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 UIEA2021100402177Valve · inoperativeR ENG BLEED OFF ADVISORY MSG WHEN STARTING DESCENT. AFTER LEVELING OFF AT LOWER ALTITUDE AND ADDING POWER, IT WENT AWAY. REMOVED AND REPLACED PRSOV IAW AMM 36-11-09. OPS CHECK GOOD IAW AMM 71-00-00.SDR UIEA2021093002145Card · inoperativeRT ENG BLD OFF EICAS DURING DECENT PERF FIM 36-10 FT 836. AIR SUPPLY BITE HAD NO FAULTS. CHECKED FOR ANY LEAKS , LEAK CHECK GOOD. REMOVED CONNECTOR D64 HELP PRSOV OPEN AND FOUND NO CONTUITY BETWEEN PIN 1 AND 2.R/R M860 R ENG BLEED CARD PE AMM 36-11-12. PERF R SDR UIEA2021093002147Shutoff Valve · false indicationL ENG HPSOV PERFORMED AIR SUPPLY CONT SYTEM BITE TEST. NO FAULTS NOTED. MESSAGE CLEARED I/A/W AMM 36-23-00.SDR P5CA2021092600363None · noneAFTER START EICAS R ENG BLEED OFF REMAINED ILLUMINATED. QRH READ, DDG CONSULTED, NOT FC DEFERRABLE(<P>REMOVED AND REPLACED #2 ENG PRSOV IAW B767 AMM 36-11-09. PERFORMED ENGINE IDLE RUN IAW B767 AMM 71-00-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIMSDR UIEA2021092602120Sensor · warning messageR ENG HPSOV STATUS MESSAGE DISPLAYED.(<P>TRANSFERED TO MDDR 154127 PER MEL 36-11-02-02, CAT "C", DUE DATE: 06OCT21.BWI STA, 29SEP: LP 1314128, ITEM M9: REMOVED AND REPLACED RT ENG FAN AIR TEMP SENSOR IAW 767 AMM 36-11-17. OPS TEST GOOD. DMI CLEARED, PLACARDS RSDR UIEA2021092402108Pneumatic System · fluctuatesPACKS FLUCTUATING WITH APU AIR.(<P>TRANSFER TO MDDR 154006 IAW MEL 36-11-04, CAT C.</P> / <P>LP 1386698: PERFORMED ENGINE RUN AND ENGAGED ENGINE ANTI-ICE SYSTEM PRESS NORMAL, NO FLUCTUATIONS OF PNEUMATIC AT NORMAL BLEED INDICATION. IAW AMM 72-00-00 AND FIM 36-SDR UIEA2021092202067Bleed Valve · false indicationRT ENG BLEED OFF CAUTION MSG WHEN DESCENDING THRU FL330. FOLLOWED QRH W/ NO FURTHER ISSUE.(<P>BITE TEST C/O IAW B767 FIM 36-20 FAULT TREE 804, BITE TEST SHOWS NO FAULTS, A/C OK FOR SERVICE.</P>)SDR UIEA2021091902055Shutoff Valve · bindingSTATUS MESSAGE R ENG HPSOV(NOTICED IN FLIGHT) 2 INTERMITTENT EICAS R ENG HPSOV(<P>PERFORMED FIM TASK 36-10 FT 833 UP TO BLOCK 40. PERF AIR SUPPLY BITE PROCEDURE IAW AMM 36-20-00. R ENG HPSOV FAULTING ON BITE. PERFORMED LEAK TEST/OPS CHECK ON HPSOV HP CONTROLLESDR AALA202109213131Control Valve · faultedAIRCRAFT WAS GROUNDED: ENGINE 1 FIRE AND OVERHEAT WARNING DURING CLIMB OUT FROM CLT. INDICATION CEASED SHORTLY AFTERWARDS. DECLARED EMERGENCY AND RETURNED TO CLT. MAINTENANCE PERFORMED AMM TASK 26-10-00-810-811 AND WAS UNABLE TO DUPLICATE OVERHEAT FAULT. MAINTSDR UIEA2021091702035Hpc · unreliableLEFT ENGINE HPSOV CLOSED AND OPEN SWITCHES DISAGREE EICAS MSG.(<P> IT WAS REPLACED THE CONTROLLER ASSY - HIGH PRESSURE IAW AMM 36-11-08-004-050-008.</P>)SDR UIEA2021091702042Sensor · inoperativeR/H ENGINE HPSOV INOP ( HIGH PRESSURE SHUTOFF VALVE (HPSOV) SYSTEMS / ALL EXCEPT CF6-80C2 )(<P>TRANSFERRED TO MDDR 153619 MEL 36-11-02-01 CAT C DUE DATE 26SEP21. PLACARD INSTALLED. REF LOGPAGE 1207824 #4 CVG 22 SEP 21 AND LOGPAGE 1207825 #9 CVG22SEP21</P> / <SDR ASAA2021091635988None · failedON CLIMBOUT, DUCT PRESSURE DIFFERENTIAL NOTED AT GREATER THAN 20PSI (R 42PSI / L 45PSI). ON LEVEL OFF AT FL340 DUCT PRESSURE NOTED AT R 43PSI / L 26PSI. GROUNDED - YES. ACCOMPLISHED #1 ENG BLEED AIR SYSTEM HEALTH CHECK TASK CARD NG-36WC-00001 & FOUND PRECOOLERSDR ASAA2021091635987None · failedAT CRUISE FL340, LEFT "BLEED TRIP OFF" AMBER LIGHT ILLUMINATED, LEFT DUCT PRESSURE INDICATED ZERO PSI. WE PUSHED TRIP RESET BUTTON PER QRH PROCEDURES AND BLEED TRIP OFF" LIGHT EXTINGUISHED AND LEFT DUCT PRESS INDICATION MATCHED RIGHT DUCT PRESS. IND. GROUNDED SDR UIEA2021091702043Controller · warning messageDURING TAKEOFF "R ENG HPSOV" ADVISORY MESSAGE DISPLAYED MOMENTARILY FOLLOWED BY R ENG HPSOV STATUS MSG(<P>TRANSFER TO MDDR 153644 IAW MEL 36-11-02-02 CAT C DUE DATE 26SEP21. MX ACTION C/W.</P> / <P>18SEP, AFW, LP 1391398, ITEM M12: T/S IAW B767 FIM 36-10 FT 84SDR UIEA2021091502026Control Card · warning lightLT ENGINE HPSOV EICAS MSG.(<P>REMOVED AND RE-INSTALLED LEFT ENGINE BLEED AIR CONTROL CARD IAW AMM 36-11-12. MSG CLEARED. OPS CHECK GOOD.</P>)SDR UIEA2021091402020Module · warning lightAFTER ENG. START AND DURING LOW POWER SETTINGS, THE RIGHT ENG BLEED VALVE LIGHT ILLUMINATES INTERMITTENTLY WITH ASSOCIATED EICAS THEN EXTINGUISHES A FEW SECONDS LATER.(<P>TRANSFERRED TO MDDR 153490 PER DDG 36-11-02-01 CAT C DUE 24SEP21. PLACARDS INSTALLED.</P>SDR ASAA2021091335945Sense Line · crackedDURING CLIMB DUCT PRESS L DUCT PRESS 18 PSI RIGHT DUCT 40 PSI. WHEN LEVELED AT FL 370 R DUCT 40 PSI & LEFT 28 PSI. GROUNDED - YES. INSPECTED #1 ENGINE PNEUMATIC SYSTEM AND FOUND SENSE LINE BETWEEN BLEED AIR REGULATOR AND PRE-COOLER CONTROL VALVE TO BE CRACKED SDR UIEA2021091102008Warning Message · false activationSTATUS MSG "R ENG HPSOV"(<P>PERFORMED BITE TEST OF THE AIR SUPPLY CONTROL SYSTEM IAW B767 AMM 36-23-00. NO FAULTS FOUND. PERFORMED DRY MOTOR OF R/H ENG IAW B767 AMM 71-00-00. NO DEFECTS NOTED AT THIS TIME. PERFORMED R/H ENG IDLE RUN IAW B767 AMM 71-00-00. NO FSDR 4DPA2021090800001Filter · clogged/JSX FLT 9401 NON REV REPO LEG, 1ST RTF, CREW DECLARED AN EMERGENCY DUE TO BLEED 2 OVER HEAT AND CABIN PRESSURIZATION SPIKE RETURNED TO FIELD NO FURTHER ISSUES. CORR ACTION FAV FILTER CLOGGED REMOVED AND CLEANED FILTER AND REINSTALLED BLEED 2 OPS TEST GOOD. 2NSDR ASAA2021090235844Shutoff Valve · inoperativeDURING HPSOV LOCKOUT PROCEDURE (ENGINE NO 1 COMPRESSOR WASH) LOCKBOLT HELICOIL BACKED OUT. GROUNDED - YES. REPLACED NO 1 ENGINE HPSOV REF B737-9 AMM 36-11-07. LEAK TEST GOOD. LRU REPLACEMENT TESTS GOOD.SDR ASAA2021083135836Shutoff Valve · inoperativeDURING CLIMB FROM 6000' TO FL390 DUCT PRESSURE SPLIT BY UP TO 25-30PSI. LEFT DUCT VARIED FROM 62 TO 75PSI, RIGHT DUCT AT 40-45PSI. WHEN LEVEL AT 390 AND POWER REMOVED TO CRZ , DUCT PRESSURES NORMALIZED. GROUNDED - YES. PERFORMED B737-900 MM TASK 36-11-00-700-8SDR 2021F00286Control Valve · damagedQRF. BLEED TRIPOFF LEFT SIDE. CABIN UNCONTROLABLE. CORRECTIVE ACTION. DISPATCH ACC MEL 36-08 CAT (C). THEN REMOVED MEL WITH THE FOLLOWING ACTION: HAS BEEN REPLACED PRECOOLER CONTROL VALVE IAWTASK 36-12-02-000-801 AND TASK 36-12-02-400-861. IN TEST NORMAL.SDR YENA2021083100551Valve · failedFLT 119, MCO-ALB. DIVERTED TO JFK. AIR ENG 1 AND 2 BLEED FAULT ECAM DURING CLIMB; R & R VALVE (6HV) IAW AMM 36-12-52. OPS CHK OK. A/C OK FOR CONT. SVC.SDR ABXA202183027082Shutoff Valve · stickingRT ENG HUNG, WOULD NOT INCREASE ABOVE 45% N2, EGT WAS CLIMBING.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. FOUND PRSOV STUCK IN MID-POSITION. REMOVED AND REPLACED PRSOV IAW AMM 36-11-09. OPS CHECK GOOD IAW AMM71-00-00. AIRCRAFT RELEASED FOR FLIGHT.SDR GTIA2021083035951Valve · faultedAIR ENG 2 BLEED FAULT - RETURN TO MCO-REMOVED AND REPLACED #2 HPV IAW 36-11-51 AND REMOVED AND REPLACED #2 PRV IAW AMM 36-11-52. OPS CHECK GOOD. A/C OKAY FOR SERVICESDR MGOR2021082701489Heat Exchanger · rupturedWHILE PERFORMING PHASE 54 INSPECTION FOUND THE LEFT PYLON PRECOOLER/HEAT EXCHANGER RUPTURED. RUPTURE CAUSED DISCOLORATION OF THE AFT ENGINE BEAM WITHIN THE PYLON AND INTO AIRCRAFT FUSELAGE. THE STRUCTURE WITHIN THE PYLON, AIRCRAFT SKIN AND ASSOCIATED FRAMES ANSDR DALA2021082304966Duct · crackedSHIP 0676- DIV- TO MTY DUE TO RT WING DUCT LEAK EICAS MESSAGE. CORRECTIVE ACTION: FOUND CRACKED DUCT FLANGE BETWEEN WING TO BODY FAIRING AND NO. 2 ENGINE PYLON. REPLACED DUCT. LEAK CHECKS OK.SDR UIEA2021082301850Warning Message · false activationSTATUS MSG R ENG PRV(<P>C/W FIM 36-10- FAULT TREE 847, OPS CHECK NORMAL.</P>)SDR UIEA2021081901827Valve · faultedL ENG BLD OVHT AT FL250, RAN QRH, MESSAGE CLEARED.(<P>REMOVED AND REPLACED FAN AIR VALVE ASSY PER MCC REQUEST IAW B767 AMM 36-11-16. OPS CHECK GOOD. LEAK CHECK GOOD AT THIS TIME.</P> / <P>ITEM M10: PERFORMED HIGH POWER ENGINE RUNS IAW AMM 71-00-00 TEST PROCEDUSDR SIMA20210817004Pneumatic System · faultedBLEED 1 AND BLEED 2 FAIL WHILE HOLDING AT FL260. FOLLOWING QRH, BLEEDS CAME BACK ONLINE AFTER RESET EMERGENCY DECLARED-C/A-PERFORMED WING ANTI-ICE OPS CHECK IAW E175 AMM 30-11-00. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICESDR NACA2021081600001Switch · faultedDISCREPANCY: RH PRSOV GROUND TEST SWITCH IS NOT RETURNING TO THE OPEN POSITION. DEFERRED PER DMI 36-11-@2130 08-18-21SDR NACA2021081650001Switch · faultedSTART OF DESCENT RIGHT STRUT DETECTION LEAK EICAS MESSAGE. DEFERRED PER MEL 36-11-08-01A CAT C ON 15AUG21 @1415Z. MAINT PROCEDURES APPLIED AND PRV SECURED CLOSED. AC REMAINS ETOPS 120. SET PRV BACK TO NORM IAW AMM 36-00-00/901. THIS ACTION CLOSED MEL 36-11-0SDR NACA2021081400001Warning Message · false indicationDISCREPANCY: IN CRUISE FLIGHT EICAS R STRUT DCT LEAK. CORRECTIVE ACTION PERFORMED FIM 26-18 FAULT TREE 804, NO FAULTS FOUND.SDR UIEA2021081301790Warning Message · false activationL BLD DUCT LEAK. TURNED LT PACK ON AND OFF, MESSSAGE CLEARED, PERFORMED OPS CHECK PER AMM 21-51-00, OPS CHECKED GOOD.SDR NACA2021081100001Control Card · fluctuatesDISCREPANCY: LEFT DUCT PRESSURE FLUCTUATES MORE THAN 20 PSI, NORMAL TO LOW RANGE AT TAKEOFF THRUST. STABLE AT CLIMB THRUST, FRM 36-10-01-01. CORRECTIVE ACTION: PERFORMED AIR SUPPLY BITE TEST PER AMM 36-23-00, FOUND L PRC WIRE FAULTS, REMOVED AND REPLACED LEFT SDR UIEA2021081201773Pneumatic System · malfunctionedAPU FAULT DUE TO PNEUMATICS SURGING(<P>FWD TO MEL AND PLAC 49-11-01A, CAT C, DUE 21AUG21. MDDR 151717.</P> / <P>REF LOGPAGE 1439202 ITEM 5: T/S PER FIM 49-11 F/T 976 TO BLOCK 28. NO SURGING OR FLUCUATION NOTED . 3 SUCCESSFUL APU STARTS ACCOMPLISHED AND LOAD PSDR I5PA2021081075704Regulator · faultyREF LP 42712 MEL 49-11-01-01 APU PNUEMATIC FUNCTION. REMOVED AND REPLACED PILOT PRESSURE REGULATOR ON LH ENG REF AMM 36-00-23. OPS CHECK OK. MEL CLEARED.SDR P5CA2021081000313Shutoff Valve · faultedAPU BLEED FUNCTION INOP(<P>FND APU DUCT PRESSURE DROP TO ZERO DURING L ENG START. PER AMM 71-00-00 PRFORM BOTH ENGINE DRY MOTORING, CONDITION NORMAL WITH GROUND PNEUMATIC SOURCE. TRANSFERRED TO MDDR 151273 IAW MEL 49-11-01-01 CAT C.</P> / <P>LP <SPAN>1483980:SDR AALA202108107358Regulator Valve · faultedAIRCRAFT WAS GROUNDED: ON DEPARTURE THRU 1500 ECAM REFLECTED #1 ENGINE AIR BLEED FAULT, SYSTEM RESET WAS ATTEMPTED BUT FAULT REOCCURRED. AN EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO PHL WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACESDR P5CA2021080600280Controller · no testFOUND #1 ENG HPC HEALTH CHECK TEST FAIL(<P>IAW AMM 36-11-08-004-006-007 REV 132 AND AMM 36-11-08-404-014-007 REV 132, REMOVED AND REPLACED #1 ENG HPC WITH NEW PARTS. IAW AMM 71-00-00-795-228-H03 #1 ENG HPC DRY MOTOR LEAK TEST RESULT. CONDITION CHECK SATISFACTOSDR P5CA2021080600281Precooler · damagedBROKEN - FOUND #2 ENG PRECOOLER RH FINS BROKEN(<P>IAW AMM 36-11-15-004-003-001 REV 132 REMOVED AND #2 ENG PRECOOLER. IAW AMM 36-11-15-404-020-001 REV 132 REV 132 INSTALL PRECOOLER AT #2 ENG WITH NEW PARTS. IAW AMM 36-11-15-404-020-001 REV 132 ACCOMPLISHED THE SDR P5CA2021080600282Precooler · damagedBROKEN - FOUND #1 ENG PRECOOLER RH FINS BROKEN(<P>IAW AMM 36-11-15-004-001-001 REV 132 REMOVED #1 ENG PRECOOLER. IAW AMM 36-11-15-404-020-001 REV 132 INSTALL #1 ENG PRECOOLER WITH NEW PARTS. IAW AMM 36-11-15-404-020-001 REV 132 ACCOMPLISH THE #1 ENG PRECOOLER SDR P5CA2021080600283Shutoff Valve · faultedPERFORM #1 ENG PRSOV HEALTH CHECK, IND BIT 26, BIT 27 CANNOT CHANGE (J/C 6736A005 PAGE 33 PART 4 STEP 11.6)(<P>IAW WDM 36-11-51 REV 34 AND WDM 36-23-11 REV 34 PERFORM WIRING CONTINUITY CHECK, THE RESULT WAS SATISFACTORY. IAW AMM 36-11-09-002-033-001 REV 132 ANSDR P5CA2021080600289Switch · intermittentFOUND ENG #2 PRSOV GROUND SERVICE SWITCH INTERMITTENT FAIL(<P>IAW WDM 36-11-51 REV 34, SWPM 20-10-11, 20-10-13 REV 77 REMOVED AND REPLACED SWITCH. IAW AMM 36-11-09-782-138-001 REV 132 PERFORM TEST, TEST PASSED.</P>)SDR P5CA2021080900303Seal · leakingFOUND #2 ENG IP CHECK VALVE COUPLING AIR LEAKAGE(<P>IAW AMM 36-11-06-004-001-001 REV 132 AND AMM 36-11-06-404-009-001 REV 132 REMOVED AND REPLACED #2 ENG IP CHECK VALVE E-SEAL WITH NEW PARTS. IAW AMM 71-00-00-795-228-H03 REV 132 PERFORM ENG DRY MOTOR LEAK CHECSDR P5CA2021080900304Check Valve · wrong partFOUND #3 ENG IP CHECK VALVE FORWARD COUPLING WRONG PARTS(<P>IAW AMM 36-11-06-004-001-001 REV 132 AND AMM 36-11-06-404-009-001 REV 132 REMOVED AND REPLACED #2 ENG IP CHECK VALVE FORWARD COUPLING. IAW AMM 71-00-00-795-228-N03 REV 132 ACCOMPLISH THE #2 ENG IP CHESDR P5CA2021080900310Sensor · faultedFOUND #1 ENG FAMV CAN NOT CLOSE(<P>IAW AMM 36-11-17-004-001 REV 132 AND AMM 36-11-17-404-017 REV 132 REMOVED AND REPLACED #1 ENG FAN AIR TEMP SENSOR WITH NEW PARTS. CONDITION CHECK SATISFACTORY AND NO LEAK FOUND</P>)SDR P5CA2021080900311Seal · leakingFOUND #2 ENG PRSOV LOWER COUPLING AIR LEAKAGE(<P>IAW AMM 36-11-09-002-033-001 REV 132 AND AMM 36-11-09-402-058-001 REV 132 REMOVED AND REPLACED #2 ENG PRSOV E-SEAL. CONDITION CHECK SATISFACTORY AND NO LEAKS FOUND</P>)SDR NACA2021080600002Controller · faultedDISCREPANCY: DUCT PRESSURE DIFFERENCE IS BECOMING LARGER. LEFT SIDE IS 15 PSI LARGER THAN RIGHT SIDE. CORRECTIVE ACTION: REPLACED PRESSURE REGULATING VALVE CONTROLLER AND OPS CHECK GOOD AMM 36-11-19, GROUND CHECK GOOD. AC REMAINS ETOPS.SDR 6CBA2021080521207Line · out of positionWHILE ENROUTE FROM KPSM TO KACK THE FLIGHT CREW HAD A ENGINE FIRE RED CAS, DIVERTED TO KHYA, THE FLIGHT CREW DECLARED AND EMERGENCY BUT LANDED WITHOUT INCIDENT. AIRPORT FIRE DEPARTMENT ARRIVED AT THE AIRCRAFT, AND FOUND NO EVIDENCE OF AN ACTUAL FIRE. REPLACED
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