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 UPS06648726Receptacle · looseINSPECTION TYPE:ETOP TET = 23173, TEC = 8097, TSLV = 1688 ATB - RIGHT ENG HPSOV MSG. *S/D* FOUND RECEPTACLE D1706P LOOSE. SECURED RECEPTACLE, PERFORMED BITE TEST. HPSOV LT ON BITE MODULE CLEARED. RAN ENG BLEED LITET & RT HPSOV EICAS MSG APPEARED. REMOVEDSDR DL738061004Regulator · failedAFTER T/O GOT LT ENG BLEED TRIP. RESET AS PER QRH. TRIPPED AGAIN. RETURNED DUE TO ICING EN ROUTE. REPLACED PRSOV REGULATOR AND HI STAGE PRESS REGULATOR PER AMM. RAN ENGINES TO T/O POWER FOR 5 MINS. BOTH ENGINES MAINTAINED 50 PSI THROUGHOUT RUN. NO BLESDR XN0A1357Valve · malfunctionedCOULD NOT GET MORE THAN 15 PSI BLEED AIR OUT OF ENGINE NR 1, OSCILLATING BETWEEN 10 PSI AND 15 PSI. REMOVED AND REPLACED NR 1 PRESSURE REGULATOR VALVE IAW A300 AMM CHAPTER 36-11-14, OPS CHECKS NORMAL.SDR 06FDEA03966Control Valve · malfunctionedAFTER TAKEOFF CLIMBING THRU 1000' WITH ENGINE AND WING ANTI-ICE ON THE NR 3 MANIFOLD FAIL LIGHT CAME ON. REMAINED OUT OF ICING. LANDED AT NEAREST SUITABLE AIRFIELD, KSTL. RT WING PRESSURE SWITCH FAULTED IN CAC. DROPPED FLAPS/SLATS AND CHECKED WING ANTI-ICESDR HALA0600859Connector · dirtyBTB - R BLD ISLN DISPLAYED R BLD ISLN VALVE LIGHT ON. INSP RT ISOLATION VALVE CONNECTOR PLUG, CLEANED PLUG AND REINSTALLED. CYCLED VALVE, VALVE OPS NML PER AMM 36-11-04-404-013.SDR MALA060594Duct · leakingDURING DEPARTURE CLIMB FROM DTW, LEFT BLEED AIR LEAK LIGHT ILLUMINATED. QRH PROCEDURES COMPLETED. AIR RETURNED TO DTW. REPLACED LT ELBOW RUBBER DUCT NEAR FUSELAGE, WHICH WAS LEAKING. RAN ENGINE. ALL CHECKS GOOD.SDR Q2SA740003Valve · malfunctionedHAD INDICATION OF NR 1 ENGINE FIRE AT FL 250. ACCOMPLISHED ENGINE FIRE CHECKLIST IAW QRH. SHUTDOWN ENGINE, ACTIVATED FIRE EXTINGUISHER, DUMPED FUEL AND RETURNED TO ZSPD. FOUND PRESSURE RELIEF VALVE (PRV) WILL NOT STAY CLOSED. REMOVED AND REPLACED PRV AND LEASDR 0602331235Connector · looseNR 2 PNEUMATIC FAIL LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABORTED AT 140 KNOTS AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND TIGHTENED LOOSE CONNECTION. CHANGED NR 2 PRECOOLER AND DEFERRED MANIFOLD DETECTOR. OPERATION CHECKS GOOD. SDR DL757060862Sensor · failedLEFT ENGINE BLEED ALERT WITH WING AND ENGINE ANTI-ICE SLECTED. WENT THROUGH QRH PROC. THEN LEFT AND RIGHT BLEED ALERTS, LOST CABIN PRESSURE. REPLACED LEFT FAN AIR TEMP SENSOR, LEFT AND RIGHT BLEEDS NOWCHECK NORMAL. AIRCRAFT DIVERTED INTO MCOSDR DL76G060861Controller · unserviceableRT BLEED OFF LIGHT ILLUMINATED WITH BLEED LATCH ON. PERFORMED BITE ON ABCU FAULTED PRC AND WIRE FAULT REPLACED PRC PERFORMED BITE FAULT CLEARED RAN ENG OPS NORMAL.SDR DELA200600004Seal · leakingDURING CLIMBOUT, LEFT AND RIGHT BLEED AIR WARNING ANNUNCIATORS ILLUMINATED. INITIAL CHECKLIST PROCEDURES EXTINGUISHED LIGHTS. BOTH LIGHTS CAME BACK ON DURING FURTHER CLIMB TO FL290 BUT WOULD NOT EXTINGUISH FOLLOWING LIMITED AFM CHECKLIST PROCEDURES DUE TO THSDR TSAA0626082Duct · crackedDURING CRUISE, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. THE CREW RETARDED THE NR 1 ENGINE THRUST LEVER AS PER QRH AND THE LIGHT EXTINGUISHED. THE CREW LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE BLEED DUCT ASSEMBLY CRACKED. SDR GM06004Shutoff Valve · malfunctionedDURING TAKEOFF HAD AN AMBER MESSAGE -BLEED PRESSURE HIGH L-. REPLACED LEFT PRESSURE REGULATOR / SHUT-OFF VALVE. AIRCRAFT RETURNED TO SERVICE.SDR UIEA200600255Relief Valve · failedNR 1 ENGINE FIRE INDICATION, FL330 2135Z, NACELLE TEMP INDICATIONS ON "B" LOOP OVER 5.0. "B" LOOP WAS DEFERRRED. FHB SECTION 3 PROCEDURES ACCOMPLISHED. FOUND OVERPRESSURE RELIEF VALVE LEAKING EXCESSIVELY AT 40-PSI. REPLACED VALVE PER AMM 36-11-00 ADJ TEST.SDR MWEA060200Line · looseTIGHT AIR SYSTEM PRESSURE LOW ANNUNCIATED. INSPECTED RIGHT ENGINE, FOUND AIR LINE LOOSE AT IN-LINE FILTER GOING TO PRESSURE REGULATOR SHUT OFF VALVE PILOT VALVE, SECURED LINE, PERFORMED LEAK CHECK OF PNEUMATIC DISTRIBUTION & CONTROL SYSTEM, OPERATION CHECKED SDR DHL2006801001Bleed Valve · warning lightENG (3) OVER PRESSURE LIGHTS ILLUMINATED ON TAKEOFF AT 67 PERCENT N1 RTO AT LESS THAN 60 KIAS LIGHT BRAKING. REPLACED NR 3 BLEED REG VALVE IAW DC-8 MM 36-12-1. OPS AND LEAKS CHECKS GOOD. RUN UP IAW JRH 12.2.SDR AALA20060676Seal · damagedMIA - LEFT ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE HIGH PRESSURE NUMBER TWO AND SIX DUCT SEALS. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AMTA200600540Sensor · malfunctionedLEFT AND RIGHT DUCT PRESSURE SPLIT AT CRUISE ALT L WAS 44 PSI AND R IS 28 PSI. REMOVED AND REPLACED OF 390 DEG SENSOR, AND SWAP OF BAR`S, RAN ENGINES AT 80 PERCENT N1 FOR 15 MINUTES, PACKS ON, LT ENGINE PRESS 43 PSI R ENGINE PRESS 38 PSI, IN LIMITS PER FIM 36SDR AMTA200600539Shutoff Valve · malfunctionedLEFT AND RIGHT DUCT PRESSURE SPLIT R-DUCT PRESSURE 10-15 PSI LOWER THAN L DUCT AT CRUISE. REMOVED AND REPLACED PRSOV, AND HP REGULATOR. PERFORMED BLEED AIR CHECK PER FIM 36-10-00-810-804, L/R BLEED PRESS`S MATCH AT ALL TESTED N1 SPEEDS. (M)SDR UIEA200600225Valve · inoperativeDURING CRUISE, COULD NOT CLOSE NR 1 PYLON VALVE WITH ASSOCIATED SWITCH, VLV CLOSED. ON ENG SHUT DOWN (DIV). DURING CRUISE, COULD NOT CLOSE NR 3 PYLON VALVE WITH ASSOCIATED SWITCH, VLV CLOSED. ON ENG SHUT DOWN (DIV). DURING CRUISE, COULD NOT CLOSE NR 4 PYLOSDR HALA0600654Shutoff Valve · failedBTB - NR 1 ENGINE NO BLEED AIR. T/S PER FIM - PNEUMATIC SUPPLY BITE MODULE FAULTED LEFT ENG PRSOV. REMOVED AND REPLACED LEFT ENG PRSOV PER M/M 36-11-09. ALSO REPLACED LEFT ENG BLEED SUPPLY CONTROL CARD IN P50 PANEL PER MM 36-11-12. RAN ENGINE AND PRSOV OP SDR HALA0600648Sensor · faultyFOUND BLEED AIR RT TEMP HIGH. REPLACED RT ENG T1 SENSOR PER AMM 3-13, OPS CK OK. NO FAULTS ON GRD RUN.SDR EIA2006203Duct · crackedRT WING PNEUMATIC DUCT CRACKED, DUCT TO GRP 2 RIGHT LED. REPLACED DUCT, LEAK AND OPS CHECK OK.SDR DJFA2006310Carbon Seal · leakingTHE CREW NOTED A STRONG MILDEW ODOR AND A BURNT PLASTIC SMELL DURING FLIGHT AFTER TAKE OFF. MAINTENANCE WAS ABLE TO VERIFY THE DISCREPANCY AS AN AFT EVAPORATOR THAT SMELLED MUSTY. THE FINS OF THE FORWARD AND AFT EVAPORATORS WERE CLEANED AND THE DRAINS WERE VSDR HALA0600625Isolation Valve · failedBTB - PNEU AIR SUPPLY -PWR CTR- CB POPPED. CENTER ISO VALVE LIGHT ON. REMOVED AND REPLACED CENTER ISO VALVE PER AMM 36-11-04, OPERATIONAL AND LEAK CHECK GOOD.SDR 2006FA0000913Shaft · shearedPILOT REPORTED INSTRUMENT AIR PRESSURE WENT TO -0- IN FLIGHT, PILOT THEN SELECTED STANDBY PUMP AND RETURNED TO BASE. UPON TROUBLESHOOTING, THE MECHANIC REMOVED THE AIR PUMP AND FOUND THE SHAFT WAS SHEARED. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. SDR 2006FA0000912Shaft · shearedPILOT REPORTED INSTRUMENT AIR PRESSURE WENT TO -0- IN FLIGHT, PILOT THEN SELECTED STANDBY PUMP AND RETURNED TO BASE. UP ON TROUBLESHOOTING THE MECHANIC REMOVED THE AIR PUMP AND FOUND THE SHAFT WAS SHEARED. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. SDR AMTA200600512Shutoff Valve · unserviceableLT DUCT PRESS FLUCTUATES BETWEEN 10 AND 60 PSI ON TAXI. PACKS ON, SMOOTHES OUT WHEN T/O POWER APPLLIED. REMOVED AND REPLACED PRSOV ON NR 1 ENG IAW MM AND SECURED SENSE LINE FOR THE PRSOV. PERFORMED ADJ AND TEST IAW MM. OPS CHECK NORMAL. (K)SDR UIEA200600207Duct · crackedAIR TURNBACK, NR 3 ENGINE IN FLIGHT FIRE. BOTH NACELLE TEMPS 8.5. NR 3 ENGINE FIRE HANDLE PULLED. NR 3 ENGINE EGT 924 DEG WITH REDUCED POWER, T/O OF 104.3 POWER REMAINED AT 103.0 FOR 6 TO 7 MINUTES. REMOVED AND REPLACED NR 3 ENGINE EDP, RETURN PRESSURE AND SDR UPS06647620Valve · inoperativeLT PRV MSG - ABORTED TAKEOFF. REMOVED AND REPLACED LT PRV PER AMM 36-11-18-4. SYS LEAKS CHECK & OP TESTED NORMAL PER AMM 36-11-18-5. M330740 CLEARED, PLACARD REMOVED.SDR XN0A1348Warning Light · illuminatedON TAXI NR 2 MANIFOLD FAULT AND APU MANIFOLD FAULT LIGHT ILLUM, WILL NOT RESET. FOUND LT FLOW CONTROL VALVE LEAKING, R&R FLOW CONTROL VALVE IAW A300 AMM CHAPTER 21-51-12 OPS CKS GOOD, NO LEAKS NOTED. (CLOSED)SDR C1HA200692004Duct · leakingAFTER ROTATION ENG 1 BLEED AIR TRIP OFF LIGHT ILLUMINATED. CREW PERFORMED COM 2.36.2 APPROX 1 OR 2 MINS AFTER COMPLETION OF COM PROCEDURE FOR ITEM 1, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. CREW RAN COM 2.36.9 CONTACTED DISPATCH. FOUND 13TH STAGE SADDLE SDR Q2SA751001Clamp · looseON CLIMBOUT FROM ZGGG, NR 3 ENGINE FIRE WARNING LIGHT AND BELL ILLUMINATED. FOLLOWED QRH PROCEDURES IAW EAC 107-47. ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO ZGGG FOR REPAIRS. FOUND LOOSE CLAMP ON HIGH STAGE VALVE. TIGHTENED CLAMP AND LEAK CHECKED GOOD.SDR AMTA200600450Regulator · unserviceableENG DUCT PRESSURE SPLIT. REMOVED AND REPLACED BLEED AIR REGULATOR ON NR 2 ENGINE, OPS CHECKED NORMAL IAW MM. (K)SDR RAIA00607046Unknown · leakingFLT NR 5535 - STL - BLEED 1 LEAK. MAINTENANCE DEFERRED THE NR 1 BLEED SYSTEM.SDR HALA0600518Sensor · malfunctionedLT HP BLEED VLV STUCK CLOSED. R AND R PM SENSOR ON LT ENGINE PER AMM 36-12-04-000-801 LK AND OPS CK GOOD.SDR AMTA200600446Shutoff Valve · unserviceableRT DUCT PRESSURE = 20 PSI, LT DUCT PRESSURE= 40 PSI BOTH IN CLIMP AND CRUISE. REMOVED AND REPLACED PRSOV VALVE AND OPS CHECKED NORMAL IAW MM. A/C OK FOR SERVICE. (K)SDR DL76L060611Controller · malfunctionedLT ENGINE BLEED WOULD NOT OPEN AFTER START. BITE AIR SUPPLY MONITOR FAULTED LT ENGINE PRV AND PRC. REPLACED PRC IAW MM . INSPECTED ALL MUSCLE LINES AND RETORQUED ALL LINE FITTINGS. RAN LT ENGINE LT ENGINE BLEED SYSTEM OPS NML NO FAULTS. ETOPS CATEGORY (E):SDR QXEA200601910Valve · failedBOI FLIGHT NR 2198, SMOKE IN CABIN ON NR 2 BLEED ON ONLY. MAINTENANCE REPLACED P2.5 SWITCHING VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR COMA0660447Duct · unserviceableDURING CLIMBOUT OF ORF RECEIVED A LEFT 14TH STAGE DUCT WARNING MESSAGE, FLIGHT RETURNED TO ORF. REPLACED THE 14TH STAGE DUCT BLEED AIR DUCT ASSEMBLY.SDR QXEA200601916Pressure Valve · leakingSEA FLIGHT 2237 IN FLIGHT AT 16000 FT FLIGHT ATTENDANT REPORTED LOW AIRFLOW IN CABIN AND UNCOMFORTABLY WARM WITH ONLY 25 PASSENGERS ON BOARD. ATTEMPTED TO COOL FROM FLIGHT DECK IN BOTH MANUAL AND AUTO MODES WITH NO SUCCESS. PERFORMED CABIN AUTO TEMP CONTROL FASDR HNAA0600074Pressure Switch · failedAFTER SELECTING NR 1 BLEED ON NR 1 ENGINE TORQUE SURGED APPROX 10 PERCENT FOLLOWED BY THE NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED. REMOVED AND REPLACED PRESSURE SWITCHES.SDR SIMA200619801O-Ring · failedE1 BLEED LEAK ON EICAS CREW CALLED MOC AND AGREED TO RETURN TO ORD DID NOT LAND OVERWEIGHT. FOUND LEAK IN UPPER CLAMP BEHIND CARGO WALL NR 1 SIDE. REMOVED AND REPLACED O-RINGS IAW EMB 145MM 36-11-10, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR CHQA20060080Duct · crackedFLIGHT 3276 - RIC-LGA - UPON CLIMB-OUT THROUGH APPROXIMATELY 6500' RECEIVED "BLEED 1 LEAK" EICAS MESSAGE ASSOCIATED WITH ILLUMINATED BLEED 1 BUTTON ON OVERHEAD. RAN THE QRH AND SHUT DOWN THE BLEED 1 AND CLOSED THE CROSS FEED. MESSAGE REMAINED FOR ABOUT 2.5 MSDR MASA200601807O-Ring · damagedASH 7160 IAD - BLEED 1 LEAK WARNING MESSAGE ON TAKEOFF. MX REPLACED O'RINGS.SDR MALA060465Precooler · malfunctionedRT BLEED CLOSING IN AUTO AND MAN MODE. THE CREW RETURNED TO MSP WITHOUT FURTHER INCIDENT. REPLACED RT PRECOOLER P/N 782779-1, S/N ON 841045. REPLACED RT ACM P/N 776910-6, S/N ON 960-646, S/N OFF 840221. INSTALLED NEW HEAT EXCHANGER P/N 779215-2, S/N ON 901SDR FDKA200607154Coupling · looseASH 6098 AUS - AIRCRAFT ABORTED TAKEOFF DUE TO BLEED 1 LEAK MESSAGE. MAINTENANCE TIGHTENED COUPLING L WING ROOT.SDR UIEA200600161Valve · leakingWHILE CRUISING AT FL LEVEL 310, NR 3 ENG OVERHEAT LIGHT CAME ON. ACCOMPLISHED PROCEDURES AS PER FHB 3.35.5.6. OVERHEAT LIGHT EXTINGUISHES WHEN THROTTLE WAS RETARDED, ALSO WITH THE BLEED AIR VALVE SWITCH IN CLOSED POSITION VALVE LIGHT FAILED TO COME ON. THERSDR UIEA200600158Duct · rupturedFOLLOWING TAKEOFF NR 4 ENG FIRE INDICATIONS NACELLE TEMPS A/B HIGH, THEN TO FIRE "F" AND FULL WARNING ENG NR 4 SHUTDOWN AS PER CHECKLIST. NR 4 ENG FIRE BOTTLE "A" DISCHARGED, FIRE WARNING EXTINGUISHED. FOUND 14TH STAGE BLEED AIR DUCT RUPTURE. REMOVED AND RESDR CA060629003Flange · debonded(CAN) WELDED TUBE ASSEMBLY REMOVED FROM AIRCRAFT TO GAIN ACCESS FOR INSPECTION. WELDED TUBE ASSEMBLY INSPECTED - FLANGE ATTACHED APPEARED TO BE BONDED TO TUBE. UPON INSTALLATION ON AIRCRAFT - WHEN CLAMP ATTACHING WELDED TUBE ASSEMBLY TO CABIN VENTILATION JUN
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