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 ASAA0852759Shutoff Valve · leakingDUCT PRESSURE SPLIT AT FLT LEVEL 350 IN CRUISE. NIS LEFT 87.7 RIGHT 87.7 PRESSURE LEFT 17 PSI RIGHT 42 PSI. ENGINE BLEEDS ON APU BLEED OFF. ISOLATION VALVE AUTO BOTH PACKS AUTO. PRESSURE THROUGHOUT CLIMB WAS L 12 R 42. FOUND PRSOV ON NR 1 ENGINE LEAKING ASDR CHQA200800057Filter Element · dirtyCLE TO RDU - WHILE CLIMBING THROUGH 7,000 FT, THE CREW RECEIVED A BLEED 1 OVERTEMP MESSAGE. THE PROPER CHECK LISTS WERE FOLLOWED IN THE QRH AND IT WAS DECIDED TO DIVERT TO CMH. THE FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT IN CMH. MAINTENANCE TROUBLESHOT SDR ANCF200800006Duct · damagedENG OVHT DISPLAYED WITH ENG OVHT LIGHT ILLUM. LIGHT EXTING AFTER THRUST REDUCTION AND CAUTION LIGHT ON. 4AW AMM 36-11-01 P.401 / 36-11-07 P.401. REMOVED AND REPLACED BOTH HP2 AND HP6 DUCT ASSY IAW AMM 71-00-00 ENG RUN PERFORMED SATISFACTORY. P/N 312N5306-1 SDR TSAA0836017Control Valve · failedETOPS FLIGHT 841 SNA-HNL - DURING CLIMB, THE CREW NOTED THE RIGHT ENGINE BLEED TRIPPED OFF. THE CREW WAS UNABLE TO RESET THE SYSTEM AND DIVERTED TO ONT. THE AIRCRAFT LANDED IN ONT WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE PRSDR DL76S080394Duct · splitCREW REPORTED HEARING LOUD POP AND FELT EARS POP THEN GOT BODY DUCT LEAK LIGHT. AFT CABIN FILLED WITH SMOKE AND CABIN GOT VERY HOT. PASSENGER SEATED AT 42A GOT A BURN TO HER LEG. PBE AND HALON BOTTLES USED, FLT DIVERTED TO GSP. MTC FOUND PNEU DUCT LOCATED SDR RAIA0803014Bleed Air Sys · malfunctionedFLT 7910 - CVG - BLEED NR 1 AND NR 2 OVERTEMP MESSAGE ON THE EICAS. MAINTENANCE PERFORMED A BLEED SYSTEM OPERATIONAL CHECK OF BOTH THE BLEED SYSTEM AND THE ANTI-ICING SYSTEM WITH NO DEFECTS NOTED.SDR RAIA00803012O-Ring · wornFLT 5571 - STL - BLEED NR 2 LEAK INDICATION ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE BLEED DUCT O-RINGS AND ADJUSTED THE CLAMP ON THE DUCT. OPS CHECKED GOOD.SDR RAIA00803003Filter · dirtyFLT 7887 - ORD - BLEED NR 2 EICAS MESSAGE DURING CLIMBOUT. MAINTENANCE CLEANED THE FAN AIR VALVE FILTER. SYSTEM OPS CHECKED GOOD.SDR CHQA200800044B-Nut · looseLGA TO GSP - AFTER TAKEOFF WHILE CLIMBING IN ICING CONDITIONS, THE CREW RECEIVED AN ENGINE NR 1 BLEED OVERHEAT AND ENGINE ANTI-ICE FAIL MESSAGE ON EICAS. THE CREW EXITED THE ICING CONDITIONS AND RETURNED TO LGA. MAINTENANCE OPENED THE AIRCRAFT AND INSPECTED SDR CHQA200800041Clamp · missingCVG TO GSP - DURING CLIMB-OUT THE CREW RECEIVED AN E1 EXCEEDANCE MESSAGE ON EICAS. THE ITT REACHED 901 FOR 25 SECONDS. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. EMINENCE PERFORMED A GVI OF THE ENGINE AND FOUND THE CUSTOMER MANIFOLD DUCTINGSDR CHQA200800042O-Ring · leakingIAH TO STL. DURING CLIMB THE CREW RECEIVED A BLEED 1 LEAK MESSAGE AT 4,000FT. THE MESSAGE DISAPPEARED AND THEN RETURNED AT 8,000 FT. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE BLEED 1 SYSTEM FOR LEAKS AND REPAIREDSDR CHQA200800043Duct · crackedIAH TO STL - THE CREW RECEIVED A BLEED 1 LEAK MESSAGE DURING CLIMB AND RETURNED TO FIELD AT IAH. MAINTENANCE SECURED THE BLEED 1 SYSTEM CLOSED AND DEFERRED THE NR 1 BLEED SYSTEM. ON THE 26TH MAINTENANCE TROUBLESHOT THE BLEED SYSTEM AND FOUND A LEAK COMING FRSDR RAIA00802022Clamp · brokenFLT 3506 - PIT - ENGINE AND APU BLEED LEAK MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED A BLEED LINE O-RING AND CLAMP. PERFORMED LEAK CHECK OF THE SYSTEM WITH NO DEFECTS NOTED.SDR 2008UALA00955Check Valve · faultyNR 1 ENGINE HAS THE L BLEED OFF EICAS MSG AND L-BLEED OFF LIGHT ON WITH BLEED SELECTED. REPLACED ISOLATION BYPASS CHECK VALVE. FOUND DIRECT SHORT AT PRSOV CONNECTOR. FOUND D22 CONNECTOR ON PRSOV BAD. REPLACED SAME. OPS CHECKED GOOD. REPLACED PRSOV. LEAKSDR CHQA200800030Duct · damagedIAD TO YOW - AFTER GEAR RETRACTION ON CLIMB THE CREW RECEIVED A LAV SMOKE EICAS MESSAGE. WHILE PREPARING TO RETURN TO IAD, THE FLIGHT ATTENDANT VERIFIED THAT THERE WAS NO VISIBLE SMOKE OR ODOR IN THE LAVATORY. SHORTLY AFTER, THE EICAS MESSAGE WENT AWAY AND TSDR Z4TA20080001Tube · contaminatedMAINTENANCE REPLACED RT BLEED AIR TUBE ASSY (P/N 101469-002) DUE TO TIME CHANGE. THE ASSY WAS INSPECTED FOR CONDITION AND RECEIVING DOCUMENTS FOR TRACEABILITY OF THE PART. NO DEFECTS WERE NOTED DURING RECEIVING INSPECTION. GROUND RUNUP OK AFTER REPLACEMENT.SDR ASAA0852547Shutoff Valve · malfunctionedLEFT DUCT PRESSURE INDICATOR FLUCTUATED DURING CLIMBOUT AT 3 SECOND INTERVALS. INITIALLY 35 PSI TO 55 PSI, ABOVE 10 000' 35 PSI TO 50 PSI. FLUCTUATION QUIT APPROACHING FL190. BOTH INDICATORS FLUCTUATED TOGETHER THEN SETTLED OUT. PERFORMED NR 1 ENGINE BLEEDSDR GUUA02100801Bleed Air Sys · contaminatedFLIGHT: 5401, DURING FLIGHT, FUNKY SMOKE ODOR IN THE COCKPIT WITH BLEED OPEN. CLEANED RESIDUAL OIL, FROM OIL SERVICING.SDR ANCF200800004Air Duct · leakingEICAS MESSAGE "L ENG OVHT" DISPLAYED, WITH "ENG OVHT" LIGHT ILLUM. LIGHT REMAINED ILLUM AFTER THRUST REDUCTION, ENGINE WAS SHUTDOWN , (LIGHT EXTINGUISHED INITIALLY AFTER THRUST REDUCTION BUT AFTER FEW SECONDS IT ILLUMINATED AGAIN). PERFORM FIM 26-11-00 AND FSDR MJN1Seal · wornCREW REPORTED SMOKE IN CABIN, FOLLOWED PROCEDURES TO CLEAR SMOKE AND ISOLATED POWER TO MEDICAL EUIPMENT BELIEVING THAT WAS THE SOURCE. NO ADDITIONAL SMOKE OR SMELL WAS OBSERVED. WHILE EN ROUTE TO MAINTENANCE FACILITY THE CREW REPORTED HEARING AND FEELING A LSDR CHQA20080021O-Ring · leakingIAH TO MCI - DURING CLIMB "BLEED 1 LEAK" MESSAGE APPEARED ON EICAS. THE CREW FOLLOWED THE QRH AND THE MESSAGE WENT AWAY. AFTER CONFERRING WITH MAINTENANCE CONTROL IT WAS DECIDED TO RETURN TO FIELD AT IAH. MAINTENANCE INSPECTED THE BLEED SYSTEM AND FOUND JOISDR MASA200800101Sensor · malfunctionedFLT 2816 - SMOKE IN FLIGHT DECK AFTER APU START. MX CHANGED BLEED TEMP SENSOR.SDR RAIA00801027Clamp · looseFLT 7892 ORD - NR 1 BLEED LEAK ON EICAS WHEN CLIMBING THROUGH 10KFT IN ICING CONDITIONS. MAINTENANCE FOUND A LOOSE DUCT CLAMP IN THE LEFT PYLON. PERFORMED AN OPERATIONAL CHECK OF THE BLEED SYSTEM WITH NO DEFECTS NOTED.SDR DJSR20080125Pressure Valve · malfunctionedNR 1 BLEED OVERHEAT LIGHT ILLUMINATED PASSING 15,000 WITH CORRESPONDING CABIN PRESSURE FLUCTUATIONS.SDR RAIA00801026B-Nut · looseFLT 8003 - IAD - NR 1 BLEED LEAK MESSAGE ON THE EICAS DURING CRUISE. MAINTENANCE RESECURED A LOOSE B-NUT AT THE NR 1 ENGINE FAN AIR VALVE REFERENCE LINE. OPS CHECKED GOOD.SDR C2XA08TY011Valve · malfunctionedBLEED 1 & 2 LOW TEMP WING ANTI ICE (2) FAIL WHILE IN ICING CONDITIONS. REMOVED AND REPLACED HIGH STAGE VALVE AND LOW PRESSURE SWITCH IAW EMB 145 XR AMM 36-11-02 & 30-11-11, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. SWITCH P/N APS7-1000, S/NSDR UPS08M51407Valve · defectiveINSPECTION TYPE:N/A ATB - LEVEL 1 ALERT; ANTI ICE FAIL MESSAGE. PER BOW#TS2220 998 WAN #1316400 PERFORMED LEAK TEST AND PROOF TEST NR 1 ENG HIGH STAGE VALVE SENSE LINE PER MM 36-10-00-5. NO LEAK NOTED. REPLACED HIGH STAGE PILOT VALVE PER MM 36-11-20. REPLASDR RAIA00801010Thermostat · malfunctionedFLT 7908 - ORD - BLEED 1 OVERTEMP MESSAGE ON EICAS WHEN CLIMBING THROUGH FL150. MAINTENANCE REMOVED AND REPLACED THE FAN AIR CONTROL THERMOSTAT. OPS CHECKED GOOD.SDR N6WA0080103Gasket · leaking5387-STL-LT ENGINE FIRE MASTER WARNING. FOUND BLOWN GASKET ON PRESSURE REGULATING SHUTOFF VALVE. REPLACED GASKET, LEAK CHECK GOOD.SDR CALA0800017Clamp · looseAT FL340 APPROX 70 MILES SOUTH OF DFW GOT CABIN WARNING HORN, SAW CABIN AT 10,500 WENT TO STBY NO HELP. EMERGENCY DESCENT TO LANDING IN DFW DUE TIME CONSTRAINTS AND TRYING TO KEEP CABIN BELOW 14000. LANDED SAFELY IN DFW. FOUND LEAK IN KEEL BEAM AREA (WHEEL SDR GLBA20061042Bleed Air Sys · contaminatedSMOKE/SMELL, PILOTS REPORTED STRONG ODOR OF SMOKE IN CABIN FOLLOWED BY SMOKE AURAL WARNING FROM LAV SMOKE DETECTOR. MAINTENANCE CLEANED BLEED DUCT AND BELLY PANEL OF GLYCOL FLUID. MAINTENANCE RAN ENGINES AND OPERATIONAL CHECKS WERE GOOD IAW MM 21-23.SDR DL76L081134Isolation Valve · inoperativeL ISOL VALVE EICAS MSG, SWAPPING WITH CTR LEFT ISOLATION VLV. REPLACED AND CHECKED OK. PN 2780539-103.SDR CA080108005Hose · cracked(CAN) ON CLIMB OUT TO CRUISE ALTITUDE, IT WAS DISCOVERED THE AC WOULD NOT PRESSURIZE, AND THERE WAS NO BLEED AIR HEAT. AC RETURNED TO BASE. FOUND BLEED AIR HOSE CRACKED. (TC NR 20080108005)SDR IXXA080001ORegulator Valve · defectiveDURING CRUISE FROM KMLB, THE CREW NOTICE THE LEFT PNEUMATIC MANIFOLD READ'S 17 PSI LOWER THAN THE RIGHT SIDE, THE LEFT SIDE READ'S 20 PSI AND THE RIGHT SIDE READ'S 37 PSI. THE LEFT SIDE MANIFOLD COULD NOT REACH 35 PSI TO DO PRESSURE DECAY CHECK, THE LEFT SIDESDR UPS08551366Bleed Air Sys · leakingINSPECTION TYPE:N/A DIVERSION - SHORTLY AFTER LVL OFF AT 370 MSTR WARNING BELL SOUNDED & EICAS W/W FIRE ILLUMINATED. LOWERED & DESCENDED IAW QRH. WHEEL WELL FIRE INDICATION STAYED ON FOR 8 MINUTES. AFTER INDICATION WENT OUT DUCT LEAK LP STATUS MSG ILLUMINATSDR C2XA08ON057O-Ring · burned outFLT 421 - SAN TO ONT - AFTER TAKEOFF FLIGHT CREW REPORTED BLEED LEAK. A/C DIVERTED TO ONT WITHOUT NOTIFICATION, BUT NO EMERGENCY WAS DECLARED, A/C LANDED WITHOUT INCIDENTS. MX PERSONNEL FOUND A BLEED LEAK IN THE CARGO COMPARTMENT, REMOVED AND REPLACED BOTH OSDR COMA0760746Duct · damagedFLIGHT 5205 - RECEIVED ANTI-ICE WARNING MESSAGE. RIGHT FUSELAGE SHOWING RED. MESSAGE CLEARED WHEN SYSTEM SELECTED FF, DID NOT GO INTO STANDBY. DECLARED EMERGENCY, RETURNED TO CVG, LANDED WITHOUT INCIDENT. REPAIRED RIGHT NR 2 DUCT (REO601-36-10-002). NO FUSDR BSAASDR0728Tube · defectiveRIGHT BLEED FAIL ILLUMINATED IN FLIGHT. ITEM INITIALLY DEFERRED. REMOVED AND REPLACED EVA TUBING, RAN AIRCRAFT OPERATIONAL CHECK GOOD.SDR QXEA200702030Switch · malfunctionedSEA - FLIGHT 2239 - NR 1 BLEED HOT CAUTION LIGHT CAME ON DURING TAXI. COMPLIED WITH CHECKLIST AND TAXIED BACK TO THE GATE. MAINTENANCE REPLACED THE BLEED OVERTEMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR QXEA200702025Switch · malfunctionedSEA - FLIGHT 2322 - NR 2 BLEED CAUTION ILLUMINATED ON TAXI. TURNED OFF THE BLEED PER THE CHECKLIST AND THE LIGHT STAYED ON. RETURNED TO THE GATE. MAINTENANCE REPLACED THE PRE COOLER OUTLET DUCT (PN 820908-3) AND THE OVERTEMP SWITCH. OPERATIONAL CHECKS GOODSDR C2XA07ON051Duct Clamp · looseFLT 210 - SMF TO ONT - FLIGHT CREW REPORTED E2 ITT JUMPED 110 DEGREES AFTER T/O WITH WF INCREASE & N1 DROP-BLEED SELECTION ONLY 10 DEGREES. MX PERSONNEL RE-ADJUSTED AND TORQUED V-BAND CLAMP OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FORSDR DHLA200700091Clamp · looseNR 1 ENG STRUT OVERHEAT DURING CRUISE. PERFORMED ABNORMALS PROCEDURE RESULTED IN IN-FLIGHT ENG SHUTDOWN ALL CHECK LISTS, PROCEDURES DONE. T/S FOUND CLAMP ON PRESSURE MODULATING VALVE LEAKING ON PRECOOLER SIDE TIGHTENED CLAMP IAW MM 36-00-1 MM 36-12-42, RAN ESDR HNAA0800008Bleed Air Sys · contaminatedDURING OPERATION, AN ODOR THAT WAS BELIEVED TO BE FUEL WAS DETECTED WHEN NR 1 ENGINE BLEED SYSTEM WAS SELECTED ON. BLEED SYSTEM FOR NR 1 AND NR 2 ENGINES, ALONG WITH THE APU, WERE INSPECTED AND FOUND TO BE IN ORDER. SYSTEM WAS RUN AT FULL HOT AND FULL COLD. SDR GUUA12180703Clamp · looseFLT 9280, IMMEDIATELY AFTER TAKEOFF, GOT LT ENVIRONMENTAL FAIL ANNUNCIATOR ILLUMINATED. CYCLED BLEED VALVE SWITCH AND LIGHT WENT OUT. TEN MINUTES LATER DETECTED SMOKE AND MELTING PLASTIC ODOR. CYCLED BLEED SWITCH OFF AND SMELL STOPPED. NOT NECESSARY TO USESDR BB07100Duct · leakingFLIGHT 790, CLT-BOS: AIRCRAFT DIVERTED TO PHL DUE TO A NUMBER 2 ENGINE OVERHEAT MESSAGE. CREW REDUCED THROTTLE TO IDLE AND WARNING WENT AWAY. MAINTENANCE REPLACED THE HP2 AND HP6 BLEED DUCTS. NO FURTHER FAULTS.SDR QXEA200701913Switch · malfunctionedSEA - FLIGHT 2322 - NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED. DUCT TEMP WAS 30 DEGREES C. RAN CHECKLIST, CAUTION WENT OUT. TURNED BLEED BACK ON, DUCT WAS AT 20 DEGREES AND CAUTION CAME BACK ON. NO HEAT IN FLIGHT COMPARTMENT. LEFT BLEED OFF. MAINTENANCE RSDR UALA2008111305114Regulator · faultyFLIGHT LOST CABIN PRESSURE, DESCENDED TO FL 100. FLT ABLE TO PRESS CABIN CLIMB TO FL240. UNABLE TO CLIMB HIGHER. CONTINUED FLIGHT TO PLANNED DESTINATION. OPENED ENGINE CHECKED REGULATOR AND SENSE LINES FOR DISCREPANCIES. SUPPLY SENSE LINE FOUND BROKEN (90SDR 07FDEA05062Valve · failedNEAR TOP OF CLIMB, NR 3 AIR SYS OFF LIGHT ILLUMINATED. NR 3 DUCT DISPLAYED RED MOMENTARILY UNTIL AUTO SHUTDOWN. DIVERTED DUE TO INABILITY TO USE WING ANTI-ICE VALVE - INOP CLOSED. DO NOT USE NR 3 PNEUMATIC SUPPLY SYSTEM." DECAY CHECK C/W PER M/M 36-00-01SDR QXEA200701914Switch · malfunctionedYVR - FLIGHT 2276 - ON FINAL APPROACH (6 MILES OUT), THE NR 1 BLEED HOT CAUTION LIGHT CAME ON. RAN THE CHECKLIST AND IT STAYED ON THROUGH THE APPROACH LANDING AND TOUCHDOWN. MAINTENANCE REPLACED THE NR 1 BLEED OVERTEMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCSDR RAIA00712017Duct · looseFLT NR 5564 - OKC - BLEED 1 & 2 LEAK. MAINTENANCE RESECURED DUCT CHECK GOOD.
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