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 UIEA2018010900048Warning Message · false activationRIGHT ENGINE PRV STATUS MESSAGE AFTER BLOCK OUT. RT BLEED SYSTEM CHECKED GOOD IAW FIM 36-10 TREE 848. AIRCRAFT OK FOR CONTINUED SERVICE.SDR ASAA2018010823137Valve · failedDUCT PRESSURE SPLIT, RIGHT 22, LEFT 45, DURING CLIMB. ACFT GROUNDED. TROUBLESHOT THE NR 2 ENGINE IAW AMM 36-11-00, THE PRSOV FAILED THE TEST. REMOVED AND REPLACED THE NR 2 ENG PRSOV IAW AMM 36-11-04-000-801. LEAK CHECKED GOOD.SDR SIMA20180106001Pressure Switch · failedDURING TAKEOFF ROLL, A NR 2 BLEED FAIL ACTIVATED ON EICAS. AN ABORT WAS INITIATED AT 80KTS. REMOVED AND REPLACED PRESURE SWITCH IAW AMM 36-11-07 AND E2 REGULATOR VALVE IAW AMM 36-11-05 OPS CHECKED GOOD.SDR YENA201801060007Duct · contaminatedFLT 1095, BOS-PUJ. RETURNED TO FIELD (BOS). AFTER TAKEOFF CLIMBING THROUGH 10,000, FUMES SMELT IN COCKPIT & CABIN. DESCRIBE SMELL AS BURNING PLASTIC. CABIN CREW DESCRIBED SMELL AS ACRID SMELL DISSIPATED IN COCKPIT & FRONT HALF OF CABIN. SMELL REMAINED IN MIDDLSDR VQIA2018F00017Valve · failedNR 1 ENGINE BLEED FAULT IN FLIGHT. THE ENGINE BLEED WAS RESET SUCCESSFULLY IAW QRH 02.02A. PFR SHOWS AIR ENG 1 BLEED SFO CLOSED FAULT WITH FAILURE MESSAGE. PRESSURE REGULATOR VALVE. R & R PRV IAW AMM 35-11-52-790-001-A. LEAK CHECKED WITH NO DEFECTS NOTED.SDR VQI2018F00013Pressure Valve · failedFLIGHT VX1717 DAL-SFO HAD THE FOLLOWING DEFECT. AIR ENG 1 BLEED FAULT IN FLIGHT. ENG BLEED RESET SUCCESSFUL IAW QRH 02.02A. PFR SHOWS AIR ENG 1 BLEED SFO CLOSED FAULT WITH FAILURE MSG PRESS REG-V 4001AA1. R&R PRV FIN 4001HA1 IAW AMM 36-11-52-790-001-A. LESDR AALA20180107001Control Valve · failedBLEED TRIP OFF LIGHT ON CLIIMB OUT (RESET ) HAPPENED TWICE, CABIN ALTITUDE LIGHT AT 34,000 STAYED ON AFTER REDBOX DID EMERGENT DESCENT TO OK. AIRCRAFT WAS GROUNDED. TROUBLESHOOTING THE RIGHT BLEED AIR SYSTEM AND CABIN PRESSURE CONTROL SYSTEM. REPLACED PRECOSDR UIEA2018010500014Controller · failedNR 1 A/C PACK AND CLIMB TROUGH 4000, LT DUCT PRESSURE 3300, RT DUCT PRESSURE, 1500. DID NOT QUIT DOWN UNTIL APPROCH FL 240. PRESSURE CONSISTANT THROUGHT FLIGHT AT 3300 - 1500. R & R PRV CONTROLLER IAW AMM 36-11-14, OPS CHECKED GOOD, LEAK CHECKED MUSCLESDR FDEA201801030005Duct · looseVERY SHORTLY AFTER LEVEL OFF, AT FL330, THE NR 1 ENGINE FIRE WARNING DISPLAYED. BEFORE INITIATING PROCEDURES, THE WARNING DISAPPEARED WITHIN A SHORT PERIOD, LESS THAN 10 SECONDS, THE WARNING DISPLAYED AGAIN AND REMAINED ILLUMINATED. COMPLIED WITH THE PROSDR ASAA2018010123072Link · wornWHILE ACCOMPLISHING IGV RING INSPECTION ON THE NR 1 ENGINE, FOUND TWO WORN ATTACH LINKS FOR THE DUCT ABOVE THE HIGH STAGE VALVE. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACH LINKS IAW 71-00-02.SDR UIEA2018010200001Valve · malfunctionedRIGHT ENGINE PRV SATUS MESSAGE. OPS THE RT ENGINE PRV MANUALLY SEVERAL TIMES, CHECKED PRVC SOLENOID, OPS OK, AND CHECKED MUSCLE AIR LINE INTEGRITY, NO LEAKS NOTED. VALVE OPERATED NORMALLY WITH REVERSE FLOW. RAN THE RT ENGINE AS REQUIRED, PRV OPERATED NSDR DALA2018010400095Duct · crackedWHILE ATTEMPTING TO REMOVE AND REPLACED FAN DUCT TEMP SENSOR FOUND CRACKS IN MOUNTING FLANGE . WELDED AND REPAIRED THE DUCT.SDR HALA2017122700321Warning Message · false indicationNR 2 ENGINE BLEED NOT CLOSED, ECAM PROBLEM, RESET IAW QRH SUCCESSFUL. TROUBLESHOT IAW TSM 36-11. SYS CHECKED NORMAL. NO FAULTS. NO HISTORY, OK FOR SERVICE.SDR HALA2017122700320Pneumatic System · malfunctionedAIR NR 2 ENGINE BLEED NOT CLOSED ON THE NR 2 ENGINE SHUTDOWN. RESET THE NR 2 ENGINE BLEED SUCCESSFUL. PERFORMED TSM 36-11-81-810-837-A, NO DEFECTS NOTED. OK FOR SERVICE.SDR DALA2017122808986Valve · failedRETURNED TO DEPARTURE DUE TO THE NR 1 ENGINE BLEED OFF AND NO NR 1 ENGINE ANTI-ICE. PERFORMED PNEUMATIC HEALTH CHECK AND FOUND THE LT PRV FAILED, REPLACED THE LT PRV, PERFORMED COMPLETE HEALTH CHECK AND ENGINE RUN. AND PERFORMED OP CHECK OF LEFT PACK.SDR RAIA20171223002Duct · leakingBLEED 1 LEAK. SECURED THE LEAK AT DUCT 9, BLEED NR 1. OPS CHECKED WITH NO DEFECT NOTED.SDR UIEA2017122302429Controller · failedON LEFT ENGINE START, AN EICAS MESSAGE FOR THE LT ENG BLEED OFF. RETURN TO BLOCKS. REMOVED AND REPLACED THE LEFT ENGINE PRVC IAW AMM 36-11-09, PERFORMED A LEAK CHECK IAW AMM 36-11-09 AND ENGINE RUNS IAW AMM 71-00-00. OPS AND LEAK CHECKED OK.SDR ASAA2017122322997Clevis · looseNR 2 ENGINE LOOSE HARDWARE ON LOWER STARTER DUCT FWD TURNBUCKLE CLEVIS AT BRACKET. ACFT GROUNDED. REPLACED THE NR 2 ENGINE LOWER STARTER DUCT FWD TURNBUCKLE CLEVIS IAW POWERPLANT BUILDUP MANUAL 71-00-02 INSTALLED NEW HARDWARE AND BUSHINGS IAW FIG 25-1 SHEET SDR CALA2017122304574Duct · damagedLEFT ENGINE OVERHEAT ILLUMINATED, FOLLOWED QRH. NO ENGINE SHUTDOWN. EMERGENCY DECLARED. RIGHT ENGINE DUCT HAS A HOLE. REMOVED AND REPLACED RT ENGINE DUCT IAW 36-11-01 404-109-001. PERFORMED ENGINE RUNS, OPS CHECKED GOOD IAW 26-12-00-300-802C1.SDR FDEA201712223427Duct · leakingAT APPROXIMATELY 700 FT DURING FINAL, LEVEL 3 ENG 2 FIRE BELL AND WARNING STAYED ON FOR 3-4 SECONDS, THEN WENT OUT. MOVED THROTTLE TO IDLE AFTER SECOND WARNING AT 500FT. WARNING WENT OUT AGAIN. DECIDED TO LAND THE ACFT. IN THE FLARE, THE WARNING OCCURED ASDR 2018F00060Clamp · unsecureTAIL COMPARTMENT TEMP HIGH WARNING LIGHT COME ON DURING CLIMB. DURING TROUBLESHOOTING, FOUND THE LT COOLING TURBINE OULET DUCT LOOSE FROM THE CLAMP, REPOSITIONED THE PNEUMATIC DUCT AND SECURED THE CLAMP, PERFORMED OPS & LEAK CHECKS, NO LEAKS NOTED IAW IAW ASDR O2JA201801190001Clamp · looseSTRONG BURNING SMELL WITH STAB WING HEAT ON ACCOMPANIED BY SMOKE COMING FROM BAGGAGE COMPARTMENT AREA AFTER 5 MIN. GAINED ACCESS TO WING ANTI-ICE BLEED DUCT. FOUND BLEED TUBE SLEEVES CLAMPS LOOSE. TIGHTENED CLAMPS. WRAPPED INSULATION ON BARE METAL AREAS. RAN ASDR 2WAA20171222011Clamp · looseTAIL COMPARTMENT TEMP HIGH WARNING LIGHT CAME ON DURING CLIMB. DURING TROUBLESHOOTING, FOUND THE RT COOLING TURBINE OUTLET DUCT CLAMP LOOSE. REPOSITIONED THE PNEUMATIC DUCT AND SECURED THE CLAMP. PERFORMED AN OPS & LEAK CHECK, NO LEAKS NOTED IAW AMM 21-51-01SDR HNAA2017122000396Clamp · looseBLEED 1 LEAK EICAS MESSAGE AT 8500 FEET. TIGHTENED CLAMP ON ACM NR 1 BLEED LINE IN REF TO AMM 21-51-03. OPS CK GOOD. GOOD FOR SERVICE.SDR HALA2017122000307Sensor · malfunctionedRECEIVED A BLEED AIR LT FAIL, WHILE CLIMBING THRU 10,000. RETURNED TO DEPARTURE. REPLACED THE LT PM SENSOR IAW AMM 36-12-04. ENGINE RUN CHECKED GOOD. WIRING CHECKED FROM PM SENSOR TO PSC CHECKED GOOD.SDR ASAA2017121522935Sensor · failedDUCT PRESSURE SPLIT, L 19 PSI, R 42 PSI READINGS CONSISTENT IN CLIMB AND CRUISE.ACFT GROUNDED. WHILE ACCOMPLISHING T/C #NG-36WC-00001 STEPS 1 TO 5 (G) (2) SUSPECTED 450 DEGREE F THERMOSTAT FAILED AND PRECOOLER CONTROL VALVE SENSOR FAILED. R AND R THE 450 DEGRSDR RAIA201712130001Warning Message · false activationBLEED 2 LEAK EICAS IN ICING CONDITIONS. PERFORMED TROUBLESHOOTING CHECKS. NO FAULT FOUND.SDR IPXA2017121324480Control Panel · unknownINSPECTION TYPE:N/ADIVERSION - RIGHT ENG BLEED EICAS MSG&RIGHT BLEED LIGHT ON,BLEED AIR PANEL AND PRONOUNCED BURING SMELL,ACCOMPLISHED QRH PROCEDURES,ALL WENT AWAY.PERFORMED AMM 05-51-56-202-001 WHICH REFS FIM 21-00-01-301 AND PERFORMED ENG 1&2 RUN,NO BURNING SDR SIMA20171211006Unknown · odorAFTER TAKEOFF FLIGHT ATTN ADVISED CABIN FILLING WITH SMOKE LAV SMOKE WARNING ON EICAS. CONFIRMED APU IS NOT THE SOURCE OF THE ODOR. OPC APU IAW EMB AMM 49-13-00. OPC GOOD.SDR UIEA2017112802331Priority Valve · no testNR 2 ENGINE PRV FAILED THUMB CHECK. NR 2 ENGINE PRV REMOVED AND REPLACED IAW AMM 36-11-18 REV 122.SDR UIEA2017121302400Shutoff Valve · failedL ENG HPSOV FAILED.(<DIV>PERFORMED FIM 36-10-00 FT 833 AND WIRE CHECKS IAW WDM 36-11-61. NO FAULTS NOTED AT THIS TIME.</DIV>)SDR UIEA2017121202395Shutoff Valve · failedL ENG HPSOV CAUTION EICAS INTERMITTENT ON AT REPEAT TAKEOFF LEVEL OFF DESCENT , L ENG HPSOV STATUS MSG ON AFTER TAKEOFF (<P>REMOVED AND REPLACED L ENG HPSOV REF AMM 36-11-07 , PERFORMED AIR SUPPLY CONTROL SYS. BITE CHECK REF AMM 36-23-00 BITE OK PASSED. LEAK CSDR P5CA2017120800380Warning Message · false activationRIGHT ENGINE BLEED OFF EICAS MSG AT APPROX. 100KTS ON T.O ROLL QRH ACCOMPLISHED (<P>PERFORMED ASBM BITE PROCEDURE AND NO FAULTS NOTED , ALSO REVIEW HISTORY SHOWS R ENG BLEED NORMAL , NO MSG ON EICAS PER AMM 71-00-00 , A/C OK FOR SERVICE </P>)SDR UIEA2017120702373Control Card · malfunctionedL ENG HPSOV STATUS MSG ALSO L ENG HPSOV CAUTION MSG FOR 5 SECONDS AFTER TAKE OFF.(<P>RE-RACKED L ENGINE BLEED CONTROL CARD M859, OPS CHECK GOOD IAW B767 AMM 36-11-12 AND SWPM 20-82-13</P>)SDR 2017FA0000616Clamp · corrodedWHILE WORKING IN THE TAIL COMPARTMENT, THE MECHANIC NOTICED CORROSION ON A CLAMP ON BLEED AIR LINE 1159AC-20023-1 WHERE IT CONNECTS TO BLEED AIR LINE 1159AC-20044-7. CLOSE VISUAL INSPECTION REVEALED THE CLAMP TO BE SEVERELY CORRODED AND READY TO FAIL.SDR UIEA2017120302345Circuit Card · malfunctionedL ENG HPSOV EICAS MESSAGE AFTER TAKEOFF QRH PROCEDURE COMPLIED WITH. REMOVED AND REPLACED LH BLEED AIR CARD (M859) IAW AMM 36-11-12 PERFORMED OPS CHECKS ALL GOOD.SDR SIMA20171202002Bleed Valve · failed"BLD 2 VLV FAIL" MESSAGE ON EICAS AFTER TAKE OFF. "BLD 1 OVERTEMP" MESSAGE ON EICAS REDUCTION IN THRUST RETURNED TEMP TO NORMAL -C/A-DEFERRED BOTH BLEED VALVES MEL 36-4 AUTH 120021DM-C. REMOVED AND REPLACED #2 BLEED VALVE IAW AMM 36-11-05-400-801, MEL RESTOREDSDR SIMA20171202001Gasket · damagedBLEED 2 LEAK INDICATION @ 14,000 FT ON CLIMBOUT-C/A-TROUBLESHOT BLEED LEAK IAW FIM 36-21-00. FOUND RT ENG PRECOOLER AFT GASKET DAMAGED. RAR RT ENG PRECOOLER AFT GASKET IAW AMM 36-11-08. PERFORMED ENGINE RUN AT 80% FOR 15 MIN ON ENG #2 PER AMM 36-00-00. NO FURTSDR ASAA2017120122749Link · worn#1 ENGINE PNEUMATIC DUCT SUPPORT LINK ASSY'S ARE WORN AT BOTH ROD ENDS OF SUPPORT LINKS. GROUNDED - YES. REMOVED & REPLACED #1 ENGINE PNEUMATIC DUCT SUPPORT LINK ASSYS REF B737-800 AMM 36-11-01.SDR UIEA2017120402353Controller · malfunctionedREPEAT WRITE UP. AFTER T/O L ENG. HPSOV EICAS MSG, C/W QRH MSG REMAINED(<P>REMOVED AND REPLACED LH HPSOV CONTROLLER IAW AMM36-11-08.<BR /></P>)SDR CALA2017120104240Gasket · leakingENG 1 OVERHEAT LIGHT LIGHT IS ON ENGINE 1 OVERHEAT LITE ILLUMINATED IN FLT. RAN QRH - LITE WENT O UT AT 50.6N1. EMERGENCY DECLARED. FOUND LEAKING GASKET ON AIR LINE TO HPTACC .REPLACED GASKET REF IPC 75-00-00 PERFORMED 5 MIN HIGH POWER RUN OPS CK GOOD. NO FAULSDR UIEA2017120102338Line · looseDURING CLIMB OUT, HAD A LEFT ENGINE HPSOV EICAS MESSAGE. PERFORMED FIM 36-10 ,FAULT TREE 833, BLOCK 1, 20, 40, ALSO PERFORMED REVERSE FLOW CHECK IAW AMM 36-11-00. FOUND AIR LINE AT HPSOV LOOSE. TIGHTEN FITTING. LEAK CHECKED OK. RAN LEFT ENGINE IAW AMM 71-00-SDR AALA201712079031Shutoff Valve · faultyAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. MIA-GYE FLIGHT RETURNED TO MIA ACCOUNT AIRFLOW EXCESSIVE AND CABIN TEMPERATURE STUCK ON FULL COLD. OVERWEIGHT LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT ENGINE BLEED AIR REGULATOR PER AMM 36-11-03 (AALA201712010SDR AALA20171201001Regulator · faultyAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. MIA-GYE FLIGHT RETURNED TO MIA ACCOUNT AIRFLOW EXCESSIVE AND CABIN TEMPERATURE STUCK ON FULL COLD. OVERWEIGHT LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT ENGINE BLEED AIR REGULATOR PER AMM 36-11-03 AND LEFT ENGINSDR UIEA2017112802330Check Valve · chafedA/C BAY, RT ISOLATION BYPASS CHECK VALVE FOUND THE HOUSING CHAFDED. THE RT ISOLATION BYPASS VALVE WAS REMOVED, REPLACED, AND LEAK CHECKED IAW AMM 21-51-15, AND 36-11-00, REV 122. FOUND SATISFACTORY.SDR UIEA2017112702297Shutoff Valve · malfunctionedDURING CLIMB, THE LT ENG HPSOV MESSAGE ILLUMINATED, MESSAGE WAS PRESENT ONLY DURING CLIMB THRUST. AFTER QRH, THE LT ENGINE BLEED OFF, LT ENGINE HPSOV CONTINUED TO DISPLAY DURING HIGH THRUST SETTINGS, CLEARED AT CRUISE THRUST. REMOVED AND REPLACED THE LT HPSOSDR DELR20171129001Gasket · failedRIGHT ENGINE FIRE LIGHT CAME ON IN FLIGHT. FIRE EXTINGUISHER BOTTLE DISCHARGED.SDR ASAA2017112222712Shutoff Valve · failedDUCT SPLIT AT CRUISE. FL 350, N1 90, L-20, R-38. FL 370, N1 90, L-18, R-40. ACFT GROUNDED. WHILE ACCOMPLISHING TC NG-36WC-00001, FOUND PRSOV UNSERVICEABLE. REMOVED AND REPLACED PRSOV, REF B737-900 AMM 36-11-04/401. COMPLETED T/C NG-36WC-00001. OPS CHECK GOOD.SDR 9JLA2017120411023Duct · brokenTHE FLIGHT CREW FOR THIS AIRCRAFT DESCRIBED HAVING AN UNEXPLAINABLE DISPLACE OF THE RIGHT RUDDER PEDAL. THEY INDICATED THAT THE PEDAL DISPLACED ABOUT HALF TRAVEL IN FLIGHT. THE CREW WAS ABLE TO TRIM OUT THE YAW MOMENT AND CONTINUE THE FLIGHT. THE CREW BELIEVEDSDR ASAA2017112122662Link · wornWHILE ACCOMPLISHING A NR 1 ENGINE INLET INSPECTION, FOUND A WORN DUCT ATTACH LINK. SECOND LINK ABOVE THE HIGH STAGE VALVE. ACFT GROUNDED. REMOVED AND REPLACED THE LINK ASSEMBLY ON THE NR 1 ENGINE IAW CFM 71-00-02.
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