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 C77A20161121002Seal · damagedAIR RETURN - NR 1 ENGINE FIRE WARNING OCCURRED ON CLIMB OUT AND FIRE BOTTLE A WAS USED AND AN EMERGENCY WAS DECLARED. THE QRH 6.5 WAS FOLLOWED AND THE MESSAGE CLEARED, PARAMETERS WERE NORMAL, NO VIBE. FIRE TRUCKS MET THE AIRCRAFT AT THE RUNWAY. THE AIRCRAFT WASDR ASAA2016111818746Duct · damagedREF T/C 78472000, NR 1 ENGINE, NOSE COWL TAI DUCT AT 12 O'CLOCK STRUT AREA HAS DAMAGE/TORN INSULATION BLANKET. GROUNDED, YES. REMOVED AND REPLACED NR 1 ENGINE INLET COWL TAI DUCT ASSY, REF PP BUILD-UP MANUAL 71-00-02. OPS AND LEAK TEST GOOD, REF B737-900 AMM 3SDR SWAA2016112109888Line · leakingCABIN PRESSURE CONTROL WARNING HORN SOUNDED. EMERGENCY DECLARED AND RETURNED TO DEPARTURE. R & R NR 2 ENGINE PNEUMATIC BLEED DISTRIBUTION SENSE LINE IAW MM.SDR IXXA20161214214Line · corrodedPNEUMATIC LINE FUSELAGE BS 1396 CORRODED ON SURFACE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS IAW 20-10-09, SECTION 4.2D, TABLE FIGURE 804.SDR RAIA201611140001Clamp · looseBLEED 2 LEAK ON CLIMB OUT. TIGHTEND CLAMPS ON THE NR 2 PRECOOLER. PERFORMED GROUND RUN, OPS CHECKED GOOD IAW AMM 36-11-04 AND 36-00-00.SDR 2016FA0000566Insulation · missingFURTHER TO PYLON INSPECTION FOR SPIGOT RETROFIT, THE FOLLOWING NON CONFORMITY WAS FOUND. THE PRECOOLER EXCHANGER INSULATIONS PN L0003009100400 AND L0003009100900 WAS FOUND MISSING. TORQUE MARK WAS NOT PRESENT ON FAV ACTUATOR 12HA3 PN 1773B010000 IN LINE WITHSDR SWIA201642800Sensor · malfunctionedRIGHT ENGINE BLEED AIR DUCT WARNING MESSAGE AT 4000 FEET AND AGAIN AT 7500 FEET. RAN QRH. REMOVED AND REPLACED BLEED LEAK SENSING ELEMENT A46WK FOR RT ENGINE IAW AMM.SDR HALA2016110600511Filter · cloggedATB, INTERMITTENT ENG 1 BLEED FAULT DURING CLIMB OUT. T/S IAW TSM 36-21-00-810-925-A22, FOUND FAN-AIR VALVE CONTROL THERMOSTAT FILTER CLOGGED. CLEAN FLITER CHECK GOOD. OK FOR SVC.SDR AALA201611029002Regulator Valve · faultyAIRCRAFT WAS GROUNDED: IN DESCENT AT FL 220 RECEIVED HIGH CABIN ALT ECAM, CAB ALT 9600. DESCENDED AND RECOVERED CAB ALT TO NORMAL RANGE. REPLACED PRESSURE REGULATOR VALVE CONTROL SOLENOID (10HA2) ON ENGINE NR 2 AMM 36-11-55. LEAK CHECK OK. AND REPLACED ENSDR AALA201611029001Solenoid · faultyAIRCRAFT WAS GROUNDED: IN DESCENT AT FL 220 RECEIVED HIGH CABIN ALT ECAM, CAB ALT 9600. DESCENDED AND RECOVERED CAB ALT TO NORMAL RANGE. REPLACED PRESSURE REGULATOR VALVE CONTROL SOLENOID (10HA2) ON ENGINE NR 2 AMM 36-11-55. LEAK CHECK OK. REPLACED ENGINESDR QXEA2016102700682Shutoff Valve · malfunctionedSMELLED FUMES OUT OF VENTS DURING DESCENT IN TO SEA. SMELL WAS CONFIRMED IN CABIN AS WELL BY FA. LANDING UNEVENTFUL. FOUND R HPSOV FAULT. REMOVED AND REPLACED NR 2 HPSOV IAW AMM 36-11-09-000/-400-801. OPS CHECKS GOOD. C/W ECMP BLEED AIR OPERATIONAL CHECKSDR DXTA2016102606323Warning Message · false activationAFTER TAKEOFF WITH ENGINES AT CLIMB POWER, THE LT PYLON BLEED LEAK RED CAS MESSAGE CAME ON. THRUST LEVER WAS REDUCED TO IDLE PER CHECKLIST. AFTER APPROX 1 MINUTE THE MESSAGE CLEARED. ENGINE WAS LEFT AT IDLE WHILE WE RETURNED FOR LANDING.SDR ASAA2016102518465Shutoff Valve · failedDIAGNOSTICS REPORTED THE NR 2 ENGINE HAS A SHIFT IN CRUISE EGT, CRUISE FUEL FLOW, AND EGT HOT DAY MARGIN. PNEUMATIC/BLEED SYSTEM LEAKS ARE SUSPECT. ACFT GROUNDED. ACCOMPLISHED AND COMPLETED STEP 3 OF TSR, NOSE COWL ANTI-ICE VALVE OPERATION, NO DEFECTS NOTESDR R61A201610230609Pressure Switch · malfunctionedDURING FLIGHT, CREW RECEIVED A BLEED 1 OVER PRESSURE MESSAGE,RAN QRH. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED HPSOV HIGH PRESSURE SWITCH IAW AMM AND OPS CHECKED GOOD.SDR SIMA20161019001Thermostat · failed"BLEED 2 OVERTEMP" IN FLIGHT, REMOVED AND REPLACED NR 2 FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06, OPS CHECK GOOD. THERMOSTAT FAN AIR CONTROL, ENGINE P/N 816624-13 S/N 9911083SDR RAIA201610170001Duct · leakingNR 1 BLEED LEAK AFTER TAKE OFF. REMOVED AND REPLACED NR 1 BLEED DUCT IN AFT CARGO BAY UNDER FLOOR. OPS CHECKED GOODSDR CALA2016101700763Clamp · looseSINGLE CONTROLLER FAILURE ON BOTH PACKS. PACK LIGHT CAME ON AND RESET MULTIPLE TIMES. ERRATIC CABIN VVI. LEVELED OFF AT 180FL AN RETURNED TO DEPARTURE FIELD. T/S FOUND BLEED MANIFOLD CLAMP LEAKING, RETORQUED CLAMP PER AMM 36-11-00. BITE PACK CONTROLS NO FSDR SIMA20161016003Bleed Valve · failedAFTER TAKE-OFF, RECEIVED BLEED 1 LEAK EICAS MESSAGE. RAN THE CHECK LIST AND RETURNED TO DEPARTURE. FOUND ENGINE BLEED VALVE TO BE BAD. REMOVED AND REPLACED LT ENGINE BLEED VALVE IAW AMM 36-11-05-000-801-A AND 36-11-05-400-801-A. OPS CHECKED GOOD NO DEFECTS NSDR IPXA2016101709503Controller · failedLEVEL 3 AIR MANIFOLD NR 2 FAILED. EMERGENCY DECLARED. RETARDED THROTTLE TO IDLE . ALERT WENT AWAY. OPERATED THE NR 2 ENGINE AT REDUCED THRUST. TROUBLESHOT IAW FIM 36-23-01. REMOVED AND REPLACED MANIFOLD FAIL DETECTOR CONTROLLER. OPS GOOD IAW AMM 36-23-01-0SDR CALA2016101200754Clamp · unsecureLOSS OF CABIN ALTIITUDE CONTROL, CABIN CLIMBING ERRATICALLY. EMERGENCY DESCENT AND DIVERSION. BLEED LOSS WING R EICAS ADVISORY BLEED AIR SUPPLY VALVES ARE LATCHED CLOSED OR THE RESPECTIVE SWI TCHES ARE OFF, SO THAT BLEED AIR IS NOT SUPPLIED TO THE RT WAI, RT SDR ASMF201611019Shutoff Valve · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DUCT PRESSURE LOW INDICATION IN THE RIGHT ENGINE, SHOWING 5 PSI. MAINTENANCE PERSONNEL PERFORMED REVISION IAW 36-11-00, DETECTING A PNEUMATIC LEAK IN THE RIGHT ENGINE PRSOV. THE RIGHT ENGINE PRSOV AND THE RIGHT PRECOOLER SDR MASA2016092512416Warning Light · illuminatedLEFT BLEED DUCT WARNING DURING FLIGHT.SDR UIEA2016091500760Controller · malfunctionedRT ENGINE PRV EICAS MESSAGE. REMOVED AND REPLACED RT ENGINE PRESSURE REGULATOR CONTROLLER ASSY IAW AMM 36-11-19 OPS & LEAK CHECKED GOOD.SDR CALA2016091400650Valve · damagedFL 390, CABIN ALTITUDE WARNING HORN AND LIGHT, PRECEDED BY RIGH T BLEED TRIP OFF LIGHT. PERFORMED NR 2 ENG HEALTH CHECK IAW AMM 36-11-00-700-803, REPLACED THE NR 2 ENG HIGH STAGE VALVE IAW AMM 36-11-06.SDR ASAA2016091217994Shutoff Valve · failedWITH BOTH PACKS IN AUTO AND BOTH BLEED SWITCHES ON, THE LEFT BLEED DUCT PRESSURE READS 20 PSI AND THE RIGHT READS NEAR ZERO. ACFT GROUNDED. PERFORMED PNEUMATIC SYSTEM TROUBLESHOOTING IAW AMM 36-11-00, FOUND PRSOV NOT OPERATING CORRECTLY. REMOVED AND REPLACEDSDR VNAA2016091100009Bellows · leakingCLIMBING OUT OF 24500, THE CREW RECEIVED A RT RED BLEED DUCT CASS MESSAGE FOLLOWED BY AN AMBER RT DUCT BLEED MESSAGE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LEAKING BELLOWS AND PERFORMED CHECKS IAW THE AMM. THSDR IPXA2016090908046Shutoff Valve · defectiveRIGHT PACK OVERTEMP AND LT ENG BLEED MESSAGE AND LOSS OF PRESSURIZATION. PERFORMED RAPID DESCENT TO FL 100 AND RETURNED TO DEPARTURE. FOUND RT ENGINE ANTI-ICE DUCT LEAK REF L/P 222523, ITEM 1. PERFORMED PNEUMATIC HEALTH CK ON LT & RT ENGINE REF W2468453. FSDR RAIA201609080001O-Ring · wornAT 10 FT, RECEIVED A BLEED 1 LEAK IN FLT AND WOULD NOT GO AWAY. REPLACED THE O-RINGS AT COUPLINGS 5, 9, 13, 15, 21 IAW AMM 36-11-10. TOURQED CLAMPS AT PRE-COOLER IAW AMM 36-11-04. LEAK CHECKED GOOD IAW AMM 36-00-00.SDR UIEA2016090900752Unknown · malfunctionedRIGHT ENGINE PERFORMED BITE ON PNEU CONTROLLER, FOUND RT PRV FAULT. RESET BOX, FOUND NO FAULTS, CLEARS EICAS MSG PERFORMED ADJ TEST IAW 36-11-18, PRV OPS NORMAL.SDR UIEA2016090800751Shutoff Valve · failedDURING TROUBLESHOOTING OF THE RIGHT BLEED, THE LEFT HPSOV FAILED A BITE CHECK ON THE PNEUMATIC CONTROLLER. REMOVED AND REPLACED THE LEFT HPSOV IAW AMM 36-11-07 OPS CHECKED GOOD.SDR ASAA2016090217910Warning Light · false activationRIGHT PACK BLEED OFF STAYED ILLUMINATED. BLEED TRIP DID NOT RESET PER QRH. LIGHT CAME ON BETWEEN 6000-7000 FEET BEFORE LANDING. ACFT GROUNDED. PERFORMED TASK CARD NG-36WC-00001. NO DEFECTS NOTED. DUE TO HISTORY REMOVED AND REPLACED RT PRE COOLER CONTROL VALSDR P5CA2016090200251Shutoff Valve · malfunctionedEICAS MESSAGE RT ENGINE HPSOV ITEM TRANSFERED TO MDDR. REOPEN 69668 IAW MEL 36-11-02-02, CAT-C PLACARD INSTALLED. PERFORMED FIM 36-10 FT 833 AIR SUPPLY BITE TEST NO FAULTS NOTED. CHECKED WIRING, NO DEFECTS NOTED, ALSO CHECK HPC AND HPSOV WIRING NO DEFECTS NSDR P5CA2016090100250Controller · faultyFOUND NR 2 ENGINE HPSOV EICAS MESSAGE IAW AMM TASK 36-11-08-004-006-007, 404-014-007, REV 119. REPLACED ENGINE HIGH PRESSURE CONTROLLER. ENGINE RUN TEST NORMAL NO MESSAGE SHOWN.SDR MASA2016082912343Warning Message · illuminatedRT BLEED DUCT WARNING, RETURN TO FIELD.SDR SIMA20160829001O-Ring · leakingAT 37000 FT, RED BLEED 1 LEAK INDICATION AND EICAS MESSAGE. EXTINGUISHED DESCENDING THROUGH 24000 FT. REPLACED O-RING AT JOINT 21 IAW AMM 36-11-10, LEAK CHECKED GOOD.SDR P5CA2016082900243Controller · malfunctionedFOUND RT ENGINE HPSOV EICAS MSG IAW AMM TASK 36-11-08-004-006-007, REPLACED NR 2 ENGINE HPC AND CONDITION CHECK, NORMAL IAW AMM TASK 71-00-00-795-034-H03, REV 119 PFM NR 2 ENGINE IDLE RUN TEST AND CONDITION CHECK NORMAL NO MSG SHOWS.SDR P5CA2016082500240Controller · defectiveRIGHT ENGINE HPSOV EICAS. TRANSFERRED TO MEL 36-11-02-02, CAT C. R & R HP CONTROLLER REF AMM 71-00-00-795. OPS CHECK NORMAL MDDR 69668, CLEARED.SDR HALA2016082400334Valve · malfunctionedLT ENG BLEED VALVE DID NOT OPEN AFTER ENGINE START. TROUBLESHOT IAW FIM 36-11-00, CYCLED NR 1 ENGINE PRV AND CHECKED CONTROLLER CONNECTOR. BITE CHECK ON AIR SYS PANEL FAULTS PRV, RESET SAME. RAN NR 1 ENGINE OP CHECKED OK. OK FOR SERVICE.SDR SWIA201642479Bleed Air Sys · overpressuredBLEED 2 OVER PRESSURE DIVERTED. CREW FOLLOWED QRH. EMERGENCY DECLARED. COMPLIED WITH SERVICE LETTER SNL 170-36-0021.SDR CALA2016082300566Shutoff Valve · failedDURING CRUISE FL380, APPROXIMATELY ONE HOUR INTO FLIGHT, THE CABIN PRESSURE ROSE AND ALTITUDE CABIN ALT WARNING. EMERGENCY DESCENT PERFORMED. REPLACED THE NR 1 ENGINE PRSOV, RAN ENGINE PER FIM WITH NO FAULTS NOTED.SDR P5CA2016082300237Engine · malfunctionedRIGHT DUCT PRESSURE DURING CLIMB THRUST 70 PSIL, NORMAL AT 40 PSI. DURING CRUISE LT & RT 36 PSI. PRESSURIZED LT AND RT PNEUMATIC SYS DURING CH 71 TEST NR 1, 3, 4, 5, 8, 9,& 10. NO FLUCTUATIONS NOTED. OPS CHECKED FOUND TO BE SATISFACTORY IAW AMM 36-00-00-8SDR VNAA2016081800019Shutoff Valve · faultyRIGHT ENGINE BLEED CAUTION ON TAKEOFF. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE 10TH STAGE HIGH PRESSURE SHUTOFF VALVE, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.SDR UIEA2016081800688Warning Message · false activationRIGHT ENG PRV STATUS MESSAGE. PERFORMED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20-00/104. NO FAULTS NOTED, EICAS MESSAGE CLEARED.SDR P5CA2016081700198Shutoff Valve · closedRIGHT ENGINE HPSOV EICAS MESSAGE. RAN QRH PROCEDURE. RIGHT ENGINE HPSOV LOCATED IN THE CLOSED POSITION. CARRIED OUT TROUBLESHOOT IAW FIM36-10, R & R HPSOV IAW AMM 36-11-07/401 AND LEAK, OPS CK OK WITH ENGINE RUN.SDR IPXA2016081707135Shutoff Valve · inoperativeEICAS FOR RT ENGINE HPSOV, LIGHT ON STEADY DURING CLIMBOUT. RT ENG BLEED LIGHT ILLUMINATED, AND DUCT PRESSURE FLUCTUATED.SDR UIEA2016081800686Warning Message · false activationRIGHT ENGINE PRV STATUS MESSAGE. PERFORMED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20-00/101 FIG 104. NO FAULTS NOTED, EICAS MESSAGE CLEARED.SDR COZA20160815086Sensor · faultyDURING GROUND ENGINE RUN NOTICED A DUCT PRESSURE SPLIT WITH RIGHT SIDE LOW. TROUBLESHOT USING FIM. REPLACED RIGHT 450 DEG THERMOSTAT SENSOR. PERFORMED ENGINE RUNS AND CONFIRMED DUCT PRESSURES MATCHED.SDR COZA20160815089Sensor · intermittentRIGHT BLEED TRIP OFF LIGHT AT FL340 DURING AIRCRAFT CLIMBOUT. USING FIM, REPLACED THE RIGHT 390 DEG TEMPERATURE SENSOR. OPERATIONAL AND LEAK CHECK OK.SDR COZA20160815088Sense Line · leakingRIGHT BLEED TRIP OFF LIGHT AT FL340 DURING CLIMBOUT. FOLLOWING FIM, LEAK CHECKED LINES ASSOCIATED WITH BLEED SYSTEM ON THE RIGHT SIDE. FOUND PRECOOLER VALVE SENSE LINE LEAKING AT END SWAGE. REPLACED LINE AND LEAK CHECK OK.SDR COZA20160815087Shutoff Valve · intermittentRIGHT BLEED TRIP OFF LIGHT AT FL 340 DURING AIRCRAFT CLIMBOUT. REPLACED RIGHT PRESSURE REGULATING AND SHUTOFF VALVE. LEAK AND OPERATIONAL CHECK OK.
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