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 = '206L4' 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 = '206L4' 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 EVCA202209290001Blower Motor · odorELECTRICAL SMELL NOTED DURING FLIGHT. FOUND TO BE THE FORWARD AIR CONDITIONER BLOWER MOTOR.SDR EVCA202209160001Blower Motor · overheatedINTERMITTENT ELECTRICAL FUMES IN CABIN AND COCKPIT IN CRUISE FLIGHT. AIR CONDITIONER AFT EVAPORATOR BLOWER MOTOR OVERHEATING.SDR EVCA091222A/C Pack · smokeAIR CONDITIONER SYSTEM PRODUCING WHITE SMOKE IN CABIN WITH ACCOMPANYING BURNING SMELL.SDR EVCA20220701001Stiffener · crackedRH CONTROL COLUMN SKIN CRACKED AT UPPER RIVET. AFT RH CONTROL COLUMN STIFFENER CRACKED.SDR EVCA202207010001Motor · overheatedELECTRICAL SMELL IN FRONT AND BACK CABIN AREA. AIR CONDITIONER AFT EVAPORATOR BLOWER MOTOR OVERHEATING.SDR EVCA20220629001Motor · odorSTRONG ELECTRICAL SMELL IN AIRCRAFT IN FLIGHT WHILE A/C IS ON.SDR EVCA0622222Motor · inoperativeSTRONG ELECTRICAL SMELL IN AIRCRAFT IN FLIGHT.SDR EVCA0622221Wire · meltedBURNT ELECTRICAL SMELL IN CABIN AREA. AIR CONDITIONER AFT EVAPORATOR BLOWER WIRE SPLICE OVERHEATED AND MELTED AT RESISTOR.SDR EVCA062222Inverter · inoperativeSHARP ACRID ELECTRICAL SMELL IN COCKPIT & CABIN 20 MIN INTO FLIGHT, EXECUTED PRECAUTIONARY LANDING AT AEL 26; NO CHANGE IN ANY ELECTRICAL INSTRUMENTS. REMOVED INVERTER PN: MD50, SN: L12-10852 AND REPLACED WITH SAME PN, SN: J15-11274 AS PER REF A.C. INVERTER SDR EVCA0407222Frame · noneRH FRAME STATION 145 CRACKEDSDR EVCA0407221Frame · noneRH FRAME STATION 145 STIFFENER CLIP CRACKEDSDR EVCA040722Frame · unknownLH FRAME STATION 145 CRACKEDSDR EVCA0330222Stiffener · crackedLH FS145 STIFFENER CLIP CRACKEDSDR EVCA030922Bulkhead · unknownTAILBOOM ATTACH FITTING BULKHEAD SUPPORT CRACKED. CRACK ORIGINATES FROM A RIVET HOLE NEAR THE UPPER LEFT ATTACH POINT MOUNT.SDR EVCA030722Frame · crackedLH FRAME STATION 145 CRACKEDSDR EVCA20220304001Resistor · noneUPON ACFT START UP WITH INCREASED THROTTLE, HEAVY SMOKE BUILD UP IN THE CABIN COMING FROM AFT A/C VENTS.
FOUND AFT BLOWER MOTOR HIGH/LOW RESISTOR ASSEMBLY OVERHEATING.SDR 8MHR021465AEDiffuser · separationFORWARD PLATE SEPARATED FROM VANE SEGMENTSDR 8MHR021404AEDiffuser · separationFORWARD PLATE SEPARATED FROM VANE SEGMENTS.SDR EVCA080921None · noneENGINE LOST POWER DURING FLIGHT AND TOT WENT TO 852 DEGREES C FOR 31 SECONDS.SDR EVCA0302180100001Pump · damagedHYDRAULIC SYSTEM FAILED ON GROUND RUN. FOUND HYDRAULIC PUMP SPLINE SHEARED.SDR EVCA202108064001Blade · debondedVAN HORN MAIN ROTOR BLADE TRIM TAB DEBONDED.SDR EVCA042820212Blade · corrodedBOTH MAIN ROTOR BLADE LEADING EDGES ARE PITTED AND HAVE CORROSION.SDR EVCA04282021Blade · corrodedBOTH MAIN ROTOR BLADE LEADING EDGES ARE PITTED AND HAVE CORROSION.SDR EVCA2021021001Stiffener · crackedDURING ROUTINE INSPECTION FOUND VERTICAL TUNNEL RIGHT REAR STIFFENER CRACKED.SDR 2GYR20200918911Nut · undertorquedWE REMOVED MAST ASSY P/N 206-040-014-107 S/N 52047 TO REPAIR A LEAKING MAST BEARING SEAL. WHEN REMOVAL OF MAST NUT P/N 206-040-078-101 WAS ATTEMPTED IT WAS FOUND TO BE IMPROPERLY TORQUED. NUT WAS APPROXIMATELY HAND TIGHT AND NOT TO SPECS OF 500-550 FT-LBS. SDR EVCA20200824001Bulkhead · crackedDURING ROUTINE INSPECTION, VISUALLY FOUND CRACK IN TAILBOOM FWD BULKHEAD PN: 206-032-400-027 AT APPROXIMATELY THE 10 O'CLOCK POSITION.SDR EVCA202007302Blade · crackedTWO CRACKS FOUND ON MAIN ROTOR BLADE NICKEL ABRASION STRIP AT BLADE STATION 204.5 EXTENDING CORD WISE 40 % AND 30% OF LEADING EDGE.SDR EVCA202007301Blade · crackedCRACK FOUND ON MAIN ROTOR BLADE NICKEL ABRASION STRIP AT BLADE STATION 203 EXTENDING CORD WISE 60% OF LEADING EDGE.SDR EVCA202003251Frame · crackedDURING ROUTINE INSPECTION, THE MAIN FUSELAGE TAILBOOM ATTACHMENT FRAME PN: 206-032-308-103 WAS VISUALLY FOUND TO BE CRACKED.SDR EVCA2020032500000Longeron · crackedDURING ROUTINE INSPECTION, THE LH UPPER TAILBOOM ATTACHMENT FITTING LONGERON PN: 206-031-314-037 WAS VISUALLY FOUND TO BE CRACKED.SDR EVCA20201210001Blade · delaminatedDURING PERIODIC INSPECTIONS MAIN ROTOR BLADE PN: 206-015-001-115 SN: A-7245 TRAILING EDGE WAS FOUND TO BE CRACKED AND DELAMINATED. DELAMINATION SPANS FROM 142 INCHES TO 150 INCHES FROM ROOT END. THE CRACK IS WITHIN THE DELAMINATED AREA AT 146.5 INCHES FROM ROOSDR EVCA202001130001Bulkhead · crackedDURING PERIODIC INSPECTION, FOUND TAILBOOM ATTACHMENT BULKHEAD CRACKED AT UPPER LH INTERCOSTAL.SDR EVCA201912130001Mast · corrodedMAIN ROTOR MAST FOUND TO HAVE CORROSION INTERNALLY DURING 12 MONTH INSPECTION. REMOVED MAIN ROTOR MAST AND REPLACED WITH SERVICEABLE.SDR EVCA201911260001Collector · crackedENGINE EXHAUST COLLECTOR HAS A 1.10 INCH CRACK LH AFT SIDE.SDR EVCA201911121Tube · crackedBY VISUAL INSPECTION, FOUND PG AIR LINE FROM ACCUMULATOR TO FUEL CONTROL CRACKED APPROXIMATELY HALF THE CIRCUMFERENCE AND 1/2 INCH FROM FITTING.SDR EVCA20191112001Attach Fitting · crackedDURING 300 HOUR INSPECTION, UPPER RH TAILBOOM ATTACHMENT FITTING FOUND CRACKED.SDR EVCA20191029002Attach Fitting · crackedDURING INSPECTION, THE TAILBOOM UPPER LH ATTACHMENT FITTING WAS VISUALLY IDENTIFIED AS CRACKED.SDR EVCA2019100100001Skin · crackedVERTICAL TUNNEL WEB SKIN RIGHT SIDE UPPER AT BOX BEAM IS CRACKED.SDR EVCA2019093000000Skin · crackedL/H AFT STIFFENER IN VERTICAL TUNNEL AND L/H VERTICAL TUNNEL SKIN CRACKED.SDR IAVA2019072900001Panel · crackedDURING POST FLIGHT INSPECTION FOUND CRACK IN ROOF. LEFT AFT CORNER FROM RIVET HOLE WHERE ROOF ATTACHES TO ROLL OVER BULKHEAD. CRACK WAS VERIFIED BY DYE PENETRANT. DURING REMOVAL OF ROOF FOUND CORROSION ON RIGHT HAND AFT CORNER.SDR EVCA201907182Motor · inoperativeBURNING SMELL COMING FROM VENTS IN THE CABIN WHEN AIR CONDITIONING OR BLOWER IS RUNNING. PROBLEM FOUND TO BE BLOWER MOTOR.SDR EVCA201906040001Stiffener · crackedRH AFT CORNER ANGLE & SKIN OF VERTICAL TUNNEL CRACKEDSDR CA190607012Stabilizer · broken(CAN) IT WAS REPORTED TO BELL: VERTICAL FIN BROKE IN FLIGHT, FOLDED ON THE RH SIDE OF THE SHIP. SHIP FLIGHT TIME 16,000 HOUR +/-. (TC# 20190607012)SDR CA190528020Blade · damaged(CAN) DURING A ROUTINE DAILY INSPECTION OF A BELL 206L-4 THE PILOT/ENGINEER NOTED THAT A COVER PLATE ON THE BOTTOM OUTBOARD END OF ONE OF THE MAIN ROTOR BLADES HAD BECOME DEFORMED AND BULGED AWAY FROM THE BLADE. UPON CLOSER INSPECTION IT WAS NOTED THAT IT LOOKSDR EVCA2019052400001Blower · inoperativeSMELLED SMOKE COMING FROM AFT AC BLOWER MOTOR. INSPECTED AIR CONDITIONING SYSTEM RELAYS BEHIND HATRACK FOR CONDITION, NO FAULTS NOTED. REMOVED AND REPLACED AFT AIR CONDITIONER EVAPORATOR BLOWER ASSY P/N ES61142-1. VACUUMED AND RE-SERVICED AIR CONDITIONING SYSSDR EVCA2019052100001Stiffener · crackedAFT RT STIFFENER IN CENTER POST CRACKED.SDR CA190526001Combustion Liner · damaged(CAN) DURING CRUISE FLIGHT A LOUD HUMMING NOISE BECAME AUDIBLE. NO POWER LOSS OR ABNORMAL INDICATIONS OCCURRED AT THIS TIME ALTHOUGH IT WAS NOTED THAT TOT WAS A LITTLE HIGHER THAN NORMAL. THE PILOT LANDED THE AIRCRAFT AND DROPPED OFF PASSENGERS AND CONTINUED SDR EVCA2019051000001Stiffener · crackedVERTICAL TUNNEL AFT RT CORNER STIFFENER CRACKED.SDR CA190521011Structure · broken(CAN) IT WAS REPORTED TO BELL:DOWNWIND LANDING TO A RIVER BED. PILOT REPORTED FEELING A VIBRATION BEFORE TOUCH DOWN BUT REPORTED NO UNUSUAL CONTROL PROBLEMS. LANDING WAS MADE WITH AN EXTREMELY TAIL LOW ATTITUDE AND PILOT REPORTED FEELING AN IMPACT AND HEARING SDR EVCA2019040300000Post · crackedDURING INSPECTION, FOUND CRACK ON BROOM CLOSET RT AFT UPPER SKIN. AT STATION 81.27, WL 67.00, BL 5.06.
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