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 HNAA2009041500121Pipe · brokenNR 2 ENGINE HIGH ITT, 765 AT 85 PERCENT AND FUEL FLOW HIGHER THAN NR 1 ENGINE. FOUND Y-PIPE JUST AFT OF NR 2 HP VALVE BROKEN. REMOVED AND REPLACED Y-PIPE USING ORIGINAL HARDWARE AND CLAMPS, OPS & LEAK CHECK GOOD IN ACCORDANCE WITH 21-11-00 AND ALL ENGINE PARSDR RAIA2009041400004Duct · crackedFLT 7983 - IAD - CREW RECEIVED A BLEED LEAK NR 1 MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED BLEED DUCTS. SYSTEM OPS CHECKED GOOD.SDR ASAA0955089Valve · defectiveDURING CLIMBOUT AT CLIMB POWER (BOTH ENGINES) RIGHT PACK PSI FLUCTUATED BETWEEN 38 AND 48 PSI STABLE AT LOW POWER SETTINGS. (LEFT PACK AT 48 PSI CLIMB POWER STABLE THROUGHOUT) MIG 2C 247415 INITIATED. INIT MIG 2C 247416. REMOVED & REPLACED DEFECTIVE HIGH STASDR UALA2009040901032Valve · failedIN CRUISE FL400 L BLEED PRESS FLUCTUATED DOWN 2 AROUND 24 PSI. THEN WENT DOWN AND STAYED AT 24 PSI MAINT TEXT: PER VERBAL FROM INBOARD CREW LT 24 PSI RT 42 PSI REMAINDER OF CRUISE FLT. REPLACED VALVE AND CONTROL PER MM 36-11-07 AND MM 36-11-08. ACCOMPLISHEDSDR RAIA2009041400001Line · defectiveFLT 3548 - STL - DURING CLIMBOUT, THE CREW RECEIVED A NR 2 ENGINE FIRE DETECTION WARNING FOR 2-3 SECONDS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A BAD ENGINE BLEED LINE. THE LINE WAS REMOVED AND REPLACED AND THE SYSTEM OPS CHECKED GOOD.SDR UALA2009040600987Shutoff Valve · faultyRIGHT ENGINE BLEED LIGHT ILLUMINATED. REPLACED RIGHT ENGINE HPSOV.SDR CHQA200900097Switch · intermittentFLIGHT 7860, IAD TO YOW. DURING CLIMB-OUT, THE CREW RECEIVED AN EICAS MESSAGE FRO BLEED 2 VALVE CLOSED. THE QRH WAS FOLLOWED BUT DID NOT CLEAR THE FAULT. DUE TO FORECAST ICING CONDITIONS THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. THE FIM WASSDR HNAA2009040800110Clamp · looseBURNED SMELL IN CABIN AT ROW 4 AND ROW 5 AREA. INSPECTED THE NORMAL CABIN LIGHTING AND EMERGENCY LIGHTING POWER SUPPLY IN THIS AREA, PERFORMED HIDDEN DAMAGE INSPECTION, FOUND NO DAMAGE, DEACTIVATED NORMAL CABIN LIGHTING AS A PRECAUTION. FOUND BLEED T-DUCT CLSDR DL76L090559Shutoff Valve · lockedON CLIMB-OUT, JFK RT ENG HPSOV EICAS FWD TO MCO/PLAC PER MEL 36-11-02. RT ENG HPSOV LOCKED OUT. JUMPER INSTALLED.SDR C2XA09CL034Switch · faultyCLE FLIGHT 2378 - THE CREW REPORTED A WING AND STAB ANTI-ICE FAIL MESSAGE IN ICING CONDITIONS DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE BLEED PUSH BUTTON SWITCH. OPESDR C2XA09RI065Thermostat · inoperativeFLIGHT 2530 - GSO - FLIGHT CREW REPORTED THAT DURING CLIMBING, AFTER ENTERING ICING CONDITIONS AT 13000FT , BLEED NR 2 OVERTEMP THEN BLEED NR 1 OVERTEMPED AS BLEED NR 2 BECAME NORMAL, ICING SYSTEM TURNED OFF THEN OVERTEMP WENT AWAY. CREW PERFORMED AIR RETURN SDR C2XA09RI064Valve · inoperativeFLIGHT 2530 - GSO - FLIGHT CREW REPORTED THAT DURING CLIMBING, AFTER ENTERING ICING CONDITIONS AT 13000FT, BLEED NR 2 OVERTEMP THEN BLEED NR 1 OVERTEMPED AS BLEED NR 2 BECAME NORMAL, ICING SYSTEM TURNED OFF THEN OVERTEMP WENT AWAY. CREW PERFORMED AIR RETURN ASDR CALA2009032500165Seal · tornCABIN ALTITUDE WARNING HORN SOUNDED WHILE CLIMBING THROUGH 33,000 FT. QRH PROCEDURE STABILIZED CABIN ALT IN MANUAL MODE, PACKS ON HIGH. PACKS IN AUTO WOULD NOT HOLD CABIN ALTITUDE. PERFORMED AN UNSCHEDULED LANDING IN PHX. BITE TEST DCPC FOUND FAULT 030, TRSDR SIMA200908501Duct · separatedON FLIGHT 4322 CREW REPORTED ON CLIMBOUT OBSERVED LEFT ENGINE OIL PRESS WITH RED INDICATION (8L); OIL TEMP INCREASING. FOLLOWED AOM PROCEDURE AND CONTINUED WITH ENGINE SHUTDOWN ON LEFT ENGINE. RETURNED TO CMH AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDESDR UALA2009032300872Shutoff Valve · faultyRIGHT ENG BLEED LIGHT & RT ENG HPSOV EICAS MSG DURING DESCENT WITH ENG BLEED SW ON & ENGINE RUNNING. REPLACED HPSOV.SDR CA090402004Duct · ruptured(CAN) CROSSOVER DUCT HAS RUPTURE AT EXPANSION BELLOWS ON OPPOSITE SIDE FROM FIRE WIRES. PART IS TRACKED AS EXPEDABLE.SDR AALA2009031400002Augment Valve · inoperativeELP - INFLIGHT SJD-DFW. TAIL COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON FOLLOWED BY ENGINE FIRE BOTTLE AGENT LOW LIGHT. LANDED ELP WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AUGMENTATION VALVE AND LEFT PRESSURE REGULATOR. SYSTEM GROUNDSDR GLBA200903141B-Nut · looseDURING CRUISE THE PILOTS REPORTED THAT THEY HAD A LOSS OF PRESSURIZATION AT 240. MAINTENANC REINSTALLED ELECTRO PNUEMATIC OUT FLOW VALVE IAW EMB120 MM. 21-30-03. FOUND INSULATION AROUND ELECTRO PNUEMATIC OUT FLOW VALVE LOOSE RESECURED INSULATION AS REQUIRED WISDR 2009FA0000195Line · cutPERFORMED SUPPLEMENTAL INSP FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSP NR 57-10-14 CARRY-THRU FWD SPAR CAP FOUND MULTIPLE PNEUMATIC LINES SPLICED TOGETHER WITH STANDARD MIL-SPEC HOSE ON LT AND RT WINGS. LINES NOT AVAILABLE FROM MFGSDR 2009FA0000194Line · cutPERFORMED SUPPLEMENTAL INSP FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUP INSP NR 57-10-14 CARRY-THRU FWD SPAR CAP, FOUND MULTIPLE PNEUMATIC LINES SPLICED TOGETHER WITH STANDARD MIL-SPEC HOSE ON LT AND RT WINGS. LINES NOT AVAILABLE FROM MFG. FABRISDR YENA20090310025Thermostat · malfunctionedDURING TAKEOFF CLIMB DUAL ENGINE BLEED FAULT APPEARED ON ECAM. AIRCRAFT RETURNED TO BASE NO EMERGENCY WAS DECLARED. NR 1 ENGINE FAN AIR THERMOSTAT WAS REPLACED IAW MM 36-11-43, ALSO NR 2 ENGINE THERMOSTAT FILTER WAS REPLACED. HIGH POWER ENGINE RUN WAS PERFSDR DL76L090374Controller · malfunctionedLEFT BLEED NO OUTPUT PRESS UNABLE TO CROSSBLEED START ENG. FOUND LT ENG PRV INOP SWAPPED WITH HPSOV FWD TO MCO PER MEL 36-11-02 HPSOV LOCKED CLOSED. REMOVED AND REPLACED PRV CONTROLLER IAW MM.SDR UALA2009031000682Shutoff Valve · faultyRTO AT APPROX 70KTS DUE TO LEFT ENG HIGH STAGE LT ILLUMINATING. REPLACED LT ENGINE HPSOV AND HIGH STAGE PILOT VALVE, NO HELP. CONTINUING TO TROUBLESHOOT. NR 1 ENG READS 4 PSI, NO HIGH STAGE AFTER HIGH STAGE AND PILOT VALVE REPLACEMENT AT IDLE. BLEED LIGHT SDR UALA2009031000679Modulating Valve · failedBLEED FAMV L LEFT ENGINE BLEED FAN AIR MODULATING VALVE (FAMV) FAILED OPEN OR CLOSED OR LEFT AIR SUPPLY AND CABIN PRESSURE CONTROLLER FAILURE. STATUS MSG-3610531 LATCHED ER MODE MSG-3610531 LATCHED ER MODE MSG-3610200 ACTIVE CL MODE MSG-3610200 ACTIVE CL MOSDR UALA2009030200679Modulating Valve · faultyLEFT ENGINE BLEED FAN AIR MODULATING VALVE (FAMV) FAILED OPEN OR CLOSED OR LEFT AIR SUPPLY AND CABIN PRESSURE CONTROLLER FAILURE. STATUS MSG-3610531 LATCHED ER MODE MSG-3610531 LATCHED ER MODE, MSG-3610200 ACTIVE CL MODE MSG-3610200 ACTIVE CL MODE. *S/D* RESDR CHQA200900067Filter · dirtyFLIGHT 3018, GSO TO LGA - DURING CLIMB WHILE PASSING THROUGH 5,000 FT WITH ANTI-ICING ON, THE FLIGHT CREW RECEIVED A BLEED 1 OVER-TEMP MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND IT WAS NOTED THAT THE BLEED 2 TEMPERATURE WAS ALSO CLOSE TO THE LIMITS. THE AIRCSDR C2XA09CL022Duct · blownCLE FLIGHT 2578 - THE CREW REPORTED A BAGG SMOKE WARNING ACCOMPANIED BY APU BLEED LEAK AND ACTUAL SMOKE IN THE COCKPIT AND CABIN WHILE PARKED AT THE GATE. CONFIGURED AS FOLLOWED APU BLEED OPEN, CROSSBLEED OPEN, PACK 1 CLOSED, PACK 2 OPEN. THE BAGG FIRE BOTTLSDR GLBA20090227BBleed Air Sys · malfunctionedFLT 5177 - UPON CLIMBING THE PILOTS REPORTED THAT THE APU BLEED WOULD NOT MAINTAIN GREATER THAN 3.5 PSI WITH PACKS IN LOW OR NORM. ENGINE BLEEDS WERE SELECTED TO AUTO & PACKS LOW AND THE AIRCRAFT COULD ONLY MAINTAIN 4.0 P.S.I. PACKS SELECTED TO NORM ACHIVED SDR RAIA2009030300001Duct · out of positionFLT 5535 - STL - CREW RECEIVED A NR 1 BLEED LEAK MESSAGE ON THE EICAS SHORTLY AFTER TAKEOFF. MAINTENANCE INSPECTED AND FOUND A LEAK AFT OF THE NR 1 PRECOOLER. THE DUCT WAS REPOSITIONED AND THE SYSTEM OPS CHECKED.SDR RAIA2009022400005Bleed Air Sys · malfunctionedFLT 5591 - MIA - CREW RECEIVED AN E1 BLEED LEAK MESSAGE ON THE EICAS. MAINTENANCE DEFERRED THE NR 1 ENGINE BLEED SYSTEM IAW MEL PROCEDURES.SDR ASAA0954486Precooler · failedIN CRUISE FLIGHT AT 37000 RIGHT DUCT PRESSURE IS 25 PSI LEFT DUCT PRESSURE 44 PSI. RIGHT DUCT PRESSURE VARIES BETWEEN 21 PSI AND 44 PSI. ACCOMPLISHED FIM TASK 36 10 00 810 804 STEP 21F 34G, PERFORMED NR 2 ENG BLEED AIR SYSTEM HEALTH CHECK. FOUND PRECOOLER BSDR UALA2009022300621Controller · failedR ENG HPSOV EICAS. REPLACED HIGH PRESSURE CONTROLLER AND RAN ENG. NO EICAS MESSAGES.SDR UPS09654817Duct · leakingINSPECTION TYPE:ETOP ATB - RIGHT BLEED SYSTEM DUCT LEAK. A/C IS CURRENTLY OOS.SDR FDEA200902170564Loop · faultedPASSING 16000 FT ON CLIMB-OUT GOT AIR SYST 2 OFF, FOLLOWED BY LEVEL 2 AIR MANIFOLD 2 FAIL. NR 2 PACK WAS SELECTED OFF AT THE TIME AND NR 2 BLEED WAS ON. PER QRH LAND AT NEAREST SUITABLE AIRPORT. PERFORMED AIR SYSTEM DECAY CHECK REF AMM 36-00-01-5. TEST PASSDR C2XA09IA050Bleed Air Sys · contaminatedIAH - FLIGHT 2371 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN AFTER TAKEOFF. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX GROUND RAN THE ENGINES TO REMOVE RESIDUAL OIL FROM THE BLEED AIR SYSTEM FROM A PREVIOUS ENGINE CHANGE, OPS TESTED SDR USA09021690344Thermostat · faultyDIVERSION - 0327ZF152 LOST BOTH ENGINE BLEEDS, DIVERTED. AIR ENG BLEED NR 2 FAULT. REMOVED AND REPLACED NR 2 ENG TEMP CONTROL THERMOSTAT. OPS CHECK WAS GOOD. (K)SDR USA09021690343Thermostat · faultyDIVERSION - 03272F152 LOST BOTH ENGINE BLEEDS, DIVERTED. AIR ENGINE BLEED 1 FAULT. REMOVED AND REPLACED NR 1 ENGINE TEMP CONTROL THERMOSTAT. OPS CHECK WAS GOOD. (K)SDR DL76G090183Pressure Sensor · inoperativeAFTER ENGINE START, LEFT ENGINE BLEED AIR INOP. MAINTENANCE IN WORK AIR SUPPLY BITE FAULTS PRSOV PRESS SENSE. REMOVED AND REPLACED PRSOV PRESS SEN PER M/M 451904 FOUND MUSCLE AIR LINE FITTING LOOSE REATTACH RAN ENG. OPS CKS OK PER M/M MFG 415G265-1.SDR RAIA2009021700003Duct · leakingFLT 5547 STL - BLEED 1 LEAK DURING CLIMBOUT. MAINTENANCE DISCOVERED DUCT LEAKING, DUCT REPLACED IAW EMB 145 AMM PROCEDURE, OPS CHECK GOOD.SDR AALA2009020601037Duct · crackedDFW - TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RETURNED TO DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED GASKET ON PNEUMATIC SUPPLY LOW TEMP SENSOR AND REPLACED CRACKED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.SDR C2XA09SH048Thermostat · malfunctionedFLIGHT 2944 (AIRCRAFT N14153-SERIAL NUMBER 761) ON JANUARY 27, 2009 HAD BLD (1) OVERTEMP IN FLT. NO EMERGENCY BUT FLIGHT DIVERTED IAH TO SHV. MAINTENANCE REMOVED AND REPLACED LT FWD AND AFT FAN AIR CONTROL THERMOSTATS IAW EMB 145XR AMM 36-11-06. OPERATIONALSDR RAIA2009020900001O-Ring · damagedFLT 8066 - ORD - VISIBLE SMOKE IN CABIN - LAV SMOKE MESSAGE ILLUMINATED - DROPPED O2 MASKS. MAINTENANCE REPLACED NR 2 BLEED O-RINGS AT ZONE 260, RT IAW EMB I45 AMM PROCEDURE. OPS CHECK GOOD. FERRY FLIGHT TO SLT WHERE MAINTENANCE REMOVED AND REPLACED PAX OXSDR UALA2009020600408Shutoff Valve · fluctuatesLEFT DUCT PRESSURE FLUCTUATED 20 PSI DURING DESCENT WITH POWER JUST ABOVE IDLE. REPLACED HPSOV. TESTED AND NO LEAK DETECTED.SDR CHQA200900044O-Ring · leakingFLIGHT 6096 LIT TO CVG. WHILE CLIMBING THROUGH 11,000FT ICING CONDITIONS WERE ENTERED, AND SEVERAL MINUTES AFTER THAT THE ANTI-ICING SYSTEMS ACTIVATED AND THERE WAS A BLEED 1 LEAK MESSAGE DISPLAYED ON EICAS. THE QRH WAS FOLLOWED AND IT WAS DECIDED TO RETURN SDR CHQA200900038O-Ring · leakingFLIGHT 6102 CMH TO BOS, THE FLIGHT CREW RECEIVED A BLEED 1 LEAK MESSAGE AFTER TAKEOFF. THE MESSAGE CLEARED WHEN THE NR 1 BLEED WAS TURNED OFF. THE FLIGHT RETURNED TO KCMH AND LANDED WITHOUT INCIDENT. WHILE TROUBLESHOOTING THE BLEED SYSTEM, THE BLEED LINE JUSDR ASAA0954324Regulator · malfunctionedFAULT CODE 361 070 00. AFTER T/O DUCT PRESS SPLIT 20 PSI. RT PRESSURE VARIABLE FROM 38PSI TO 58PSI. LT PRESSURE STAYED CONSTANT AT 42 PSI. N1 AT CLIMB POWER 97.8%. OAT 08 DEGREES C. ALTITUDE 3000'MSL. WING AND ENG ANTI ICE OFF ISOLATION VALVE AUTO. LT & SDR UALA2009012800307Duct · crackedRT ENG BLEED AIR SUPPLY DUCT CRACKED AT CONN TO RT PACK SUPPLY LINE. NEW DUCT IN HAND, INSTALLING NOW. CLOSE UP TO FOLLOW. OPS CHECKS GOOD AFTER REPLACEMENT OF RT ENG BLEED AIR SUPPLY DUCT DUE TO CRACKS.SDR VNAA2009012800012Shutoff Valve · failedCREW REPORTED 'L ENG BLEED' CAUTION AFTER TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TESTED AND REMOVED AND REPLACED THE LT ENG PRSOV PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.SDR C2XA09IA027Duct · leakingFLIGHT 2087, THE CREW REPORTED A BLEED 1 LEAK AT FL180. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R&R THE LT HORIZONTAL BLEED DUCT, OPS AND LEAK CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVISDR C2XA09IA026Duct · leakingIAH - FLIGHT 2087, THE CREW REPORTED A BLEED ONE LEAK AT FL180. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R&R THE LT SIDE HORIZONTAL BLEED DUCT, OPS AND LEAK CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RE
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