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 QXEA2016051100316Propeller · malfunctionedON PREFLIGHT INSPECTION FOUND THE NR 1 PROPELLER NOT FULLY FEATHERED. C/W PROPELLER FEATHER CHECK IAW AMM TASK 71-00-00-868-819. NR 1 PROPELLER CHECKS GOOD. NO DEFECTS FOUND. RETURNED TO SERVICE.SDR ME4R2016050300205Arm · crackedLINK ARM CRACKED. FOUND DURING ROUTINE O/H USING MAG PARTICLE INSPECTION.SDR ME4R2016FA0000204Block · crackedCRACK WAS FOUNDON THE PITCH CHANGE BLOCK, FOUND DURING ROUTINE O/H USING MAG PARTICLE INSPECTION.SDR ME4R2016FA0000203Collar · crackedGUIDE COLLAR HAS A CRACK ON THE TOPSIDE OF THE NR 1 BUSHING HOLE. THE CRACK WAS FOUND DURING A ROUTINE O/H USING THE FLUORESCENT PENETRANT INSPECTION. NO RECOMMENDATIONS ON HOW TO PREVENT.SDR CA160126010Propeller · malfunctioned(CAN) ON TAXI OUT TO RUNWAY IN PREPARATION FOR TAKEOFF, CREW NOTED NR 1 ENGINE PROPELLER ENCOUNTERED AN OVERSPEED CONDITION. THE CREW CONFIRMED THE OVERSPEED WAS UN-COMMANDED IN NATURE AND SUBSEQUENTLY PERFORMED AN ENGINE SHUTDOWN. THE ACFT RETURNED TO GATE SDR QXEA2016011100019Unknown · unknownNR 2 ENGINE DID NOT COME OUT OF FEATHER AFTER ENGINE START. INTEROGATED CDS, NO FAULTS FOUND, AS PERCAUTIONARY R & R NR 2 ENGINE OVERSPEED GOVERNOR IAW AMM 61-20-26-000-801, 61-20-26-400-801, KR 44607 1-10-2016. PERFORMED OPS TEST OF THE PROPELLER OVERSPEED SDR HNAA2015111900341Propeller · vibrationSHORTLY AFTER ROTATION, EXPERIENCED STRONG VIBRATION, NR 2 PROP ASSY. RETURNED IMMEDIATELY TO THE FIELD. ON ROLLOUT, GOT NR 2 DC GEN CAUTION LIGHT. ON TAXI WAY SHUTDOWN NR 2 ENGINE. ALL ENGINE AND PROP PARAMETERS GOOD.
SDR QXEA2015111700614Propeller · vibrationENROUTE, ONCE CLEAR OF ICING CONDITIONS WE PICKED UP CONSTANT STRONG VIBRATION FROM BOTH ENGINES. AIRFRAME MODE SELECT SWITCH WAS SET TO FAST WITH ENGINE INTAKE BYPASS DOORS OPEN. ALL INDICATIONS ON ED WERE NORMAL. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDISDR QXEA2015092300507Propeller · unknownDURING TAKEOFF, NR 2 PROPELLER DID NOT REACH 1020 TILL 100 KTS. NR 2 PROP INDICATED 1010 TILL 100 KTS. NR 2 PROP WAS A LITTLE SLOW TO COME OUT OF FEATHER AT START. PERFORMED ENGINE TREND DOWNLOAD FROM EMU MTC 6773101, PERFORMED OPS TEST OF THE PROPELLER OVESDR CA150818001Brake · burned(CAN) DURING FLIGHT, THE ALARM, PROPELLER BRAKE UNLOCK, FLASHED ONE TIME, AFTER LANDING DURING TAXIING A THICK WHITE SMOKE FROM THE FRONT OF RT ENGINE WAS OBSERVED, PROPELLER BREAKS WERE NOT ENGAGED. AFTER ENGINE SHUTDOWN CUSTOMER WITNESSED A LOT OF HYD FLUIDSDR QXEA2015072300394Propeller · unknownNR 1 PROP SLOW TO COME OUT OF FEATHER WHEN CONDITION LEVER SET TO MAX. C/W FIM TASK 61-20-00-810-801, STEPS 1-5A, 10 AND, 6. NO FAULTS NOTED IN CDS FOR EMU. NO EXTERNAL PROPELLER LEAKS NOTED. PROP UNFEATHER NORMALLY WITH FEATHER PUMP. R & R NR 1 OVERSPEED GSDR QXEA2015071300388Electronic Unit · malfunctionedNR 1 PEC CAUTION WITH POWERPLANT MESSAGE, PROP RPM 1060. SHUTDOWN ENGINE IAW EMERGENCY CHECKLIST 7.14 EMEGRENCY CHECKLIST. LANDED UNEVENTFUL. EMU INTEROGATED FOR FAULT CODES. FIM TASK ACCOMPLISHED FOR DISCOVERED FAULTS. PEC GROUND RUNS COMPLIED WITH IAW MSDR CA150429008Controller · malfunctioned(CAN) DURING CRUISE POWERPLANT MESSAGE CAME ON. CREW ELECTED TO DIVERT. NR 1 PEC REPLACED. OK ON GROUND RUN.SDR QXEA2014121601100Propeller · malfunctionedTAKEOFF ABORTED DUE TO NR 2 PROPELLER ONLY REACHING 1010 RPM. ALL OTHER ENGINE INDICATIONS NORMAL. SPEED 97 KNOTS. CHECKED CDS FOR FAULT CODES, NOT FOUND. C/W POWER ASSURANCE ENGINE RUN FOR NR 2 ENGINE AND APPLICABLE ENGINE RUNS. COULD NOT DUPLICATE DISDR SWIA2014120140227Control Unit · malfunctionedRETURNED TO DEPARTURE AFTER A RIGHT PROP OVERSPEED. PERFORMED FIM PROCEDURE HIGH NP IAW AMM. CND FAULT. FOUND NP OVERSPEED TO BE WITHIN LIMITS IAW AMM. CHANGED RT PCU.SDR 2014FA0000626Bearing · failed10-1-14, 15:43 LOCAL TIME, ACFT WAS ON A PRACTICE ILS APPROACH, RECEIVING VECTORS FROM SOCAL ON 125.5 HEADING OF 030 AT APPROX 3500`, WHEN PILOT ENCOUTERED UNCOMMANDED HIGH RPM. PILOT IMMEDIATELY REDUCED THROTTLE, RPMS SETTLED AT APPROX 1500 RPMS. PILOT FOUNSDR CA141006014Propeller · overspeed(CAN) DURING CLIMB, THE PROPELLER HAD AN OVERSPEED AND THE PILOT SHUTDOWN THE ENGINE. ELECTED TO RETURN TO ORIGIN WHERE AN UNEVENTFULLY LANDING WAS PERFORMED. ALSO DURING CLIMB, THE PILOT SHUTDOWN THE ENGINE AFTER TORQUE FLUCTUATION OCCURRED. AT THIS TIME TSDR QXEA2014090400741Propeller · malfunctionedNR 2 PROPELLER FAILS TO UNFEATHER WHILE IN MAINTENANCE MODE. REPLACED FEATHERING PUMP, STILL FAILS CHECKS. PLACED ON MEL 61-20-1. RETURNED TO SERVICE.SDR QXEA2014072100605Unknown · unknownDURING DAILY SYS CHECK, AUTOFEATHER CHECK IS ABORTING TEST ON LT SIDE, SEVERAL ATTEMPTS. NO FAULTS IN CDS. OP'S CHECK OF THE PROPELLER AUTOFEATHER SYS IAW AMM TASK 61-20-00-710-801. OP'S CHECKED GOOD. COULD NOT DUPLICATE. RETURNED TO SERVICE.SDR CA140721010Propeller · malfunctioned(CAN) IT WAS REPORTED THAT THE ACFT EXPERIENCED AN UNCOMMANDED AUTOFEATHER DURING CLIMB. MORE DETAILS WERE REQUESTED TO THE CUSTOMER.SDR HNAA2013123000643Relay · failedON TAKE OFF ROLL, AUTO FX DID NOT ARM. RTO SYS TESTS OK AFTERWARDS. R & R RELAY 6121-K5. GROUND-RAN AIRCRAFT IAW -8 RUNUP MANUAL. OK FOR SERVICE.SDR PNSA2013121904Unknown · vibrationUNIDENTIFIED VIBRATION VISUALLY INSPECTED EXTERIOR, INSPECT MOTOR MOUNTS AND BALANCED RT PROP. FLIGHT CHECK OK.SDR CA131215002Propeller · failed(CAN) DURING CLIMBOUT, THE PROPELLER FEATHERED WITHOUT THE PILOT INPUT. THE PILOT THEN NOTICED THAT OIL PRESSURE HAD REDUCED INTO THE RED AND THE LOP WARNING ILLUMINATED. THE ON GROUND INSPECTION REVEALED THAT THE PROP WAS STIFF TO TURN.SDR CA131202010Signal Cond Unit · malfunctioned(CAN) SHORTLY AFTER TAKEOFF, NR 2 ENGINE FEATHERED. FLIGHT CREW SHUTDOWN THE ENGINE AND DECLARED AN EMERGENCY. THE ACFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. FLIGHT CREW REPORTED 155 PERCENT TORQUE ON THE NR 2 ENGINE. FLIGHT DATA RECORDER WAS DOWNLOSDR CA131111016Propeller · malfunctioned(CAN) DURING TAKEOFF ROTATION, THE NR 1 PROPELLER FEATHERED. THE TORQUE RAPIDLY INCREASED ABOVE NORMAL OPERATING LIMIT AND FLIGHT CREW SHUTDOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED, LANDED WITHOUT FURTHER INCIDENT. SOLID STATE FLIGHT DASDR CA130921008Propeller · out of rig(CAN) THE ACFT EXPERIENCED ENGINE NR 2 VIBRATION DURING THE DESCENT, THAT EVENTUALLY BECAME HEAVY WITH OIL ODOR AND SOME SMOKE IN THE CABIN. SEVERAL ALARMS THEN WENT OFF AND ACFT ENTERED A DIVE REACHING OVERSPEED. THE PILOT TOOK MANUAL CONTROL, IN VFR, DECLASDR HNAA2013073000435Propeller · vibrationAFTER TAKEOFF, ENGINE VIBRATION FELT AND CONTINUED TO WORSEN UNTIL RUNUP, NR 1 ENGINE VIBRATION INCREASES WHEN OUT OF FEATHER. COMPLIED WITH INSPECTION IAW AMM 05-50-65 AND REPLACED NR 1 PROP ASSY IAW CARDS 61-10-06 AND 61-10-07 FOR BLADE R & R. RUN AND LEAKSDR HNAA2013070500390Propeller · malfunctionedUNABLE TO GET NR 1 PROP RPM BELOW 927. ADJUSTED NR 1 PCU SPEED TRIM SCREW IAW MM 61-22-00. PROP SPEED AT 911 RPM. OK FOR SERVICE.SDR CA130704002Propeller · slow(CAN) ERI REPORT PT6A 2013-048 R1, POWER SECTION MODULE WAS SENT FOR INVESTIGATION AFTER THE CUSTOMER REPORTED THAT THE PROPELLER SPEED WOULD NOT HOLD AT THE MAXIMUM SPEED. PROPELLER SPEED WOULD SLOWLY RECEDE FROM THE MAXIMUM.SDR CA130530002Control Lever · malfunctioned(CAN) DURING T/O AND INITIAL CLIMB, THE PROPELLER WAS NOT MAINTAINING STEADY RPM. THE PROP. LEVER WAS SET TO FEATHER BUT THE PROPELLER DID NOT FEATHER UNTIL LATER ON FINAL APPROACH, DURING THE RETURN TO THE AIRPORT. AN UNEVENTFUL LANDING FOLLOWED. TROUBLESHOOTSDR CA130603001Bearing · damaged(CAN) PILOT REPORTED VIBRATIONS ON DESCENT AND REDUCED POWER TO COMPLETE LANDING. ON INSPECTION MAINTENANCE CREW FOUND PROPELLER BLADE RETAINING BEARINGS AND RACE TO BE DAMAGED.SDR VGCA20130401001Propeller · malfunctionedNR 2 PROPELLER AUTOFEATHER AFTER TAKEOFF.SDR HNAA2012082900934Warning Horn · activatedBETA WARNING HORN SOUNDED INTERMITTENTLY AFTER LANDING, DURING TAXI. BETA WARNING HORN SYS WITH MOD VERIFIED OPS CHECK OF BETA LOCKOUT SYS IAW CREW ORIGINATING CHECKLIST. PULLED AND COLLARED CIRCUIT BREAKER C8.SDR 2014FA0000522Filler · crackedREPLACED SPINNER AND ADAPTER PLATE WITH PN 103585F2 WHEN PROPELLER HAD 29.96 TSMOH AND SINCE NEW THAT WAS INSTALLED IAW THE MM. DURING A RECENT ANNUAL INSPECTION, REMOVED THE SPINNER FOR INSPECTION AND LUBRICATION OF THE PROPELLER. FOUND CRACK EMANATING FROMSDR CA130115008Bearing · spalled(CAN) DURING APPROACH THE PROPELLER SPEED DROPPED BELOW LIMITS. ENGINE WAS SHUTDOWN AND ACFT LANDED SAFELY. MAINTENANCE REPLACED THE PROPELLER VALVE HOUSING AND THE ACFT WAS RETURNED TO SERVICE. THE O/H FACILITY REPORTED SUBSTANDARD BEARINGS SUSPECTED.SDR CA120307003Plate · damaged(CAN) THE STEEL PROP SECURING PLATE IS BENDING, THE BOLT HOLES ARE BEING DAMAGED BY THE BOLT. EVERY 100 HR INSP THE PROP BOLTS NEED TO BE TORQUED BECAUSE THEY ARE LOOSE. THIS PART HAS BEEN SENT FOR SUPPORT FOR ANALYSIS. THE OWNERS HAVE BEEN RE-TORQUEING THE SDR CA111123014Control Cable · damaged(CAN) UPON RIGGING PROP CONTROLS AFTER CABLE REPLACEMENT ON RT ENGINE, FOUND SUSPICIOUS LT PROP CONTROL ATTACHMENT. JOINT ASSEMBLY PN 469-153 WAS RUSTED, BUT MOST UNUSUAL WAS THAT A FIBRE LOCK NUT WAS USED AS SECURING DEVICE AND THAT THREADS WERE WELL BELOW FSDR CA110916002Gear · damaged(CAN) LEFT ENGINE SPOOLED DOWN AT TAKEOFF POWER.SDR CA110414001Shaft · cracked(CAN) OPERATOR DISCOVERED THAT THE PROPSHAFT WAS CRACKED. THE OPERATOR WAS INVESTIGATING REPEATED OIL LEAKAGE AROUND THE PROP AREA WHEN THE CRACK WAS DISCOVERED. THE CRACKING OF THE PROPSHAFT WAS A RESULT OF HYDROGEN EMBRITTLEMENT.SDR GUUA94276040411APropeller · malfunctionedPILOT REPORTED WHEN PULLING PROPS BACK FROM 1550 RPM ON THE DESCENT TO 1400 RT PROP LAGGED ABOUT A KNOB AND HALF FROM LT SIDE PROPS WERE OUT OF SYNC AND COULD NOT GET INTO SYNC. WHEN PROPS PUSHED FULL FWD LT PROP REACHED ABOUT 1700 RPM WHILE RT PROP INCREASEDSDR GUUA94161022511AAnnunciator · no indicationPILOT REPORTED WITH N1 AT 95 PERCENT "AFX DISABLE" ANNUNCIATOR WAS ILLUMINATED AND LT AFX WAS NOT ILLUMINATED. RERACKED ANNUNCIATOR FAULT DETECTION PCB AUTOFEATHER TEST OPS CHECK GOOD.SDR 2011FA0000002Unknown · unknownUNCOMMANDED AUTOFEATHER ON APPROACH.SDR QXEA2010122000923Unknown · unknownON PREFLIGHT NR 2 AND NR 1 PROP NOT FEATHERED. GROUND RAN ACFT, CYCLED PROPS SEVERAL TIMES, NO DEFECTS NOTED, ACFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.SDR 2010F00212Unknown · unknownUNCOMANDED AUTOFEATHER ON APPROACH.SDR V0DR967YBJam-Nut · defective(V0DR) DURING ASSY OF A PROPELLER ASSY, THE JAM-NUTS (PN B-3368) WERE INSTALLED AND THE BETA RING RUN-OUT TOLERANCE COULD NOT BE MAINTAINED. FURTHER TROUBLESHOOTING IDENTIFIED THE JAM-NUTS (PN B-3368) WERE MFG WITH THE THREADS NOT TRUE. CAUSING THE RUN-OUT TSDR V0DR967Y001Jam-Nut · defectiveDURING ASSY OF A PROPELLER, THE JAM-NUTS, PN B-3368 WERE INSTALLED AND THE BETA RING RUN-OUT TOLERANCE COULD NOT BE MAINTAINED. FURTHER TROUBLESHOOTING IDENTIFIED THAT THE NUT PN B-3368 WAS MFG WITH THE THREADS NOT TRUE. CAUSING THE RUN-OUT TO BECOME EXCESSISDR HNAA201004200079Unknown · malfunctionedNR 1 PROP WILL NOT GO ABOVE 1188 ON TAKEOFF ROLL AT 90 PERCENT TORQUE. ABORTED TAKEOFF. DURING TAXI WHEN MOVING POWER LEVERS FROM DISC TO FLIGHT IDLE, PROP INCREASED FROM 785 TO 802. INSPECTED ECP, NO EEC FLAGS NOTED. CYCLED NR 1 ENGINE ECU CIRCUIT BREAKERSDR HNAA2010012200009Beta Switch · failedNR 2 ENG TORQUE SURGED APPROX 30 PERCENT RANGE JUST AFTER TAKEOFF. AFTER TAKEOFF NR 2 ENGINE TORQUE SURGED TO APPROX 119 PERCENT AND PROP SURGED TO APPROX 1000 RPM. ACFT AT 100 AGL AND CLEARED UP AFTER LANDING. REACTIVATED BETA LOCKOUT SYS. R & R NR 2 ENG SDR LR7A2009101900143Housing · unknownDURING DECENT CREW REPORTED NR 4 ENG RPM OUT OF LIMITS. PERFORMED ENG SHUTDOWN IAW QRH. NR 4 VALVE HSG REPLACED IAW JOB CARD HN61135, OPS CHECK GOOD. LOG PAGE 34387 ITEM M1.SDR 2009FA0000873Nut · crackedWHEN REMOVING PROPELLER FOR RESEAL, FOUND 2 MOUNTING NUTS CRACKED. THE PROP HAS 93.5 HRS SINCE INSTALLATION. THE PROPELLER PREVIOUSLY HAD THE BLADES REPLACED DUE TO PROP STRIKE.
Back to JASC 6100