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 GTIA9700264Clamps · looseON TAKEOFF TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. AMBIENT TEMP WAS 82 F AND APU HAD BEEN OFF FOR 10 MIN. RAN T/O POWER W/13TH STAGE BLEED ON. FOUND LOOSE CLAMPS ABOVE AND BELOW AIR CONDITIONING PRESSURE REGULATOR AND OUTBOARD CLAMP AT AVERAGE VALVE. SDR AU970313Seal · leaking(AUS) ANTI-ICE AIR DUCT SEALS LOCATED AT REAR END OF SPINE LEAKING -NO4 ENGINE AIR VALVE CONNECTOR. SUSPECT MOISTURE INGRESSSDR 97ZZZX1900Non Return Valve · crackedVALVE FLAPPERS DEVELOP CRACKS. FLAPPER TO BODY HINGE HAS PREMATURE WEAR CAUSING HINGE TO SEPARATE FROM BODY. SUBMITTER STATED COMPONENT CONSTRUCTION IS ALUMINUM ALLOY. TIME CONTROL OF COMPONENT MAY ELIMINATE EXCESSIVE WEAR CONDITIONS ELIMINATING OPERATOR DISDR DLM88970528Augmentation Vlv · malfunctionedDURING CLIMBOUT, F/A CALLED WITH STRONG BURNING SMELL INBACK. GOT RT ICE PROT HI-LIGHT. BOTH XFEEDS CLOSED. REDUCED PWR ON RT ENG AND SELECTED HP BLEED OFF ON RT PACK. LIGHT WENT OUT. ADVANCED RT THROTTLE, LIGHT CAME BACK ON. REDUCED PWR LIGHT WENT OUT. SDR 97ZZZX2972Clamp · looseNR 3 ENGINE FIRE WARNING ON CLIMB. TIGHTENED 8TH STAGE BLEED AIR DUCT CLAMP AND FIRE LOOP CONNECTOR. REF: OPERATOR CONTROL NR 97ZZZX2973. (X)SDR 97FDEA00185Duct · separatedNR 2 ENG TEMP ADV IN CRUISE WITH NR 2 NAC TEMP = 270 DEGREES C, FOLLOWED BY NR 2 THROTTLE WOULD NOT MOVE, FOLLOWED BY NR 2 BLEED FAULT. SHUT DOWN ENG NR 2 TO LAND, ALL OTHER ENG PARAMETERS PRIOR TO SHUTDOWN NORMAL. NR 2 OIL PRESS WAS NOT OBSERVED PAST SHUTDOSDR RAIA970312Seal · failedJFK - FLT 7650 - LEFT DUCT FAIL LIGHT ILLUMINATED. MAINTENANCE REPLACED LEFT DUCT BLEED AIR SEALS. (X)SDR DHL97741001Coupling · looseLOWER AFT BODY O'HEAT LIGHT ILLUMINATED AFTER TAKEOFF. NR 3 THRUST LEVER REDUCED BELOW 1.6 EPR. LOWER AFT BODY O'HEAT LIGHT WENT OUT. FOUND RUBBER BOOT LOOSE. REPOSITIONED BOOT, CLAMP AND ASSOCIATED DUCTS. OPS CHECK GOOD, NO LEAKS NOTED.SDR COMA9760064Bleed Valve · failedANTI-ICE DUCT WARNING ON EICAS, 14TH STAGE BLEED VALVE WOULD NOT CLOSE. REPLACED THE RT 14TH STAGE BLEED VALVE.SDR 97ZZZX1363Bolt · failedFOUND EVIDENCE OF A BLEED AIR LEAK ON THE INBOARD UPPER COWL OF THE NR 2 ENGINE. REMOVED COWL AND FOUND BLEED AIR FLANGE (ITEM NR 159C REF PAGE 2) SEPARATED APPROXIMATELY .1250 INCH. BOTH BOLTS (ITEM NR 160) HAD THEIR HEADS SHEARED OR POPPED OFF. THE GASKETSDR M3HA97051Clamp · brokenHNL - FLT 654 - AFTER TAKEOFF FROM HNL, NR 2 ENGINE LEFT ON CAP CAME ON. NR 2 ENGINE ITT AND TEMPERATURE NOTED HIGH, FOLLOWED BY ENGINE FIRE INDICATION, SECURED ENGINE. DISCHARGED ENGINE FIRE EXTINGUISHER. FIRE INDICATION WENT OUT. AIRCRAFT RETURNED TO HNLSDR USAAF97028Line · loosePIT - FL 305 - CREW NOTED MFDU MESSAGE WING ANTI-ICE LOW CAPACITY. SHORTLY THEREAFTER, THE TAIL ANTI-ICE FAULT ILLUMINATED. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE LINE FROM THE LEFT ENGINE TMSOV TO THE PNEUMATIC THSDR P5CA9700424Precooler · crackedNR 3 PRECOOLER CRACKED. WELDED PER BAC 5975.SDR 97ZZZX1209Valve · failedDURING ROUTINE PRIMARY INSPECTION, FLAPPER VALVE TEST WAS PERFORMED IAW BEECH MODEL 90 MM. VALVE FAILED TEST AND WHEN REMOVED, IT WAS DISCOVERED THAT THE RUBBER DIAPHRAGM INSIDE THE VALVE HAD SEPARATED FROM ITS HINGE AND WAS CARRIED INTO THE BLEED AIR DISTRIBSDR G60A007Cdp Tube · rupturedAFTER T/O FROM JFK, CREW REPORTED NR 2 ENG FIRE LIGHT ILLUMINATED AT 500 FT FOR BOTH LOOPS AND STAYED ON UNTIL CLIMB POWER SELECTED. APPROX 30 SECONDS LATER AS CLIMB CONTINUED AT APPROX 3000 FT LOOP 'A' LIGHT CAME ON AND 15 SECONDS LATER LOOP 'B' LIGHT AND FSDR SWIA97874Press Reg Valve · malfunctionedDUCT LEAK LIGHT ILLUMINATED ON RIGHT ENGINE. RETURNED TO FIELD. REMOVED AND REPLACED RIGHT PRESSURE REGULATOR VALVE IAW MM 30-10-00. RAN RIGHT ENGINE. PRESSURE REGULATOR VALVE OPS CHECKS NORMAL WITH NO LEAKS NOTED AND NO DUCT LEAK LIGHTS.SDR SWIA97873B-Nut · looseDUCT LEAK LIGHT ILLUMINATED. SHUTDOWN RIGHT ENGINE AND RETURNED TO FIELD. FOUND B-NUT FITTING LOOSE ON 18 PSI REGULATOR. TIGHTENED FITTING AND RAN ENGINE TO TAKEOFF POWER. NO DUCT LEAK LIGHT NOTED AND OPS CHECKS GOOD.SDR REXA97052Pre-Cooler · oil soakedLEFT BLEED AIR PRE-COOLER HAS SMOKE COMING FROM IT. CLEANED LT PRE-COOLER WITH TRYC AND WATER. (M)SDR REXA97033Precooler · oil soakedSMOKE COMING OUT OF LEFT PRE-COOLER INTAKE. CLEANED AND INSPECTED LEFT ENGINE BLEED PRE-COOLER. PERFORMED GROUND RUNS. (X)SDR 97ZZZX2690Manifold Assy · failedJFK/ MIA - AT ABOUT 17:39Z: APPROXIMATELY 3-4 MINUTES AFTER TAKEOFF, NR 1 FIRE WARNING/LOOPS/SOUNDED, UPON THROTTLE RETARDING, THE LIGHT WENT OUT. COMPLETED FIRE SHUT DOWN LIST AND FIRED BOTH FIRE BOTTLES. DUMPED ABOUT 20,000 POUNDS OF FUEL. TURNED BACK TOSDR 97ZZZX2084Bleed Manifold · rupturedJFK/MIA - FLT 23 - AT ABOUT 17:30: APPROXIMATELY 3 TO 4 MINUTES AFTER TAKEOFF, NR 1 FIRE WARNING/LOOPS/SOUNDED. UPON THROTTLE RETARDING, THE LIGHT WENT OUT, COMPLETED FIRE SHUT-DOWN LIST AND FIRED BOTH FIRE BOTTLES. DUMPED ABOUT 20,000 POUNDS OF FUEL, TURNESDR UPS97822233Clamp · brokenNR 2 ENGINE FIRE WARNING CAME ON, THROTTLE BACK WARNING WENT OUT. FOUND NR 2 ENG HIGH STAGE VALVE CLAMP FAILED. NR 2 ENGINE INBD THRUST REVERSER DAMAGED. REMOVED AND REPLACED NR 2 ENG INBD THRUST REVERSER IAW MM 78-30-00 PN ON CFM56BRO2BRH.SDR CALA9700299Thermo Valve · inoperativeTHE RT PACKED TRIPPED AT 6,000 FEET LEAVING EWR AND SMOKE BEGAN TO ENTER THE CABIN. SHORTLY AFTERWARDS THE BLEED TRIPPED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE 450 DEGREE THERMO VALVE WAS REMOVED AND REPLACED, AN ENGINE BLEESDR UPS97822166Bleed Air Line · out of positionINSPECTION TYPE-N/A, AIR TURNBACK DUE TO NR 3 FIRE BELL INADVERTENTLY RINGING. NR 3 FIRE DETECT CIRCUIT WOULD NOT TEST IN FIRE TEST POSITION OR SHORT CIRCUIT TEST. REMOVED AND REPLACED PYLON LOOP PER MM 26-10-00, DUE TO HISTORY AND AGE. FOUND BLEED AIR LINE SDR P5CA9700381Precooler · crackedCRACK ON NR 2 ENGINE PRECOOLER. WELD REPAIR PERFORMED PER BOEING SPECIFICATION 5975.SDR P5CA9700363Duct · crackedCRACKED NR 3 ENGINE COMPENSATOR DUCT. REMOVED AND REPLACED DUCT PER BOEING MAINTENANCE MANUAL 36-11-16.SDR VTZA97155O-Ring · failedFLT 6320 - IAD-RDU - DURING TAXI, RETURNED TO GATE DUE TO LEFT DUCT FAIL LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BLEED AIR COUPLING O-RING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M)SDR 97UAL900156Prsov · failedRETURNED TO EZE, DUE TO RIGHT ENGINE BLEED VALVE FAILURE. SUPPLEMENTAL DATA UPDATE PRSOV (PRESSURE REGULATING AND SHUTOFF VALVE) FAILED DUE TO CLOGGED MAIN INLET FILTER. REPLACED PRSOV.SDR CALA9700229Duct · rupturedTHE NR 1 ENGINE HAD A FIRE WARNING WHILE EN ROUTE. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A NR 1 ENGINE PNEUMATIC DUCT RUPTURED. THE DUCT WAS REMOVED AND REPLACED, LEAK AND OPERASDR ABXA9700040Duct · leakingTAIL COMPARTMENT TAIL LIGHT CAME ON MULTIPLE TIMES ON GROUND. THE LIGHT DID NOT GO OUT AND STAY OUT WITH ABNORMAL PROCEDURES, ONLY WENT OUT TEMPORARILY. REPLACED LOWER INNER EXHAUST ELBOW THAT WAS LEAKING IAW DC-9 MM 49-80-1.SDR MZZA97032Clamp · leakingGUM - FLT 958 - L/P 7916635 AND 7916636. ON FIRST OCCURRENCE DURING CLIMB AT 1,000 FEET, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. CREW AIR RETURN TO GUM. MTX FOUND SECONDARY AIR FLEX DUCT AT GENERATOR SHROUD BLOWN. THE DUCT WAS REPLACED. ENG RUN FOUND NSDR AU970115Gasket · failed(AUS) ENGINE TO PYLON BLEED AIR DUCT GASKET BLOWN OUT AND TWO DUCT SECURING NUTS MISSING (BOLTS INTACT) - SUSPECT BOLTS NOT TORQUED DURING ENGINE INSTALLATION - PERSONNEL/MAINTENANCE ERRORSDR MZZA97030Duct · failedFLT 840 - NRT - DURING CRUISE, A LOUD BANG WAS HEARD FROM THE AFT CABIN IN CONJUNCTION WITH BODY OVERHEAT LIGHT ILLUMINATING AND LOSS OF EPR IND AT NR 2 ENG. PULLED THROTTLE TO IDLE PER CHECKLIST PROCEDURE AND LIGHT WENT OFF. DIVERTED TO NRT. MX FOUND THE RSDR TWRA97223 Way Valve · failedDURING INITIAL CLIMB, NR 2 ENGINE BLEED OVERHEAD LIGHT ILLUMINATED. BLEED SELECTED CLOSED. LIGHT STAYED ON. NR 2 ENGINE WAS THROTTLED BACK TO IDLE. LIGHT WENT OUT AFTER 5 MINUTES. NR 2 THROTTLE ADVANCED WITH NR 1 ENGINE AND NR 2 ENGINE BLEED. SELECTED CLOSSDR VJ970115Sensor · failedTAIL COMPARTMENT HIGH LIGHT CAME ON IN CLIMB, FLIGHT CREW ISOLATED PROBLEM TO LEFT PACK USING AIRCRAFT OPERATIONS MANUAL. FLIGHT DIVERTED TO MCO. TIGHTENED LOOSE CLAMP ON LT AUGMENTATION VALVE. SUBSEQUENTLY, ITEM REPEATED FOLLOWING DAY AND TAIL COMPARTMENT SDR 97UAL90013113th Stage Duct · rupturedAT 500 FEET ON TAKEOFF, AIRCRAFT EXPERIENCED THRUST LOSS OF NR 2 ENGINE FOLLOWED BY AN OVERHEAT INDICATION. OVERHEAT LIGHT EXTINGUISHED WITH THROTTLE AT IDLE. LANDED WITHIN 10 MINUTES. THE 13TH STAGE SADDLE DUCT RUPTURED AROUND THE DOUBLER WELD. THE SADDLSDR HEEA978983Shut Off Valve · sticksSTICKS IN OPEN POSITION. SENT TO HELICOPTER SUPPORT, INC. FOR INSPECTION AND REPAIR.SDR 97UAL900123Regulator · failedAFTER TAKEOFF, CABIN FILLED WITH SMOKE. RIGHT PACK COMPRESSOR TEMPERATURE WENT INTO YELLOW BAND. MAIN SUPPLY TEMPERATURE EXCEEDED 160 DEGREES. REPLACED BLEED AIR REGULATOR.SDR CA970220002Clamp · loose(CAN) AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. ALL MODES UNSUCCESSFUL. BLEED AIR CLAMP LOOSE AND JUMPED OVER FLANGE. DUCT AND CLAMP SECURED.SDR COMA9760032Connector · looseLEFT ENGINE WILL NOT START. SECURED LOOSE WIRING CONNECTOR AT ENGINE BLEED AIR VALVE.SDR USAAD97032Clamp · failedFLT 1020 - RSW-CLT - IN FLIGHT AT FL 240, THE NR 2 FIRE WARNING LIGHT ILLUMINATED. SELECTED B LOOP. RIGHT ENGINE FIRE HANDLE ILLUMINATED. FIRED NR 1 FIRE BOTTLE, SHUT DOWN RIGHT ENGINE. SINGLE ENGINE TIME WAS 15 MINUTES. REPLACED CLAMP ON 13TH STAGE DUCT SDR MWEA97097Augmentation Vlv · inoperativeLEFT ICE PROTECTION TEMP HIGH ANNUN ILLUMINATED, FOLLOWED SHORTLY BY LEFT AIR CONDITIONING SUPPLY TEMP HIGH ANNUN. DIVERTED TO MKE FROM OMA. MAINT REMOVED AND REPLACED LEFT AUGMENTATOR VALVE.SDR AALA970212Clamp · looseDFW - FLT 1604 - AFTER TAEKOFF DFW DURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT RETURNED TO DFW, LANDING OVERWEIGHT WITHOUT INCIDENT. RETORQUED NR 1 ENGINE 13TH STAGE MODULATION VALVE. ACCOMPLISHED OSDR P2EA97002Bleed Duct · damagedFLT 612 - DEN - AFTER DEPARTING DEN, FLIGHT ATTENDENT INFORMED ME OF A SMELL COMING FROM THE CABIN, HAD ELECTRICAL ODOR. RETURNED TO DEN FOR INSPECTION. FOUND BLEED DUCT WITH HOLE, FORWARD CARGO PIT, RT AFT CEILING. DUCT REPLACED, RAN PACK, NO SMOKE IN CABISDR COMA9710037Pneumatic Lines · frozenHYDRAULIC LOW PRESS LEFT ILLUMINATED. THAWED AND PURGED PNEUMATIC LINES.SDR 97FDEA00047Duct · crackedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED 5 MINUTES AFTER TAKEOFF WITH WING AND ENGINE ANTI-ICE OPEN. ALTITUDE 10,000 FEET AT CLIMB. POWER LIGHT EXTINGUISHED ONE MINUTE AFTER CLOSING WING ANTI-ICE. CRACKED DUCT FOUND IN AFT AIRSTAIRS AREA. CANNIBALIZED DUCSDR TC8A97001Crossfeed Valve · malfunctionedPNEUMATIC CROSSFEED VALVE WON'T OPEN. REMOVED AND REPLACED CROSS FEED VALVE, SYSTEM OPS CHECKS GOOD IAW MM 36.SDR ORJA9706Peri Seal · leakingTAIL COMPARTMENT TEMP HIGH LIGHT CAME ON AFTER TAKEOFF. PERFORMED MEMORY ITEMS AND CHECKLIST. LIGHT WENT OUT WHEN LEFT THROTTLE RETARDED TO IDLE. AFTER TURNING LEFT AIR COMP SWITCH TO OFF AND ADVANCING LEFT POWER CVR LIGHT RE-ILLUMINATED. BELOW 15 EPR LIGHSDR 97ZZZM154'Y' Duct · corrodedFOUND CORROSION ON THE FORWARD PIT BY 'Y' DUCT IN THE SKIN BLOWN OUT (LEVEL 2) AT STATION 580L 30 RIGHT SIDE AND FOWARD OF STATION 580L 30. REMOVED FASTENERS, REMOVED CORRODED AREA IN INTERNAL SKIN, FABRICATED FILLER AND REPAIR DOUBLER, DRILLED, TREATED AND ISDR GLBA97003Eva Tube · failedPHX - 'BLEED AIR FAIL' ILLUMINATED INFLIGHT. MAINTENANCE REPAIRED EVA TUBING. OPERATES NORMAL. (M)
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