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 P5CA2015082700105Shutoff Valve · failedFAIL, FOUND NR 1 ENG PRSOV BIT 29 DOES NOT CHANGE TO 1 IAW AMM 36-11-09-002-033, REV 112 AND AMM 36-11-09-402-058, REV 112, REPLACED THE NR 1 ENG WITH SERVICEABLE PARTS IAW AMM 36-11-09-402-058, REV 112, DO THE NR 1 ENG PRSOV INSTALLATION TEST. RESULTS, CONDISDR CA150824001Switch · failed(CAN) NR 1 BLEED HOT CAUTION ILLUMINATED IN CRUISE. QRH PROCEDURE CARRIED OUT AND THE LIGHT EXTINGUISHED. INVESTIGATION BY MAINTENANCE DISCOVERED THAT THE LH NACELLE DUCT LEAK OVERTEMP SWITCH WAS FAULTY. THE SWITCH WAS REPLACED AND THE SYSTEM TESTED SERVICEABLSDR CALA2015082100693Shutoff Valve · faultyRIGHT BLEED TRIP OFF LIGHT ON, WOULDN`T RESET AFTER TAKEOFF. PERFORMED RT ENG BLEED HEALTH CHECK IAW AMM 36-11-00. FOUND 390 SENSOR & PRSOV BAD. REPLACED IAW AMM 36-12-03 & AMM 36 -11-04. ENG RUN CHECKED OK. BLEED TRIP OFF LIGHT STAYS OFF.SDR C77A20150821002Valve · inoperativeBLEED 1 FAIL MSG IN FLIGHT WITH BLEED 2 DEFERRED WITH RAPID DECOMPRESSION. PERFORMED QRC .5 & QRH 2.5. DEFERRED IAW MEL 36-00-00-3, TRANSFERRED TO SDI LOG, NO MX PROCEDURES REQUIRED. PLACARD INSTALLED, ACFT OK FOR SERVICE. BLEED 1 FAILED IN FLIGHT. PERFORSDR CA150827001Boot · out of position(CAN) LEFT BLEED DUCT WARNING DURING FLIGHT. COMPLIED WITH QRH. RT BLEED CLOSED CAUSING ULTIMATE LOSS OF PRESSURE. CREW INITIATED AN EMERGENCY DESCENT DUE TO THE LOSS OF CABIN PRESSURE, THE PASSENGER OXYGEN MASKS WERE RELEASED. INSPECTED LT BLEED DUCTS, FOSDR SWIA201541401Shutoff Valve · malfunctionedLT BLEED OVERHEAT WARNING AT FL340. FOLLOWED QRH, FLT 3469, F/O: 08/20/2015 VISUALLY INSPECTED THE ACFT AND BLEED AIR DUCTS FOR DAMAGE OR LEAKS, NONE FOUND. C/W FIM PROCEDURES FOR BLEED AND ANTI-ICE DUCT LEAK, LEAK RUN EVENT TEST. NDC SHOWED FAULT HISTORY FSDR AALA20150820001Duct · leakingAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB TAIL COMPARTMENT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED CARS 0930 & 26-96-11. FOUND LEAK AT RT DUCT. RE-FLANGED & RESEATED DUCTS. PERFORMED OPERATIONAL CHECKS. SYS CHECKEDSDR FDEA201508152551Controller · failedON DESCENT, WITH ENG & WG ANTI-ICE ON, GOT NUMEROUS LVL 1 & 2 ALERTS FOR AIR SYS PROBLEMS. WITH CABIN ALT RISING DID A HIGH SPEED DIVE TO 10,000 T. CABIN ALT GOT TO 7800 FT & STARTED BACK DOWN TO NORMAL. VALUES OF CABIN ALT, THEREAFTER ALERTS INCLUDED LVL 2SDR FDEA201508152550Valve · failedON DESCENT WITH ENG & WG ANTI-ICE ON, GOT NUMEROUS LVL 1 & 2 ALERTS FOR AIR SYS PROBLEMS. WITH CABIN ALT RISING, DID A HIGH SPEED DIVE TO 10,000 FT. CABIN ALT GOT TO 7800 FT & STARTED BACK DOWN TO NORMAL. VALUES OF CABIN ALT, THEREAFTER ALERTS INCLUDED LVL SDR SIMA20150815001Valve · malfunctionedICE PROTECTION TEST PNEUMATIC IN FLIGHT FAILED TWICE. EICAS MSG WARNING BLD 2 OVERTEMP. R & R NR 2 FAN AIR VALVE IAW AMM 36-11-03. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED.SDR P5CA2015081300089Actuator · leakingFOUND NR 2 HPSOV ACTUATOR LEAKAGE THUMB TEST FAIL IAW AMM 36-11-07-024-001 AND AMM 36-11-07-424-016. REPLACED NR 2 ENGINE HPSOV IAW AMM 36-11-27-424-016, TEST CK NORMAL.SDR P5CA2015081300088Seal · leakingTHE PNEUMATIC DUCT LEAK AT BODY CROSSOVER AIR SUPPLY SYS IAW AMM 36-11-01-004-131-001 REV 112 AND AMM 36-11-01-404-142-001. REPLACED SEAL AT BODY CROSSOVER DUCT OPS CK NORMALSDR P5CA2015081300091Controller · malfunctionedFOUND NR 1 ENGINE FAILED HEALTH CHECK TEST IAW AMM 36-11-08-004-006 AND AMM 36-11-08-404-014. REPLACED NR1 ENGINE HPC IAW AMM 36-11-08-404-014, REV 112. TEST RESULT PASS.SDR N6WA2015081103Valve · leakingRIGHT BLEED DUCT WARNING. HOT AIR COMING FROM HOLE IN CROSS BLEED VLV. R & R CROSS BLEED VLV IAW AMM 36-13-15.SDR CA150811002Duct · cracked(CAN) FLIGHT CREW REPORTED WING BODY OVERHEAT INDICATION LT AND RT CAME ON. LT WING - BODY OVERHEAT INDICATION EVENTUALLY EXTINGUISHED. LT WING BODY OVERHEAT INDICATION CAME ON AGAIN AFTER APPROXIMATELY 30 MINUTES AND RT PACK INDICATION ILLUMINATED. ALL 3 ISDR CA150810003Bleed Valve · failed(CAN) LEFT ENGINE 14TH STAGE DUCT WARNING MESSAGE ON CLIMB OUT. RETURNING TO AIRPORT. ECS PAGE SHOWED NORM. ANTI ICE PAGE SHOWED RED BETWEEN THE CMD VALVES ON LT SIDE. MESSAGE CONTINUED TO GO ON/OFF. MAINTENANCE INSPECTED AND CHECKED LT 14 STAGE SENSE LOOPS ELSDR CA150807006Isolation Valve · leaking(CAN) LT ENGINE 14TH STAGE BLEED AIR DUCT WARNING MESSAGE FLICKERING ON CLIMBOUT THROUGH 7,000`. CREW ACTIONED QRH, LH 14TH SELECTED OFF AND 14TH ISOL VALVE OPEN. MESSAGE WAS STILL FLICKERING. QRH DIRECTED THEM TO LAND AT NEAREST SUITABLE. FLT RETURNED. MAINTESDR ASOA20150807044RValve · odorPILOT REPORTED BLEED 1 & 2 OVERTEMP IN ICING THEN ODOR OF SOMETHING BURNING. MAINTENANCE R & R NR 1 ENGINE FAN AIR VALVE, FAN AIR THERMOSTATS 1 & 2, A HIGH STAGE PRESSURE SWITCH WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR HALA2015080600153Sensor · malfunctionedNR 2 ENGINE BLEED ECAM DURING DESCENT. R & R RIGHT ENGINE EXCHANGER OUTLET SENSOR IAW AMM 36-11-17-400-804-A.SDR VNAA2015080500009Shutoff Valve · failedCREW REPORTED LT PACK DID NOT PRESSURIZE AND LT PRESSURE REGULATING SHUTOFF VALVE DID NOT WORK AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R TENTH STAGE SHUTOFF VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASSDR ASAA2015080312664B-Nut · looseDUCT SPLIT RT DUCT 44, LT DUCT BOUNCING BETWEEN 25 AND 30 PRESSURIZATION WAS NORMAL AFTER ALMOST 4 HRS IN FLT, RT DUCT 44, LT DUCT 35. ACFT GROUNDED. FOUND LEAK ON CONTROL PRESSURE SENSE LINE AND SUPPLY PRESSURE SENSE LINE. TIGHTENED B-NUTS DURING MM TASK 3SDR UIEA2015080300401Ball Joint · out of adjustLEFT BLEED DUCT LEAK EICAS, PERFORMED AIR SUPPLY BITE CHECK IAW AMM 36-23-00. RE-RACKED M859 CARD FILE IAW AMM 36-11-12 & ADJUSTED BALL JOINTS IAW MM 36-11-01. SYSTEM NORMAL AT THIS TIME.SDR SWIA201541381Warning Message · false activationRETURNED TO FIELD WITH LT BLEED WARNING MESSAGE. CLOSED, FOUND NO FAULTS IN THE MDC. RAN AILC SELF TEST, TEST PASSED. HOOKED UP AILC BREAKOUT BOX, ALL RESISTANCE CHECKED GOOD. RAN ENGINES, COULD NOT DUPLICATE.SDR YENA20150728292Shutoff Valve · failedNR 2 BLEED FAILED WITH NR 1 BLEED ON MEL. CABIN TEMPERATURE FLUCTUATING. TROUBLESHOT IAW FIM REF 36-11-00-810-810-A. FOUND NR 2 ENGINE NAPRSOV BUTTERFLY VALVE SEAL DETONATED AND NOT HOLDING PRESSURE. R & R ENGINE NAPRSOV, OK FOR SERVICE.SDR AALA20150727014Shutoff Valve · faultyDURING CLIMB RT ENG BLEED OFF ILLUMINATED. DIVERTED, EMERGENCY DECLARED, AND LANDING UNEVENTFUL. R & R RT ENGINE PRESSURE REGULATING & SOV IAW MM 36-11-09. PERFORMED OPERATIONAL CHECKS. SYS CHECKED NORMAL.SDR ASAA2015072612593Shutoff Valve · no testNR 2 ENGINE PRSOV AND PRECOOLER CONTROL VALVE FAIL CONTROL PRESSURE CHECK, REF T/C NG-36WC-00001. FOUND BRAIDED LINE LEAKING ON NR 2 ENGINE. ACFT GROUNDED. REPLACED NR 2 ENGINE PRSOV REF MM 36-11-04. REPLACED NR 2 ENG PRECOOLER CONTROL VALVE, REF MM 36-12-SDR WX0A2015072700065Clamp · looseTAIL COMPARTMENT HIGH WARNING LIGHT ILLUMINATED DURING CLIMBOUT. FOLLOWED QRH 21-4 & LEFT NP BLEEDS OFF FOR REMINDER OF FLIGHT. COMPLIED WITH TASK CARD 21-059-005. SEVERAL SMALL AIR LEAKS NOTED. RETORGUED CLAMPS. NO FURTHER LEAKS NOTED. COMPLIED WITH ENGSDR ASAA2015072512592Regulator · failedA/C DUCT SPLIT PRESSURE DIFFERENTIAL 20 PSI RIGHT DUCT 17, LT DUCT 37. ACFT GROUNDED. REPLACED PRECOOLER CONTROL VALVE, REF AMM 36-12-02. REPLACED HIGH STAGE REGULATOR REF AMM 36-11-07. REPLACED HIGH STAGE VALVE REF AMM 36-11-06. NO LEAKS NOTED. RAN BOTH SDR ASAA2015072512574Regulator · failedDUCT PRESSURE SPLIT INFLIGHT, LT PRESSURE 22, RT PRESSURE 45 AT FL360. ACFT GROUNDED. ACCOMPLISHED TC NG-36WC-00001. ENGINE BLEED AIR HEALTH CHECK. NR 1 ENGINE HIGH-STAGE REGULATOR FAILED HEALTH CHECK. REPLACED IAW 36-11-07-000-801 & 36-11-07-400-801. OPSSDR WX0A2015072700062Sensor · failedTAIL COMPARTMENT TEMP HIGH, ANNUNCIATOR ILLUMINATED AFTER TAKEOFF. COMPLETED QRH PROCEDURE ON PG 2 1 4. ANNUNCIATOR EXTINGUISHED 2 MIN AFTER TURNING APU OFF. APU AIR WAS OFF, PACKS AUTO ON TAKEOFF OAT 38C. FOUND TAIL COMPARTMENT HIGH SENSORS LEFT & RIGHT BSDR 2015FA0000348Clamp · leakingDUCT NR 2 OVERTEMP. PERFORMED QRH PROCEDURE AND RETURNED TO DEPARTURE. INSPECTED ACFT AND FOUND RT TMV DUCT CONNECTOR LEAKING. ADJUSTED CLAMP ON TMV AND SECURED. ACCOMPLISHED FULL POWER ENGINE RUNS IAW AMM 71-00-00. NO BLEED LEAKS OR INDICATIONS DURING RSDR SIMA20150723001Precooler · failedBLEED 1 LO TEMP, TRANSFERRED TO NRWC 808-ABI-01810. REMOVED AND REPLACED LT PRE-COOLER IAW EMB 140 AMM 36-11-04. SEE NRWC 808-ABI-01811 FOR OPERATIONAL TEST OF THE BLEED AIR SYSTEM. REGULATOR VALVE P/N 3215886-2 P/N 1367C. BLEED TEMPERATURE P/N 0132ADT S/NSDR AALA20150721003Shutoff Valve · defectiveAIR INTERRUPT, RETURNED, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. THE LT ENG BLEED OFF LIGHT ILLUMINATED, BLEED AIR WOULD NOT RESET & ACFT WOULD NOT HOLD PRESSURIZATION ON SINGLE PACK OPERATION. REPLACED THE LT ENG PRESS REGULATING & PRSOV IASDR MASA2015072112255Shutoff Valve · malfunctionedRT ENGINE BLEED CAUTION IN FLT LOST CABIN PRESSURE. R & R RT PRSOV, OPS GOOD.SDR IPXA2015071991273Warning Message · false activationCRUISING AT FL290 WITH ALL ANTI-ICE ON, LEVEL 1 AIR SYS 2 OFF ILLUMINATED FOLLOWED BY TAIL ANTI ICE DISAGREE. DECAY CHECKED OK, AS 19.5 IAW AMM 36-00-01-700-802, FOUND NO HISSING SOUND, ALL SENSORS AND WIRES SECURED THEN R & R MFDC PRECAUTIONARY, THEN AIR SDR IPXA2015072291416Controller · inoperativeDIVERSION, RECEIVED BLEED 1 ADVISORY EICAS MSG AND BLEED OVERPRESS 1 STATUS LVL MESSAGE. FOUND CMC FAULT MSG 36226, PRV & CONTROLLER FAIL. R & R WITH NEW PRV & CONTROLLER IAW AMM 36-11-13 & 36-11-20. THEN OPS TEST OF NR 1 ENGINE PRV WITH ENGINE IDLE RUN . WSDR SIMA20150714001Clamp · looseBLEED 1 LEAK AFTER ACCEL ALT IN CLIMB THRUST, MODE WARNING EXTINGUISHED 30 SECONDS AFTER BLEED 1 SELECTED OFF. FOUND CLAMP LEAKING IN LT PYLON, RETIGHTENED CLAMPS ON Y DUCT IN LT PYLON IAW AMM 36-11-09.SDR CA150713012Clamp · failed(CAN) BLEED DUCT MASTER WARNING, RETURN FROM FLIGHT, IT WAS REPORTED THE CLAMP AT THE RT MODULATING SHUTOFF VALVE WAS BAD.SDR CA150714002Shutoff Valve · failed(CAN) FLIGHT DEPARTED WITH LT ENG BLEED INOPERATIVE. AFTER DEPARTURE THE RT ENG BLEED FAILED, ATTEMPTS TO RESET WERE UNSUCCESSFUL. FLIGHT DIVERTED FOR MX. LANDING WEIGHT WAS BELOW MAXIMUM LANDING WEIGHT. RESOLUTION NR 2 ENG PRSOV REPLACED IAW AMM 36-11-01 SDR AALA20150711004Controller · faultyAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB RECEIVED LT ENG PRESS REGULATING VLV EICAS MSG, LT ENG BLEED LIGHT ILLUMINATED. R & R LT PRESS REGULATING VLV CONTROLLER IAW AMM 36-11-19. ACCOMPLISHED ALL REQUIRED CHECKS & ENSDR ASAA2015071012382Valve · no testDUCT PRESSURE DIFF OF 21PSI NOTICED A 37,000FT. LT IS 19 PSI, RT IS 40 PSI. PRESSURIZATION REMAINS NORMAL. ACFT GROUNDED. ACCOMPLISHED BLEED AIR HEALTH CHECK T/C NG-36WC-00001 ON NR 1 ENGINE, FOUND THE PRECOOLER CONTROL VALVE WOULD NOT OPEN OR CLOSE PROPERLYSDR HALA2015070800133Warning Message · illuminatedDURING CLIMB, LT ENG HPSOV MESSAGE DISPLAYED, ENGINE HIGH STAGE BLEED VALVES.SDR RAIA201507030001Line · looseBLEED 2 OVERTEMP, STABILIZER AND WING A/I FAIL IN ICING CONDITION DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND FOUND BLEED LINE LOOSE FROM THERMOSTAT TO FAN AIR VALVE. RESECURED LINE FITTING AND OPS AND LEAK CHECK GOOD.SDR CA150702005Pump · failed(CAN) PILOT REPORTED LT PNEO LIGHT ILLUMINATED DURING FLIGHT. UPON INVESTIGATION MAINTENANCE FOUND THE SHAFT OF THE DRY AIR PUMP HAD SHEARED OFF. PUMP WAS REPLACED AND GROUND RUN CARRIED OUT SERVICEABLE.SDR RAIA201507020001Line · wornBLEED 2 OVERTEMP IN ICING CONDITION, RETURNED TO BLOCK. MAINTENANCE REPLACED BLEED AIR LINE, OPS AND LEAK CHECK GOOD.SDR DALA2015070104066Boot · unsecureON LANDING DESCENT AT 37K, AS THROTTLES WENT TO IDLE, THE CABIN ALTITUDE HORN SOUNDED AT 10,000 FEET. CREW DECLARED AN EMERGENCY, DESCENDED RAPIDLY AND CABIN STAYED AT 10,000 FEET TILL LEVEL. MAINTENANCE FOUND APU BLEED DUCT RUBBER BOOT LOOSE. SECURED AND TSDR ASAA2015062712239Diaphragm · failedWHILE ACCOMPLISHING A FUNCTIONAL CHECK OF PRECOOLER CONTROL VALVE, FOUND PRSOV WITH BLOWN DIAPHRAGM, REQUIRED CHANGE, NR 1 ENG PRSOV. ACFT GROUNDED. NR 1 ENGINE PSROV R & R REF AMM 36-11-04. OP CHECK GOOD.SDR R61A201506220384Loop · faultedCREW RECEIVED A BLEED 1 LEAK MESSAGE ON EICAS. CREW RAN QRH, SHUTOFF REMAINING BLEED, DECLARED AN EMERGENCY AND DROPPED TO 10000 FEET. CREW DIVERTED TO WHERE THEY LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R FAULTY LOOP 3 SECTION PL046 IN THE PYLSDR ASAA2015062112172Regulator · malfunctionedIN CLIMB, THRU FL 300, LT DUCT PRESSURE 20 PSI, RT 47 PSI IN CRUSE AT FL 350, LT 22 PSI, RT 31 PSI BOTH PACKS IN AUTO AND ANTI-ICE OFF. ACFT GROUNDED. PERFORMED T/C NG-36WC-00001 "ENGINE BLEED AIR SYS HEALTH CHECK" ON NR 1 ENGINE. PRE-COOLER CONTROL VALVE FSDR WX0A2015062272680Control Valve · out of adjustDURING CRUISE, PNEU PRESS READ 30 PSI WITH BOTH XFEED LEVERS CLOSED. WHEN EITHER LT OR RT AIRFOIL SWITCH TURNED ON PSI DROPPED TO ZERO. WHEN EITHER LT OR RT AIRFOIL SWITCH TURNED OFF, PNEU PSI WOULD SLOWLY BUILD BACK UP TO 30 PSI WITH BOTH XFEED LEVERS CLOSE
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