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 HALA2009061500239Duct · leakingETOPS SIGNIFICANT SYSTEM, R BLEED DUCT LEAK NOTED W/APU AIR ONLY. PERFORMED FUNCTIONAL CK PER AMM 26-18-00-715-001-001. OPS CK NORMAL, NO FAULTS NOTED.SDR 2009FA0000516Duct · failedPN 128-550011-11, BLEED AIR DUCT, WIRE BRAIDING FAILED AT BOTH (2) OF THE BELLOWS ASSEMBLIES. DUCT EXPANDED AT BELLOWS PORTION OF DUCT BUT DID NO ADDITIONAL DAMAGE TO ACFT. DEFECT WAS DISCOVERED AT TROUBLESHOOT OF DIFFERENT PROBLEM IN AFT FUSELAGE. AD 2001-0SDR UALA2009061501711Regulator Valve · malfunctionedPACK ISSUE & NR 2 ENGINE BLEED FAULT. RTFL. ECAM FAULT AIR ENG 1 BLEED ABNORM PR, BMC1 FAULT PRESS REG-V 4001HA1 OR SOL 10HA1 OR SENSE LINE. REPLACED SOL 10HA1. ALSO CHECKED FOR LEAKING LINES 114830TO 10HA1 BOTH LINES, AND ACCOMPLISHED PRV TEST PER MT36-001SDR RAIA2009061700002Valve · defectiveCREW RECEIVED A BLEED 1 OVERTEMP MESSAGE ON THE EICAS DURING CRUISE. MAINTENANCE REMOVED AND REPLACED THE FAN AIR CONTROL THERMOSTAT AND THE FAN AIR VALVE IAW AMM PROCEDURES. FOLLOW-ON OPERATIONAL CHECK WAS GOOD.SDR USAA2009061791498Computer · inoperativeFLT 1485 - SFO-PIT - EMERGENCY LANDING - LOST BOTH BLEEDS AND PACKS. REMOVED AND REPLACED NR 1 AND NR 2 BLEED MONITORING COMPUTER (BMC). ACCOMPLISHED OPERATIONAL TEST OF THE BLEED AIR SYSTEM ON ENGINE RUN. OPERATIONAL TEST WAS GOOD.SDR USAA2009061791497Computer · malfunctionedFLT 1485 - SFO-PIT - EMERGENCY LANDING - LOST BOTH BLEEDS AND PACKS. REMOVED AND REPLACED NR 1 AND NR 2 BLEED MONITORING COMPUTER (BMC). ACCOMPLISHED OPERATIONAL TEST OF BLEED AIR SYSTEM ON ENGINE RUN. OPERATIONAL TEST WAS GOOD.SDR C2XA09TY105O-Ring · blew outTYS - AIRCRAFT LEFT TYS AND RETURN BACK TO TYS WHEN CREW HAD A EICAS MESSAGE OF BLEED LEAK. MAINTENANCE CHANGED O-RINGS AT LOCATIONS 3, 5, 7 AND 9 IAW EMB 145 AMM 36-11-10. ALSO CHANGED O-RING FWD OF THE STAB ANTI-ICE VALVE IAW EMB 145 XR AMM 36-11-10. PERFSDR C2XA09IA154O-Ring · wornCRP - FLIGHT 2820 - DURING FLIGHT THE CREW REPORTED A BLEED TWO LEAK. THE AIRCRAFT DIVERTED TO CRP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLEED O-RINGS FORWARD OF THE GROUND START CONNECTION, OPERATIONALLY & LEAK CHECKED WITH SDR UALA2009060901634Duct · unknownBLEED LOSS ON FINAL. FOUND APU BLEED DUCT BLOWN IN AFT CARGO AREA, DUCT REPLACED. LEAK AND AFOLDS CHECK OKAY. PERMANENT REPAIR ACCOMPLISHED. AIRCRAFT OK FOR SERVICE.SDR UALA2009060401609Controller · faultyBLEED DOES NOT OPEN AT IDLE-INTERMITTENTLY WITH PWR LVL RAISED. REPLACED PRVC CONTROLLER, OP CK'D NORMAL.SDR UALA2009060301599Shutoff Valve · failedLEFT PACK OFF LIGHT ON. REPLACED NR 1 ENG PRSOV BLEED SYSTEM, OPS CHECKS NORMAL AT ALL ENG PWR SETTINGS. LEFT PACK OPS CHECKS NORMAL.SDR DL76G091000Shutoff Valve · malfunctionedLEFT SYS BLEED FAILED AFTER TAKEOFF WOULD NOT RECOVER. TROUBLESHOT PER FIM REPLACED L AIR BLEED CONTROL CARD NO HELP. REPLACED LEFT HPSOV CHECKED HPSOV PEP M/M. RAN ENGINES AND THE LEFT BLEED AIR CHECKED GOOD.SDR UALA2009060201586Valve · damagedBLEED ENG L EICAS MSG. RTFL. FOUND SHAFT SHEARED. REPLACED HP VALVE, OPS CHECK OKAY.SDR UALA2009060101584Shutoff Valve · faultyNR 1 ENGINE BLEED INOPERATIVE. BITE MONITOR FAULTED PRV, PRVC, PRESS SENSOR, HPSOV AND WIRE FAULT. REPLACED CARD M859, NO HELP. INOPED PRSOV. REPLACED HPSOV AND HP CONTROLLER. REACTIVATED PRSOV, RAN ENG. NO BLEED PRESSURE FROM NR 1 ENG INOP'D PRSOV.SDR DL76L090971Isolation Valve · stuckLT ISOLATION VALVE STUCK IN OPEN POSITION. REMOVED AND REPLACED ISOLATION VALVE PER M/M, OPS CHECK VLV.SDR IPXA09B56182Shutoff Valve · malfunctionedINSPECTION TYPE:N/A DIVERSION - ENGINES NR 1 & NR 3 BLEEDS INOP AND LOSS OF ICING PROTECTION ON NR 3 ENGINE. REPLACED AIR SUPPLY CONT & TEST UNIT PER MM 36-11-30-4. REPLACED NR 1 ENG HP SHUT-OFF VALVE AS PER MM 36-11-05-4 & HP CONTROLLER AS PER MM 36-11-06-4SDR Y9PA199HE5.29.09Valve · failedCREW NOTICED CABIN DUCT TEMP HI LIGHT ON MASTER WARNING PANEL, CABIN AIR COMING INTO CABIN WAS HOT, CREW FOLLOWEWD ACFT CHECK LIST TO EXTINGUISH THE WARNING LIGHT AND COULD NOT EXTINGUISH. CREW ALSO NOTED THAT THE AUTO TEMP CONTROL CIRCUIT BREAKER HAD POPPED, SDR UALA2009052901543Regulator · malfunctionedDUAL BLEED LOSS PROBLEM. FLIGHT DIVERTED. ACCOMPLISHED PNEUMATIC SYSTEM TROUBLESHOOT NR 2 ENG WITH TEST UNIT. REPLACED LEFT & RIGHT BLEED AIR REGULATORS AND NR 2 ENG BLEED OVERHEAT SWITCH. ACCOMPLISHED BLEED AIR SYSTEM TEST NR 1 & NR 2 ENG AND BLEED AIR PRSDR FDEA200905271803Clamp · looseON CLIMBOUT PASSING 30000 FT, RECEIVED LT ENG OVERHEAT, PULLED THRUST LEVER BACK AND WARNING EXTINGUISHED. INSPECTED ENG FOR EVIDENCE OF DUCT LEAKS. FOUND FOIL WRAP MISSING FROM IP DUCT IN STRUT. DUCT CLAMP WAS NOT TIGHT. TIGHTENED CLAMP NEEDS ENG RUN. SDR C2XA09RI109Valve · inoperativeFLIGHT 2036 - ALB - FLIGHT CREW REPORTED BLEED 1 AND 2 OVER TEMP IN ICING CONDITIONS. CREW DIVERTED FLIGHT TO ALB AND LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED NR 2 FAN AIR VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETSDR C2XA09RI108Valve · inoperativeFLIGHT 2036 - ALB - FLIGHT CREW REPORTED BLEED 1 AND 2 OVER TEMP IN ICING CONDITIONS. CREW DIVERTED FLIGHT TO ALB AND LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED NR 1 FAN AIR VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETSDR HUNA846EMixing Valve · weakWHILE CLIMBING THROUGH FL 220 THERE WAS A FAINT POP, FROM THE PRESSURIZATION SYS. THE ACFT STARTED TO LOSE CABIN PRESSURE, THE FLIGHT CREW INITIATED A DESCENT TO A LOWER ALTITUDE. THE CABIN ALTITUDE RECHED APPROX 6,000 FT THE MASKS DID NOT DROP. ONCE THE ACFTSDR ASAA0955774Valve · defectiveBLEED SYS HEALTH CHECK INFO SENT VIA ACARS ON F872 24 MAY 2009 INDICATES RT DUCT PRESS AT 30 PSI THIS IS BELOW OPERATIONAL LIMITS IAW AMM 36 11 00 710 801 FIG 502 GROUNDED YES. PERFORMED PNEUMATIC SYS T/S OF RT ENG REF MM 36 00 00. FOUND PRECOOLER VALVE DEFECTSDR R61A20090024Gasket · defectiveCREW RECEIVED A BLEED 1 LEAK WHILE ON CLIMBOUT OF PHL. CREW DESCENDED A/C TO BURN OFF FUEL TO RETURN TO PHL AND NOTICED A BURNING RUBBER SMELL IN CABIN. DECLARED EMERGENCY AND DIVERTED TO ORF, LANDED WITHOUT INCIDENT. ON-CALL MAINTENANCE WAS DISPATCHED TO TSDR C2XA09CL073O-Ring · deterioratedEWR - FLIGHT 2038 - THE CREW REPORTED A BLEED 1 LEAK IN ROUTE TO MSN. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED DUCT O-RINGS IN THE AFT AVIONICS BAY. OPERATIONAL CHECKS WERE GOOD.SDR YENA20090522053Thermostat · failedFLT 180, PHX-JFK, CRUISING AT 37,000, BLEED 2 THEN BLEED 1 FAULTED (BLEED AIR SUPPLY SYSTEMS). REMOVED AND REPLACED NR 1 ENG BLEED AIR SUPPLY SYS THERMOSTAT IAW 36-11-43-04, LEAK CHECK & OPS CHECKS OK.SDR ASAA0955727Line · leakingAT 33000, NOTICED DUCT PRESSURE SPLIT RIGHT SIDE AT 45 PSI AND LEFT SIDE AT 7 PSI. CABIN ALTITUDE WAS CLIMBING. DESCENDED TO 25,000. CABIN PRESSURE OK N1'S 82.0, N2 91.0. OAT 29 DEG CELSIUS GROUNDED ACFT. NR 1 ENG PERFORMED FIM TASK REF FIM-36-10-00-810-804SDR DHLA200900031Duct · blownDURING TAKEOFF ROLL MASTER FIRE WARNING ON GLARESHIELD AND SECOND OFFICERS FIRE WARNING LIGHT AND FIREBELL, REJECTED TAKEOFF AT 100 KTS. NO LIGHT IN HANDLES, LIGHTS AND BELL EXTINGUISHED UPON STOPPING. FOUND 9TH BLEED AIR DUCT BLOWN. REPLACED DUCT ASSY PER SDR ASAA0955689Sense Line · leakingLEFT A/C PACK READS 20 25 PSI BELOW RIGHT PACK IN CLIMB AND CRUISE. GROUNDED YES. LEAK CHECKED ALL SENSE LINES FOUND LINE FROM PRSOV LEAKING. REMOVED AND REPLACED LINE REF MM 36 11 04.SDR DL76L090877Shutoff Valve · malfunctionedON TAXI OUT L HPSOV MESSAGE W/OVERHEAD BLEED LIGHT ON. PERFORMED QRH CYCLED BLEED MESSAGE AND LIGHT CAME BACK ON 2 TIMES. FWD TO MCO AND PLACARD IAW MEL 36-11-02 T/S IAW FIM REMOVED AND REPLACED LT HPC. PERFORMED BITE CK AND RAN ENG ALL CKD NML. REPLACED HPC SDR HALA2009051600175Shutoff Valve · malfunctionedETOPS SIGNIFICANT SYSTEM, ATO, DUE TO HPSOV LIGHT AND EICAS MSG, ABORTED AT 40 KNTS NR 1 ENG. REPLACED HPSOV PER AMM 36-11-07. LEAK CK GOOD. PERFORMED ENG PWR RUN PER AMM 71-00-00 AND AR 767-36-001. TEST GOOD. NO LIGHTS, NO MSGS.SDR C2XA09RI1001Thermostat · inoperativeFLIGHT 2966, FLIGHT CREW REPORTED PACK NR 2 OVERTEMP AND BLEED 1 AND 2 OVERTEMP INDICATIONS ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED FAN AIR THERMOSTAT AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TSDR C2XA09RI100Pressure Switch · inoperativeFLIGHT 2966, FLIGHT CREW REPORTED PACK NR 2 OVERTEMP AND BLEED 1 AND 2 OVERTEMP INDICATIONS ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED PRESSURE SWITCH AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO SDR C2XA09RI099Precooler · inoperativeFLIGHT 2966, FLIGHT CREW REPORTED PACK NR 2 OVERTEMP AND BLEED 1 AND 2 OVERTEMP INDICATIONS ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED PRECOOLER AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN SDR C2XA09IA120Clamp · leakingIAH - FLIGHT 2944, THE CREW REPORTED AN ENGINE ONE BLEED LEAK INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE UPPER BLEED DUCT CLAMP IN THE CARGO COMPARTMENT, OPERATIONAL AND LEAK CSDR C2XA09IA119O-Ring · blownIAH - FLIGHT 2944, THE CREW REPORTED AN ENGINE ONE BLEED LEAK INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE UPPER O-RING IN THE CARGO COMPARTMENT, OPERATIONAL AND LEAK CHECKED WITSDR CHQA200900122Duct · crackedFLIGHT 3066, SDF TO PHL - THE FLIGHT CREW REPORTED AN E1 ITT OF 920 DEGREES FOR 2-3 SECONDS DURING CLIMB AND DURING FLIGHT THE E1 ITT WAS ABOUT 80 DEGREES HIGHER THAN E2 WITH SIMILAR THRUST SETTINGS. THE AIRCRAFT DIVERTED TO BWI WHERE IT LANDED WITHOUT INCIDESDR DL76L090822Shutoff Valve · malfunctionedL ENG HPSOV ILLUMINATED DURING TAKEOFF ROLL FWD TP MCO PER MEL 36-11-02. HPSOV DEACTIVATED AND JUMPER INSTALLED PER MEL. REMOVED AND REPLACED LT ENG HPSOV PER AMM VALVE IS IN UNLOCKED POSITION ALSO T3 TERMINAL BROKEN AT VALVE 680596. RETERMINATED T3 WIRE IASDR C2XA09RI086O-Ring · leakingFLIGHT 600 - RIC - FLIGHT CREW PERFORMED AIR RETURN DUE TO NR 2 BLEED LEAK INDICATION. CREW LANDED ACFT UNEVENTFULLY. RIC MX REMOVED AND REPLACED LEAKING O-RING ON THE BLEED TUBE IN THE PYLON AREA AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROSDR RAIA2009050400001Duct · brokenFLT 8088 - IAD- BLEED 2 OVERTEMP MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 2 LOWER FUSELAGE DUCT. OPERATIONAL CHECK OF THE SYSTEM WAS GOOD.SDR UALA2009042701217Shutoff Valve · faultyNR 2 ENG BLEED VALVE WILL NOT OPEN. REPLACED PRSOV, NR 2 ENG OPS GOOD.SDR VNAA2009042600016Isolation Valve · malfunctionedCREW REPORTED THE 10TH STAGE ISOLATION VALVE STUCK IN THE OPEN POSITION. AIRCRAFT RETURNED TO GPT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE 10TH STAGE ISOLATION VALVE SWITCH BODY. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL SDR UALA2009042301178Valve · failedL ENG PRV EICAS MSG ON T/O ROLL. REJECTED T/O AT 75KTS. REPLACED PRV.SDR RAIA2009042700001Duct · damagedFLT 3547 - PIT - BLEED NR 2 LEAK INDICATION DURING CLIMB. MAINTENANCE PERFORMED AN INSPECTION OF THE NR 2 BLEED SYSTEM AND FOUND A BLOWN DUCT. THE NR 2 SYSTEM WAS DEFERRED IN ACCORDANCE WITH MEL PROCEDURES.SDR UALA2009042101159Valve · failedDUCT PSI FROM ENGINES SPLIT DURING TAKEOFF OR CLIMB, WITH L & R ISOL VALVES CLOSED & BLEED SWITCHES ON. L & R DUCT PRESS ARE. CREW COMMENTS: DUCT PRESS SPLIT LEFT ENG 20 AND RT ENG 35 PSI DURING CLIMB. REPLACED FAMV, NO HELP. REPLACED HPSOV. REPLACED PRVSDR UALA2009042001138Controller · faultyLT DUCT PRESSURE FLUCTUATES DURING TAKEOFF OR CLIMB, WITH L & R ISOL VLVS CLOSED, & BLEED SW ON. DUCT PSI FLUCTUATES BETWEEN. CREW COMMENTS: SPLIT DURING CLIMB. NO SPLIT AT CRUISE. PRESSURES: L-20 R-3. REPLACED PRESSURE REGULATING VALVE CONTROLLER.SDR 2009FA0000334Line · looseDURING ROUTINE INSP FOUND P2 LINE LOOSE AT FUEL CONTROL. THE B-NUT WAS STILL TIGHT. APPLIED LIGHT UPWARD FORCE AND LINE PULLED OUT OF B-NUT. REMOVED B-NUT AND FOUND REMAINDER OF BROKEN FLARE. SLEEVE WAS ALSO SEIZED IN B-NUT. RECOMMEND PERIODIC REMOVAL ANDSDR HNAA2009041600122Pipe · leakingFLIGHT ATTENDANT REPORTS SULFUR ODOR BETWEEN ROWS 2 THRU 5 IN-FLIGHT AND ON GROUND. REMOVED AND REPLACED RIGHT CENTER WING BLEED PIPE. OPS CHECKS GOOD. OK FOR SERVICE.SDR UALA2009041601107Valve · faultySTATUS MSG BLEED AIR FAMV R DISPLAYED. REPLACED NR 2 FAMV. CHECKS GOOD, MESSAGE CLEARED.SDR SWAA092447Precooler · crackedAT FLT 360 GOT ALTITUDE WARNING HORN. NO CAUTION LIGHT NOR PRESSURIZATION PANEL LIGHTS CABIN WAS AT 10,000FT. FOUND NR 2 ENGINE PRE-COOLER CRACKED. REMOVED AND REPLACED NR 2 ENGINE PRE-COOLER PER MM.
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