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 P5CA2018121320381Duct · low pressureDURING CRUISE WITH ANTI-ICE ON L DUCT PRESS DROPS TO 5 PSI WITH INTERMITTENT L BLEED OFF EICAS.(<P>T/S PER FIM 36-10 F/T 837. CKD ALL LINES FOR PROPER CONDITION RE-TORQUE ALL B NUTS CKD WIRING CLEANED CONNECTOR RAN ENG NO FAULTS, A/C OK FOR SERVICE.</P>)SDR AALA20181213001Controller · malfunctionedFLT 206 EN-ROUTE MIA - MXP. THE AIRCRAFT WAS GROUNDED. LT ENG PRV EICAS MSG. QRH PROCEDURE COMPLIED WITH. MSG ACCOMPANIED W/LOSS OF LT DUCT PRESS. WOULD NOT RESET HAPPENED ON CLIMB OUT LIGHT STAYED ON DUCT PRESS STAYED LOW UNTIL SHUT DOWN. MAINTENANCE REMSDR P5CA2018121200378Duct · low pressureW/ ENGINE ANTI-ICE ON LEFT DUCT PRESSURE DROPS TO 7 PSI AND MOMENTARILY L ENG BLEED OFF EICAS(<DIV>NO FAULT SHOWN IN STATUS PG. BITE CHK IN THE AIR SUPPLY BITE MODULE, NO FAULT IAW AMM 36-23-00-715. ITEM CLOSED, OKAY TO CONTINUE.</DIV>)SDR CALA2018121102555Wire Harness · shorted2 ENGINE BLEED TRIP OFF LIGHT ON STAYS ALLUMINATED AFTER CHECKLI ST CONTACT TOMC UNLOCKED FOR UPDATE REMOVED CANNON PLUG D528(OVER TEMP SWITCH), WOULD NOT RESET. REMOVED CANNON PLUG D30184, RESET BLEED LIGHT, LIGHT WENT OUT. REMOVED CANNON PLUG D30404 AND FOUNSDR FDEA201812073451Warning Message · false activationDURING CLIMBOUT BELOW 18000 FEET RECEIVED LVL 1 AIR SYS OFF ALERT. AT FIRST SYSTEM 2 WENT FROM RED ON SYNOPTIC BUT QUICKLY TURNED AMBER. C/W PNEUMATIC MANIFOLD 2- ESC LRU INOP, RESET IAW AMM-21-08-01-5 AND ECS RTS, TEST PASSED. C/W NR 2 PNEUMATIC SYSTEM DESDR HALA2018120600634Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - ECAM: ENGINE AIR BLEED NOT CLOSED NR 2 ENG. REMOVED AND REPLACED NR 2 ENG PRV PER AMM 36-11-52. OPS CK & LEAK CK OK. A/C OK FOR SVC.SDR 2018FA0000526Precooler · degradedIN ON OF PRE BUYS INSPECTIONS WE CAME ACROSS SEVER DELAMINATION & WARPING FROM THE HEAT CREATED BY THE BYPASS AIR IN THE PRE-COOLER EXHAUST DUCTS. THESE WAS FOUND ON BOTH OF OUR PYLONS. I HAVE REACHED OUT TO OTHER OPERATORS AND THEY HAVE ALSO ACKNOWLEDGED THSDR P5CA2018120750369Valve · making metalLH ENG BLEED OFF MESSAGE INTERMITTENT ON TAKEOFF AND CLIMBOUT(<P>TRANSFERRED TO MEL 36-11-08-01-01A, MDDR # 103939 CAT C DUE 15DEC18</P><P>(NOTE: PRV INOP IN OPEN POSITION, HPSOV BLOCKED CLOSED AND FAN AIR VALVE BLOCKED IN THE INTERMEDIATE POSITION PER DDG PRSDR ASAA2018120427217Regulator · failedJUST AS WE STARTED A DESCENT FROM FL410 THE CABIN CLIMB INDICATOR SHOWED THE CABIN CLIMBING AT 3000 FPM. WE THEN GOT A CABIN ALTITUDE WARNING. INITIATED AN EMERGENCY DESCENT TO 10,000 FEET. PACK OPERATION APPEARED TO BE NORMAL THROUGHOUT AND OUTFLOW VALVE OPERSDR UIEA2018120402783Controller · not reportedPER MCC REPLACE LEFT ENGINE PRVC. REMOVED AND REPLACED LEFT ENGINE PRVC IAW AMM 36-11-19. OPS CHECK GOOD AT THIS TIME.SDR BUEA20181205001Tube · crackedCAPTAIN REPORTED THAT ON LEG FROM KPIR TO KDEN PASSENGERS IN THE REAR CABIN COULD SMELL WHAT WAS DESCRIBED AS "HOT PLASTIC" AND A UNUSUAL LOUD SOUND OF AIR MOVEMENT THIS WAS REPORTED TO THE CREW AFTER AN UNEVENTFUL LANDING IN KDEN (IT WAS NOTED THE LOUD SOUND SDR ASAA2018120327200Regulator · failedAFTER START WITH ENGINES AT IDLE LEFT DUCT PRESSURE INDICATES 8 PSI. GROUNDED - YES. PERFORMED FIM TASK 36-10-00-810-804, FOUND HIGH STAGE VALVE AND REGULATOR BAD. REMOVED AND REPLACED HIGH STAGE REGULATOR PER AMM 36-11-07. REMOVED AND REPLACED HIGH STAGE VALVSDR UIEA2018120402769Valve · malfunctionedSTATUS MESSAGE R ENG PRV. PERFORMED BITE PROCEDURE IAW FIM TASK 36-10 FT 847 PRV FAULT DISPLAYED. REMOVED AND REPLACED PRV V352 IAW AMM 36-11-18. OPERATIONAL CHECK IS NORMAL.SDR QXEA2018120300446Control Valve · malfunctionedTAKEOFF ABORTED < 40 KTS FOR #1 BLEED HOT CAUTION. REMOVED FROM SERVICE. FOUND FAULT IN CDS L NAPSOV,PACK FCV. CLEAR FAULT. GROUND RUN #1 & #2 ENG. NO AIR FLOW IN CABIN.FAULT RETURNED IN CDS. REMOVED AND REPLACED #1 NACELLE SHUTOFF VALVE REF AMM TASK 36-11-19-SDR ASAA2018120312719Regulator Valve · failedAIR ENGINE 2 BLEED A PRESSURE GROUNDED - YES. REMOVED AND REPLACED BLEED PRESSURE REGULATOR VALVE ON #2 ENG REF AMM 36-11-52 ENG RUN STILL REQUIRED TO COMPLETE OPS AND LEAK CHECKSDR DALA2018120316975Buffer Valve · leakingWHILE TAXIING IN, DURING APU START-UP, OILY FUEL FUMES ARE NOTICEABLE THROUGHOUT THE ENTIRE CABIN AND COCKPIT. SMELL DISSIPATES A MINUTE OR TWO AFTER APU RUNNING. C/W NO GO ODI CHECK STEPS 1 THRU 5 PER STEP 6 REMOVED L/H AND R/H BUFFER VALVES, R/H SHOWS NO OBVSDR IPXA2018113036432Valve · malfunctionedAFTER TAKEOFF, RECEIVED A LEFT ENGINE PRV EICAS MESSAGE. COMPLETED QRH CHECK LIST. R & R THE LT ENG PRV IAW AMM 36-11-19. THE LT PRV OPS CHECKED OK. NO LEAKS NOTED.SDR ASAA2018113087156Regulator · leakingAFTER STARTING BOTH ENGINES, AND PLACING BOTH PACKS IN AUTO, ISOL VALVE AUTO, ENGINE BLEED SWITCHES ON, APU BLEED OFF, THE RIGHT DUCT PRESSURE WAS 20 PSI AND THE LEFT WAS 8 PSI WITH ENGINES AT IDLE. PACKS AND ENGINE BLEED VALVES WERE CYCLED OFF, THEN BACK ON/ASDR ASAA2018113087138Warning Message · illuminatedCLASS II MAINT STATUS MESSAGE DISPLAYED AFTER SHUTDOWN 'AIR BLEED'. GROUNDED - YES. ON DEFERRALSDR 9WGA20181129801Clamp · detachedEICAS MESSAGE AT TOP OF CLIMB "BLD DUCT LEAK (2)". RETURNED TO KORD FOR REPAIRS. FOUND CLAMP BLOWN OFF LEADING EDGE DUCT ON LEFT HAND SIDE.SDR ASAA2018113067155Regulator · failedDURING CLIMB FROM FL 350 TO FL 370, LEFT DUCT PRESSURE = 46 PSI, RIGHT = 23 PSI, EXCEEDS 20 PSI MAX. DURING CRUISE @ FL 370 RT = 34 LEFT = 43. GROUNDED - YES. FOUND PRSOV FAILED HEALTH CHECK, PRECOOLER CONTROL VALVE FAILED HEALTH CHECK AND HIGH STAGE VALVE FAISDR ASAA2018112657042Status Message · false activationAIR BLEED MTNCE STATUS MESSAGE IN WHITE ON SD PAGE GROUNDED - YES. COMPLETED BITE TEST BMC 1+2 AMM 36-00-00 TEST PASSED AND CLASS II MSG CLEARED.SDR ASAA2018112657040Controller · malfunctionedENG 1 BLEED DID NOT CLOSE ENGINE SHUTDOWN GROUNDED - YES. RESET BMC SYSTEMS. PERFORMED TEST OF BMCS TEST OK. NO FAULTS FOUND REF AMM 36-11-00SDR UIEA2018112632684Controller · malfunctionedR ENGINE PRV STATUS MSG. REMOVED AND REPLACED RH ENGINE PRV CONTROLLER IAW AMM 36-11-19 </P>)SDR UIEA2018112632680Warning Message · false activationRIGHT ENGINE PRV STATUS (<P>PERFORMED BITE TEST. NO FAULTS NOTED AT THIS TIME AS PER AMM 36-23-00</P>)SDR UIEA2018112102668Warning Message · false activationSTATUS MESSAGE: R ENG PRV.(<P><SPAN>PERFORMED / BITE CHECK IAW AMM 36-23-00. NO FAULTS NOTED AT THIS TIME.</SPAN></P>)SDR UIEA2018112102655Warning Message · false activationRIGHT ENGINE PRV STATUS MESSAGE (<P>PERFORMED BITE TEST ON AIR FLOW BITE MODULE. NO FAULT NOTED, MESSAGE CLEARED PER FIM 36-10 FAULT TREE 847 BITE 36-20 FAULT TREE 804</P>)SDR UIEA2018111602628Warning Message · false activationLEFT ENGINE HPSOV STATUS MESSAGE (<P>PERFORMED FIM TASK 36-10 FT 833 BITE PROCEDURE. NO DEFECTS NOTED. GROUND RAN #1 ENGINE IAW B767 AMM 71-00-00, COULD NOT DUPLICATE DISCREPANCY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE</P>)SDR UIEA2018111602634Seal · leakingRH ECS BAY AFT LWR CROSSOVER DUCT O/B OF VALVE IS LEAKING(<P>REMOVED AND REPLACED RH ECS BAY AFT LOWER CROSSOVER DUCT SEALS IAW AMM 36-11-01, NO LEAK DETECTED.</P>)SDR UIEA2018111642614Sense Line · chafedLH WING TO BODY AREA, BLEED AIR DUCT SENSE LINE RUBBING AGAINST AROUND STUD INSIDE ACCESS PANEL #193KL(<P>REMOVED AND REPLACED BLEED AIR SENSE LINE IAW AMM 20-10-09. PERFORMED LEAK CHECK, NO LEAKS NOTED IAW B767 AMM 36-11-00.</P>)SDR UIEA2018111432596Warning Light · false activationON LANDING, EICAS FOR THE LT BLEED ISOLATION VALVE. ENGINE ANTI-ICE WAS ON AT TIME OF LANDING. PERFORMED APU RUN AND CYCLED THE LT BLEED ISOLATION VALVE AND FOUND IT TO OPERATE NORMAL IAW MM 49-00-00.SDR UIEA2018111302592Circuit Card · malfunctionedDURING CLIMB, THE LEFT DUCT WENT TO ZERO, NO EICAS OR BLEED LIGHTS ILLUMNATED. REMOVED AND REPLACED PRINTER CIRCUIT CARD, LEFT BLEED AIR CONTROL IAW AMM 36-11-12 AND AMM 20-10-01. OPS CHECKED GOOD, ENGINE RUN PERFORMED IAW AMM 71-00-00, OPS CHECKED GOOD, SDR UIEA2018111602637Warning Message · false activationR ENG PRV STATUS MSG(<P>PERFORMED R ENG PRV OPS CHECK I/A/W 36-11-18 OPS CHECK GOOD AT THIS TIME. MSG IS CLEARED<BR /></P>)SDR DALA2018111436624Converter · contaminated(AIRCRAFT 6801, L/P 3751740) VERY STRONG WET SOCK SMELL FROM AIR CONDITIONING SYSTEM ON APPROACH. PERFORMED BSI OF THE 2.5 BLEED PORT FINDINGS TURNED OVER TO LEAK AND MCC. FOUND EVIDENCE OF OIL CONTAMINATION IN 2.5 BLEED PORT AREA R/R LT PACK OZON CONVERTER PESDR 2018FA0000497Precooler · malfunctionedDURING CLIMB, WHEN PASSING FL300, HAPPENED RIGHT PACK TRIP-OFF LIGHT ILLUMINATED. CONTINUING CLIMBING, AT FL350 TWO BLEED LIGHT ILLUMINATED. USING FIM 21-52 TASK 825 AND FIM 36-10 TASK 801, EVERYTHING FOUND OK. BY FLIGHT TEST, AT FL230 HAPPENED AGAIN AND A RESSDR 2018FA0000500Warning Message · illuminatedFROM KEUG TO KVNY, ON DESCENT TO KVNY "BLEED 1 FAIL" CAS MESSAGE ON PFD.SDR AALA201811149023Regulator Valve · failedTUL FLT 9668 EN-ROUTE TUL - TUL. THE AIRCRAFT WAS GROUNDED. DURING DESCENT BELOW 15,000 THROTTLES AT IDLE LEFT ENG PRV STATUS MSG DISPLAYED WITH ASSOCIATED EICAS AMBER MSG DURING DESCENT BELOW 15,000 THROTTLES AT IDLE LEFT ENG PRV STATUS MSG DISPLAYED WITHSDR IPXA2018111205835Valve · malfunctionedRIGHT ENGINE PRV EICAS MESSAGE AND STATUS MESSAGE DURING TAKEOFF. R & R THE RT ENGINE PRVC IAW AMM 36-11-19-401. INSTALLATION TEST PASSED. RAN THE RT ENGINE IAW AMM 71-00-00-201.SDR A6WA2018111246144Unknown · malfunctionedAT CRUISE FL250 NOTICED RT PACK OFF STATUS MESSAGE AND RT PACK OFF SWITCH LIGHT ILLUMINATED. CYCLED RT PACK SWITCH TWICE. PACK REMAINED OFF. SELECTED ECS PAGE ON EICAS. RT 10TH STAGE BLEED CLOSED. CYCLED R 10TH SWITCH CLOSED THEN OPEN. PRESSURIZATION RESUMED. SDR UIEA2018111402560Duct · leakingPNEUMATIC LEAK BY CENTER ISOLATION VALVE (LEFT WHEEL WELL).(<P>REMOVED AND REPLACED PNEUMATIC DUCT BEHIND ISOLATION VALVE OPS'S CK,LEAK CK NORMAL IAW </P><P>36-11-02.</P><P><BR DATA-MCE-BOGUS="1" /></P>)SDR ASAA2018110826821Check Valve · defectiveNR 2 ENGINE HAS REPORTS OF HUNG STARTS WITH LOW EGT AND LOW N2. GROUNDED - YES. REPLACED NR 2 ENGINE 5TH STAGE BLEED AIR CHECK VALVE REF AMM 36-11-02-400-801 AND ACCOMPLISHED INSTALLATION TEST. TEST OK, NO LEAKS NOTED. REMOVED AND REPLACED NR 2 ENGINE SPAR VALSDR P5CA2018110980348Controller · malfunctionedL ENG HPSOV STATUS MSG(<P>TRANSFER TO MDDR 102441 IAW MEL 36-11-02-02 CAT DUE DATE 18 NOV18</P><P><BR DATA-MCE-BOGUS="1" /></P><P>REMOVED & REPLACED HP CONTROLLER IAW AMM 36-11-08 OPS CK & ENG RUNS NML IAW AMM 71-00-00</P>)SDR UIEA201811092529Seal · leakingDURING PNEUMATIC LEAK CHECK FOUND LEAK AT PRV MUSCLE LINE AT UNION AND FITTING. REMOVED AND REPLACED SEAL AT PRV MUSCLE LINE IAW AMM 36-11-18 NO LEAKS DETECTED.SDR SIMA20181104001Sleeve · damagedBLEED 1 LEAK CLIMBING OUT OF 6,000 AND CABIN ALT CONTINUED TO CLIMB. REMOVED PACK 1 PANEL IAW 06-41-01 OF AMM. PERFORMED GVI OF PACK 1 FOUND COUPLER ABOVE ACM LEAKING ISOLATED PACK 1 AND RAN ENGINE FOR 5 MIN IAW GHC WITH BLEED 1 SELECTED NO MESSAGES NOTED. REMSDR REXA2018110201040Check Valve · malfunctionedLEFT ENGINE FLAME OUT AT TOP OF DECENT. FLAMEOUT WAS PRECEDED BY 2 SEPARATE VIBRATIONS AND THEN ENGINE FLAMEOUT. FOLLOWED QRH GUIDANCE, ENGINE RELIT NORMALLY. AS ENGINE FLAMEOUT ITT WENT INTO RED MOMENTARILY CAUSING LITT EXCEED B STATUS MESSAGE TO POST AFTER ESDR UIEA2018110202493Shutoff Valve · malfunctionedLEFT ENGINE BLEED EICAS AT LEVEL OFF. REMOVED AND REPLACED THE LT ENGINE PRSOV IAW AMM 36-11-09, RAN THE ENGINE IAW AMM 71-00-00, ENGINE BLEED SYS NORMAL.SDR UIEA201811022485Warning Message · false activationLEFT ENG BLEED EICAS DURING CLIMB. ACCOMPLISHED FIM 36-10/837. NO FAULTS NOTED ON BITE TEST.SDR UIEA201811012460Circuit Card · malfunctionedDURING CLIMB, THE LT ENGINE BLEED OFF EICAS MESSAGE. QRH 2.16 COMPLIED WITH. ACCOMPLISHED FIM 56-10/ 857, NO FAULTS NOTED ON AIR SUPPLY BITE. REPLACED THE BLEED AIR CARD M-859 IAW AMM 36-11-12. RAN ENGINES IAW AMM 71-00-00. OPS CHECKED GOOD.SDR UIEA2018102902428Valve · malfunctionedSTATUS MESSAGE L ENG PRV ON TAXI OUT OF ONT. REMOVED AND REPLACED PRV IAW AMM 36-11-18. OPS CHECK GOOD.SDR AALA201811029014Duct · leakingLEFT ENGINE FIRE WARNING ACTIVATED INTERMITTENTLY, EVENTUALLY STOPPED BEFORE ENGINE SHUTDOWN. EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED HP2 AND HP6 DUCTS IAW MM 36-11-01 AND ACCOMPLISHED
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