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 HNAA2017041700124Clamp · looseNR 1 BLEED LEAK ECAS WARNING MESSAGE ALONG WITH LEAK ILLUMINATED ON THE NR 1 BLEED SWITCH. COMPLIED WITH THE QRH AND BOTH MESSAGES EXTINGUISHED. APU WAS OFF. INSPECTED THE DUCTS AND SENSE LINES AT THE NR 1 PRECOOLER AREA AND FOUND SEVERAL CLAMPS LOOSE. SECUSDR UIEA2017041400581Valve · warning messageRIGHT ENGINE PRIORITY VALVE EICAS MESSAGE RECEIVED AFTER ENGINE START. DISAPPEARED AFTER 5 MINUTES. REMOVED AND REPLACED THE RT ENGINE PRIORITY VALVE IAW AMM 36-11-18. CHECKED OK.SDR HALA2017041400100Shutoff Valve · faultyATB, AIR SYS L PRESS LO INDICATION IN CLIMB OUT ( PRESSURE REGULATOR AND SHUTOFF VALVE (PR ). REMOVED AND
REPLACED LEFT ENGINE PRSOV PILOT VLV PER AMM 36-12-03. OPS CHECK GOOD. DURING ENGINE GROUND RUN RETURNED ACFT TO NORMAL OPERATING STATUS REMOVED PLACARD SDR HNAA2017041700121Warning Message · false activationNR 1 BLEED LEAK WARNING DISPLAYED. RECONFIGURED IAW QRH WARNING WENT OUT AFTER 2 MINUTES 50 SECONDS. GROUND RAN AIRCRAFT WITH BLEEDS ON, NO WARNING MESSAGE DISPLAYED. CHECKED MFD FOR MESSAGES, NO BLEED LEAK MESSAGES DISPLAYED. INSPECTED THE NR 1 BLEED PISDR P5CA2017041300086Shutoff Valve · malfunctionedLEFT ENGINE BLEED AIR MESSAGE. REPLACED PRSOV IAW AMM 36-11-09. OPS CHECKED OK IAW AMM 71-00-00.SDR ASAA2017040920411Setscrew · brokenNR 1 ENGINE PRSOV VALVE INDICATION SET SCREW BROKEN OFF. GROUNDED - YES. REMOVED & REPLACED PRSOV, REF AMM 36-11-04-000-801 AND AMM 36-11-04-400-801. OPS CHECK GOOD. LEAK CHECK GOOD.SDR C77A20170410001Gasket · leakingNR 2 BLEED LEAK IN FLIGHT, WITH NR 1 BLEED ON MEL. OUTLET DUCT GASKET REPLACED IAW AMM 36-11-08.SDR ASAA2017040320353Panel · looseWHILE ACCOMPLISHING T/C 78472000 FOUND TWO FAN DUCT, BLEED VALVE PANELS LOOSE AT OUTBOARD SIDE 8 O'CLOCK & 10 O'CLOCK POSITION. ACFT GROUNDED. TORQUED FAN DUCT, BLEED VALVE PANELS IAW AMM 72-23-07.SDR ASAA2017040320352Bearing · wornWHILE ACCOMPLISHING T/C 48742000 FOUND THE NR 1 ENGINE DUCT ATTACH LINKS FROM DUCT TO FAN CASE WORN AT BEARING ENDS FWD & AFT POSITION. ACFT GROUNDED. REPLACED FWD & AFT ATTACHMENT LINKS ON THE NR 1 ENGINE START DUCT TO FAN CASE 71-00-02, FIG. 25-1.SDR RAIA201703310001Duct · unsecureNR 2 BLEED LEAK DURING CLIMB OUT. R & R THE BLEED AIR DUCT AND BOTH CLAMPS FWD OF THE VALVE IN NR 2 PYLON IAW AMM 36-11-05. OPS CHECKED GOOD.SDR T17A201704034020Gasket · failedDURING CLIMB OUT AT 17000 FT, WITH ENGINE AND WING ANTI-ICE ON, RECEIVED A BL DCT FAIL ANNUNCIATOR. PERFORMED BLEED AIR DUCT FAILURE ABNORMAL CHECKLIST. ANNUNCIATOR EXTINGUISHED AFTER 90 SECONDS. DID NOT RETURN. .MAINTENANCE FOUND AN AIR LEAK AT THE PNEUMATSDR SIMA20170328002Shutoff Valve · failedBLD 2 VALVE FAIL THEN PHL LANDING A/I INOP. THEN A/I FAIL IN CLOUDS W/ICE COND AT 12000 ON CLIMBOUT. REMOVED AND REPLACED E-2 PRSOV IAW AMM CH 36-11-05 OPS CK GOODSDR P5CA2017032800080Regulator Valve · failedAFTER ENGINE START, THE LEFT ENGINE BLEED OFF EICAS MESSAGE DISPLAYED, ASSOCIATED LEFT PACK OFF. REMOVED AND REPLACED PRESSURE REGULATING VALVE IAW AMM 36-11-09 OPS CHECKED NORMAL.SDR ASAA2017032720283Flex Line · leakingDURING A NR 2 ENGINE AMM TASK 36-11-00-710-801, FOUND IT FAILED BLEED AIR CROSSOVER OPERATIONAL TEST. FOUND UPPER BLEED AIR FLEX LINE LEAKING. REPLACED THE FLEX LINE IAW AMM 36-11-00-700-805. SYSTEM OPS CHECKED NORMAL,SDR FDEA201703270995Duct · rupturedCARGO FIRE WARNING DURING TAXI, BOTTLES DISCHARGED, STATUS MESSAGE FOR BOTTLE 1B AND BOTTLE 1A. REPLACED A RUPTURED DUCT.SDR SIMA20170327001Valve · faultyNR 1 BLEED OVERTEMP. REMOVED AND REPLACED NR 1 FAN AIR VALVE IAW AMM 36-11-03. OPS CK GOOD IAW AMM 36-00-00 LEAK CK GOODSDR ANCF2017032201Regulator Valve · failedDURING INITIAL CLIMB AFTER TAKE OFF, AIR ENGINE 2 BLEED FAULT APPEAR ON ECAM; COMPUTER RESET WAS DONE SUCCESSFULLY. TROUBLESHOOTING IN ACCORDANCE WITH TSM 36-11-00-810-B39-A WAS ACCOMPLISHED; AS RESULT, BLEED PRESS/REGULATING VALVE FAIL. THIS VALVE WAS REMOVEDSDR IPXA2017032215413Shutoff Valve · leakingDURING CLIMB, THE RT ENGINE HPSOV CAUTION MESSAGE ILLUMINATED, RAN THE CHECK LIST AND COULD NOT GET BLEED LIGHT TO GO OUT. TROUBLESHOT IAW FIM 36-10-00. FOUND THE HPSOV LOOSE AT VALVE STEM AND LEAKING THRU STEM. R & R AREA AT BOTTOM OF VALVE. R&R'D HPSOV SDR SWIA201743128Warning Message · false activationENROUTE, LT 14TH DUCT WARNING MESSAGE INTERMITTENTLY APPEARED THROUGHOUT FLIGHT. THE DUCTING BETWEEN THE LEFT 14TH SOV AND WING ANTI ICE VALVE ILLUMINATED RED. COMPLIED WITH THE QRH, BUT MESSAGE INTERMITTENTLY PERSISTED. DECLARED EMERGENCY AND DIVERTED. PSDR SIMA20170321001Gasket · failedBLEED LEAK ON SYSTEM 1. REMOVED AND REPLACED THE NR 1 PRECOOLER OUTLET DUCT GASKET IAW AMM 36-11-08. OPS & LEAK CHECKED GOOD.SDR HALA2017032100074Isolation Valve · malfunctionedAFTER ENGINE START, THE RT BLEED ISOLATION VALVE EICAS DISPLAYED AND RT ISOLATION VALVE LIGHT ON OVERHEAD, REMAINED DISPLAYED WITH RT ISOLATION SWITCH LATCHED IN OR OUT. REMOVED AND REPLACED RIGHT BLEED ISOLATION VALVE IAW AMM 36-11-04-404-013. LEAK AND OPS SDR HALA2017031800075Valve · failedSYSTEM FLIGHT FAILURE, NR 2 ENGINE BLEED FAULT ILLUMINATED. TSM 36-11-81-810-914A C/O PRV FOUND FAULTY. PRV REPLACED IAW AMM 36-11-52, REV 56-03. OPS TESTED WITH NO DEFECTS.SDR RAIA201703160001Unknown · malfunctionedBLEED 1 LEAK IN FLIGHT. INSPECTED LT AND RT BLEED BOTH ENG'S AT PACK CARGO & AT AVIONICS NO LEAK NOTED. RAN BOTH ENGINES COULD NOT DUPLICATE.SDR RAIA201703140001Clamp · looseNR 1 BLEED LEAK. FOUND CLAMPS LOOSE ON E1 PRSOV, TIGHTENED CLAMPS. ALSO R2 BLEED SEALS AT POS 9, 17 AND 23 IAW EMB 145 AMM 36-11-09. OPS CHECK GOOD IAW AMM 36-11-05.SDR UIEA2017031400346Switch · failedRT ENGINE BLEED AIR SWITCH DOES NOT POP OUT COMPLETELY WHEN TURNED OFF. REMOVED AND REPLACED THE SWITCH IAW SWPM 20-84-14. OPS CHECKED GOOD.SDR SIMA20170309003O-Ring · leakingAFTER SUCCESSFUL ICE TEST, THE NR 1 ENGINE BLEED LEAK ON EICAS, WENT OUT AFTER DESELECTED THE BLEED SWITCH. REMOVED AND REPLACED O-RINGS AT JOINT NR 1 AND 28. REPLACED THE BLEED DUCT IN AVIONICS COMPARTMENT ALL WORK PERFORMED IAW AMM 36-11-09 AND LEAK AND OPSDR ASAA2017030220016Valve · failedLEFT BLEED TRIP OFF ILLUMINATED. QRH ACCOMPLISHED. RESET SUCCESSFUL AT FL380. ACFT GROUNDED. ACCOMPLISHED WRENCH CHECK OF ALL VALVES. NO FAULTS FOUND, IAW AMM 36-00-00. REMOVED AND REPLACED PRE-COOLER CONTROL VALVE IAW AMM 36-12-12. REMOVED AND REPLACED HIGSDR C77A20170301001Gasket · rupturedDURING CRUISE CREW RECEIVED A NR 1 BLEED LEAK EICAS MESSAGE DURING FLIGHT. CREW PERFORMED QRH, MESSAGE EXTINGUISHED. FLIGHT RETURNED TO DEPARTURE DUE TO ICING CONDITIONS ENROUTE. NO EMERGENCY DECLARED. MAINTENANCE FOUND THE AFT PRECOOLER GASKET RUPTURED. RESDR RAIA201702250001Shutoff Valve · leakingNR 1 BLEED LEAK IN FLIGHT. R & R THE PRSOV. OPS CHECKED GOODSDR RAIA201702240001Warning Light · false activationNR 2 BLEED LEAK IN ICING CONDITONS. PERFORMED AN OPS TEST OF ENGINE BLEED VALVES IAW AMM 36-11-05. NO FAULTS OR LEAKS FOUND. INSPECTED BLEED DUCTS IAW AMM 36-11-09, NO LEAKS FOUND AT THIS TIME.SDR AALA201702249011Check Valve · faultyNR 2 ENGINE STALLED AT 55KTS DURING TAKEOFF ROLL. FLIGHT CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE ACCOMPLISHED TSM 71-00-00-810-A14-A. REPLACED RIGHT ENGINE IP CHECK VALVE PER TASK 36-11-41. AIRCRAFT WAS GROUNDED.SDR YADA20170224001Intake Duct · unsecurePILOT REPORTED THE RIGHT HAND ENGINE FIRE LIGHT ILLUMINATED DURING TAKEOFF ROLL, ORIGINAL TAKEOFF WAS ABORTED. MAINTENANCE FOUND #2 ENGINE INBOARD NACELLE INTAKE HEAT DUCT WAS UNSECURED. SECURED DUCT AND OPERATIONAL TEST WAS SUCCESFULL.SDR GTIA2017022201799Computer · malfunctionedNR 1 IAW AMM 36-11-00 OPS CHECK GOOD. NO FAULTS AT THIS TIME. SWAPPED BMC NR 1 WITH BMC NR 2 FOR TROUBLESHOOTING PURPOSES. BITE TEST GOOD IAW AMM 36-11-00. BMC NR 1 P/N 785002-9 S/N 2845 IS IN NUMBER 2 POSITION.
BMC NR 2 P/N 785002-8 S/N 6360 IS IN NUMBER 1 PSDR P5CA2017022100065Packing · tornLEFT DUCT PRESSURE SURGES BETWEEN 20 TO 50 PSI DURING CHANGES IN ENGINE POWER SETTINGS. DISCOVERED LT ENGINE PRSOV INLINE FILTER FREE OF DEBRIS, PLUG HAD TORN PACKING. REMOVED AND REPLACED PACKING. PRSOV OPS CHECK AND DUCT PRESSURE MODULATION CORRECTED ON ENGSDR ASAA2017021519835Regulator · faultedLEFT DUCT PRESSURE IS 10 PSI AT IDLE TRUST ON THE GROUND. ACFT GROUNDED. ACCOMPLISHED THE PNEUMATIC SYSTEM TROUBLESHOOTING IAW AMM 36-11-00-700-804 - NO DEFECTS WERE NOTED. REMOVED AND REPLACED THE NR 1 ENG HIGH STAGE VALVE IAW AMM 36-11-06-00-000-801 ANDSDR DXTA2017021306371Valve · defectiveUPON INITIATING DECENT, WHEN THE THROTTLES WERE REDUCED AND THE PAC HP VALVE OPEN L-R CAS MESSAGE APPEARS, THERE IS A STRONG ODOR OF BURNING RUBBER. REMOVED AND REPLACED A DEFECTIVE HP VALVE ON NR 1 ENGINE. LEAK AND OPS CHECKED GOOD IAW AMM 36-10-00.SDR ASAA2017021319800Link · damagedFOUND LINK DAMAGED ON INBD SIDE OF DUCT FOR LOWER SIDE OF PRSOV VALVE. ACFT GROUNDED. REMOVED AND REPLACED THE LINK IAW 71-00-02, FIG 16-1.SDR ASAA2017021319799Link · damagedDURING INSPECTION. FOUND STAND-OFF LINK ON LWR FWD SIDE OF PRSOV VALVE DAMAGED AT BOTH ENDS. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE LINK ON LOWER FWD SIDE OF PRSOV IAW PBM 71-00-02, FIG 16-1.SDR ASMF20170301002Warning System · activatedAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CRUISE, THE RIGHT SIDE WING BODY OVERHEATS LIGHT TURNED ON AND RIGHT PACK AIR CONDITIONED WAS DEFERRED, SHOWING BETWEEN 12 PSI AND 15 PSI. MAINTENANCE PERSONNEL PERFORMED REVISION, CONFIRMING THE FAILURE; SO THE RIGHT SDR ASAA2017020519692Duct · wornNR 1 ENGINE INTERSECTION MANIFOLD DUCT ASSEMBLY ATTACH LINK WORN. ACFT GROUNDED. REMOVED AND REPLACED THEE INTERSECTION MANIFOLD DUCT ASSEMBLY ATTACH LINK IAW AMM 36-11-01-400-802.SDR ASAA2017020419672Rod End · worn#1 ENG LOWER STARTER DUCT FWD ROD-END ASSY & BRACKET WORN. ACFT GROUNDED. REPLACED ROD END ASSY & BRACKET.SDR J7SA20170203001Bleed Air Sys · contaminatedAIR TURNBACK DUE TO STRONG OIL ODOR IN AIRCRAFT, AFTER BLEEDS WERE TRANSFERRED TO ENGINES FROM APU. LANDED WITHOUT INCIDENT. PERFORMED ENGINE HIGH POWER RUNS WITH ALTERNATING BLEED SOURCES. VERIFIED OIL ODOR. CONTINUED TO RUN SYSTEM TO CLEAR OIL FROM BLEED SDR HNAA2017020300038Pressure Switch · malfunctionedDURING CLIMB, NR 2 BLEED LEAK EICAS MESSAGE ILLUMINATED ALONG WITH PB LEAK ILLUMINATED. CLEARED MESSAGE. REMOVED AND REPLACED NR 2 LOW PRESSURE, OPS CHECKED OK AT THIS TIME. SWITCH REPLACED IAW MM 30-11-00-810-811-A.SDR ASAA2017013019605Bleed Valve · failedDURING CLIMB OUT, CABIN CLIMB INDICATION FLUCTUATED FROM 200-900 FPM. LEFT DUCT PRESSURE STEADY AT 40 PSI WITH RIGHT DUCT FLUCTUATING FROM 40-60 PSI. REACHING FL 340, CABIN CLIMB INDICATOR CONTINUES TO FLUCTUATE FM -300 TO + 350 FPM WHILE LEFT DUCT PRESSURE RSDR ASAA2017013019604Valve · failedWHILE ACCOMPLISHING TC: NG-36WC-00001 FOUND HIGH STAGE VALVE BAD. ACFT GROUNDED. REMOVED AND REPLACED NR 2 ENGINE HIGH STAGE VALVE IAW AMM 36-11-06-000-801 AND 36-11-06-400-801. LEAK CHECKED GOOD. ACCOMPLISHED ENGINE BLEED AIR CROSSOVER OPS TEST IAW AMM 36-11SDR RAIA201701280001Valve · inoperativeHS VALVE NR 2 FAILED EICAS, AGAIN ON CLIMBOUT. R & R THE NR 2 HIGH STAGE VALVE, OPS CHECKED GOOD, NO FAULTS FOUND.SDR P5CA2017012700048Precooler · damagedNR 2 ENGINE PRECOOLER EXHAUST FIN DAMAGED. REPLACED THE PRECOOLER IAW AMM 36-11-15-004-003-001 REV120 AND AMM 36-11-15-404-020-001 REV 120. LEAK CHECKED GOOD.SDR P5CA2017012700049Shutoff Valve · malfunctionedFOUND NR 2 ENGINE PRSOV CAN NOT OPEN WHEN PERFORMING A PNEUMATIC SYSTEM HEALTH CHECK IAW AMM 36-11-09-002-033-001 REV 120 AND AMM 36-11-09-402-058-001 REV 120. NR 2 ENGINE PRSOV WAS REMOVED AND REPLACED IAW AMM 36-11-09-402-058-001 REV 120 AND AMM 36-11-09-78SDR P5CA2017012700050Pneumatic System · malfunctionedFOUND NR 2 ENGINE HPC BIT UNIT CANNOT CHANGE WHEN PERFORMING A PNEUMATIC SYSTEM HEALTH CHECK IAW AMM 36-11-08-004-006-007 REV 120. REMOVED THE NR 2 ENGINE HPC AND REPAIRED IAW AMM 36-11-08-404-014-007 REV 120. LEAK CHECKED GOOD.SDR P5CA2017012700052Shutoff Valve · malfunctionedFOUND NR 1 ENGINE HPSOV CANNOT CLOSE DURING PNEUMATIC SYSTEM HEALTH CHECK. REPLACED HPCIAW AMM 36-11-08-004-006-007 REV 120 AND AMM 36-11-08-404-014-007 REV 120. PERFORMED A NR 1 ENG DRY MOTORING FOR HPC PNEUMATIC LINE CONNECTIONS, LEAK CHECK RESULTS: NO LE
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