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 S2YA05072Pressure Switch · inoperativeON TAKEOFF OF FLIGHT, THE CREW REPORTED THE RT ENVIRONMENTAL BLEED AIR SYSTEM FAILED AND ABORTED THE TAKEOFF. THE SYSTEM WAS PUT ON MEL AND THE AC WAS RETURNED TO SERVICE. REPLACED A BAD PRESSURE SWITCH AND WITH NO FURTHER DISCREPANCIES RETURNED THE AC TO SESDR 05FDEA03589Clamp · out of positionDURING CLIMB-OUT ENG NR 1 STRUT OVHT LIGHT ILLUMINATED ACCOMPLISHED ABNORMAL CHK LIST AFTER BLEED AND PACK SW'S CLOSED AND THRUST LEVER TO IDLE LIGHT OUT. INSPECT ALL THE CLAMPS ON THE NR 1 STRUT. PRESSURIZING THE DUCTS USING APU AIR FOUND CLAMP ADJACENT TOSDR SIMA200529309Duct · crackedORD - FLT 4402 - LAVATORY SMOKE WARNING CAME ON DURING TAXI AND WENT OUT. INSPECTED CUSTOMER SERVICE MANIFOLD ON LEFT ENGINE AND FOUND HIGH STAGE BLEED TUBE CRACKED. REPLACED BLEED TUBE. PERFORMED FUNCTIONAL TEST FLIGHT AND PASSED. OPERATIONAL TEST OF SMOKSDR 2005FA0001480Clamp · looseIN CRUISE FLIGHT, 2500 RPM, 35 HG, PILOT NOTED L/ENGINE LOST POWER. PILOT FEATHERED PROPELLER AND POWERED ENGINE. MAINT NOTED INTERCOOLER DUCT, PN 102-389003-3 LOOSE AT DUCT SERV CLAMP WAS LOOSE, DUCT WAS PARTIALLY DETACHED. REPLACED DUCT, RUNUP OK. (K)SDR AU510001507Valve · faultyLT BLEED ISOLATION VALVE FAULTY. WORKSHOP INVESTIGATION FOUND THE FAILURE WAS DUE TO AN WORN AND INOPERATIVE MOTOR ASSEMBLY.SDR RAIA005100001Duct · blownFLT 3553 - LGA - SMOKE IN CABIN DURING CRUISE. INSPECTED AND FOUND BLOWN DUCT. SYSTEM DEFERRED.SDR DL76P050576Clamp · looseON TAKEOFF HAD RT DUCT BLEED CAUTION LIGHT AND EICAS MSG . RTO AT 70 KTS. MTC FOUND THE UPSTREAM CLAMP ON THE RT BLEED ISLN VALVE LOOSE. SECURED SAME.SDR 05FDEA03161Line · crackedAT 800' AGL AND 180 KIAS NR 2 FIRE LIGHT ILLUMINATED PERFORMED PHASE 1 AND CHECKLIST LANDED UNEVENTFULLY.SDR COMA0560522Shutoff Valve · inoperativeFLIGHT 5528 - LEFT BLEED AIR WILL NOT OPEN. CND, OPERATIONAL CHECK NORMAL.SDR TSAA0536040Transducer · failedETOPS FLIGHT 484 HNL-SNA. DUCT PRESSURE SPLIT ON CLIMB (FL 290) LEFT DUCT AT 26 PSI. RIGHT DUCT AT 46 PSI. N1 AND N2 THE SAME ON BOTH ENGINES. AT FL370 LEFT DUCT AT 20 PSI. RIGHT DUCT AT 44 PSI. N1 AND N2 SAME ON BOTH ENGINES. CREW RETURNED TO HNL WITHOUSDR 1262091005Plug · unknownAIRCRAFT YAWS LEFT AND RIGHT ABRUPTLY DURING ALL PHASES OF FLIGHT.SDR DL76L050529Shutoff Valve · failedRIGHT ENGINE BLEED VALVE WOULD NOT OPEN WHEN SELECTED ON. TRIED NEW PRSOV FILTERS, NO HELP. RERACKED RIGHT ENGINE BLEED CARD, NO HELP. REPLACED RIGHT ENGINE PRSOV, OPS OK.SDR DL76L050498Valve · malfunctionedRTB - LEFT ENGINE BLEED LIGHT WITH PRV STATUS MSG . REPLACED VALVE.SDR DXTA200500927Sensor · malfunctionedON DESCENT, PYLON BLEED LEAK, ILLUMINATED EMERGENCY PROCEDURES COMPLETED, WARNING LIGHT EXTINGUISHED WHEN IDLE, BUT CAME BACK ON WHEN POWER WAS ADDED. REMOVED PANEL 412DB TO GAIN ACCESS TO SENSOR TT018 AND TT020 VISUALLY INSPECTED BOTH SENSORS, NO DEFECTS NOTSDR 05FDEA02598Duct · leakingPASSING FL 330 GOT NR 2 BLEED LEAK LT IAW ECAMS SHUTOFF NR 2 BLEED VALVE. A/C WOULD NOT HOLD CABIN PRESS AT 310,280,OR EVEN 12,000 FT WITH NR 1 PACK. PACK BAY FOUND SENSOR LOOPS TOUCHING THE BLEED AIR SUPPLY DUCT GOING TO THE NR 2 ENG, ALSO FOUND SMALL LEASDR AWXA200501017Duct · damagedPHX - AIR TURN BACK - FLT 0049 - DURING CLIMB, AFTER TAKEOFF CREW RECIEVED NR 2 ENGINE OVERHEAT EICAS DURING CLIMB. CREW FOLLOWED QRH AND ISOLATED BLEED SOURCE. CREW DECIDED TO RETURN TO PHX. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND DUCT LEAKING SDR 2005000013Valve · malfunctionedNR 2 PNEUMATIC TEMP HI LIGHT ILLUMINATED. ASSOCIATED PNEUMATIC TEMP INDICATOR WAS IN THE RED ZONE. REMOVED AND REPLACED NR 2 ENGINE FAN AIR VALVE IAW 36-13. PERFORMED ENGINE RUN, NO DEFECTS NOTED.SDR CVU2005F00003Shaft · shearedPUMP FAILED UNDER NORMAL OPERATING CONDITIONS (VFR, DAY).SDR XN0A1258Regulator · failedON CLIMBOUT, GOT NR 1 ENGINE TEMP HIGH AND REGUL FAULT LIGHTS. TEMP WAS PEGGED AT 300 DEGREES C. PERFORMED QRH WITH NO CHANGE. LT AND CENTER MANIFOLD LIGHTS CAME ON. REDUCED THROTTLE TO IDLE. TEMP REDUCED AND LIGHTS EXTINGUISHED. REMOVED AND REPLACED NR SDR DL76L050457Valve · failedL HPSOV EICAS MSG AT 80 PERCENT N1 ON T/O ROLL. REPLACED VALVE.SDR 2005FA0001117Regulator Valve · rupturedUPON RUN UP, PILOT CYCLED BOOTS. BOOT CYCLE STATUS LIGHT CAME ON BUT EXTINGUISHED BEFORE 6 SECOND INFLATION CYCLE TIMED OUT. (PRESS TO TEST SHOWED LAMP OK) BOOTS REMAINED PARTIALLY INFLATED AND WOULD NOT DE-FLATE. PILOT SPOOLED ENGINES DOWN AND BOOTS DE-INFLASDR 2005FA0001116Regulator Valve · rupturedUPON RUN UP, PILOT CYCLED BOOTS. BOOT CYCLE STATUS LIGHT CAME ON BUT EXTINGUISHED BEFORE 6 SECOND INFLATION CYCLE TIMED OUT. (PRESS TO TEST SHOWED LAMP OK). BOOTS REMAINED PARTIALLY INFLATED AND WOULD NOT DE-FLATE. PILOT SPOOLED ENGINES DOWN AND BOOTS DE-FLATSDR TSAA0549035Connector · damagedNON-ETOPS ON TAXI AFTER LANDING THE CREW GOT AN APU FIRE WARNING LIGHT, COMPLETED APU FIRE CHECK LIST, SHUTDOWN APU AND DISCHARGED APU FIRE BOTTLE. FIRE WARNING LIGHT EXTINGUISHED. AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED APU FSDR AMTA200500634Seal · unserviceableON TAKEOFF AND CLIMB OUT, LT HIGH STAGE BLEED LIGHT ILLUMINATED ACCOMPANIED WITH EICAS MESSAGE RETURNED TO DEPARTURE. T/S IAW FIM, FOUND HPSOV BUTTERFLY SEAL BROKEN. REPLACED IAW FIM MM, LEAK CHECK GOOD. (K)SDR CA050824006Fitting · loose(CAN) ON APPROACH, THE CREW NOTED A VIBRATION/SHUDDER WITH A CORRESPONDING DECREASE IN ENGINE AND MAIN ROTOR SPEEDS AND A LOW ROTOR WARNING ANNUNCIATION. THIS CALUMNIATED IN A HARD LANDING. SUBSEQUENT INSPECTION REVEALED LOOSE PNEUMATIC FITTINGS ON THE ENGINESDR QXEA200501143O-Ring · leakingPDX FLIGHT NR 2036, STARTED NR 2 ENGINE, TURNED ON NR 2 BLEED, GOT HAZE IN COCKPIT AND CABIN. SMELLED LIKE DIRTY GYM SOCKS. REMOVED, CLEANED AND REINSTALLED NR 2 ENGINE P2.5/P3.0 AIR PRESSURE SWITCHING VALVE. NO DEFECT FOUND. REPLACED DAMAGED O-RINGS ON NLSDR P5CA0501382Controller · malfunctionedSTATUS MESSAGE NR 3 ENG PRV / OVHT. (RETURN TO BLOCK) DEFERRED PER MEL 36-11-8C.SDR DLM88050400Boot · failedTAIL COMPT HIGH TEMP MSG ON CLIMB-OUT. REPLACED FAILED BOOT ON MIX MANIFOLD.SDR MZZA0500003Actuator · leakingA FUEL ODOR WAS NOTICED THOUGHOUT THE CABIN DURING LANDING AT GUM. THE FIRE TRUCKS WERE REQUESTED. MX FOUND NR 1 ENGINE VSV ACTUATOR LEAKING AT ENGINE VENT. THE NR 1 ENGINE RT VSV ACTUATOR WAS REMOVED AND REPLACED IAW MM. NR 1 ENGINE WAS RUN, OPS AND LEAKED CHSDR 2005FA0001090Pump · vibratesPILOT REPORTED WHINING NOISE COMING FROM ENGINE AND FELT A VIBRATION COMING THROUGH THE MIXTURE CONTROL CABLE. TROUBLESHOOTING, THE MECHANIC FOUND THE AIR PUMP WAS VIBRATING. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. (K)SDR RAIA00507013Duct · leakingFLT 3524 - STL - BLEED 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED BLEED HOSE DUCT.SDR ASMF200507015Thermostat · failedTHE AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HERMOSILLO (HMO) DUE TO LEFT ICE PROTECT TEMP HIGHT LIGHT TURNED ON AND USTB LEGEND IN RADAR COME ON SEVERAL TIMES. THE LEFT PNEUMATIC SYSTEM THERMOSTAT AND ANTICIPATOR WERE REPLACED IAW MM 36-10-06 AND TRANSCEISDR QXEA200501113Valve · malfunctionedDEN - FLIGHT NR 4327 ITT 840 C. - MAINTENANCE REPLACED NR 1 ENGINE HIGH PRESSURE SHUTOFF VALVE. OPERATION CHECK GOOD AIRCRAFT RETURNED TO SERVICE.SDR GTIA050214Sensor · cloggedUPON CLIMB-OUT, "TAIL COMPT TEMP HI" LIGHT ILLUMINATED, AIR RETURN BACK TO ACY. ENGINE GROUND POWER RUN PERFORMED, LEFT AND RIGHT PACKS OPERATED. NO DUCT LEAKS FOUND, RAN PACKS OFF OF AP. NO LEAKS FOUND. FOUND VENTURI SENSOR CLOGGED WITH DEBRIS, OIL SUBSTASDR DL75K050363Coupling · leakingL BLEED DUCT LK EICAS MSG AND OVERHEAD DUCT LEAK LIGHT ON LEFT SIDE ILLUMINATED AFTER T/O. FOUND BUSTED CLAMP ON DUCT LEADING TO LT WING A/I VALVE ON TOP OF LT PYLON. INSTALLED CLAMP AND SEAL ON WING A/I DUCT AND LEAK CHECKED PER M/M. LEAK CHECKS GOOD. AIRSDR RAIA00507005O-Ring · leakingFLT 3505 - PIT - BLEED 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED O-RINGS AT LOCATIONS NR 5, 11, AND 17.SDR 05FDEA01750Warning Light · illuminatedBLEED AIR NR 1 FAULT WITH ANTI-ICE SELECTED AFTER SELECTING WITH ANTI ICE THEN BOTH PACKS WOULD FAULT AND NOT RESET COULD NOT MAINTAIN CABIN PRESSURE WITH APU BLEED NR 2 BLEED WAS DEFERRED NR 1 ENGINE BLEED WOULD NOT RESET. UNSCHEDULED LANDING T/S PER A310 TSMSDR RAIA00506035Filter · dirtyFLT 7954- TYS- BLEED NR 2 OVERTEMP. MAINTENANCE CLEANED THE FAN AIR VALVE FILTER. OPS CHECKED GOOD.SDR P5CA0501367Valve · stuckON TAKEOFF NR 1 ENGINE A-FIRE LOOP WENT TO 4.0. B-FIRE LOOP WENT TO 5.0 AND STAYED THERE UNTIL THROTTLES WERE RETARDED FOR DESCENT. FOUND NR 1 ENGINE HIGH STAGE VALVE STUCK OPEN, LOCKED CLOSED, OPENED MEL 36-01-3B.SDR 2005UALA00577Line · leakingLEFT WING BLEED LEAK. LEFT WING BLEED LEAK IN CRUISE. FLIGHT RETURNING TO DEN DUE TO ICING AND WX. FOUND VERY LARGE LEAK ON THE RT PACK OZONE CONVERTER AFT CLAMP, REMOVED CLAMP RE-ADJUSTED SEAL AND SECURED CLAMP, LEAK WAS BLOWING AT OVERHEAT LOOP ON KEELBEAMSDR 2005FA0000926Pump · weakPILOT REPORTED LOW INSTRUMENT AIR PRESSURE AT 1000 RPM. TROUBLESHOOTING SYSTEM FOUND TO BE OK, DETERMINED AIR PUMP WAS NOT PUTTING OUT SUFFICIENT PRESSURE. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. (K)SDR GTIA050165Augment Valve · stuckNR 1 ENGINE AUGMENTATION VALVE APPEARS TO STICK OPEN AT HIGHER POWER SETTINGS, AIRCRAFT TAIL SWAP WITH N821NK. FOUND LINE BEHIND AUG VALVE ON DUCT TO PNEUMATIC PRESSURE REGULATOR LOOSE, FOUND CRUSH GASKET WORN. REPLACED GASKET AND SECURED LINE. ENGINE RUN ASDR 2005UALA00541Clamp · failedNR 2 ENGINE BLEED FAULT. RIGHT WING BLEED LEAK DISPLAYED AFTER TAKEOFF. FOUND LEAK ABOVE NR 2 ENG PYLON AT DUCT CLAMP (REF IPC 36-11-05 FIG 02 ITEM 20). REPLACED CLAMP. LEAK WAS 2 INCHES IN FRONT OF RT WING LOOP -A- ELEMENTS 43HF AND 44HF.SDR P5CA0501377Clamp · failedCREW REPORTED NR 1 ENGINE FIRE WARNING SOUNDED ON DESCENT. CLOSED THRUST AND START LEVER, LIGHT WENT OUT. FIRE HANDLE WAS NOT PULLED. REPLACED CLAMP TO HIGH STAGE VALVE, MM 36-13-00. OPS AND LEAK CHECK OK MM 71-00-00.SDR P5CA0501362Clamp · failedNR 1 ENGINE FIRE WARNING SOUNDED ON DESCENT. CLOSED THRUST AND START LEVER, LIGHT WENT OUT. FIRE HANDLE WAS NOT PULLED. REPLACED CLAMP TO HIGH STAGE VALVE. OPS AND LEAK CHECK OK PER MM 36-13-00 AND 71-00-00.SDR AWXA200500648Controller · malfunctionedON CLIMB-OUT, BOTH NR 1 AND NR 2 ENGINE BLEED AIR FAULTS OCCURRED. TURNED BACK AND LANDED WITHOUT FURTHER DIFFICULTY. MX R & R NR 1 BMC IAW AIRBUS MM 36-11-34. ALSO REPLACED FAN AIR VALVE CONTROL THERMOSTATS ON BOTH NR 1 AND NR 2 ENGINES IAW AIRBUS MM 36-11SDR GTIA050158Seal · leakingTAIL COMPARTMENT TEMP HIGH LIGHT CAME ON AFTER TAKEOFF, AIR RETURN BACK TO FLL AND AIRCRAFT TAIL SWAP WITH N815NK. REMOVED AND REPLACED SEALS ON LEFT AND RIGHT ACM DUCTS, SECURED TWO LOOSE CLAMPS, RAN ENGINES AT ALL PARAMETERS. OPS AND LEAK CHECKS GOOD. (M)SDR A6WA200540173Shutoff Valve · faultyL-PACK HIGH PRESS WHINE, XFERRED TO ENGINE BLEED. WHEN DUCT PRESS 60 PSI OR GREATER. REMOVED AND REPLACED L-PRSOV IAW AMM 2-151-43. FUNCTIONAL TEST OF PRSOV GOOD IAW AMM 21-51-43. (M)SDR DL738050271Pneumatic System · contaminatedABORTED T/O FOR SMOKE IN COCKPIT AND CABIN. PERFORMED OIL CONTAMINATION REMOVAL FROM AIR COND AND PNUEM SYS. NO SMELL OF CONTAMINATION NOTED. RAN PACKS AND ENGS TO T/O. NO SMOKE NOTED.SDR DL767050267Shutoff Valve · sticksWHEN POWER INITIALLY REDUCED TO START INITIAL DESCENT A SMELL DEVELOPED IN THE AIRCRAFT. REPLACED NR 1 HPSOV.
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