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 2003F00232Regulator Valve · malfunctionedON APPLICATION OF TAKEOFF POWER, AMBER EICAS MESSAGE 'HP DUCT 'O' PRESS R' CAME ON. ABORTED TAKEOFF. RIGHT HIGH PRESSURE REGULATING VALVE FAILED TO REGULATE PROPER BLEED AIR PRESSURE. REPLACED RIGHT HP BLEED AIR REGULATOR VALVE. OPERATION NORMAL. (M)SDR AMTA200300317Duct · damagedEICAS STATUS MESSAGE RIGHT STRUT O/H DET 1 DISPLAYED. REMOVED AND REPLACED RIGHT ENGINE SUPPLY HIGH PRESSURE DUCT IAW MM 36-11-01. OPS CHECK NORMAL. (M)SDR DL76L030217Controller · failedRIGHT PRV INOPERATIVE. SWAPPED HPSOV AND PRV. AFTER TAKEOFF RIGHT ENG BLEED FAILED. DUE TO FORECAST WEATHER IN JFK DECISION WAS MADE TO DIVERT TO FRA. FOUND PRV CONTROLLER AT FAULT. REPLACED PRV CONTROLLER, OPS CHECK ON R/U OK.SDR AALA20030264Clamp · looseCCS - FLT 2140 - EN ROUTE CCS-MIA, RIGHT ENGINE FIRE WARNING/OVERHEAT LIGHT ILLUMINATED. RETARDED THROTTLE LIGHT EXTINGUISHED AFTER A FEW MINUTES. ADVANCED THROTTLE AGAIN OVERHEAT LIGHT ILLUMINATED. SHUTDOWN RIGHT ENGINE AS A PRECAUTION, NO OVER TEMPERATURESDR 2003UALA00229Duct · damagedLEFT WING LEAK ECAM DISPLAYED. FOUND LEFT HAND CROSSBLEED DUCT DAMAGED AT HIGH PRESSURE GROUND CONNECTION. REPLACED DUCT.SDR GLBA2003025Tube · disconnectedRIGHT BLEED AIR FAIL. RECONNECTED EVA TUBING ON LT INBOARD WING, OPS CHECK GOOD.SDR 2003UALA00200Shutoff Valve · failedNR 2 BLEED EICAS CAME ON DURING TAKEOFF. FLIGHT CONTINUED TO CRUISE, THE HIGH PRESSURE SHUTOFF VALVE WAS DEFECTIVE. REPLACED VALVE.SDR 2003UALA00180Controller · failedRT ENGINE HIGH STAGE LIGHT ON DURING TAKE OFF ROLL. SUPPLEMENTAL DATA UPDATE ROOT CAUSE: HIGH STAGE CONTROLLER OVER PRESSURE SENSOR & ANTI-ICE SWITCHER CALIBRATION WAS OUT. REPLACED CONTROLLER.SDR 2003F00244Manifold · crackedDURING CLIMB-OUT AT KANSAS CITY, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED AND HORN SOUNDED. EMERGENCY CHECKLIST FOLLOWED. ENGINE WAS SHUTDOWN AND NR 1 FIRE BOTTLE DISCHARGED. AIRCRAFT RETURNED TO KANSAS CITY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLASDR MALA030151Sensor · malfunctionedON TAKEOFF OF FLIGHT 3649, INTAKE LO PRESS ILLUMINATED COULD NOT RESET IN CLIMB AFTER POWER REDUCTION LIGHT WENT OUT, ON AGAIN WITH POWER INCREASE. ON DESCENT WITH WING AND TAIL ICE ENGINE NR 1 AIR FAULT AND AIR LO TEMP ILLUMINATED WITH N2 LESS THAN 88. AIR SDR WRLA200228Valve · failedNR 1 PNEUMATIC TEMP HIGH LIGHT. PNEUMATIC TEMP EXCEEDED RED LINE. PNEUMATIC TEMP CONTINUED TO RISE TOWARD RED LINE. DUMPED 40,000 LBS OF FUEL TO REACH MAXIMUM LANDING WEIGHT. RETURNED TO DEPARTURE STATION FOR REPAIRS, NR 3 SYSTEM PNEUMATIC FAN AIR VALVE WASDR RAIA00302037O-Ring · leakingPIT- LT BLEED LEAK WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED O-RING AT LT BLEED LINE COUPLING.SDR DEL2003F00000Periseal · leakingLEAKING PERI SEALS (2 EA) IN THE BLEED AIR LINES IN THE LEFT PYLON, CAUSED THE FIRE DETECTION SYSTEM TO ILLUMINATE.SDR 2003F00351Line · crackedWHILE PERFORMING THE ELEVATOR HARD OVER PROTECTION TEST, FOUND THE ELEVATOR DISCONNECT HANDLE GUIDE FOR THE PNEUMATIC ASSIST TO BE CRACKED. THE ELEVATOR DISCONNECT HANDLE ASSY WAS REPLACED, APPROPRIATE OPERATIONAL CHECKS PERFORMED PER THE G-V MM AND THE AIRCRSDR MYW2003F00001Regulator Valve · inoperativeON DEPARTURE, NR 1 ENGINE SUPPLY PRESSURE (DUCT PRESSURE) REACHED 95 PSI FOLLOWED BY STRUT OVERHEAT AND PACK TRIP. RETURN AIRCRAFT. AIRCRAFT PREPED FOR TWO ENGINE FERR. ACCOMPLISHED TWO ENGINE FERRY TO MIA IAW MM. REMOVED AND REPLACED 13 STAGE MODULATING RSDR 03FDEA00053Duct · blownDURING CLIMBOUT WITH STANDARD TAKEOFF POWER SET, NR 1 ENGINE FIRELIGHT ILLUMINATED WITH HORN ON. SHUT DOWN ENGINE IAW WITH CHECKLIST. REMOVED AND REPLACED MAIN OIL STRAINER DUE TO INFLIGHT SHUT DOWN OF NR 1 ENGINE. ENGINE WINDMILLED FOR APPROXIMATELY 10 MINSDR DL78K030072Thermostat · leakingON TAKEOFF RIGHT DUCT PRESSURE DROPS TO 10 PSI. REPLACED 450 DEGREE THERMOSTAT.SDR VJ32003F00019Pump · failedDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHTER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERLY. BELIEVE DRY AIR PUMP VANESDR VJ32003F00020Pump · wornDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHTER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERLY. BELIEVE DRY AIR PUMP VANESDR 2003UALA00046Controller · failedLEFT ENGINE BLEED PRESSURE REGULATING AND SHUTOFF VALVE FAILURE PRIOR TO ENTERING ETOPS ENVIRONMENT. SUPPLEMENTAL DATA UPDATE HIGH STAGE PILOT CONTROLLER FAILED. REPLACED HIGH STAGE PILOT CONTROLLER.SDR ASAA0380054Support · crackedOKC - FOUND DURING 30K CHECK, PNEUMATIC DUCT ANGLE SUPPORT CRACKED AT AFT END OF WHEELWELL IN KEEL BEAM. REPLACED ANGLE PER SRM 51-10-2 AND 51-10-4. (M)SDR COMA0360006CouplingFLIGHT 5239 LEFT 14TH STAGE BLEED AIR DUCT WARNING.TIGHTENED LOOSE BLEED AIR COUPLING AT THE T/R PDUSDR C2XA03CL002Tube · leakingCLE FLIGHT 3091 THE CREW REPORTED BLEED 1 LEAK INDICATION ON EICAS,THEN RETURNED TO CLE .AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PYLON BLEED TUBE ASSEMBLY AND IT LEAK CHECKED GOOD.SDR VJ32003F00000Pump · failedDURING GROUND RUN UP, OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHT RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERTY. BELIEVE DRY AIR PUMP VANESDR DL767021462Coupling · leakingLEFT DUCT LEAK ON CLIMBOUT. RESEALED COUPLING ON BODY CROSSOVER DUCT IN LEFT AC BAY. RAN TO TAKEOFF POWER PER PFHB. OK FOR SERVICE.SDR MGO2002F00000Line · splitPNEUMATIC LINE PROVIDES FOR A MOISTURE DRAIN POINT FOR THE PNEUMATIC MANIFOLD WHICH PROVIDES REGULATED AIR PRESSURE TO THE HYDRAULIC PACKAGE THE PRIMARY OUTFLOW VALVE, THE COCKPIT ALTERNATE AIR VALVE AND PASSENGER DOOR SEAL. LINE IS BULGED AND SPLIT 1.250 INCSDR VJ32003F00013Pump · failedDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM.SDR BAQA081603Shutoff Valve · intermittentSHUTOFF VALVE INTERMITTENT. REPLACED WITH SERVICEABLE UNIT.SDR UIEA200200066Duct · rupturedJFK-ORD - AIR TURNBACK, AT 10,000 FEET WITH CRUISE POWER, LOUD BANG AND BUMP. NR 1 ENGINE EGT CLIMBED TO 850 DEGREES AND NACELLE TEMPS TO 4.5 BLEED VALVE CLOSED. EGT CONTINUED ABOUT 100 DEGREES ABOVE OTHER ENGINES. SAW T/R BLOW-OUT PANEL OPEN. RETURNED TO SDR GLBA2002193Splice · damagedLEFT BLEED AIR FAIL ANNUCIATOR ILLUMINATED, REPAIRED EVA TUBE SPLICESDR DL777021411Valve · inoperativeLEFT ENG BLEED INOP. R/R LEFT ENG PRSOV PER M/M AND RAN ENG CHECK GOOD PER M/M 36-10-00-5 SDR DL73K021406Regulator Valve · leakingAIR TURNBACK FROM FLL TO BDL, RETURNED TO FLL. BLEED TRIP OFF NR 1 ENG ON TAKEOFF ROLL. REPLACED PRESSURE REGULATOR BLEED LINES FOR LEAKING.SDR VJ32003F00017Pump · failedDURING GROUND RUN UP, OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM.SDR VJ32003F00015Pump · failedDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM.SDR P5CA0200709Duct · separatedNR 4 ENG - FIRE INDICATION AFTER TAKEOFF IN CLIMB. PRECAUTIONARY ENGINE SHUTDOWN & FUEL DUMP PERFORMED. FIRE BOTTLE NOT REQUIRED. FOUND 8TH STAGE BLEED CROSSOVER DUCT SEPARATED FROM DUCTING SYSTEM. REPLACED WITH CROSSOVER DUCT & PRECOOLER DOWNSTREAM DUCT. SDR UPS02139922Sensor · inoperativeLT HYD PUMP FAILED. NR 1 HIGH PRESS BLEED VALVE LIGHT ILLUMINATED. EMERGENCY DECLARED. *SUPPLEMENTAL* REACTIVATED SYSTEM PER DMP 36-11-03. REPLACED HP SENSOR 47HA PER AMM 36-11-23. BITE TESTED PER AMM 36-11-00, CHECKS GOOD.SDR SIMA200232401Clamp · looseFWA - FLT 4173 - DURING CRUISE FLIGHT, CREW REPORTED A 'BLEED NUMBER 1 LEAK' MESSAGE ON EICAS. CREW DIVERTED TO FWA DUE TO NO CABIN/COCKPIT HEAT AND WEATHER AT DESTINATION. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND AND TIGHTENED SOME LOOSE CLAMPS IN THE SDR 2002F01060Valve · inoperativeDURING CRUISE, RT ENGINE BLEED OFF DISPLAYED. MAINTENANCE REMOVED AND REPLACED FAN AIR MODULATING VALVE IAW MM 36-11-16. OPERATIONAL CHECKS NORMAL.SDR GAIAOP156Clamp · looseFLIGHT 1111 - LAX-STL - AFTER TAKEOFF, WHILE AT CLIMB POWER THE FLIGHT CREW NOTICED THAT THE AFT BODY OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED AOM PROCEDURE AND THE LIGHT EXTINGUISHED. THE AIRCRAFT DIVERTED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. INSPECTSDR 2002UALA01718Duct · leakingFLIGHT DIVERTED DUE TO A LEFT WING BLEED MESSAGE. FOUND SOURCE OF LEAK AT HIGH PRESSURE GROUND AIR CONNECTION DUCT/CLAMP. REPLACED DUCT AND CLAMPS.SDR RAIA00211314Gasket · leaking5538-STL- RIGHT ENGINE DID NOT MAKE TORQUE, MAINTENANCE REMOVED AND REPLACED A GASKET IN THE HP BLEED LINE, OPS CK OK.SDR SIMA200231503Clamp · looseORF - FLT 4025 - CREW REPORTED A BLEED LEAK MESSAGE ON EICAS DURING CRUISE FLIGHT. CAPTAIN DECLARED AN EMERGENCY AND CONTINUED TO ORF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A LOOSE V-BAND CLAMP IN THE AFT AVIONICS COMPARTMENT. CLAMP WAS TIGHSDR 000222Clamp · looseBLEED 2 LEAK TIGHTENED BOTH U CLAMPS AT THE LINE AND REPLACED BOTH UPPER AND LOWER BLEED O'RINGS IN CARGO COMPTSDR AALA20021621Duct · damagedSLC - FLT 360 - EN ROUTE SLC-DFW, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED SOON AFTER TAKEOFF ROTATION. ANTI-ICE NOT ON. CLOSED CROSSFEED AND SE PACK TO HIGH PRESSURE BLEED OFF, BUT LIGHT REMAINED ILLUMINATED. FLIGHT ATTENDANTS REPORTED BURNING SSDR 000221Warning System · false indicationBLEED 2 LEAK. PERFORMED GROUND RUN FOR BLEED LEAKS NO LOCK NOTED AND NO EICAS MSG FOR BLEED LEAK NOTED,SDR 000220Warning System · false indicationBLEED 2 LEAK. PERFORMED GROUND RUN FOR BLEED LEAKS NO LOCK NOTED AND NO EICAS MSG FOR BLEED LEAK NOTEDSDR WX0A02009ADuct · rupturedLAS - TAIL COMPARTMENT HIGH TEMP ANNUNCIATOR INDICATION ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED TAIL COMPARTMENT AND ASSOCIATED PRESSURIZATION DISTRIBUTION SYSTEM FOR CAUSE OF HIGH TEMP INDICATION. MX DISCSDR WXOA02009Duct · rupturedLAS - TAIL COMPARTMENT HIGH TEMP ANNUNCIATOR INDICATION ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED TAIL COMPARTMENT AND ASSOCIATED PRESSURIZATION DISTRIBUTION SYSTEM FOR CAUSE OF HIGH TEMP INDICATION. MAINTENSDR C7WA200200039Duct · looseNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON TAKEOFF WHILE CLIMBING 200 FEET. EPRS 2.08/2.11. THROTTLES BACKED OFF TO 1.7 EPR LIGHT EXTINGUISHED. TROUBLESHOOTING FOUND DUCT CONNECTION TO NR 3 ENGINE PRECOOLER LOOSE. TIGHTENED, NO FURTHER LEAKS, MM 36-11SDR C7WA200200037Clamp · looseNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON TAKEOFF, EPRS 2.01/2.03 WHEN THROTTLES BACKED OFF TO 1.7 EPR LIGHT EXTINGUISHED. TIGHTENED LOOSE CLAMP IN STRUT AREA PER MM 75-00 AND 20-80-1. (M)
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