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 3EJA2018100500407Precooler · rupturedCREW REPORTED RH ENGINE HIGH ITT AT TAKE OFF POWER ALONG WITH AN ITT SPLIT OF OVER 50 DEGREES BETWEEN LEFT AND RIGHT. UPON LANDING AFTER FURTHER INVESTIGATION BY MAINTENANCE, IT WAS DISCOVERED THAT THE RH BLEED AIR PRE-COOLER HAD RUPTURED CAUSING SOME SCORCHINSDR UIEA2018091801994Control Box · malfunctionedTURNING ON WING ANTI-ICE RIGHT BLEED FAILED AND PACK OFF LIGHT ILLUMINATED. PERFORMED IDLE ENGINE RUN AFTER RESETTING BLEED CONTROL BOX RT BLEED WORKING OK AS PER AMM 71-00-00.SDR HALA201809180424Sensor · malfunctionedDURING CLIMB, HAD A PACK FLOW DISAGREE FOLLOWED BY RT BLEED AIR FAIL PRESSURE REGULATOR AND SHUTOFF VALVE (PR). REACTIVATED RT PRSOV FOUND MUSSLE FROM PRSOV PILOT VALVE TO FAN AIR VALVE. REMOVED AND REPLACED AIR LINE LEAK AND SECURITY CHECK GOOD. REMOVED ASDR VNAA2018091611101Stand Off · unsecureSUPPLEMENTAL INFORMATION: SECURED RH BLEED LOOP STAND OFF, TIGHTENED RH PACK PLENUM SLEEVE, REPLACED RH FLOW CONTROL VALVE FWD CONNECTOR DUCT AND CW WING A-ICE OPS CHECK. OPS AND LEAK CHECK GOOD.SDR UIEA2018091201955Controller · defectiveAFTER TAKEOFF LEFT BLEED PRESSURE SURGING FROM 35 PSI TO 0 EVERY 10 SECONDS. LT ENG HPSOV LOCKED CLOSED. REMOVED AND REPLACED HIGH PRESSURE CONTROLLER IAW AMM 36-11-08, OPS CK AND LEAK CK OK.SDR UIEA2018091201952Relief Valve · stickingLEFT ENGINE BLEED OFF INDICATION WHEN TURNING WING ANTI-ICE ON (DUCT PRESS 10 PSI). WHEN USING WING AND ENGINE ANTI-ICE ON DESCENT THE LEFT ENGINE BLEED OFF INDICATION ON EICAS. FOLLOW QRH AND RIGHT DUCT PRESS WAS NOT ENOUGH TO SUPPLY THE DEMAND FOR THE ANTI-ISDR UIEA2018091101946Shutoff Valve · malfunctionedDURING CRUISE RECEIVED EICAS RT ENG, QRH FOLLOWED, MESSAGE WENT AWAY HIGH STAGE. FOLLOWED IMMEDIATELY BY LT ENG HIGH STAGE. PERFORMED FIM 36-10 FAULT TREE 978 BLOCK 48. REMOVED AND REPLACED LT ENG HPSOV. OPS CHECK GOOD.SDR UIEA2018091201954Shutoff Valve · failedLEFT ENG PRSOV BITE FAILED. REMOVED AND REPLACED LEFT PRSOV, OP'S CHECK NORMAL. NO LEAKS IAW AMM 36-11-09.SDR UIEA2018090901928Valve · faultyAPU NOT SUPPLYING DUCT PRESSURE. REMOVED AND REPLACED APU BLEED AIR VALVE IAW AMM 36-11-10. OPS CHECK GOOD.SDR DALA2018091105548Fitting · damagedNR 2 PYLON PRE COOLER HAS DEBRIS IN INLET AND OUTLET. FOUND INBD AFT BUSHING AND FITTING DAMAGED. REPLACED INBD AFT BUSHING & FITTING ASSY PER BAC DWG 311N3654. INSTALLED SERVICEABLE PRE-COOLER AND REINSTALLED FAN AIR VALVE PER AMM 36-11.SDR P5CA2018091100218Shutoff Valve · failedPFM NR 1 ENG HEALTH CHK FOR PRSOV FOUND REGULATED FUNCTIONAL FAIL. IAW AMM 36-11-09-002-033-001 REV 125 AND AMM 36-11-09-402-058-001 REV 125 REPLACED NO 1 ENG PRSOV. IAW AMM 36-11-09-402-058 REV 125 STEP G PRM PRSOV TEST RESULT NORMAL. IAW AMM 36-11-09-402-058SDR P5CA2018091100269Precooler · damagedFOUND NR 2 ENG PRECOOLER OUTLET FINS FLAKED AWAY. IAW AMM 36-11-15-004-003-001 REV125 AND AMM 36-11-15-404-020-001 REV125 REPLACED NR 2 ENG PRE-COOLER. IAW AMM 36-11-09-782-138-001 REV 125 NO2 ENG PRE-COOLER LEAK CHECK.SDR QXEA2018090700322Ecu · malfunctionedAFTER TAKE-OFF NR 2 BLEED HOT CAUTION ILLUMINATED. CAUTION LIGHT WAS RESET VIA E&A CHECKLIST BUT RE-ILLUMINATED. BLEED HOT CAUTION NOT ILLUMINATED WITH BLEED SELECTED OFF. BLEED FLOW WAS SELECTED TO MIN FOR APPROPRIATE TIME FRAME PRIOR TO DEPARTURE (BLEED SYSTSDR UIEA2018090701924Circuit Card · not seatedLEFT ENG BLEED LIGHT ON DURING TAKEOFF AND INITIAL CLIMB. EXTINGUISHED APPROX 7 MIN AFTER TAKE OFF. NO EICAS MSG. NO FAULTS NOTED ON AIR SUPPLY BITE PER FIM 36-20-00. RERACKED LEFT BLEED AIR CONTROL CARD REF AMM 36-11-12. NO DEFECTS NOTED AT THIS TIME.SDR UIEA2018090501894Controller · malfunctionedOVERHEAD LEFT ENGINE BLEED LIGHT ILLUMINATED ON CLIMB OUT. NO EICAS MSG, REPLACED LT ENG HP CONTROLLER IAW AMM 36-11-08. OPS & LEAK CHECK OK.SDR UIEA2018090501895Circuit Card · dirtyLT ENG BLEED LIGHT ON, ON TAKEOFF ROLL NO EICAS MSG LIGHT GOES OUT AFTER FIRST POWER REDUCTION ALL PARAMETERS NORMAL. CLEANED PINS ON M859 LT BLEED AIR CONTROL CARD AT P50 PANEL. RE-RACKED. ALL OPS OK PER AMM 36-11-12. NO FAULTS ON BITE.SDR GTIA2018090202825Unknown · odorDIRTY SOCK SMELL DURING DECENT BELOW 10000 ISOLATED TO ENG 2 BLEED. PERFORMED TSM 02-50-00-810-831-A ISOLATED SMELL TO ENG 2 BLEED SEE ITEM 234709601 FOR CORRECTIVE ACTION AIRCRAFT OK FOR CONT SERVICE.SDR ASAA2018090526020Computer · malfunctionedCLASS II AIRBLEED MSG GROUNDED - YES. RESET BMC1 & BMC2 IAW AMM 36-11-00-740-001.SDR UIEA2018090401885Valve · malfunctionedLT ENGINE BLEED OFF MSG, FAMV FAULT. REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-16. PERFORMED TEST OK.SDR UIEA2018083001852Modulating Valve · faultyLEFT ENGINE BLEED INOP / (FAN AIR (PRECOOLER) CONTROL SYSTEMS. REMOVED AND REPLACED FAN AIR MODULATING VALVE IAW AMM 36-11-16 , PERFORMED OPERATIONAL TEST AND FAN AIR VALVE BITE TEST IAW AMM 36-11-16 NO FAULTS NOTED, THE SYSTEM WORKS NORMAL AT THIS TIME.SDR ASAA201808305964Unknown · unknownAIR ENG 1 BLEED FAULT GROUNDED - YES. PERFORMED BITE TEST ON BMC 1,2 IAW AMM 36-11-00-740-001 TESK OK A&P 3757417SDR KC8A2018090409118Modulating Valve · faultyTROUBLESHOT EXCESSIVE HEAT IN CABIN, FOUND LEFT ENGINE MODULATING SHUT-OFF VALVE DEFECTIVE, STAYING IN FULL PRESSURE BLEED. VALVE WAS NOT REGULATING CORRECTLY. REPLACED VALVE WITH REPAIRED VALVE, PERFORMED PRESSURIZATION OPERATIONAL CHECKS. NO DEFECTS NOTED. ASDR RAIA201808270001Clamp · unsecureBLEED 2 LEAK AT 20,000 FT IN ICING CONDITIONS. CHECKED SECURITY OF ALL BLEED 2 COUPLINGS. NO FURTHER LEAKS NOTED AT JOINTS 18, 20, 22, OR 24. SECURED 3 CLAMPS IN #2 PYLON AND REPLACED SEAL AT LOCATION 8. PERFORMED BLEED OPS CHECK WITH CREW.SDR QXEA2018082800311Warning Light · false activationAFTER V1, THE NR 1 AND 2 BLEED HOT CAUTION ILLUMINATED. UNABLE TO PRESSURIZE. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTEROGATED CDS AND FOUND FAULT CODES 7008 ON LT AND RT SIDE PERFORMED IAW FIM 36-10-00-810-857 AND 36-10-00-810-856.SDR SIMA20180826001Duct · leakingNR 2 BLEED LEAK, IN FLIGHT, MESSAGE STAYED PRESENT FOR AT LEAST 5 - 6 MINUTES BEFORE GOING AWAY. DIVERTED BACK TO DEPARTURE. FOUND THE DUCT IN THE NR 2 PYLON LEAKING, REMOVED AND REPLACED THE DUCT IAW AMM 36-11-09, OPS AND LEAK CHECKED GOOD.SDR ASAA2018082855927Warning Message · false activationCLASS II MAINTENANCE MESSAGE FOR THE AIR BLEED DISPLAYED, A & P 3687395. ACFT GROUNDED. RESET BOTH BMC IAW AMM 36-11-00, NO FAULT FOUND.SDR ASAA2018082835897Valve · faultedNR 2 ENGINE BLEED AIR ABNORMAL. HP VALVE FAULTED. ACFT GROUNDED.SDR SWIA2018082345007Shutoff Valve · failedAFTER TAKEOFF, SWAPPED BLEEDS FROM THE APU TO THE ENGINES AND THE NR 2 PACK SHUTOFF. THEN GOT A NR 1 PACK HIGH PRESSURE. LEVELED THE PLANE AT 10000, AND THE CABIN ALTITUDE BEGAN TO CLIMB. DECLARED THE EMERGENCY AND RAN THE QRH. A NORMAL LANDING WAS ACCOMPLISSDR UIEA2018082701811Shutoff Valve · malfunctionedLEFT ENGINE BLEED OFF. CYCLED PRSOV, OPS CHECK GOOD IAW MM 71-00-00.SDR SWAA2018082324549Regulator · faultyAIR TURNBACK, DURING CLIMB OUT AT APPROXIMATELY 21,000 CABIN WARNING HORN CAME ON-CABIN APPROXIMATELY 10-11000FT. DESCENDED AND RETURNED TO PHX. R&R NR 2 ENGINE HIGH STAGE REGULATOR PER MM.SDR SWAA2018082324548Regulator · faultyAIR TURNBACK, DURING CLIMB OUT AT APPROXIMATELY 21,000 CABIN WARNING HORN CAME ON-CABIN APPROXIMATELY 10-11000FT. DESCENDED AND RETURNED TO PHX. R&R NR 1 ENGINE HIGH STAGE REGULATOR PER MM.SDR SWAA2018082324547Shutoff Valve · leakingAIR TURNBACK, DURING CLIMB OUT AT APPROXIMATELY 21,000 CABIN WARNING HORN CAME ON-CABIN APPROXIMATELY 10-11000FT. DESCENDED AND RETURNED TO PHX. R&R NR 2 PRESSURE REGULATORY SHUTOFF VALVE PER MM.SDR P5CA201808220199Check Valve · damagedBOTH SIDE ISOLATION BYPASS CHECK VALVES INSIDE SPRINGS WERE BROKEN. REPLACED THE ISOLATION VALVE IAW AMM 36-11-05-004-002, AND AMM 36-11-05-404-009, REV 124. TESTED AND FOUND NO LEAKS IAW AMM 36-11-05-404-009, REV 124.SDR P5CA201808220200Duct · chafedCHAFING ON THE LIP SURFACE OF THE NR 2 ENGINE RT CORE COWL PRECOOLER EXHAUST DUCT. REPLACED THE DUCT IAW AMM71-11-06-714-014, AND AMM 71-11-06-714-013, REV 124.SDR P5CA201808220202Precooler · leakingFOUND THE NR 2 ENGINE PRECOOLER OUTLET PORT FINS FLAKED AWAY. REPLACED THE PRECOOLER IAW AMM 36-11-15-004-003 AND AMM 36-11-15-404-020, REV 124. LEAK CHECKED GOOD IAW AMM 36-11-09-782-138, REV 124.SDR P5CA201808220203Precooler · damagedFOUND THE NR 1 ENGINE PRECOOLER OUTLET PORT FINS FLAKE AWAY. REPLACED THE PRECOOLER IAW AMM 36-11-15-004-003, AND AMM 36-11-15-404-020, REV124. PRECOOLER LEAK CHECKED NORMAL IAW AMM 36-11-09-782-132, REV 124.SDR AALA2018082109028Warning Light · illuminatedNR 2 ENGINE BLEED FAULT, HOT ACRID ODOR WITH NOTABLE HEAT INCREASE IN COCKPIT TEMPERATURE NOTICED BEFORE THE NR 2 BLEED FAULT. NR 1 & 2 ENGINE BLEED SYSTEM OPS CHECKED GOOD IAW AMM 36-11-00-710-003A. ACCOMPLISHED J/C 26L00021001 WITH NO FINDINGS OF ODOR IAWSDR SWAA2018082024288Control Valve · stuckDIVERSION, JUST PRIOR TO LEVEL OFF LEFT "PACK TRIP OFF" ILLUMINATED. STARTED EMERGENCY DECENT. CABIN ALTITUDE WARNING HORN SOUNDED. FOUND PRECOOLER CONTROL VALVE STUCK CLOSED. R&R RIGHT ENGINE PRECOOLER CONTROL VALVE PER AMM.SDR FDEA2018081762048Warning Message · false activationREJECTED TAKEOFF, DUE TO A LT ENG BLEED OFF MESSAGE. DURING TAXI BACK, CREW PERFORMED SYSTEM TESTED IAW MM 36-11-00-5. COULD NOT DUPLICATE. OPS CHECKED OKAY. NO HISTORY IN PAST 30 DAYS.SDR UIEA2018081601715Controller · failedNR 2 ENG PRV CONTROLLER FAILED. PNUEMATIC HEALTH CHECK (PRESS NOT BTWN 47.65 AND 90 PSI. R&R NR 2 ENG PRV CONTROLLER OP & LK CHECK SATISFACTORY IAW AMM 361119 AND 710000. PASSED CHK PSI TASK CARD 6736A005-2.SDR UIEA2018081301678B-Nut · looseDURING CRUISE LEFT DUCT PRESSURE 10 PSI THE BLEED DISCRET LIGHT ON OVERHEAD PANEL CAME ON FOR SEVERAL SECONDS. REF LOG PAGE 0965172 ITEM 3. T/S BLEED SYSTEM AND FOUND LOOSE B NUT ON PRV SUPPLY PRESSURE LINE, TIGHTEN B NUT OPS CK WITH ENGINE RUNNING GOOD IAW FISDR ASAA201808135748Bushing · looseACCOMPLISHING T/C 78472000, ON THE NR 2 ENGINE, FOUND A LOWER SUPPORT LINK ON INTERSECTION MANIFOLD DUCT BUSHING DISLODGED. ACFT GROUNDED. REMOVED AND REPLACED SUPPORT LINK IAW AMM 36-11-01.SDR UIEA2018081301674Seal · damagedLEFT DUCT SHOWING 5 PSI IN FLIGHT AT CRUISE. RECONNECTED SEPARATED LT ENGINE PNEUMATIC SUPPY DUCT, AND REPLACED SEAL UPSTREAM OF LOW AND HIGH PRESSURE "Y" MANIFOLD PER MM CH 36-11-01. LK & OPS-CK GOOD ON ENGINE MX RUN IAW MM CH 71-00-00 AND CH 36-00-00.SDR UIEA2018081001646Shutoff Valve · malfunctionedRT ENG HPSOV EICAS MESSAGES. BLEED LIGHT ANNUNCIATION WHEN THRUST REDUCED. REPLACED RIGHT ENG HPSOV CONTROLLER IAW AMM 36-11-08, OPS CHECK. S/N OFF 2D17101114 P/N 773289-15. REPLACED RIGHT ENG HPSOV IAW AMM 36-11-07, OPS CHECK OK.SDR UIEA2018081301676Duct · separatedLEFT ENG BLEED OFF EICAS MESSAGE DURING FLIGHT. RECONNECTED SUPPLY DUCT, PERFORMED ENG RUNS IAW 36-11-00 AND 71-00. ALL OPS NORMAL.SDR DXTA201808231283Controller · malfunctionedDURING ENGINE START AT DESTINATION, HAD BOTH CYAN LEFT AND RIGHT BLEED FAULT CAS MESSAGES AFTER ENGINE START. VERIFIED ON GO, NO GO, OK. AFTER TAKEOFF AND AFTER WING ANTI-ICE SWITCH WAS PLACED ON THE TRIM AIR FAULT CAS MESSAGE AND WING ANTI-ICE CAS MESSAGSDR AALA2018081308014Controller · malfunctionedDURING FLIGHT, THE RIGHT ENGINE BLEED OFF LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED AND RETURNED TO DEPARTURE. THE AIRCRAFT WAS GROUNDED. REPLACED RIGHT REVERSE FLOW VALVE CONTROLLER IAW AMM 36-11-18.SDR AALA201808159034Duct · faultyAFTER TAKEOFF, TAIL COMPARTMENT TEMPERATURE LIGHT AND MASTER WARNING LIGHT ILLUMINATED. LIGHTS REMAINED ON APPROXIMATELY 10 SECONDS AFTER COMPLETING MEMORY ITEMS ON CHECKLIST. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO DFW. AIRCRAFT LANDED WITHOUT INCIDESDR AALA201808107007Valve · faultedAFTER TAKEOFF, TAIL COMPARTMENT TEMPERATURE LIGHT AND MASTER WARNING LIGHT ILLUMINATED. LIGHTS REMAINED ON APPROXIMATELY 10 SECONDS AFTER COMPLETING MEMORY ITEMS ON CHECKLIST. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. SDR ASAA2018080625694Warning Message · false activationBLEED AIR CLASS 2 MX MESSAGE. ACFT GROUNDED. PERFORMED BMC NR 1 BITE TEST IAW AMM 36-11-00, OPS CHECKED GOOD, NO FAULTS.
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