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 NACA2022010300006Not Reported · not reportedIDLE DISAGREE AFTER LANDING. CORRECTIVE ACTION SAME AS NACA2022010300005: FOUND PRV CONTROLLER SENSE LINE CHAFING, REMOVED AND REPLACED PRV CONTROLLER SENSE LINE IAW AMM 20-10-01 AND OPS CHECK NORMAL IAW AMM 78-31-00SDR NACA2022010300005Not Reported · not reportedRIGHT REVERSER DID NOT STOW AFTER LANDING. NOTE: RTL WOULD NOT ADVANCE FORWARD AFTER LANDING. REVERSER LIGHT WAS GREEN AND ONLY WHEN IT BECAME AMBER DID TL ADVANCE FAILED. FOUND PRV CONTROLLER SENSE LINE CHAFING, REMOVED AND REPLACED PRV CONTROLLER SENSE LINE SDR NACA2022010300004Not Reported · not reportedRIGHT DUCT PRESSURE @5 PSI, LEFT @ 20 PSI. PERFORMED FIM 78-34 FAULT TREE 810 AND FOUND NORMAL.SDR ASAA2021123137056Unknown · unknownWITH BOTH ENGINES RUNNING, BOTH PACKS AUTO ISOLATION VALVE AUTO, BOTH ENGINE BLEED VALVES ON, LEFT DUCT PRESSURE 0 PSI, RIGHT 20 PSI. GROUNDED - YES. PERFORMED B737-800 FIM 36-10 TASK 805 FOUND CONNECTOR ON BLEED AIR REGULATOR DISCONNECTED, RECONNECTED CONNECTSDR ASAA2021123037055Sensor · faultyAFTER TAKE OFF, L DUCT PRESS READ ZERO WITH # 1 ENG BLEED SWITCH ON. (PRESS READ NORMAL WHEN ISOLATION VALVE SWITCH POS TO "OPEN"). GROUNDED - YES. DIVERSION TIME 26 MINUTES. PERFORMED FIM PROCEDURE REF B737-800 FIM 36-10 TASK 805, REMOVED & REPLACED 450 DEGRESDR ASAA2021122737028None · inoperativeWHILE ACCOMPLISHING T/C 31-0005-00 FOUND SCHEDULED MAINTENANCE TASK MESSAGE (BLEED FAMV RVDT R) LATCHED. GROUNDED - YES. REF LP 60266761 REPEAT PLT SEAMC ANDT NOTIFIED THIS CLEARS PLT DEF.SDR ASAA2021122637027Unknown · faultyUPON COMPLETION OF TASK CARD 31-005-00 FOUND FAULT "BLEED FAMV RVDT R" (361-452-42). GROUNDED - YES. PERFORMED IFIM TASK 31-00-00-810-803, NO CORRELATED FAULTS NOTED. REPLACED #2 ENGINE FAMV PER AMM 36-12-03 PG# 401, SYSTEM TEST PASS, FAULT CLEARED. THIS CLEARSDR YENA2022010400005Heat Exchanger · leakingFLT 468, FLL-ATL (AIR TURN BACK TO FLL). BLEED 1 LEAK ON EICAS AFTER TAKEOFF AT ABOUT 13K FT ; ACCOMPLISHED FIM TASK 36-21-00-810-813-A FOUND DC4 GREASE (INCREASES CAPACITANCE CHANGES IMPEDANCE) ON LOOP3 L/H PACK CERAMIC PINS CHA & B . CLEANED & REPLACED CERASDR DALA2021122708052None · noneSHIP 3277 - ATO - DUE TO ENG 1 BLEED NOT CLOSED ECAM MESSAGE. CORRECTIVE ACTION: SECURED LOOSE SENSE LINE TO HPV. REPLACED PRV AND CONTROL THERMOSTAT. FAULT RETURNED. REPLACED SOLENOID TLT 10HA1. BLEED TEST OK. NO LEAKS NOTED. OK FOR SERVICE. (8266521)SDR FDEA202112223140Engine · damagedPDIS 609 36-10 1516 22DEC21 ICN OPEN U CLIMBING THROUGH 3500 COCKPIT FILLED WITH LIGHT GRAY SMOKE. DECLARED EMERGENCY, RAN APPROPRIATE CHECKLISTS, RETURNED TO INCHEON. DID NOT DUMP FUEL. NO OTHER ISSUES NOTED ENG 1 WAS CAUSE OF SMOKE. FACSDR ASAA2021122236976Unknown · leakingAFTER TAKE OFF, DUCT PRESSURES INDICATED 60 PSI LEFT SIDE, 10 PSI RIGHT SIDE. PRESSURIZATION WAS NORMAL. GROUNDED - YES. DIVERSION TIME 13 MINUTES. PERFORMING B737-800 FIM 36-10 TASK 811 FOUND #2 PRSOV LEAKING. REMOVED AND REPLACED #2 PRSOV REF B737-800 AMM 36SDR DALA2021122708073Shutoff Valve · faultedSHIP 649 IMMEDIATELY AFTER T/O GOT R ENG BLEED AND R PACK OFF MSGS AND LITES. DID QRH FOR RT BLEED OFF. BLEED MSGS RECURRED. NOTED ODOR FROM RT PACK PRIOR TO BLEED AND PACK ANOMALY. CORRECTIVE ACTION: PRESSURIZED PNEUMATICS W/ APU, RAN RT PACK FOR 30 MINS . NOSDR NACA2021122000001None · noneLH AC PACK CONNECTOR ASSY SEALS WORN. REMOVED AND REPLACED LH AC PACK CONNECTOR ASSY SEAL IAW AMM 36-11-01, NO LEAKS NOTED.SDR NACA2021121900001None · noneLEFT ENGINE PRV EICAS STATUS MESSAGE ILLUMINATED IN FLIGHT. PERFORMED EICAS MSG ERASE PROCEDURE PER AMM 31-41-00. L ENG PRV STATUS MESSAGE CLEARED. PERFORMED AIR SUPPLY STATUS BITE PER AMM 36-23-00, FOUND L PRV WIRE FAULT. REPLACED K/46 AIR/GROUND RELAY. AIR BSDR GTIA2021122036177Control Unit · faultedON CLIMB OUT RECEIVED AIR ENG 1 BLEED LEAK. PERFORMED AIR RETURN -PER TSM 36-22-00-810-803-A R&R #1 ENG PYLON OVERHEAT ELEMENT IAW AMM 36-22-15 AND R&R #1 ENG FAN AIR VLV CNTC-THERMOSTAT IAW AMM 36-11-43. PERFORMED HIGH POWER RUN IAW 71-00-00. NO LEAK OR FAULTSDR ASAA2021121536916Unknown · unknownOVHD MAINT LIGHT ILLUMINATED AFTER LANDING. GROUNDED - YES. FOUND FAULT BLEED FAMV L FAULT CODE 36112541 MAINTENANCE MESSAGE 36-12020. PERFORMED B737-9 IFIM TASK 36-12-00-810-801 AND PNEUMATIC ENGINE ON- SYSTEM TEST REF B737-9 AMM 36-00-00-736-801. SYSTEM TESTSDR DALA2021121607807None · noneSHIP 3266 RT PYLON UPPER IB CHANNEL CRACKED. CORRECTIVE ACTION: REPLACED RT PYLON UPPER I/B CHANNEL IAW A320 SRM 51-44-11. (2052030)SDR DALA2021121307678None · noneSHIP 8124 - DIV - TO JFK DUE TO L BLEED FAIL MESSAGE WITH ICING ENROUTE. CORRECTIVE ACTION: L BLEED MEL 36-12-05B APPLIED AND FLIGHT WAS CONTINUED.(8364192)SDR NACA2021121000001Isolation Valve · unknownDURING PRE-DEPARTURE SERVICE CHECK, FOUND LEFT ISOLATION VALVE CB POPPED OUT. REMOVED AND REPLACED LEFT ISOLATION VALVE IAW B767 AMM 36-11-04, OPS CHECK GOOD. NO PART INFORMATION AVAILABLE, VALVE NO LONGER IN SYSTEM.SDR DALA2021121307677None · noneSHIP 8137 - DIV - TO DFW DUE TO L BLEED FAIL MESSAGE WITH ICING ENROUTE. CORRECTIVE ACTION: L BLEED MEL 36-12-01B APPLIED AND FLIGHT WAS CONTINUED. (8267219)SDR DALA2021121007612Valve · shortedSHIP 3165 - DIV - TO BIL DUE TO DUE C/B FOR CROSS BLEED VALVE POPPED IN FLIGHT. COULD NOT CONTINUE DUE TO ICING CONDITIONS. REPORTED THAT VALVE FUNCTIONS IN MANUAL MODE BUT C/B POPS WHEN LEFT IN AUTO MODE. CORRECTIVE ACTION: REPLACED CROSS BLEED VALVE PER A319SDR NACA2021120700001None · noneLEFT ENGINEHPSOV EICAS MESSAGE APPEARED ON FINAL THEN WENT AWAY. STATUS PAGE SHOWS L ENG HPSOV. DEFERRED LEFT HPSOV PER MEL 36-11-02-02 CAT C ON 12-7-21@ 2157Z, MAINTENANCE PROCEDURES COMPLIED WITH.SDR 4DPA2021120500001None · noneISSUE-CREW EXPERIENCED PACK 2 OVERLOAD MESSAGE INFLIGHT. WITH POTENTIAL WEATHER IN THE DAL AREA CREW DECIDED TO RETURN TO MIA. CORR ACTION AFTER TROUBLESHOOTING DISCOVERED SLEEVE DISCONNECTED. RECONNECTED SLEEVE AND OPS TESTED NORMAL.SDR ASAA2021120136779Regulator · damaged#1 ENGINE BLEED AIR REGULATOR HAS DAMAGED WIRES. GROUNDED - YES. REMOVED AND REPLACED BLEED AIR REGULATOR REF AMM 36-11-03. OPS CHECK, LEAK CHECK GOOD.SDR IPXA2021120276554None · noneINSPECTION TYPE:N/A**ATB**NO EMERG ACTION** A/C LANDED W/OUT INCIDENT**AFTER TAKE-OFF THE FLIGHT CREW EXPERIENCED A LOSS OF THE RIGHT ENGINE BLEED SYSTEM. THE FLIGHT CREW PERFORMED AN AIR TURN BACK TO RFD & ARRIVED W/OUT INCIDENT.REMOVED AND REPLACED R/H REVERSDR IU6R2021113001Flapper Bearing · corrodedMALFUNCTION: FLAPPERS PN 3170719-2 WERE MODIFIED AS PER INSTRUCTIONS IN HONEYWELL SB 3202222-36-1888 IAW FAA AD 2020-16-51 IN FEB 2021, AND WERE INSTALLED ON CUSTOMERS AIRCRAFT. UNIT WAS RETURNED TO REPAIR FACILITY SHOWING SIGNS OF BINDING AND CORROSION.
PSDR ABXA20211124124Valve · faultedR ENG HPSOV EICAS AND STATUS MSG DURING FLIGHT. AFTER DEPARTING FROM C-CHECK. CREW ELECTED TO DO AN AIR TURN BACK TO TAMPA. MAINTENANCE GROUNDED THE AIRCRAFT, RIGHT HPSOV WAS REPLACED IAW 36-11-07 AMM. AIRCRAFT RETURNED TO SERVICE.SDR 2021F00362Duct · crackedFORWARD CARGO COMPARTMENT PNEUMATIC DUCT FOUND WITH 6" CRACK. REF NRC# B000386.SDR 21GA20211119001Cooling Duct · rupturedLEFT ENGINE FIRE MASTER WARNING MESSAGE AT FLIGHT LEVEL 260. SHUTDOWN LEFT ENGINE AND RETURNED TO AIRPORT. FOUND LEFT ENGINE LOW PRESSURE TURBINE CASE COOLING DUCT RUPTURED. REPLACED DUCT.SDR HNAA2021112900565None · nonePDIS 659 36-11 2572481 18NOV21 PHL CLOSE
BLD 2 LOW TEMP DISPLAYED ON DESENT WITH N2 ABOVE 86 PERCENT.
FACT 19NOV21 16:03 PHL
CMC MESSEGE PRECOOLER 2 TEMP CTL FAIL.R/R FAN AIR CONT THERMOSTAT.REQUIRES OPS CHECK.REF AMM 36-11-06.SDR ASAA2021111036569Regulator · failedPERFORM HEALTH CHECK ON NO. 2 ENG BLEED AIR SYS PER FOLLOW UP REPORT OF RIGHT BLEED PRESSURE FLUCTUATING. GROUNDED - YES. FOUND NO. 2 ENG HIGH STAGE REGULATOR AT FAULT PER T/C NG-36WC-00002-2 STEP 04(L). REMOVED AND REPLACED HIGH STAGE REGULATOR PER B737-900 ASDR DXTA2021111151650Sensor · defectiveLEED AIR: AT FL430 NORMAL ENGINE ONLY BLEEDS, PAX NOTIFIED US OF SMOKE/HAZE IN CABIN/ INITIATED QRC / UPON ENTERING CABIN I NOTICED A HAZE/ NO PERCEPTIBLE SMOKE/ BUT A SLIGHT ODER, DECLARED EMERGENCY/ DIVERTRED/ FOLLOWED QRC/QRH PROCEEDURES///SIGN-OFF////REMOVSDR ASAA2021110836548Regulator · inoperativeWHILE PERFORMING TASK CARD NG-36WC-00002-2, FOUND BLEED AIR REGULATOR'S SOLENOID NOT WORKING, ENGINE #2. GROUNDED - YES. REMOVED & REPLACED BLEED AIR REGULATOR IAW B737-900 AMM 36-11-03. OPS CHECK GOOD. NO LEAKS NOTED.SDR ABXA2021115109Valve · intermittentAFTER START L BLEED OFF EICAS MESSAGE WAS DISPLAYED BLEED SWITCH LIGHT ALSO ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED & REPLACED #1 ENG PRSOV IAW B767 AMM 36-11-09. OPS & LEAK CHECK GOOD; PERFORMED LEFT ENGINE RUN IAW AMM 71-00-0SDR ASAA2021103136460Precooler · inoperative#2 ENGINE FAN AIR VALVE SEAL DISLODGED AND SITTING ON TOP OF ENGINE CORE. REF B737-900 IPC 36-12-02-01A ITEM 30. (ATTACHED TO PRE-COOLER). GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE PRECOOLER VALVE REF. 36-12-02. GROUND OPS CHECKS GOOD. PERFORMED A FOD INSSDR ASAA2021102936531Valve · inoperative#2 ENG ANTI ICE INDICATING ON WHEN IT IS NOT DIM BLUE LIGHT ON WITH SWITCH IN OFF POSITION TAI SHOWS OFF, CAME ON AFTER LANDING. GROUNDED - YES. PERFORMED B737-800 FIM 30-11 TASK 803, DURING OPERATIONAL CHECK FOUND PRSOV NO SUPPLYING AIR PRESSURES TO ENGINE #2SDR NACA2021102900002Valve · unknownDISCREPANCY: LEFT ENGINE HPSOV EICAS MESSAGE ON SHORT FINAL, TURNED INTO A STATUS MESSAGE. NO CHANGE IN DUCT PRESSURE. CORRECTIVE ACTION: REPLACED LH HPSOV OPS CHECK NORMAL IAW AMM 36-11-06, ETOPS GROUND VERIFICATION COMPLIED WITHSDR NACA2021102900001None · noneDISCREPANCY: BOTH BLEED DUCT PRESSURES ERRATIC ON TAKEOFF THROUGH 8000 FT. LEFT PRESSURE FLUCTUATED OVER 30 PSI ACCOMPANIED BY LOUD WHOOSHING SOUND. PERFORMED FIM TASK 36-10-00 AND BITE CHECKED THE ASCTV NO FAULTS FOUND. SYSTEM OPERATES NORMALLY OK TO CONTINUESDR SIMA20211028001None · noneCLIMBING OUT OF RNO AT 300 FT AGL BLEED 1 AND 2 OVERPRESSURE EICAS MSG RECEIVED. FOLLOWED QRH PROCEDURE BOTH OVERPRESSURE MSG CAME BACK. RETURNED TO RNO. MAX PRESSURE WAS 100 PSI.DECLARED EMERGENCY FLT CONT. -C/A-CMC FAULT CODE 36146225AM1. PERFORMED ENGINE BLSDR AALA202110269196Regulator Valve · faultyAIRCRAFT WAS GROUNDED: ICING RESTRICTION AND ENGINE 2 BLEED FAULT AT 36000 FT, QRH RESET INEFFECTIVE; FLIGHT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED BLEED PRESSURE REGULATOR VALVE WITH SERVICEABLE UNIT IAW AMM 36-11-52-400-042-A6, LEAK AND OPS CHSDR NACA2021102300002None · unknownDISCREPANCY: DUCT PRESSURE GAUGE INDICATES 15 PSI DIFFERENCE BETWEEN RIGHT AND LEFT. RIGHT IS 15 PSI LESS THAN LEFT AT TAKEOFF AND CLIMB POWER. CORRECTIVE ACTION: REMOVED AND REPLACED RH PRSOV IAW AMM 36-11-09. OPS CHECK GROUND CHECK ETOPS VERIFICATON OK.SDR NACA2021102300001None · noneDISCREPANCY: PER CUSTOMER REQUEST REMOVE AND REPLACE RH PRSOV FILTERS. CORRECTIVE ACTION: REMOVED AND REPLACED RH ENGINE PRSOV FILTERS IAW AMM 36-11-09 OPS AND LEAK CHECK GOOD, ETOPS GROUND VERIFICATION COMPLIED WITH.SDR HNAA2021102600524None · nonePDIS 699 36-11 2600211 23OCT21 PHL CLOSE
BLEED 2 OVERTEMP DISPLAYED ON EICAS.
FACT 23OCT21 16:02 PHL
R+R E2 AIR VAILVE FILTER IAW AMM EMB 145 36-11-03, R+R E2 HSV FILTER IAW AMM EMB 145 36-11-02. OPS CHECK IAW AMB AMM 145 36SDR ASAA2021102336392None · wornWHILE PERFORMING T/C 78472000 ENGINE INLET AND FAN BLADE DETAILED INSPECTION FOUND INTERSECTION MANIFOLD DUCT SUPPORT LINK WORN TO POINT OF BALL ON ENGINE END HAS FALLEN OUT OF LINK. GROUNDED - YES. REPLACED INTERSECTION MANIFOLD DUCT SUPPORT PER POWERPLANT BUSDR YENA2021102100709Bleed Air Sys · looseFLT # 1937, SJU-SDQ(AIR TURN BACK TO SJU). BLEED 2 INOP (FAIL) RESET TWICE PER QRH ; FOUND MULTIPLE BLEED LINES LOOSE. REAJUSTED CLAMP LINES IAW AMM 36-11-08. PERFORMED ENGINES RUN. OPS CHECK OKAY. SEE LOG PG. 3188041 ITEM 1 AND 2 FOR R/R OF RH ENG FAN AIR VLVSDR NACA2021101400001None · noneDISCREPANCY: STATUS SCREEN LH PRV DISPLAYED. CORRECTIVE ACTION: ERASED STATUS MSG L PRV PER AMM 31-44-00. MSG CLEARED AND BITE AIR SUPPLY MODULE 36-23-00, NO FAULT FOUNDSDR ASAA2021100836229Tube · damagedON CLIMB OUT DUCT PRESSURE SPLIT RIGHT PRESSURE FLUCTUATED 40-45 PSI, LEFT PRESSURE PEGGED @ 80 PSI. ON CLIMB PHYSIOLOGICAL SENSING IN EARS WITH A PULSING SENSATION. GROUNDED - YES. DIVERSION TIME 38 MINUTES - ACCOMPLISHED NO. 1 ENG BLEED AIR SYSTEM HEALTH CHESDR ASAA2021100836228Valve · faulty"MAINT" LIGHT ILLUMINATED AFTER LANDING. GROUNDED - YES. CHECKED AND FOUND STATUS MESSAGE - BLEED FAMV R MAINT MSG 36-12021. CHECKED AND FOUND FAMV FAILED IN OPEN POSITION. DUE TO HISTORY REMOVED AND REPLACED #2 ENG FAN MODULATING VALVE REF B737-9 AMM 36-12-03SDR DALA2021100406030None · noneSHIP 3226 AIR ENG 1 BLEED FAULT WHICH CAUSED A DIVERSION. CORRECTIVE ACTION: R/R #1 ENG BLEED PRESSURE REGULATOR VALVE PER A320 AMM 36-11. OP CHECK GOOD AND LEAK CHECK GOOD. PREFORMED VISUAL OF THE SENSE LINE ON ENGINE #1 FOUND NO LOOSE LINE. OK FOR SVC. (5362SDR QXEA2021100400461None · noneABORTED TAKE OFF DUE TO ILLUMINATION OF #2 BLEED HOT CAUTION - ABORTED OCCURRED BELOW 70 KIAS, NO REVERSE AND MINIMAL BREAKING APPLIED. REMOVED FROM SERVICE. INTERROGATED CDS. FOUND FAULT 1006-R NAPRSOV. COMPLIED WITH FIM 36-10-00-810-801. REPLACED RIGHT NACEL
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