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 HALA0700554Unknown · unknownETOPS SIGNIFICANT SYSTEM, APU PNEUMATIC AIR INOP. BITE CHECK ECU PER AMM 49-11-00. NO FAULTS NOTED. APU STARTED ON FIRST ATTEMPT. OK FOR SERVICE. APU AIR OPS CK GOOD.
SDR HALA0700550Unknown · unknownETOPTS SIGNIFICANT SYSTEM, RT ENG BLEED OFF LIGHT ON AFTER START UNTIL POWER IS APPLIED (APPX 60 PERCENT N1) THEN OPERATED NORMALLY FOR REST OF FLIGHT. BIT AIR SUPPLY MODULE AS PRECAUTIONARY. NO FAULTS NOTED. OKAY FOR SVC. REFERENCE AMM 36-23-00-715-001.SDR SIMA200734402Button · failedEMERGENCY DECLARED, RIGHT AFTER TAKEOFF AT ABOUT 2000 FEET WING AND STAB FAIL CAUTION CAME ON FOLLOWED BY ICE CONDITION A/I INOP WARNING ON EICAS. RETURNED FOR LANDING AT ORD. VISUALLY INSPECTED PRESSURE SWITCH MANIFOLD, WING ANTI ICE VALVES, AND SENSE LINESSDR QXEA200701646Warning System · false activationPDX FLIGHT NR 2058 - DURING CLIMB-OUT, NR 1 BLEED HOT CAUTION MESSAGE. PER CHECKLIST TURNED BLEED SELECTOR TO MIN LIGHT STOPPED CYCLING. PERFORMED BLEED AIR FUNCTIONAL TEST COULD NOT DU0PLICATE PROBLEM REPLACED NR 1 BLEED AIR OVERTEMP SWITCH AS A PRECAUTIONASDR 2007UALA04247Bleed Air Sys · unknownLEFT ENGINE BLEED PROBLEM. REPLACED UPPER FLOW CONTROL ISOLATION VALVE. OP CHECKS GOOD & AIRCRAFT RETURNED TO SERVICE.
SDR QXEA200701373Indicator · malfunctionedSJC FLIGHT NR 2404: ON PUSHBACK AS APU BLEED WAS TURNED OFF, OPEN LIGHT WILL NOT EXTINGUISH. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE PERFORMED TEST OF THE APU BLEED AIR SYSTEM WITH NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR HALA0700289Unknown · unknownETOPS SIGNIFICANT SYSTEM, PNEUMATIC PRESSURE DRIPS EXCESSIVELY WHEN USING APU AIR FOR ENGINE STARTS. OPS CHECKED APU BLEED AIR PEC AMM 49-11-00-802, OPS CHECKED GOOD ALSO CHECKED FIM 36-10-00 FIG 118. NO FAULTS NOTED.SDR AMTA200700296Unknown · unknownAT START OF TAKEOFF, WITH BLEEDS OFF, LT BLEED TRIP LIGHT CAME ON. ABORTED TO AT SLOW SPEED. RESET BLEED TRIP LIGHT. (K)SDR DXTA200702244Clamp · leakingAPPROX 5 MIN AFTER TAKEOFF, REAR BAY OVERHEAT LIGHT CAME ON. [06-15-07] RAN AIRCRAFT AT POWER AND FOUND NR 1 MAV LEAKING AT BOTH CLAMPS. O/B CLAMP WAS LEAKING DIRECTLY ON TEMP SENSOR. REMOVED NR 1 MAV AND REPLACED SEALS WITH NEW P/N 6-646-1 PAR AND 240SDR HALA0700278Controller · malfunctionedATO - DUE TO HPSOV AND PRV EICAS MSG ILLUMINATING AS THROTTLE WERE ADVANCED FOR TAKE OFF ROLL. REPLACED PRV CONTROLLER PER AMM 36-11-19, OPS CK LK CK OK. LOCKED OUT HPSOV PER MEL 36-11-2 ENTERED IN MIC SHT PLAC. INSTALLED PER MEL SHORTING CONNECTOR PLUG INSSDR 2007UALA01783Engine · overheatedRTFL DUE TO RIGHT ENGINE BLEED OVERHEAT INDICATION. [07-10-07] REPLACED FAN AIR VALVE AND FAN AIR TEMP SENSOR, PERFORMED HIGH POWER RUN, PS CK OK . AIRCRAFT OK FOR SERVICE.SDR AMTA200700049Valve · unserviceableEICAS MSG R ENG BLEED OFF DISPLAYED R ENG BLEED OFF LIGHT ILLUMINATED, CUICT PRESS NO RM 2119Z. REMOVED AND REPLACED FLOW CONTROL AND SHUTOFF VALVE PER AMM 21-51-01-2. RAN ENGINE, OPS CHECK NORMAL. (M)SDR HALA0700028Filter · unknownAIR SYS FAULT PRIOR TO T/O. REMOVED AND REPLACED RT ENG INLINE FILTER PER AMM 36-11-08 OPS AND LK CK OKAY.SDR HALA0700030Unknown · unknownBTB: ON LEFT ENG START BLEED LIGHT CAME ON. DISCONNECTED START, BLEED LIGHT WENT OUT. ACCOMP SUCCESSFUL LEFT ENG GRD RUN PER AMM 71-00-00 BLEED LIGHT REMAINED EXTINGUISHED. NO EICAS MSGS. ALL PNEUMATIC FUNCTIONS NORMAL. ACCOMP BLEED AIR SUPPLY MODULE BITESDR HALA0600915Controller · unknownRT ENG PRV DISPLAYED ENG BLEED LIGHT ILLUM DUCT PRESS HIGH. REMOVED AND REPLACED PRV AND PRV CONTROLLER IAW AMM 36-11-18 AND 36-11-19 PERFORMED ENG RUN IAW AMM 71-00-00. ACCOMPLISHED AR 767-36-001. CK NORMAL PRV MPN 802170-10 S/N ON 891249 S/N OFF 9904065 SDR 2007FA0000452Piston · failedINSTALLED A PISTON AIR PUMP (PN IU478-003, SER NR T568A) ON AUG 25, 2005. THE PUMP DRIVE COUPLING FAILED BY 12/06 WITH LESS THAN 66 HOURS ON IT. COUPLING FAILED INTERNALLY IN PUMP, WITH PLASTIC/SILICON DEBRIS IN ENG/DRIVE INTERFACE. (K)SDR RAIA00611042Seal · unknownFLT NR 7931 - ORD - ENGINE 2 BLEED LEAK INDICATION DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE AFT BLEED SEALS ON BLEED DUCT IN FECU BAY. OPS CHECKED GOOD.SDR 2007FA0000003Pump · out of limitsPILOT REPORTED SUCTION INDICATOR WAS BELOW LIMITS, AC RETURNE TO BASE. UPON TROUBLESHOOTING, THE MECHANIC REMOVED THE AIR PUMP AND NOTICED THE SHAFT WAS VERY EASY TO ROTATE, HAD NO RESISTANCE TO IT. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. (K)SDR VNAA0610038Element · failedCREW REPORTED AN ANTI ICE DUCT RED WARNING MESSAGE. MAINTENANCE INSPECTED AND FOUND A RIGHT HAND BLEED AIR LEAK. MAINTENANCE REMOVED AND REPLACED THE BLEED AIR SENSING ELEMENT. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.SDR NSVA200600132Shutoff Valve · malfunctionedLT DUCT OVERTEMP LIGHT ILLUMINATED ON TAXI. REMOVED AND REPLACED LT HIGH PRSOV PN ON/OFF 321935 SN OFF 557A, SN ON 982CD, SN OFF 557A.SDR XN0A1345Line · looseNR 2 BLEED REGULATOR FAULT 90 DEGREE CELSIUS, 0 PSI, COULD NOT PRESSURIZE. NR 1 BLEED OVER TEMP, COULD NOT PRESSURIZE, USED APU FOR PRESSURIZATION, LIMIT 15000 FT, RETURNED TO VHH. FOUND LOOSE SENSE LINE, SECURED LINE OPS CHECK NORMAL IAW A300 AMM CHAPTER 36SDR 139807152006Isolation Valve · malfunctionedPNEUMATIC ISOLATION VALVE OPENS AND CLOSES DURING FLIGHT WITH NO INPUT FROM CREW.SDR P5CA0601486Seal · failedCREW REPORTED AT TOP OF CLIMB (CRUISE) MULTIPLE EICAS MESSAGES -BLEED DUCT L-. REPLACED SEALS AT FLEX COUPLING AT WBL 450 LEADING EDGE PNEUMATIC DUCT PER MM 36-11-02.SDR COMA0670119Bleed Air Sys · contaminatedFLIGHT 4985 - SMOKE FORWARD LAV WARNING MESSAGE CAME ON DURING TAXI THEN WENT OUT. INSPECTED FORWARD LAV NO EVIDENCE OF SMOKE OR FIRE. SUSPECT GLYCOL INGESTION IN BLEED SYSTEM.SDR 06FDEA0919Controller · malfunctionedON T/O CLIMBING OUT AT 5000FT, MASTER WARNING ILLUMINATED WITH -AIR MANF 2 FAIL- ALERT DISPLAYED AIR SYSTEM SHOWED NR 2 INDICATING RED WITH NR 2 BLEED OFF AND PACK 2 & 3 OFF. SYNOPTIC WARNED NOT TO PRESSURIZE MANIFOLD NR 2 RED -MANF- DISPLAYED ON OVERHEAD PANSDR PCSA02090602Modulating Valve · malfunctionedFLIGHT 839 DURING PREPARATION FOR TAKEOFF, THE CREW REPORTED THE NUMBER 1 ENGINE BLEED TRIPPED WHEN TAKEOFF POWER WAS SET, 95 PSI DUCT PRESSURE INDICATED. THE AIRCRAFT RETURNED TO THE BLOCK WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESHOT AND REPLACED TSDR QXEA200600020Shutoff Valve · malfunctionedSEA FLIGHT NR 2167, ON TAXI IT WAS NOTED 100C DIFFERENCE ITT ALL OTHER ENGINE INSTRUMENTS ABOUT THE SAME. WITH NR 1 BLEED OFF NO CHANGE IN ITT. WITH NR 2 BLEED OFF ITT CHANGED SIGNIFICANTLY. MAINTENANCE REPLACED NR 1 HPSOV, NORMAL ITT CHANGED NOTED WITH APPSDR DLM88050488Switch · failedTHE 26K TAIL COMPT TEMP HIGH MASTER WARNING CAME ON. FOUND LEFT TEMP SWITCH STUCK IN CLOSED POSITION. REPLACED SAME.SDR RYNA200500023Gasket · failedTAIL COMPARTMENT TEMPATURE HIGH LIGHT ILLUMINATED DURING CLIMB. REMOVED AND REPLACED TWO GASKETS ON THE PNEUMATIC ICE CONTROL ANTICIPATOR AND BLEED AIR SUPPLY HIGH TEMPERATURE SENSOR. OPERATIONALLY CHECKED NORMAL, NO LEAKS NOTEDSDR QXEA200501107Odor · detectedCREW REPORTS FOUL ODOR IN AIRCRAFT. MAINTENANCE INSPECTED WATER SEPARATION, MIXING MANIFOLD FOR WATER AND SCUM. FOUND POOLED WATER IN BOTTOM. CLEANED OUT WATER. NO OTHER DEFECTS NOTED. NO SCUM NOTED. OPERATIONAL CHECK AND LEAK CHECK OF DUCTING GOOD. NO PSDR WRLA2005086Coupler · damagedAIR TURNBACK INITIAL CLIMB OBSERVED MASTER WARNING & ENG FIRE WARNING LIGHT & BELL CAME ON & THEN OFF. NR 2 ENG NACELLE TEMP 260 DEG, NR 1 & 3 160 DEG. REDUCED ENG THRUST LEVER TOWARD IDLE TEMP FOLLOWED, PUSHED LEVER FORWARD & TEMP INCREASED, TESTED FIRE WARSDR 2005FA0000864Clamp · defectiveDURING FLIGHT, THE CREW HEARD A POP AFTER WING DEICE HAD BEEN TURNED ON. THEY PERFORMED THE NESSARY PROCEDURES ACCORDING TO THE CHECKLIST. DETAILED INSPECTION REVEALED THAT THE SUSPECT CLAMP HAD SEPARATED AND CAUSED ENGINE BLEED AIR TO DUMP INTO THE AFT EQUISDR XN0A1236Warning Light · illuminatedDURING EMERGENCY DESCENT, LT DUCT OVERHEAT LIGHT TRIP, PERFORMED ALL CHECKLIST.SDR UIEA200500066Precooler · crackedPYLONS NR1, 2, 3, AND 4, PRECOOLER EXHAUST CUT OUT LOWER EDGE CRACKED. REPAIRS ACCOMPLISHED IAW MM. (K)SDR S2YA05028Shutoff Valve · inoperativeDURING TAKEOFF OF FLIGHT, THE CREW REPORTED LOW PRESSURE BLEED SOV FAIL CAS MESSAGE AFTER POWER UP FOR TAKE OFF. THE CREW ABORTED THE TAKEOFF AND RETURNED TOT HTE GATE. MECHANIC INSPECTED THE SYSTEM AND REPLACED LT PACK FLOW CONTROL VALVE BUT THE SYSTEM STILSDR CA050506004Duct · separated(CAN) DUCT ASSEMBLY (13TH STAGE BLEED AIR) SEPARATED FROM FLANGE.SDR P5CA0501336Shutoff Valve · failedDURING CLIMBOUT, NR 1 ENGINE NACELLE LOOPS A & B WENT INTO RED, SET WARNING BELLS OFF. ENGINE SHUTDOWN. OIL PRESSURE 45 PSI. REPLACED NR 1 ENGINE HIGH PRESSURE SHUTOFF VALVE PER MM 36-11-05. LEAK CHECK OIL, OPS CHECK NORMAL ON HIGH POWER RUN UP PER MM 71-0SDR FX7A200500003Shutoff Valve · defectiveDURING CLIMB ENGINE NR 1 STRUT OVER HEAT LIGHT ILLUMINATED.SDR ASMF200503012Pneumatic System · malfunctionedAIRCRAFT RETURNED TO PLATFORM DURING PUSH BACK, THE PNEUMATIC WAS NOT ENOUGH TO START THE ENGINES. THE ENGINES WERE STARTED WITH EXTERNAL PNEUMATIC PLANT IAW MM 49-50-00, TESTED CORRECT AND THE PNEUMATIC AUXILIARY POWER UNIT WAS DEFERRED IAW MEL 49-7. DURING TSDR VNAA0503006Shutoff Valve · failedDURING CLIMB (CLT TO PWM) UPON SELECTION OF COWL ANTI ICE, THE L COWL A/I & L ENG BLEED CAUTION MESSAGES ILLUMINATED. THE SYNOPTIC PAGE SHOWED VALUES IN WHITE NOT IN AMBER. THE CREW OF FLIGHT 2234 RETURNED TO CLT AND MADE AN UNEVENTFUL LANDING. AFTER TROUBLSDR 4511302132005Clamp · looseCREW ADVISED, THE RIGHT PYLON OVERHEAT ILLUMINATED IN CLIMB AT FL 17.0 WITH NAC AND ANTI-ICE SELECTED TO THE OFF POSITION. CREW REDUCED RIGHT ENGINE N1 TO 75 PERCENT FOR 1 MINUTE THEN TO IDLE FOR 2 MINUTES. CAS MESSAGE WOULD NOT EXTINGUISH. CREW FOLLOWED ACSDR 05010Duct · looseAT FL 34.0, NR 2 ENG START VALVE LIGHT ILLUMINATED; FOLLOWED CHECKLIST. NR 2 THROTTLE SEIZED; RAN SEVERE DAMAGE CHECKLIST. ALL ENGINE INDICATIONS NORMAL. PERFORMED VISUAL INSPECTION TO ENGINE. FOUND 8TH STAGE BLEED DUCTS LOOSE AND START VALVE DAMAGED. INSSDR WRNA200400015Valve · leakingNR 2 ENGINE EXCEEDED 960 DEGREE C DURING TAKE OFF (REACHED 962 DEGREE C FOR APPROX. 10 SECONDS W9TH AMBER EGT LIGHT) N1 WAS INDICATING 100.2 PERCENT. ABORTED THE TAKE OFF. AT IDLE NR 2 ENG 24.8 N1, 601 EGT, 66.4N2, 1700 F/F. CHECKED NR 2 ENGINE INLET AND EXHASDR 2004UALA00853Warning Light · illuminatedBLEED LOSS WING LEFT AND BLEED LOSS BODY LEFT EICAS MSGS. ALSO HYD PRESS DEMAND CI MSG. FOUND THE LOWER FLOW CONTROL VALVE INSTALLATION CLAMP BROKEN WITH APPRECIABLE BLEED AIR LEAKAGE. FURTHER INVESTIGATION OF THE CLAMP FOUND FAILURE OCCURED AT A SPOT WELD SDR TSAA0436069Bleed Air Sys · malfunctionedFLIGHT 280, HNL-KOA: PASSING THROUGH 8000 FT ON CLIMB-OUT, THE RT DUCT PRESSURE WAS OBSERVED AT ABOUT 40PSIG WITH THE ISOLATION VALVE CLOSED AND THE RT BLEED & RT PACK OFF. THE PRESSURE THEN DECREASED TO 14 PSIG, AND THEN DECREASED FURTHER WHEN POWER WAS REDUCSDR VNAA0408014Valve · failedDURING CLIMBOUT, THE CREW RECEIVED A RT LOW PRESSURE VALVE FAILED INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND LOW PRESSURE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERATIONAL CHECKS WERE PERFORMED ASDR UIEA200400124Thermal Switch · failedSHORTLY AFTER LEVEL OFF AT FL30.0 RIGHT WING OVERHEAT LIGHT ILLUMINATED. CHECK LIST PERFORMED, LIGHT EXTINGUISHED BEFORE 5 MINUTES CONTINUED AGAIN, COMPLETED CHECKLIST LIGHT STAYED ON NR 3 AND NR 4 BLEED VALVES CLOSED, RIGHT ISOLATION VALVE CLOSED ZERO AIR PRSDR 04FDEA02037Duct · failedFIVE MINUTES AFTER T/O RECEIVED HYD PUMP 1R OFF ALERT. HYD SYS SNOPSIS SHOWED -T- OVER 1R PUMP, 1 MINUTE LATER HYD SYSTEM FAILED, PRESSURE WENT TO -0-. ALSO NOTED AMBER -T- OVER LEFT PUMP PRIOR TO HYD 1 SYS OFF. REPLACED NR 1 ENG LOW PRESS TURBINE SUPPLY AISDR TSAA0436048Sensor · failedTHE NR 2 ENGINE BLEED TRIPPED IN FLIGHT, DIVERTED TO HNL. PERFORMED ENGINE GROUND RUN-UP TO VERIFY BLEED TRIP AND OPS CHECK, RUN-UP OK. REMOVED AND REPLACED THE NR 2 ENGINE BLEED AIR REGULATOR FOR TROUBLESHOOTING IAW AMM 36-11-03-4, LEAK AND OPS CHECK OK. RSDR GUU2004F00019Hose · looseDURING FLT, LT RED T HANDLE LIGHT ILLUMINATED. RESECURED LT ENGINE BLAST TUBE. OPERATIONAL CHECK NORMAL.
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