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 = '3600' 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 = '3600' 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 2021FA0000380Pressure Switch · inoperativePILOT REPORTS HP BLEED ARI LEAK INDICATION APPEARED. COMPLIED WITH R&R OF HP BLEED AIR PRESSURE SWITCH. OPS CHECKED GOOD. AIRCRAFT OK FOR RTS.SDR FDEA202012173172Switch · failedDURNING CRUISE AFTER TURNING OFF WING ICE THE RED MANF LIGHT ILLUMINATED ON #3 WITH ASSOCIATED "MAN 3 FAIL" LEVEL 1 ALERT. FOUND PRESSURE SWITCH FAULT BALL DROPPED IN WINDOW ON PNEUMATIC MANIFOLD FAULT INDICATOR. RESET FAULT BALL. SUPPLIED PNEUMATIC AIR USINSDR M3XA2020011801Filter · overservicedPILOT MADE A PL BACK TO HOSPITAL PAD WITH A PATIENT ON BOARD AND REPORTED AFTER 2 MINUTES INTO THE FLIGHT WITH CABIN HEAT APPLIED, CABIN BAGAN TO FILL WITH SMOKE ON THE CEILING. MECHANIC TROUBLESHOT AND FOUND EXCESS INLET BARRIER FILTER FLUID IN THE ENGINE ISDR J7SA2019123127001Computer · malfunctionedMULTIPLE CAS MESSAGES FL450: TRIM AIR LOOP FAIL, R BLEED LOOP FAIL , BLEED LOOP FAULT , TRIM AIR LEAK AND R BLEED LEAK, REMOVED NR 2 IASC AND INSTALLED REPAIRED UNIT. OPS CHECK GOOD AT THIS TIME. ALL WORK PERFORMED IAW AMM 21-31-01. EMERGENCY DECLAREDSDR MASA2019111912144Warning Message · illuminatedLH BLEED DUCT WARNING WITH RT ON MEL.SDR 2018FA0000499Dpu · abnormalRH EHSI FAILED ABOVE 10000 FEET, RETURNED TO KMIA. CORRECTIVE ACTION: R/R RH DPU IAW SAAB AMM OPS CHECKED GOODSDR UIEA2018112102672Duct · unknownBEFOREE ENG START DUCT PRESSURE WAS 15 PSI. AS #2 ENG WAS STARTING DUCT PRESSURE CLIMBED TO 30 PSI(<P><SPAN>RAN / BOTH ENG'S TO OPS CHECK DUCT PRESSURE. OPS CHECK GOOD AT THIS TIME IAW AMM / 36-21-00 & 72-10-00</SPAN></P>)SDR UIEA2018011600076Sensor · faultedDUCT PRESSURE SENSOR M1843 FAULTY. REMOVED AND REPLACED THE DUCT PRESSURE SENSOR IAW AMM 36-21-08. OPS CHECKED NORMAL.SDR DJFA20171113001Warning Message · false activationDUCT NR 2 OVERTEMP CAS MESSAGE DURING CLIMB OUT. DECLARED EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. RESET THE CIRCUIT BREAKER AND COMPLIED WITH AN ELECTRICAL CHECK. NO FAULTS FOUND..SDR E07A2017072101Ahrs · failedDUAL AHRS FAILURESDR ASOA201701103001Clamp · wornTHE CREW REPORTED BLEED NR 1 LEAK WARNING IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE CLAMP ON LEFT PRECOOLER FORWARD DUCT. OPERATIONAL CHECKS WERE GOOD.SDR UIEA2016113000946Hose · damagedNR 2 PYLON ANTI-ICE HOSE AND UNION DAMAGED. HOSE ASSY REPLACED IAW AMM 30-11-02/401.SDR VNAA2016091300010Sensor · faultyRIGHT ENGINE 14TH STAGE BLEED WARNING MESSAGE. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE RIGHT HAND PYLON SENSING ELEMENT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRASDR I5EA201606273601Unknown · multiple failBOTH ENGINE BLEED AIR GAUGES READ 0 AND ACFT WOULD NOT PRESSURIZE, F/O INSTRUMENTS ALL FLAGGED, AND CAPTAINS, COMPUTER, FLAG INTERMITTENT. R & R THE CABIN PRESSURE CONTROLLER PANEL IAW AMM 21-31-25. OPS CHECK IAW 21-31-00. CAPTAIN ADI COMPUTER FLAG, NAV COMPUSDR LOMA2015FA0000280Warning Light · illuminatedRIGHT FUSELAGE BLEED WARNING CAME ON.SDR SWIA201438703Loop · failedLEFT BLEED DUCT WARNING ILLUMINATED AT APPROXIMATELY FL 270. WITHIN A MINUTE WARNING CHANGED TO LEFT PACK FAIL. CABIN CLIMBED TO FL 180, PAX OXYGEN MASKS AUTOMATICALLY DEPLOYED. DECLARED EMERGENCY AND RETURNED TO FIELD. REPLACED MT 139 LOOP A & B AND SUPPORSDR FDEA201401120085Valve · failedAFTER TAKEOFF AT APPROXIMATELY 2000 FT, RECEIVED ECAM WARNING, NR 1 ENG RUN, BLEED, TEMPERTURE KEPT RISING UNTIL NR 1 PACK TRIPPED, RECEIVED A AVIONICS SMOKE & MIN EQUIPMENT WARNINGS, ALONG WITH ASSOCIATED AURAL WARNINGS. REPEATED SEVERAL TIMES. NR 1 PNUEMATSDR UALA2013050603160Valve · failedCIRCUIT BREAKER POPPED 2 HOURS AFTER TAKEOFF, FL390. LEFT ENGINE AMBER MAX RADL HIGHER THAN RIGHT ENGINE. FOUND HIGH STAGE VALVE STICKING AND HIGH STAGE PILOT SOLENOID LOOSE. REMOVED AND REPLACED HIGH STAGE VALVE 36-11-07 AND HIGH STAGE PILOT REF MM 36-11-SDR CALA2013050300262Controller · inoperativeAFTER T/O "ENG BLEED LT OFF EICAS" LT BLEED VALVE FUEL DUMP AND RETURNED TO EWR. REFER TO L/P 7351111 PARTS CHANGE AND OPS TEST.SDR UIEA2013041400217Warning Message · false activationRIGHT PRV FAULT, PERFORMED AIR SUPPLY CONTROL SYSTEM TEST WITH NO FAULTS NOTED.SDR UIEA2013041400216Warning Light · false activationLEFT PRSOV BITE SWITCH WIRE FAULT. PERFORMED AIR SUPPLY CONTROL SYSTEM TEST WITH NO FAULTS NOTED.SDR UIEA2013031200126Warning Message · illuminatedLEFT ENGINE HPSOV EICAS MESSAGE.SDR ASOA20120629121TBleed Air Sys · multiple failACFT DIVERTED WITH A BLEED LEAK ISSUE. MX RETORQUED NR 2 ENGINE BLEED VALVE AND THE Y DUCT. RETORQUED SEVERAL NR 2 SYSTEMS PACT DUCTS. OPS AND LEAK CHECKED GOOD IAW CHRONIC WORKSHEET,CONTROL NR 594620. BLEED LEAK TASK CARD 6836001 ON NR 2 SIDE ONLY. ACFT WASDR HALA2012060500159Warning Light · false activationRT ENG BLEED OFF EICAS AND LIGHT APPEARED TWICE DURING FLIGHT. FIRST DURING CLIMB FOR 30 SECONDS, SECOND DURING CRUISE DESCENT FOR 10-15 SECONDS. RAN NR NR 2 ENGINE IAW AMM 71-00-00. NO FAULTS OR ABNORMALITIES NOTED. OPS CHECKED GOOD. NO FAULTS NOTED ON AISDR ASOA201200981Controller · inoperativeLEFT BLEED WARNING, ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED. R & R AILC IAW AMM 30-12-12, OPS CHECKED GOOD.SDR 2011FA0000724Bleed Air Sys · contaminatedSEVERAL DAYS AFTER A ENGINE COMPRESSOR WASH WAS COMPLETED, IN WHICH THE MM PROCEDURES WERE FOLLOWED FOR ENGINE RUNS AFTER A COMPRESSOR WASH THE ACFT DEPARTED AND AFTER SWITCHING FROM APU BLEED AIR TO ENGINE BLEED AIR THE CABIN FILLED WITH SMOKE FROM RESIDUAL CSDR IPXA0660636Pneumatic System · inoperativeINSPECTION TYPE:ETOP, APU PNEUMATIC INOP; REF 427849 AND WAN NR 1631215. T/S IAW FIM 49-11-00 AND ECU TEST PASS IAW AMM 49-11-00-5, ITEM CLOSED. BOW COMPLETED.SDR HALA2010061000251Guard · damagedETOPS SIGNIFICANT SYS- DUCT LEAK INDICATION ON BOTH SIDES ON O/H PNEUMATIC CONT PANEL & L&R STRUT DUCT LEAK ON EICAS. ACCOMPLISHED WIRING CHECK IAW WDM 26-18-12 FOUND STRUT TEST SWITCH GUARD SPRING WAS HITTING SWITCH ON TEST POSITION. REPOSITIONED SWITCH GUARSDR UALA2010032200952Valve · malfunctionedRIGHT ENG BLEED OFF AND RT PACK OFF LIGHTS CAME ON DURING T/O ROLL AND STAYED ON THRU CLIMB AND L-O, THEN BLEED SHUTS OFF. DID BITE CHECK ON AIR SUPPLY BITE MODULE. HITS PRV AND WIRING. SWAPPED LT AND RT AIR SUPPLY CONTROL CARDS-NO HELP, RETURNED CARDS TO OSDR C2XA10RI027AHose · leakingFLIGHT 2217 - CVG - FLIGHT CREW REPORTED BLEED 1/2 OVERTEMP ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED SENSE LINE AND NR 2 FAN AIR THERMOSTAT.SDR C2XA10IA014Unknown · unknownFLIGHT 2055, THE CREW REPORTED A BLEED TWO LEAK. THE AIRCRAFT RETURNED WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE AIRCRAFT AND PERFORMED HIGH POWER RUNS WITH NO LEAKS OR DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR YYFA20090002Sensor · dirtyDURING CLIMB , TAIL COMPARTMENT HIGH LIGHT ILLUMINATED.SDR DL76L091026Unknown · unknownON TAXI OUT NR 1 ENGINE COULD NOT GENERATE ENOUGH PRESSURE TO START NR 2 ENGINE - 20 PSI AT 82 PERCENT N2. NO PSI FOR NR 2 ENGINE. SUSPECT DUCT LEAK. CHECKED ENG. NR 1 DUCTS FOR LEAK AND LT PACK. PERFORMED ENG. NO RUN BY CREW AND CROSSBLEED START NR 2 DUCT SDR DL76G091001Isolation Valve · inoperativeACFT RTB DUE TO RIGHT ISOLATION VALVE INOP. REMOVED AND REPLACED RT ISOLATION VALVE PER M/M.SDR GLBA20090524092Sensor · dirtyPILOTS REPORTED A STALL HEAT CAUTION ANNUNCIATOR WOULD NOT TURN OFF WITH THE SWITCH IN THE ON POSITION. MAINTENANCE CLEANED CONNECTIONS ON A1 & A2 STALL WARNING CURRENT SENSORS. FUNCTIONAL CHECKS WERE GOOD.SDR UALA2009051101341Line · leakingDURING CLIMB RIGHT PACK INOP PACK OFF AND ENGINE BLEED OFF LIGHTS ILLUMINATED SIMULTANEOUSLY. PERFORM BITE CHECK ON CONTROLLER. NO FAULTS NOTED.REPAIRED TWO LEAKS IN PNEUMATIC LINES. RPL OVERHEAT SWITCH PRECAUTIONARY. RAN PACKS ON APU AND NR 2 ENG BLEED, NO FSDR CHQA200900008Unknown · unknownAFTER TAKEOFF THE CREW RECEIVED A PACK 1 OVERHEAT EICAS MESSAGE AND WOULD NOT RESET. SHORTLY AFTER THE ACFT ENTERED ICING CONDITIONS AND BLD 1 AND 2 LOW TEMP MESSAGES APPEARED FOLLOWED BY BLEED 1 AND 2 VALVE CLOSED MESSAGES. THE QRH WAS FOLLOWED AND THE ACFTSDR 2009FA0000026Pump · low pressurePILOT REPORTED INSTRUMENT AIR PRESSURE LOW AT IDLE ON RUN UP. ON TROUBLESHOOTING, THE MECHANIC DETERMINED THE AIR PUMP WAS NOT PRODUCING ENOUGH PRESSURE AT IDLE. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. (K)SDR BSY2008F00002Clamp · failedAFTER TAKEOFF AT 4,000 FT RT ENGINE FAILED AND ACFT RETURNED WITH NO PROBLEMS. MAINT FOUND INDUCTION TUBE CAME OFF INTER-COOLER REDUCING MANIFOLD PRESSURE TO A NORMALLY ASPIRATED ENGINE. REPLACED WITH NEW DUCT AND CLAMP. (K)SDR P5CA0801575Shutoff Valve · defectiveNR 1 ENGINE AUTO START FAILED. TROUBLESHOT AND FOUND NR 1 PRSOV DEFECTIVE AMM36-11-04. (K)SDR 2008UALA03768Pneumatic System · fluctuatesRT DUCT PRESSURE FLUCTUATES DURING DESCENT, WITH ENG RUNNING, LT & RT ISOL VLVS CLSD, & BLD SW ON. DUCT PSI FLUCTUATES BETWEEN 998. CREW COMMENTS: 18 PSI TO 32 PSI. FLUX ALSO SEEN IN EPR +-- .03 AND N1+-- .3.
SDR 2008UALA03359Shutoff Valve · faultyNR 1 ENG PRSOV FAILED HEALTH CHECK REFERENCE PRESSURE LOW. *S/D* DURING HEALTH CHECK FOUND PRESSURE REGULATING SHUT OFF VALVE FAULTY. REPLACED PRSOV. AC OK FOR SERVICE.SDR 2008UALA03231Pneumatic System · malfunctionedENGINE NR 1, PNEUMATIC PRESSURE IS 10 PSI AT IDLE REQUIRED ENG TO RUN UP TO BLEED SHIFT BEFORE IS STARTS TO WORK. THEN GOT 31 PSI ON IDLE. RAN ENG TWICE SAME ISSUE, SUSPECT HI STAGE. REPLACED PRV AND PRV CONTROLLER. OP CHK NORMAL.SDR HALA0800583Precooler · crackedETOPS SIGNIFICANT SYSTEM, DURING ENG CHANGE FOUND CRACK APPROX 1 IN LONG IN FWD INBD CORNER OF NR 1 ENG PRECOOLER. ACCOMPLISHED PROCEDURE WELDMENT IAW H/S MANUAL 36-12-12 PG 601. TASK ACCOMPLISHED BY UAL.
SDR 05212008001Clamp · failedTHE CREW REPORTED THAT AFTER A NORMAL TAKEOFF AND CLIMB, AND AFTER GOING INTO CRUISE THE LEFT ENGINE WOULD NOT PRODUCE GREATER THAN 70 PERCENT N1, 80 PERCENT N2 AND 1.00 EPR. THEY ALSO REPORTED THAT EICAS REPORTED A LEFT ENGINE OVERTEMP OF 451 DEGREES. THE CSDR CHQA200800078Switch · faultyFLIGHT 6360, CVG TO STL - DURING CLIMB IN ICING CONDITIONS, CREW RECEIVED AN E1 BLEED VALVE FAIL MESSAGE, WITH THE ASSOCIATED BLEED VALVE CLOSED AND WING ANTI-ICE FAIL MASTER WARNING. THE CREW RAN THE APPROPRIATE QRH CHECKLISTS AND RETURNED TO CVG. THE AIRCRSDR P5CA0801556Duct · leakingWITH NR 2 ENGINE FIRE LOOP "B" ON DEFERRAL AND APPROXIMATELY 140NM OUT OF ICN AT FL29 LOOP "A" FIRE DETECTOR LIGHT AND FAULT LIGHT ILLUMINATED FOLLOWED BY FIRE WARNING BELLS. THE ENGINE WAS SHUTDOWN AND FIRE HANDLE PULLED WITH OUT DISCHARGING BOTTLES. OIL PRSDR 2008UALA02078Pneumatic System · contaminatedDURING ENGINE START LEFT ENGINE GOT CAUTION: L ENG PRV WITH LEFT BLEED LIGHT. AFTER EXTENSIVE TROUBLE SHOOTING OF LT PNEUMATIC SYSTEM. FOUND WATER INSIDE OF SENSE LINE PORT OF OVER PRESSURE SWITCH. REPLACED OVER PRESSURE SWITCH PER MM 36-21-03. ALSO COMPLETEDSDR P5CA0801552Relief Valve · wrong partRETURN TO BLOCKS DUE TO "BLD 1 OVHT/PRV" EICAS MESSAGE. FINDING THAT THE INCORRECT PRV VALVE WAS DELIVERED, MAINTENANCE SWAPPED THE NR 3 HPSOV WITH NR 1 PRV AND THEN DEFERRED THE NR 3 HPSOV, PER MM 36-11-00.SDR CA080331008B-Nut · failed(CAN) FOLLOWING AN ANNUAL INSP AND A SATCOM AVIONICS UPGRADE IN THE INITIAL CLIMB PHASE OF A TEST FLIGHT , CABIN PRESSURE WAS INCREASING AT A MAXIMUM RATE. ECS WAS PROMTPLY SHUTDOWN ,CABIN DUMPED, AC LEVELED OFF AND RETURNED TO AIRPORT FOR LANDING. THE SENSE L
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