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 jasc_code = '6100' 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 jasc_code = '6100' 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 GLBA2001154Circuit Board · inoperativeLEFT AUTO FEATHER INOPERATIVE, REPLACED PCB OPS CHECKED SYSTEM STATISFACTORYSDR GLBA2001150Indicator · stuckRIGHT PROP RPM INDICATOR FAILED ON T/O, REPLACE INDICATOR AND TACH GENERATORSDR SIMA20011662Gauge · inoperativeROC - FLT 4877 - CREW ABORTED TAKEOFF DUE TO THE RIGHT PROPELLER RPM INDICATOR GOING TO ZERO. MAINTENANCE REMOVED AND REPLACED THE INDICATOR IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200116203Indicator · failedLGA - FLT 4515 - ABORT TAKEOFF RIGHT PROP ERRATCI. REMOVED AND REPLACED PROP SPEED INDICATOR IAW AMM 61-40-00. OPS CHECK GOOD. (M)SDR SIMA200116103Indicator · failedLAX - FLT 3080 - ON TAKEOFF ROLL, RIGHT PROP OIL TEMP AND PRESSURE GAUGE WENT TO ZERO. ABORTED TAKEOFF. NO OTHER PROBLEM NOTED. REMOVED AND REPLACED PROP OIL TEMP INDICATOR IAW AMM. PERFORMED GROUND RUNS. OPS CHECK GOOD. (M)SDR SIMA20011193BladeMIA - FLT 5257 - DURING CLIMB-OUT, CREW NOTICED UNUSUAL PROPELLER VIBRATION. REDUCING POWER ON NR 1 ENGINE REDUCED THE VIBRATION. MAINTENANCE REMOVED AND REPLACED THE NR 1 BLADE ON THE NR 1 PROPELLER IAW ATR MM. OPS WAS GOOD AND AIRCRAFT WAS RETURNED TO SERSDR SIMA0683Propeller · vibrationBGR - FLT 9753 - CREW REPORTED VIBRATION IN FLIGHT AT 1396, 1270, AND 1230 PROPELLER RPM. CREW COULD NOT TELL IF VIBRATION WAS FROM LEFT OR RIGHT ENGINE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. MAINTENANCE PERFORMED AN INTENSIVE INSPECTION OF FUSELAGE SDR SIMA0641Pcu · malfunctionedDFW - FLT 3251 - RIGHT PROP WENT TO FEATHER WHEN POWER WAS ADVANCED FOR TAKEOFF, THERE WAS NO TORQUE INDICATION AT THIS POINT. PROP CAME OUT OF FEATHER WHEN THE AUTOCOARSEN WAS TURNED OFF, STILL WITH NO TORQUE INDICATION. RAI RIGHT ENGINE PCU IAW HAMILTON STSDR CA010223002Blade · corroded(CAN) EXTRA WORK REQUIRED TO REMOVE CORROSION FROM BLADE FACE (CAMBER FACE) IN ACCORDANCE WITH MCCAULEY MANUAL 730720.SDR 20010220CW001Propeller · blownAIRCRAFT WAS COLD SOAKED, OUTSIDE TEMPERATURE BEFORE DEPARTURE WAS 15 DEGREES. SUBMITTER FEELS THIS WAS A CONTRIBUTING FACTOR TO THIS SEAL BEING DEFECTIVE. COMPANY INITIATED PROCEDURES NOT TO CHANGE PROP BLADE ANGLE UNTIL MINIMUM OF 40 DEGREE OIL TEMPERATURESDR 20010126CW013Counterweight · brokenMIR / DAL - RIGHT ENGINE SURGING AFTER TAKE OFF, RETURNED TO AIRPORT. FOUND COUNTERWEIGHT COLLAR BROKEN. REMOVED PROP AND SENT TO PROP SHOP FOR INSPECTION, EDDY CURRANT INSPECTION AND REPAIR. RETURNED TO SERVICE REINSTALLED ON AIRCRAFT.SDR CA001228025Blade · damaged(CAN) DURING PREFLIGHT INSPECTION #2 HEATER ELEMENT FOUND BURNED. BLADE REPLACED IAW AMM, A/C RETURNED TO SERVICE.SDR CA001123029Propeller · failed(CAN) PILOTS FLIGHT OCCURRENCE REPORT: DURING TAKEOFF ROLL, WE DIDN'T GET A/F ARMED, ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPORT: MAINTENANCE LOG ENTRY FOR RECTIFICATION OF DEFECT AS FOLLOWS: REF LOG SEQUENCE NO L072 PROPELLERS; A/F NOT ARMED SDR 20001109SH026Nut · looseTHE REAR PROPELLER WAS SUBMITTED FOR REPAIR OF A LOOSE BLADE FOUND DURING AN ANNUAL INSPECTION. UPON DISASSEMBLY, FOUND THE RED DYE OIL REQUIRED BY AD 91-15-04 HAD BEEN REMOVED AND THE PROPELLER WAS HAND PACKED WITH GREASE. THE LOOSE BLADE CONTAINED A CRACKESDR CA001018011Bearing · failed(CAN) PROPELLER PARTS CORRODED BEYOND REPAIR. BLADE BEARING RACES AND BALLS. BLADE SPLIT RETAINING RINGS. PISTON AND PISTON PINS. CYLINDER ACTUATING PINS. NOTE: THESE PARTS CORRODED AFTER 6 YEARS, NOW REGULATION IS 10 YEARS. (X)SDR 20001013SH021Drive Gear · failedREVELANT MAG PARTICLE INDICATION IN TEETH AREA. (X)SDR CA000928002Propeller · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.SDR CA000907014Propeller · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. (X)SDR 20000814SH016Propeller · leakingPILOT/OWNER REPORTED OIL ON PROPELLER BLADES, WINDSHIELD. INSPECTION OF PROPELLER HUB FOUND RED DYE LEAKING FROM HUB SERVICE PLUG. SUBMITTER STATED THIS IS THE SECOND 182S MCCAULEY PROPELLER WITH A LEAK FROM PLUG. ALSO, A CESSNA 206H MCCAULEY PROPELLER WAS SDR EY2R57093Pin · corrodedACTUATING PIN CORRODED ON SURFACE OF PIN. REPLACED. (X)SDR EY2R57053Hub · corrodedHUB CORRODED INSIDE EXTENSION AT THE PARTING SURFACE.SDR EY2R57052APin · corrodedACTUATING PIN CORRODED ON SURFACE. (QTY. 2) REPLACED.SDR EY2R57052Nut · corrodedCORROSION IN THREADS OF BLADE NUT. REPLACED PART.SDR EY2R5703Bumper Block · crackedFORK BUMPER CRACKED AT THE START OF THE THREADS. REPLACED.SDR EY2R56492CCylinder · corrodedCYLINDER CORRODED ON INNER SURFACE BEYOND LIMITS.SDR EY2R56492BFerrule · corrodedFERRULE CORRODED IN THREADED AREA.SDR 20001103AP007Block · wornFLT 9410 - MIA/EYW - AFTER ROTATION, RIGHT PROP RPM DROPPED TO APPROXIMATELY 1200 RPM. RETURNED TO MIA. DETERMINED RIGHT BETA BLOCK TO BE WORN. REPLACED RIGHT BETA BLOCK AND RIGGED. (M)SDR EY2R56607Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. 8 EACH CRACKS.SDR EY2R56608Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. 1 EACH CRACK.SDR MALA000118Sensor · malfunctionedDTW - FLT 2907 - WHILE EN ROUTE AT 11,000 FT LEFT ENGINE PROPELLER GEAR BOX OIL TEMP FLUCTUATED OUT OF GREEN ARC INTO YELLOW ARC ALMOST TOUCHING RED LINE. GAUGE FLUCTUATED BETWEEN LOW GREEN ARC AND RED LINE. MAINTENANCE REPLACED LEFT PGB OIL TEMP BULB, IAW GSDR 20000828SH036Belt · failedDURING TAKEOFF, BOTH PROPELLER DRIVE BELTS BROKE CAUSING LOSS OF THRUST. ACFT DESCENDED RAPIDLY AND IMPACTED THE TERRAIN. BELTS HAD CONSUMED 220 HOURS OF THE 300 HOUR REPLACEMENT TIME. FAILURE NOT SPECIFICALLY DETERMINED, BUT COULD INCLUDE CAUSAL FACTORS OFSDR 20000712SH027Propeller · malfunctionedPROPELLER IS UNCONTROLLABLE, TO LOWER PITCH, AT HIGH ALTITUDE (COLD TEMPERATURE). NEW PROPELLER FROM MANUFACTURER. INSTALLED SERVICEABLE PROPELLER. ALL SYSTEMS WORK NORMALLY. INSTALLED ANOTHER NEW PROPELLER, ALL SYSTEMS WORK NORMALLY. POSSIBLE WRONG GREASSDR PLGA990528O-Ring · failedLGA - FLT 6582 - AFTER TAKEOFF FROM LGA, LEFT PROP OIL PRESSURE STARTED TO DROP. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED 6 O-RINGS ON THE TRANSFER TUBES TO THE PROP PCU, PERFORMED THE REQUIRED LEAK CHECKS, AND RETURNED THE SDR LR7A9823Cap · looseNR 2 ENGINE SHUTDOWN IN CLIMB AT 1750 Z DUE TO PROP OIL LOW LIGHT ON. RESECURED PRESSURIZED CAP ON NR 2 PROP. RESERVICED IAW HAM STD MM PARA 7-10, 7-11 PF 706 AND 707, OPS CHECK NORMAL.SDR AU970952Propeller · fod(AUS) PILOTS VISOR FLEW OFF AND STRUCK PROPELLER CAUSING A SMALL SECTION OF THE LEADING EDGE TO SEPARATE - THIS DEFECT WAS RECEIVED FROM THE AUF AND IS FOR INFORMATION ONLYSDR 97ZZZX1010Blade · splitWHILE IN STABLE FLIGHT AT 7,500 FEET MSL IN SMOOTH AIR, PART OF THE WOODEN PROPELLER CAME APART. THE SEPARATION OCCURRED LENGTHWISE DOWN ONE BLADE OF THE TWO-BLADED PROPELLER. THERE WERE NO SIGNS OF BIRDS PRIOR TO THE SEPARATION NOR WERE THERE ANY SIGNS OF ASDR 97031300148Blade · separationWHILE IN STABLE FLIGHT AT 7,500 FEET MSL IN SMOOTH AIR, PART OF THE WOODEN PROPELLER CAME APART. THE SEPARATION OCCURRED LENGTHWISE DOWN ONE BLADE OF THE TWO-BLADED PROPELLER. THERE WERE NO SIGNS OF BIRDS PRIOR TO THE SEPARATION NOR WERE THERE ANY SIGNS OF ASDR COMA9610409Pitchlock Screw · failedPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FROM AIRCRAFT FOR ENGINE RELATED MAINTENANCE. ONCE REMOVED, IT WAS DISCOVERED THAT THE ACTUATOR FEATHER STOP TAB HAD BEEN DISPLACED APPROXIMATELY .25 INCH. PITCH LOCK SCREW WAS REMOVED FROM SERVICE AND RETURNED TO MASDR CA960612022Guide Pins · dry & dirty(CAN)ON TAKEOFF, RIGHT HAND PROPELLER DID NOT REACH TAKEOFF RPM. TAKEOFF ABORTED. BETA RING GUIDE PINS FOUND DIRTY AND DRY, CLEANED AND LUBRICATED.SDR 96ZZZX687Safety Wire · errorPERTAINS TO AD 95-21-01 WHICH REFERS TO MCCAULEY SB 219 WHICH HAS A STEP-BY-STEP INSTRUCTION ON PERFORMING THIS AD TO THE PROPELLER. STEP 2F STATES THAT MOUNTING BOLTS ARE TO BE SAFETIED WITH .032 INCH SAFETY WIRE. AC 43:13 STATES THAT .041 INCH STAINLESS STSDR 95ZZZX3980Bolt · failedDURING POWER CHANGE IN PATTERN, PROPELLER DEPARTED AIRCRAFT. EXAMINATION OF ALL SIX .25 INCH BOLTS REVEALED THEY HAD FAILED AT A POINT FLUSH WITH CRANKSHAFT FLANGE. ALL APPEARED TO HAVE BEEN OVERTORQUED AT INSTALLATION ONLY 11 HOURS PRIOR. SUGGEST OPERATOR SDR 95ZZZX3981Propeller · departedUNCERTIFICATED AMATEUR BUILT AIRCRAFT DEPARTED AIRPORT ON FIRST FLIGHT SINCE COMPLETION. PROP HUB ATTACH BOLT UNSCREWED AND PROP DEPARTED AIRCRAFT. THE VW CONVERSION WAS PERFORMED BY HAPI. THE PROP HUB BOLT RETAINING COTTER PIN WAS FOUND SHEARED. THE OWNERSDR 95ZZZX1432Bolt · failedAIRCRAFT IN CRUISE AT 6000 M.S.L. WHEN THE PROPELLER SEPARATED FROM THE ENGINE. THE AIRCRAFT LANDED IN A FIELD AND HAD SUBSTANTIAL DAMAGE. THE PILOT WAS NOT INJURED. SUSPECT IMPROPER BOLTS USED WHEN PROPELLER WAS ATTACHED. THE BOLTS AND/OR PROPELLER WERE N
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