THE 5:00 IS 1.5 " IN LENGTH ON THE IN SERVICE PORT LOCATED AT THE 6:00 RT ABOVE THE DRAIN PORT LENGTH IS 1.0".SDR QMLA2012111112175Blade · crackedPILOT FOUND CRACKS IN TOP SKIN OF MAIN ROTOR BLADE ON NOV 11, 2012 DURING MORNING PRE-FLIGHT CHECK.SDR EVCA2012111200038Spline · failedIN FLIGHT, HYD CAUTION LIGHT ILLUMINATED FOLLOWED WITH IN 10-15 SECONDS A COMPLETE LOSS OF HYD PRESSURE. PILOT PERFORMED EMERGENCY PROCEDURE UNABLE TO RESTORE HYD PRESSURE. LANDED AS SOON AS PRATICAL. MX REMOVED THE HYD PUMP BUT FOUND THE TRANSMISSION OIL PUMSDR QMLA2012110912177Blade · crackedMAIN ROTOR BLADE ABRASION STRIP CRACKED CHORDWISE AT BLADE STATION 199, FROM WEIGHT POCKET THROUGH L/E RADIUS.SDR ALGA2012110729082Chip Detector · contaminatedDURING CLIMB, TRANSMISSION CHIP LIGHT ILLUMINATED AND RETURNED TO BASE. MX FOUND INSIGNIFICANT AMOUNT OF METAL ON LOWER CHIP PLUG. COMPLIED WITH GROUND RUNS, NO DEFECTS.SDR ALGA2012110729142Master Switch · inoperativeAFTER START UP, THE AVIONICS MASTER SWITCH DID NOT SUPPLY POWER TO AVIONICS AFTER IT WAS TOGGLED ON. REPLACED AVIONICS MASTER SWITCH.SDR M3X2012F00000Transmission · making metalPICKED UP PATIENT, ENROUTE, TRANSMISSION CHIP LIGHT CAME ON. UNEVENTFUL PRECAUTIONARY LANDING MADE. CHIP PLUGS CHECKED, FOUND SILVER FLAKES, TRANSMISSION BEING REMOVED FOR REPAIR.SDR QMLA2012100912166Blade · delaminatedON ROLL UP/DOWN OF THROTTLE, PILOT ENCOUNTERED EXCESS VIBRATION (FELT AND HEARD). INSPECTED BLADES AROUND TRIM TABS AND DISCOVERED DELAMINATION FORWARD OF THE TRIM TAB ON THE BOTTOM SIDE OF THE BLADE, APPROX THE SPAN OF THE TAB (10") AND THE EXTENDS APPROX SDR CA121015011Ecu · faulted(CAN) THE ACFT FIRST STARTED EXPERIENCING NUISANCE FADEC DEGRADE FAULTS IAW RR CSL-6125 ON JULY 19, 2012. SINCE JULY THESE FAULTS HAVE REOCCURRED ON AN INCREASING BASIS WITH HRS FLOWN AND PRIOR TO SOFTWARE UPGRADE WERE REOCCURRING ALMOST EVERY FLIGHT. THE ECSDR ALGA2012092104Bearing · failedENGINE MAKING METAL, FOUND CAUSE FOR METAL IN OIL TO COME FROM NR 2 BEARING FAILURE.SDR ALGA2012092103Blade · crackedL/E ABRASION STRIP CRACKED. FOUND L/E ABRASION STRIP CRACKED IN SEVERAL PLACES AT APPROX 144-158.SDR ALGA2012092102Bearing · wornLARGE QUANTITY OF METAL ON LOWER TRANSMISSION CHIP DETECTOR. FOUND NO EVIDENCE OF MAKING METAL. PERFORMED A 4500 HR O/H. CHANGED OUT BEARING, DUE TO WORN ROLLERS.SDR QMLA2012091412152Warning Light · illuminatedPILOT REPORTED ENGINE CHIP LIGHT, PREPARING TO REFUEL, AND ACCORDING TO PMSP, PERFORMED PROCEDURE TO INSPECT, CLEAN AND REINSTALL CHIP DETECTORS. PERFORMED A 30 MINUTE GROUND RUN. NO DEFECTS. PROCEEDED BACK TO BASE AND UPON ARRIVAL AT BASE PULLING INTO HOVESDR CA120914009Duplex Bearing · making metal(CAN) MAIN TRANSMISSION MAKING METAL FOUND EVIDENT IN TRANSMISSION FILTER AND SUMP CHIP PLUG. TRANSMISSION REPLACED AND SENT TO O/H FOR EVALUATION. TRANSMISSION TEAR DOWN REPORT INDICATES DUPLEX BEARING, PN 407-340-032-101, SN ZV10283-B HAS 2 SPALL MARKS ON SDR QMLA2012091112150Frame · crackedTAILBOOM ATTACH FRAME, PN 407-030-027-101 WAS REPLACED BY UNITED ROTORCRAFT DUE TO CRACKING. A CRACK WAS DISCOVERED IN FRAME INSTALLATION ANGLE, PN 206-032-308-107 IN THE APEX OF THE BEND WHERE IT ATTACHES TO ABOVE MENTIONED TAILBOOM ATTACH FRAME. CRACKS IN SDR QMLA2012090612153Unknown · odorAFTER REACHING CRUISING ALITITUDE ENROUTE. NOTICED AN UNUSUALLY STRONG ODOR OF FUEL IN FLIGHT. PERFORMED A VISUAL INSPECTION OF ALL LINES AND AREAS AROUND THE ACFT AND FOUND NOTHING OUT OF THE ORDINARY. TOOK OFF AGAIN AND THE ODOR WAS GONE AND PROCEDED ONSDR HEEA20120906722Bearing · spalledENGINE REMOVED DUE TO IMPELLER RETIREMENT. NR 5 BEARING SPALLING IN OUTER RACE AT SPLIT. REPLACED WITH NEW NR 5 BEARING.SDR HEEA20120904748Bearing · spalledENGINE REMOVED DUE TO CYCLED WHEELS. NR 5 BEARING EXHIBITED LIGHT SPALLING AT OUTER RACE SPLIT. REPLACED WITH NEW NR 5 BEARING.SDR EOPA20120809001Longeron · crackedCOMPLETING THE 150 HR INSPECTION FOR ASB 407-11-95. A CRACK WAS FOUND IN ONE OF THE LONGERONS.SDR HEEA20120804485Bearing · spalledENGINE REMOVED DUE TO TURBINE OVERHAUL. NR 5 BEARING EXHIBITED SPALLING BALLS ON OUTER RACE. REPLACED WITH NEW BEARING.SDR CA120802017Support Angle · cracked(CAN) CRACK DISCOVERED ON LT HORIZONTAL STABILIZER UPPER SUPPORT ON TAILBOOM. CRACK WAS ON THE FORWARD PORTION OF THE DOUBLER.SDR QMLA2012072612122Skin · crackedWHILE PERFORMING PREFLIGHT INSPECTION, A CRACK WAS FOUND ON THE LEADING EDGE OF THE VERTICAL FIN ON THE TAIL. THE CRACK IS ABOUT 2" LONG AND STARTS AT THE LEADING EDGE AND GOES TO THE INBD SIDE OF THE VERTICAL FIN. THE ACFT WAS TAKEN OUT OF SERVICE AND A NEWSDR HEEA20120725351Combustion Case · crackedREMOVED DUE TO CRACKED AROUND FUEL NOZZLE BOSS. REPLACED COMBUSTION CASE.SDR CA120912011Grease Fitting · failed(CAN) IT WAS REPORTED THAT THE BALL AND SPRING OF 1 OF THE SWASHPLATE GREASE FITTINGS LEFT THE FITTING AND LOGGED IN THE SWASHPLATE BEARING CAUSING A PREMATURE WEAR AND REMOVAL OF THE PART. BLACK MUD WAS COMING OUT WITH THE GREASE.SDR ALGA2012071801Shaft · damagedUPON COMPLIANCE WITH A 3000 HR INSPECTION, FOUND SHAFT DAMAGED BEYOND REPAIR.SDR CA120912005Beam · cracked(CAN) IT WAS REPORTED THAT OPERATOR DISCOVERED A 3.5" CRACK ON THE ROOF PANEL ASSY IN FRONT OF THE RT FWD PYLON BEAM FOOT, APPROXIMATELY WL 72, BL 18, STAT 110. NO DAMAGE WAS DISCOVERED INSIDE THE CABIN, BELOW THE BEAM FOOT. THE BEAM WAS REPAIRED.SDR ALGA2012071702Stop · damagedON DISASSEMBLY, DUE TO BROKEN SPRING RETAINER, FOUND HOUSING, STOP ASSY, DAMAGED BEYOND REPAIR AND WAS REPLACED.SDR ALGA2012071601Bearing · making metalBEARING MAKINGMETAL IN ENGINE OIL.SDR CA120716010Blade · damaged(CAN) ON THE DAILY INSPECTION THE PILOT NOTICED THE SKIN ON THE TAIL ROTOR BLADE T/E WAS DELAMINATED, THE SKIN HAD SEPARATED. THE ACFT WAS GROUNDED, MAINTENANCE STAFF INSPECTED THE BLADE AND CONFIRMED THE DEFECT. A NEW BLADE WAS ORDERED AND INSTALLED. MFG PRSDR ALGA2012071302Adapter · corrodedDURING COMPLIANCE WITH 3000 HR O/H OF THE F/W UNIT ASSY, THE ADAPTER WAS DISCARDED DUE TO PITTING AND CORROSION BEYOND MFG LIMITS.SDR CA120912009Drive Shaft · cracked(CAN) PHI REPORTED THAT A T/R DRIVESHAFT ATTACHEMENT FLANGE WAS CRACKED NEAR THE OTBD BOLT HOLE. THE PART WAS SCRAPPED AND REPLACED WITH A NEW T/R DRIVESHAFT.
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