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 VJ32002F00056Pump · failedIN FLIGHT THE INSTRUMENT VACUUM SYSTEM FAIL. THE AIRCRAFT RETURNED TO MAINTENANCE AND AN INSPECTION OF THE SYSTEM FOUNDED THAT THE ROTOR SHAFT HAD SHEARED. PUMP WAS REMOVED AND A NEW PUMP INSTALLED. OPERATIONAL CHECK OF THE SYSTEM CHECKED NORMAL. PART SENTSDR Q2S2002F00001Valve · malfunctionedAIR TURN BACK: AFTER LIFT OFF, HIGH STAGE LIGHT ILLUMINATED ABOUT 200 FEET. FIRE DETECTION LIGHT ILLUMINATED AT MASTER CAUTION PANEL, NO LIGHT IN HANDLE. A AND B NEEDLE INDICATORS WERE AT 7.5. TESTED SYSTEM, NR 3 LIGHT CAME ON AND STAYED ON. SHUT DOWN ENGSDR PCAA0206065Seal · leakingPHL-SYR FLIGHT 3814. WHILE IN CRUISE FLIGHT CREW REPORTED REAR BAY OVERHEAT CAUTION LIGHT FOR APU ILLUMINATED. CREW DECLARED AN EMERGENCY AND DIVERTED TO MDT. MAINTENANCE FOUND A BLEED LEAK IN REAR BAY. O-RING AND PERRY SEALS REPLACED ON BLEED LINES. OPERSDR DL757020665Valve · malfunctionedAT FLT 350-370 LT ENG FLUCTUATED EPR 1.11-1.24, EGT 438-460 AND N1 79.1-82.2. DUCT PRESS FLUX 30-60 PSI. MCC REQUESTED TURN OFF LT BLEED AND FLUX STOPPED. DIVERTED TO MCO DUE TO EN ROUTE WX. PERF PFHB TEST 06 AND 13, NO ANOMALIES NOTED. REPLACED HIGH STAGSDR GLBA2002085Tube · damagedRT BLEED AIR FAILED IN FLIGHT. FOUND CHAFED HOLE IN EVA TUBING RT WING. REPAIRED HOLE.SDR AWXA200200489Filter · cloggedON CLIMBOUT, CREW RECEIVED ECAM MESSAGE FOR NR 1 ENG BLEED FAULT; BLEED TEMP REACHED 280 DEGREES & CROSSFEED VALVE OPENED; ACFT TURNED BACK TO PHX. MX REPLACED THE FAN AIR THERMOSTAT AND OPERATIONALLY CHECKED OUT SYS BY RUNNING ENG FOR AN EXTENDED PERIOD OF TSDR 02FDEA00370Duct · leakingLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AFTER 1+10 FLIGHT TIME. DID RED TAB PROCEDURE. ISOLATED LEAK ON NR 3 ENG BETWEEN BLEED VALVE AND RIGHT PACK VALVE. FOUND STARTER DUCT LEAKING ON NR 3 ENG BLEED MANIFOLD. STARTER DUCT WAS MISALIGNED, REALIGNED STARSDR AUS20020496Controller · faulty(AUS) BLEED AIR PRV CONTROLLER SUSPECT FAULTY.SDR AUS20020471Duct · cracked(AUS) RT ENGINE LP SUPPLY DUCT CRACKED.SDR 02FDEA00337Valve · failedON CLIMB NR 2 PNEU TEMP HI LIGHT ILLUM'D. SHUTDOWN PNEU SUPPLY SEL. PERFORMED RED TAB PROC. REMOVED AND REPLACED THE NR 3 PACK FLOW VALVE AND THE NR 1 PNEU PRESS REGULATOR VALVE. ALL CHECK OK.SDR COMA0260313Overheat LoopFLIGHT 5280 LEFT ENGINE 14TH STAGE BLEED AIR LEAK WARNING.COULD NOT DUPLICATE. RESET SYSTEM, NO DEFECTS FOUND.SDR 02FDEA00332Clamp · leakingDURING INITIAL CLIMB, ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, WING ANTI ICE VERIFIED CLOSED, NR 1 ENG BLEED AIR SWITCH CLOSED AND NR 1 ENG THRUST LEVER TO IDLE IAW RED TABS, STRUT OVERHEAT LIGHT EXTINGUISHED AFTER 3 MINS AND OVERHEAT SYSTEM TESTED SATISFACTSDR AALA20020645Duct · blownEWR - FLT 1927 - ON CLIMB-OUT, EN ROUTE EWR-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER AIRFOIL ANTI-ICE SWITCHES PLACED ON. LIGHT WENT OUT AFTER COMPLETED PROCEDURE. PRESSURIZATION FLOW LIGHT ALSO CAME ON SEVERAL TIMES. RETURNED AND LANDSDR 02FDEA00326Clamp · looseLOWER AFT BODY OVERHEAT LIGHT FLICKERED SEVERAL TIMES THEN REMAINED ON STEADY FOR APPROX 20 SEC IN FLT WHILE EXECUTING PROC IN ORH LIGHT WENT OUT. PERFORMED RESISTANCE CHECKS OF OVERHEAT ELEMENTS. ALL RESISTANCE CHECKS ARE GOOD PER MM 26-14-001-2. GAIN ACCESDR GLBA2002060Tube · damagedLEFT BLEED-AIR FAILURE. REPAIRED DAMAGED ENA TUBING AT WING, OPS GOOD.SDR GAIA2002F0000Duct · blownAFTER TAKEOFF, THE NR 3 FIRE WARNING CAME ON. THE CREW DECLARED AN EMERGENCY, SHUT DOWN NR 3 ENGINE AND THE WARNING LIGHT EXTINGUISHED. THE FLIGHT RETURNED TO AIRPORT AND LANDED UNEVENTFULLY. MAINTENANCE FOUND THE 13TH STAGE DUCT FROM THE PRBC AND FUEL HEATSDR KBMA113826Line · wornP2 LINE WAS WORN BEYOND LIMIT. REPLACED WITH NEW P2 LINE.SDR COOSDR02112Duct · crackedAIR CONDITIONING BAY STA 850 PNEUMATIC DUCT CRACKED.SDR AWXA200200383Filter · contaminatedON CLIMBOUT, CREW RECEIVED ECAM MESSAGE FOR NR 1 ENG BLEED FAULT; BLEED TEMP REACHED 280 DEG & CROSSFEED VALVE OPENED; ACFT RETURNED. MX REPLACED FAN AIR THERMOSTAT & OPERATIONALLY CHECKED OUT SYS BY RUNNING ENG FOR AN EXTENDED PERIOD OF TIME AT POWER, CHECKESDR AWXA200200379Computer · faultyEN ROUTE FLT CREW RECEIVED ECAM MESSAGE FOR NR 2 ENG BLEED FAULT TEMP AT 70 C AND 70 PSI; DUE TO ICING CONDITIONS AT IND, ACFT TURNED BACK TO PHX. MX TROUBLESHOT & REPLACED NR 2 BLEED MONITORING COMPUTER, BITE CHECK GOOD, NR 2 ENG PRESSURE TRANSDUCER REPLACEDSDR GAIA02038OPClamp · out of positionFLT 874 - LAX-FWA - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, AND OPERATED AT REDUCED THRUST TO EXTINGUISHED THE LIGHT. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. ADJUSTED SHIMS AND REPSDR GAIA02036OPClamp · out of positionFLIGHT 863 - EWR-FWA - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, AND OPERATED AT REDUCED THRUST. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. REPOSITIONED CLAMP ON HIGH PRESSURE BLEED DUCSDR MEX2002116Duct · leakingFLT 489 - SJD-ACA - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCES OF HIGH TEMPERATURE IN ENGINE NR 2 (470 GRADES), ENGINE WAS STARTED WITH A PNEUMATIC POWER GETTING 380 GRADES. DURING OVERNIGHT SERVICE WERE REPAIRED TWO PNEUMATIC LINES WITH LEAKS, TESTS WERE SDR VJ32002F00022Pump · inoperativeNO INSTRUMENT AIR PRESSURE AT 1000 RPM, SYSTEM CHECKED AND FOUND THE AIR PUMP HAD NO OUTPUT. PUMP WAS REMOVED AND A NEW PUMP INSTALLED. GROUND RUN OF THE AIRCRAFT SYSTEM CHECKED NORMAL.SDR GAIA02035OPClamp · looseFLT 864 - FWA-EWR - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, THE LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT EWR WAS UNEVENTFUL. FOUND AIR LEAK AT THE NR 3 BLESDR GAIA02034OPClamp · looseFLT 879 - FWA-SJC - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, THE LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT SJC WAS UNEVENTFUL. FOUND SEVERAL LOOSE CLAMPS ANDSDR P2EA2002M024Duct · cloggedTAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED AFTER TAKEOFF OUT OF LAX. INSPECTED TAIL COMPARTMENT, FOUND THE LEFT HAND SENSOR OFF AND THE DUCT TO CHECK VALVE CLOGGED WITH DEBRIS. SECURED THE LEFT HAND SENSOR AND CLEANED DUCT. OPS CHECKED, ALL PARAMETERS NORSDR QXEA0200630Valve · malfunctionedSEA- HAZE IN CABIN AND COCKPIT AFTER START UP. CLEARED SHORTLY AFTER. APPEARS TO BE DURING START UP OF NR 1 ENGINE. REMOVED AND REPLACED SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR AWXA200200257Heat Exchanger · crackedPHX - DIVERSION - FLT 0546 - WHILE ENROUTE FROM LAS TO DFW THE R/H WING TO BODY OVERHEAT LIGHT ILLUMINATED, AIRCRAFT DIVERTED TO PHX. MAINTENANCE INSPECTED THE R/H PACK BAY AND FOUND 2 LOOSE/LEAKING CLAMPS. A FOLLOW UP (FUP) WAS ISSUED FOR A PNUEMATIC DUCT ANDSDR 02FDEA00219Periseal · failedAFTER T/O NR 3 PNEU MANIFOLD FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED PERISEALS PER SMP.SDR MWEA020173Regulator · defectiveRIGHT AIRFOIL ICE PROTECTION TEMP HIGH LIGHT CAME ON DURING TAIL PORTION OF ICE PROTECTION CYCLE. FOLLOWED QRH AND GOT RIGHT AIR TEMPERATURE HIGH LIGHT. REMOVED AND REPLACED PNEUMATIC PILOT PRESSURE REGULATOR. REF MM 36-10-02 PER T/S CHECKED DUCT TEMPS, FOUSDR GAIA02025OPDuct · warpedFLT 873 - FWA-LAX - DURING CLIMB-OUT, THE NR 1 STRUT OVERHEAT LIGHT CAME ON FIVE MINUTES AFTER TAKEOFF. THE AIRCRAFT RETURNED TO FWA AND THE LANDING WAS UNEVENTFUL. FOUND THE 13 STAGE DUCT IN THE STUB WING AT THE HIGH PRESSURE WING ANTI-ICE VALVE FLANGE WARPSDR 2002FA0000407Tube · meltedRIGHT INSTRUMENT AIR PRESSURE WAS AT ZERO ON THE GROUND AND WOULD INCREASE AS CABIN PRESSURE INCREASED IN FLIGHT. FOUND PNEUMATIC SUPPLY LINE FROM COMMON TEE TO FORWARD PRESSURE BULKHEAD MELTED. REPLACED TUBING WITH SUPERSEDED (PN P610051) TWICE. BOTH TIMESSDR 2002FA0000406Tube · meltedRIGHT INSTRUMENT AIR PRESSURE WAS AT ZERO ON THE GROUND AND WOULD INCREASE AS CABIN PRESSURE INCREASED IN FLIGHT. FOUND PNEUMATIC SUPPLY LINE FROM COMMON TEE TO FORWARD PRESSURE BULKHEAD MELTED. REPLACED TUBING.SDR 2002FA0000405Tube · meltedRIGHT INSTRUMENT AIR PRESSURE WAS AT ZERO ON THE GROUND AND WOULD INCREASE AS CABIN PRESSURE INCREASED IN FLIGHT. FOUND PNEUMATIC SUPPLY LINE FROM COMMON TEE TO FORWARD PRESSURE BULKHEAD MELTED. REPLACED TUBING.SDR CHQ000131Duct · leakingBLEED LEAK IN CARGO BIN, FIRE BOTTLES DISCHARGED, AND OVERWEIGHT LANDING.SDR VJ32002F00012Pump · inoperativeLOW OUTPUT FROM PUMP TO AIRCRAFT, REMOVED PUMP AND INSTALLED NEW PUMP OPERATION WAS NORMAL. PUMP SENT IN FOR WARRANTY.SDR 02022502Duct · leakingDURING CLIMB, PASSING THROUGH 8,000 FT MSL, LENG OVERHEAT EICAS MESSAGE CAME ON. SECURED BLEED VALVE, RETARDED THRUST; MESSAGE EXTINGUISHED. INVESTIGATION REVEALED HP6 DUCT LEAKING. REPLACED HP6 DUCT, LEAK CHECKED GOOD.SDR DL764020223Cooler · failedFOUND METAL IN OZONE CONVERTER. METAL CONTAMINATION A RESULT FROM A FAILED/MELTED ENGINE PNEUMATIC PRECOOLER, 767-400 FLEET HISTORY. REMOVED RT ENG RT CORE COWL. REMOVED PRECOOLER. INSTALLED PRECOOLER PER MM. INSTALLED CORE COWL, LEAK CHECK GOOD. ALSO RESDR AWXA200200157Duct · disconnectedPHX - AIR TURNBACK - FLT 0081 - O - ON TAKEOFF OUT OF PHX EN ROUTE TO BWI THE NR 1 ENGINE FIRE WARNING SYSTEM ACTIVATED WITH THE FIRE SWITCH HANDLE ILLUMINATING, A RED MASTER WARNING LIGHT, A RED FIRE LIGHT ON INSTRUMENT PANEL, A RED FUEL CONTROL SWITCH, THE FSDR WRLA200204Duct · rupturedEMERGENCY LANDING DUE TO MODERATE CABIN SMOKE/CARGO DECK. REMOVED AND REPLACED AFT LEFT SIDE DUCT ASSEMBLY, P/N AAM7241-1, DUCT ASSY AFT WELDED. REMOVED AND REPLACED AFT LEFT SIDE DUCT ASSY AFT WELDED. LEFT SIDE AFT FUSELAGE PNEUMATIC DUCT ASSY. (M)SDR PCS2002F00007Coupling · looseCREW REPORTED NR 3 STRUT OVERHEAT LIGHT CAME ON. FOLLOWED AJT ABNORMAL PROCEDURE LIGHT WENT OUT. AFTER THROTTLE ADVANCEMENT LIGHT CAME BACK ON. AIRCRAFT DIVERTED BACK, DUMPED 30,000 LBS OF FUEL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A LOOSESDR C2XA02IA031Clamp · brokenIAH- DURING FLIGHT 3630 THE CREW NOTED THAT THE #1 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING CLIMBOUT. THE CREW SHUT DOWN THE #1 ENGING,PULLED THE #1 ENGING FIRE BOTTLE HANDLE,DECLAIRED EMERGENCY, AND, RETURNED TO IAH WITHOUT INCIDENT. IAH- MAINTENANCE SDR 02072635Insulation · failedDuring cruise of the flight from SAV to ORD, the crew reported that the L/H engine 14th stage duct EICAS message illuminated. The crew accomplished the QRH procedures and diverted to CAE where the aircraft was landed without incident. Maintenance personnel fSDR USAABB02014Duct · leakingLAX - FLT 46 - CREW RECEIVED THE LEFT ENGINE 'OVHT' LIGHT AFTER TAKEOFF FROM LAX. FLIGHT RETURNED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED FIM PROCEDURES 26-11-00 AND RAN THE LEFT ENGINE FOR FIVE MINUTES. NO FAULTS WERE FOUND AND THSDR F3LA200200031Duct · damagedAIR TURNBACK. FLIGHT CREW REPORTED RT WING/BODY OVERHEAT LIGHT ILLUMINATED AND AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACARD THE RT PACK INOPERATIVE PER MEL 21-2 AND SUBSEQUENTLY REPLACED DAMAGED DUSDR 02FDEA00091Controller · malfunctionedON CLIMBOUT NR 2 BLEED FAULTED. REMOVED AND REPLACED PSC 2.SDR CNMA200200001Regulator Valve · inoperative#3 PNEUMATIC SUPPLY PRESSURE READS ZERO WITH SUPPLY SELECTOR IN ANY MODE. COM PROCEDURES ACCOMPLISHED ON CLIMBOUT. #2 PNEUMATIC SUPPLY HI TEMP ILLUMINATED. TEMP GUAGE INDICATED RE LINE.SDR 2002UALA00171Shutoff Valve · defectiveRIGHT ENGINE BLEED OFF MSG PER CREW AND NO DUCT PRESSURE ON RIGHT SIDE AND LOST RIGHT PACK. PRSOV MANUAL HEX OVERRIDE NUT OUT OF OPEN DETENT AND SAFETY WIRE BROKEN. REPLACED PRSOV.SDR USAASB02017Regulator · failedBOS - FLT 926 - CLIMBING-OUT FROM PHL, EN ROUTE TO PWM AT FL250, THE NR 2 ENGINE BLEED TRIP LIGHT ILLUMINATED. CREW TRIED TO RESET BLEED WITH NO HELP. WITH NR 2 BLEED INOPERATIVE, PRESSURIZATION WAS OK AT FL250 FOR 15 MINUTES, BUT THEN THE CABIN PRESSURE BEG
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