JASC 3610
Service difficulty reports · 7,150
Reports filed under 3610 · Pneumatic Distribution System, newest first.
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 = '3610' 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 = '3610' 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 UIEA2017112002260Switch · malfunctionedRIGHT ENGINE BLEED OFF LIGHT INOPERATIVE. REMOVED AND REPLACED THE SWITCH IAW SWPM 20-84-15. OPS CHECKED NORMAL.SDR UIEA2017112002261Controller · malfunctionedRIGHT ENGINE PRV MESSAGE DURING TAKEOFF. REPLACED THE PRV CONTROLLER IAW AMM 36-11-18. OPS CHECKED GOOD. NO DEFECTS NOTED.SDR ASMF201801004Line · failedCAPTAIN REPORTED THAT THE LEFT AND RIGHT POINTER DUCT PRESSURE NOT HAD THE SAME SPLIT EITHER POINTER BELOW 18 PSI DURING TAKEOFF, CLIMB AND CRUISE, DUE TO THE ENGINE IS THE BLEED SOURCE LEFT 35 PSI AND RIGHT 14-15 PSI. THE FLEX LINE BETWEEN PRSOV AND BAR WAS SDR CALA2017111704069Fitting · galledSTATUS MESSAGE FOR THE LT STRUT OVERHEAT DETECTOR 1. EMERGENCY DECLARED. REPLACED PRSOV IAW AMM 36-11-09. FOUND PNEU FITTING ON VALVE GALLED. NO LEAKS NOTED WITH DUCTS PRESSURIZED IAW AMM 36-11-09, ACCOMPLISHED ENGINE RUNS 80 PERCENT N1, 10 MINUTES, NO STSDR SIMA20171116001Pressure Switch · failedNR 1 BLEED OVERPRESSURE, NR 1 BLEED FAIL AT 1500 FT DURING CLIMB. FOLLOWED QRH. REPLACED THE LT BLEED OVERPRESSURE SWITCH, OPS CHECKED GOOD IAW 35-14-01SDR ASAA2017111422581Line · brokenLEFT PACK DUCT PRESSURE 5 PSI. RIGHT PACK DUCT PRESSURE 45 PSI. ACFT GROUNDED. FOUND THE NR 1 ENGINE PRECOOLER CONTROL VALVE SUPPLY PRESSURE SENSE LINE BROKEN. REMOVED AND REPLACED THE SENSE LINE IAW AMM 36-12-400-801, STEP 3. F. (9), AND (10). ACCOMPLISSDR ANCF2017111001Bleed Valve · failedNR 2 ENGINE BLEED ILLUMINATED IN FLIGHT, AIR ENG 2 BLEED FAULT ON ECAM. FOUND OXYGEN MASK IN ALL STATIONS DEPLOYED. IAW TSM TASK 36-11-00-810-B39-. A FAILURE OF REGULATION OF THE BLEED-PRESSURE REGULATING VALVE DURING TAKE-OFF ON ENGINE 2 WAS ACCOMPLISHED ANSDR 5BMA2017111301Precooler · failedAFTER TAKE OFF DURING CLIMB, THE CREW RECEIVED A RT BLEED AIR OVER HEAT ANNUNCIATOR. FOLLOWED CHECKLIST AND THE OVER TEMP ANNUNCIATOR TO EXTINGUISHED AFTER SELECTING LT SOURCE AND REDUCING RT ENGINE POWER TO IDLE. RETURNED TO DEPARTURE. MX DISCOVERED THE RT PSDR CALA2017111003968Duct · leakingSTATUS MESSAGE FOR THE LT STRUT OVERHEAT DETECTOR NR 1. EMERGENCY DECLARED. ACCOMPLISHED FIM 26-12-00-300-802C1. FOUND A LEAK IN THE Y DUCT IN THE LEADING EDGE ABOVE THE NR 1 PYLON. REMOVED AND REPLACED THE DUCT IAW AMM 36-11-01-004-083-001.SDR FDEA201711083198Line · failedCLIMBING THROUGH 12000FT, THE NR 1 BLEED VALVE FAULT LIGHT ILLUMINATED. TURNED OFF & ON BLEED VALVE SWITCH MULTIPLE TIMES WITH NO RESET. FAULT LIGHT REMAINED AFTER MULTIPLE ATTEMPTS. FOLLOWED QRH WITH NO SUCCESS. . VERIFIED NR 2 PACK OFF. JUMPSEATER INSDR UIEA2017120702374Shutoff Valve · malfunctionedL ENG HPSOV CAUTION EICAS INTERMITTENT ON AT REPEAT TAKEOFF LEVEL OFF DESCENT L ENG HPSOV STATUS MSG ON AFTER TAKEOFF(<DIV>REMOVED AND REPLACED L .ENG HPSOV REF AMM 36-11-07 PERFORMED AIRSUPPLY CONTROL SYSTEM BITE CHECK OK REF AMM 36-23-00 BITE OK PASSEDSDR UIEA2017110802200Controller · no testNR 2 ENGINE PRV CONTROLLER, PNEUMATIC HEALTH CHECK FAILED. REMOVED AND REPLACED THE NR 2 ENGINE PRV CONTROLLER IAW AMM 36-11-19. OPS CHECKED NORMAL.SDR UIEA2017110402173Pin · out of positionSTATUS MESSAGE FOR THE LEFT ENGINE BLEED OFF. FOUND PRSOV LOCK OUT PIN NOT IN THE STOWED POSITION. STOWED THE PIN IN PRSOV IAW AMM 36-00-21, OPS CHECKED IAW AMM 36-11-07. PERFORMED ENGINE RUN IAW AMM 71-00-00.SDR SIMA20171103002Pressure Switch · failedNR 2 BLEED OVERPRESSURE INDICATION MESSAGE DURING INITIAL CLIMB AFTER TAKEOFF. REVIEWED CMC AND TROUBLESHOOT IAW CMC MESSAGES. RT NACELLE PRSOV OPEN AND FAILURE OF RH PRSOV OVERPRESSURE SWITCH AUX RELAY. R & R BLEED OVERPRESSURE SWITCH IAW AMM 36-14-01.SDR UIEA2017110302168Coupling · unsecureDURING AN OPS CHECK OF THE FAN AIR VALVE FOUND BLEED LEAK ON THE NR 1 ENGINE. TROUBLESHOOTING AND FOUND THE PNEUMATIC DUCT BETWEEN THE PRECOOLER AND PRSOV LOOSE AT THE FLANGE COUPLING ABOVE THE PRECOOLER. SECURED THE FLANGE COUPLING IAW IAW AMM 36-11-01. OPSSDR UIEA2017110402171Controller · failedRIGHT ENGINE PRV EICAS MESSAGE ANNUNCIATED DURING CLIMB AT APPROXIMATELY 10000 FT. REPLACED THE NR 2 ENGINE PRV CONTROLLER IAW AMM 36-11-19, OPS CHECKED OK.SDR UIEA2017110202163Valve · failedEICAS ILLUMINATED FOR THE LEFT ENGINE BLEED OVERHEAT. REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-16. OPS CHECKED GOOD.SDR UIEA2017110102157Duct · looseEICAS LEFT PACK OFF, LEFT ENGINE BLEED OFF, LEFT ENGINE BLEED OVERHEAT. ACCOMPLISHED THE CHECK LIST. SECURED A LOOSE DUCT ON LEFT ENGINE FAN AIR VALVE. NO OTHER LEAKS NOTED IAW AMM 36-11-15 AND 36-11-16.SDR AALA20171029005Shutoff Valve · faultyAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DFW-EZE FLIGHT RETURNED TO DFW ACCOUNT LEFT ENGINE BLEED WENT TO OFF FOLLOWED BY ISLN CLOSED THEN LEFT PACK OFF. OVERWEIGHT LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT HIGH PRESSURE SHUTOFF VALVE PER AMM 36-11-0SDR AALA201710319077Controller · failedTHE AIRCRAFT WAS GROUNDED.. AT FL 360 CABIN ALTITUDE REACHED APPROXIMATELY 10,000 FEET. THE CABIN ALTITUDE WARNING HORN SOUNDED. THE COCKPIT CREW DONNED THEIR OXYGEN MASKS AND STARTED A DESCENT TO 10, 000 FEET. DURING DESCENT CABIN ALTITUDE WAS AT 10,000SDR ASAA2017102722355Regulator · failedHIGH STAGE REGULATOR ON THE NR 1 ENGINE FAILED A HEALTH CHECK. REVERSE FLOW DIAPHRAM FAILED. ACFT GROUNDED. REMOVED & REPLACED THE NR 1 HIGH STAGE REGULATOR IAW AMM 36-11-07. ACCOMPLISHED ENGINE BLEED AIR CROSSOVER TEST IAW AMM 36-11-00-710-801. OPS TESTED GSDR UIEA2017103102142Control Valve · malfunctionedPRVC LT ENGINE INOP. REMOVED AND REPLACED LT ENGINE PRVC VALVE PER AMM 36-11-18.SDR ASAA2017102622356Valve · failedLEFT BLEED TRIP OFF LIGHT ILLUMINATED INFLIGHT. RESET WITH THE TRIP RESET BUTTON PUSHED IAW QRH. ACFT GROUNDED. PERFORMED FIM 36-10, TASK 801. FAILED STEP F.2.C. FOUND HIGH STAGE VALVE NOT CLOSING COMPLETELY. REMOVED AND REPLACED THE NR 1 ENGINE HIGH STAGSDR UIEA2017102502017Valve · damagedPYLON NR 2 PRV FOUND WITH DAMAGE. REMOVED AND REPLACED NR 2 PRV.SDR UIEA2017102502092Cable · damagedRIGHT A/C BAT BYPASS CROSSOVER SUPPLY DUCT CONNECTOR ASSY FOUND 2 OUT OR 3 CABLES ASSY WORN ON THREAD AREA . THE CABLE ASSY WAS REPLACED.SDR UIEA2017102602108Blanket · tornAFT CARGO APU PNEUMATIC DUCT AT BS 1600 BLANKETS TORN. REMOVED AND REPLACED THE PNEUMATIC DUCT BLANKETS.SDR UIEA2017102502041Bearing · missingDURING REMOVAL OF THE NR 1 ENGINE PRSOV, FOUND STRUT PNEUMATIC DUCT ABOVE THE PRSOV, FWD SUPPORT ROD HAS MISSING ROD END BEARING. REMOVED AND REPLACED THE ROD END IAW AMM 36-11-01-404-046-001.SDR UIEA2017102702131Sensor · crackedNR 1 ENG. PRSOV AIR TEMP SENSOR PRESSURE SWITCH PLASTIC WIRE HOUSING CRACKED AND HAS EXPOSED WIRES. REMOVED AND REPLACED THE NR 1 ENG PRSOV FAN AIR TEMP SENSOR IAW AMM 36-11-17-004-001 AND 36-11-17-404-017. LEAK CHECKED GOOD IAW AMM 36-11-17-404-017 AND BITE SDR UIEA2017102602124Warning Light · false activationDURING TAKE OFF ROLL, THE RT ENGINE BLEED OFF EICAS AND OFF LIGHT ILLUMINATED ZERO DUCT PRESSURE INDICATED. COMPLIED WITH FIM 36-20 FT 104. RT ENGINE PRSOV FAULT, INSPECTED RT ENG PRSOV VALVE, SENSE LINES, AND ELECTRICAL CONNECTOR , BITE CHECKED THE AIR SUSDR UIEA2017102502049Clamp · brokenNR 2 ENGINE PNEUMATIC SENSE LINE ADEL CLAMP ABOVE OIL COOLER IS BROKEN. REMOVED AND REPLACED THE CLAMP IAW AMM 70-50-00-912-001-H00.SDR UIEA2017102502057Regulator Valve · no testNR 2 ENGINE PRESSURE REGULATOR VALVE CONTROLLER FAILED EO6736A005. REMOVED AND REPLACED THE VALVE IAW AMM 36-11-19, OPS CHECKED GOOD.SDR UIEA2017102502062Bolt · damagedNR 2 ENGINE PRECOOLER AFT INLET DUCT CLAMP BOLT, THREADS ARE DAMAGED. REMOVED AND REPLACED THE CLAMP IAW AMM 36-11-15.SDR UIEA2017102502059Regulator Valve · no testNR 1 ENGINE PRESSURE REGULATOR VALVE FAILED EO6736A005-CS. REMOVED AND REPLACED THE NR 1 ENG PRV IAW AMM 36-11-18-404-018-001, OPS AND LEAK CHECKED GOOD.SDR HALA2017102500261Controller · unknownETOPS SIGNIFICANT SYSTEM, RIGHT ENGINE PRV EICAS IN DESCENT BETWEEN FL230 AND 17000 FT. REPLACED PRVC PER AMM 36-11-19.SDR ASAA2017102422307Link · wornWHILE ACCOMPLISHING A NR 2 ENGINE INLET INSPECTION, FOUND A LINK WORN ABOVE HIGH STAGE VALVE. ACFT GROUNDED. REMOVED AND REPLACED THE WORN LINK ABOVE HIGH STAGE VALVE IAW AMM 36-11-01-400-802, AND 71-00-02.SDR HALA201710230026Regulator Valve · inoperativeAIR ENGINE NR 1 BLEED FAULT. PERFORMED BITE TEST OF BMC. FAULTED NR 1 PRESSURE REG VALVE, REMOVED AND REPLACED NR 1 PRESSURE REG VALVE PER AMM 36-11-52. LEAK CHECK AND BITE TEST GOOD. OK FOR SERVICE. VALVE, BLEED, P OFF 33-3611-9-0002 01965 ON 33-3611-9-0002 0SDR UIEA2017101901985Warning Message · false activationBLEED 4 EICAS. FOLLOWED QRH PROCEDURES AND EXPERIENCED ENGINE STALLS AFTER OPENING ENG BLEED 4. ALL GROUND CHECKS ACCOMPLISHED, NO FINDINGS IAW AMM 36-00-00.SDR UIEA2017101801974Controller · malfunctionedON FINAL APPROACH AND TAXI IN AT IDLE RPM, LEFT ENGINE BLEED OFF MESSAGE. EXTINGUISHED AT HIGHER RPM. REMOVED AND REPLACED THE LT ENGINE HIGH PRESSURE CONTROLLER IAW IAW AMM 36-11-08. OPS CHECKED GOOD.SDR SWAA2017102017242Regulator · faultyDECLARED EMERGENCY, AT FL 320 LT PACK TRIP FOLLOWED BY RAPID DECOMPRESSION. R&R NR 1 ENGINE HIGH STAGE REGULATOR PER AMM.SDR SWAA2017102017236Regulator · faultyDECLARED EMERGENCY, AT FL 320 LT PACK TRIP FOLLOWED BY RAPID DECOMPRESSION. R&R NR 2 ENGINE HIGH STAGE REGULATOR PER AMM.SDR UIEA2017101901981Shutoff Valve · failedRIGHT ENGINE IDG OUT TEMP MAINTENANCE MESSAGE. REMOVED AND REPLACED THE NR 2 ENGINE AIR SHUTOFF VALVE IAW AMM 24-11-07, OPS CHECKED GOOD.SDR LR7A2017101401295Duct · crackedDURING A SCHEDULED FLIGHT, THE NR 2 NACELLE OVERHEAT ILLUMINATED. THE NR 2 ENGINE SHUTDOWN RETURNED TO DEPARTURE. REMOVED AND REPLACED A CRACKED BLEED AIR MANIFOLD UPPER DUCT ASSY IAW SMP 581 36A-10.SDR HALA2017101600251Bleed Valve · faultedNR 1 ENGINE BLEED FAULT DURING CLIMB. RESET IAW MOC, OPS NORMAL. TROUBLESHOT IAW TSM 36-11-81-810-909-A. REMOVED AND REPLACED THE NR 1 ENGINE BLEED VALVE IAW AMM 36-11-52. OPS CHECKED OK. NO FAULTS NOTED. BITE CHECKED BMC, OK. LEAK CHECKED OK. NO LEAKS. SDR ASAA2017101322202Link · looseWHILE ACCOMPLISHING TC 78472000, FOUND THE UPPER CLEVIS ROD END LINK LOOSE JUST FWD OF PRSOV ON THE NR 2 ENGINE. ACFT GROUNDED. REMOVED & REPLACED THE CLEVIS ROD END LINK ASSY.SDR AALA201710119045Bypass Valve · failedFLIGHT DIVERTED DUE TO A LEFT AIR CONDITIONING PACK FAILED AND THE COCKPIT TEMPERATURE WOULD NOT GO ABOVE 50 DEGREES. LANDING UNEVENTFUL. REMOVED AND REPLACED SECOND STAGE TURBINE BYPASS VALVE IAW AMM 21-52-32. LEAK AND OPS CHECKED GOOD.SDR UIEA2017091901705Check Valve · damagedLEFT ISOLATION BYPASS CHECK VALVE HOUSING FOUND CHAFED, AND FLAPPER LOOSE. THE CHECK VALVE WAS REMOVED, REPLACED AND TESTED IAW AMM 36-11-05, REV 122. FOUND SATISFACTORY.SDR UIEA2017091901707Check Valve · chafedRT ISOLATION BYPASS CHECK VALVE INTERNAL, FOUND THE HOUSING CHAFED AND FLAPPER LOOSE. THE ISOLATION BYPASS CHECK VALVE WAS REMOVED, REPLACED, AND TESTED IAW AMM 36-11-05, REV 122, FOUND SATISFACTORY.SDR AALA201710109002Solenoid · failedAFTER TAKEOFF NR 2 ENGINE BLEED ABNORMAL LIGHT ILLUMINATED. ENGINE BLEED RESET WAS UNSUCCESSFUL. ACCOMPLISHED ECAM CHECKLIST RETURNED TO DEPARTURE FOR LANDING, REMOVED AIRCRAFT FROM SERVICE FOR TROUBLE SHOOTING OF RIGHT ENGINE BLEED SYSTEM. MAINTENANCE REPLSDR UIEA2017100601931Shutoff Valve · malfunctionedDURING CLIMB & DESCENT, LEFT PRESSURE VARIES & SURGES 10 PSI TO 40 PSI TO 10 PSI, OPERATES NORMALLY ON GROUND AND CRUISE. REMOVED AND REPLACED LG PRSOV IAW AMM 36-11-09, OPS CHECKED GOOD.SDR ASAA2017100622138Bracket · wornFOUND THE UPPER ROD END LINK LOOSE JUST FWD OF PRSOV ON NR 2 ENGINE. ACFT GROUNDED. REPLACED PNEUMATIC DUCT CLEVIS AND MOUNTING BRACKET IAW AMM 36-11-01-400-802.
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