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.

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)Mar 7, 2003 · N5115 · Cessna 750SDR 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)Mar 6, 2003 · N521AT · Boeing 75728ASDR 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.Mar 4, 2003 · N196DN · Boeing 767332SDR 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 TEMPERATUREMar 2, 2003 · N660AM · Boeing 757223SDR 2003UALA00229Duct · damagedLEFT WING LEAK ECAM DISPLAYED. FOUND LEFT HAND CROSSBLEED DUCT DAMAGED AT HIGH PRESSURE GROUND CONNECTION. REPLACED DUCT.Feb 28, 2003 · N415UA · Airbus A320232SDR GLBA2003025Tube · disconnectedRIGHT BLEED AIR FAIL. RECONNECTED EVA TUBING ON LT INBOARD WING, OPS CHECK GOOD.Feb 27, 2003 · N204GL · Beech 1900DSDR 2003UALA00200Shutoff Valve · failedNR 2 BLEED EICAS CAME ON DURING TAKEOFF. FLIGHT CONTINUED TO CRUISE, THE HIGH PRESSURE SHUTOFF VALVE WAS DEFECTIVE. REPLACED VALVE.Feb 24, 2003 · N176UA · Boeing 747422SDR 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.Feb 16, 2003 · N522UA · Boeing 757222SDR 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 REPLAFeb 12, 2003 · N7638U · Boeing 727222SDR 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 Feb 6, 2003 · N522XJ · Bac AVRO146RJ85ASDR 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 WAFeb 3, 2003 · N352WL · Doug DC1030SDR RAIA00302037O-Ring · leakingPIT- LT BLEED LEAK WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED O-RING AT LT BLEED LINE COUPLING.Feb 3, 2003 · N809HK · Emb EMB145SDR DEL2003F00000Periseal · leakingLEAKING PERI SEALS (2 EA) IN THE BLEED AIR LINES IN THE LEFT PYLON, CAUSED THE FIRE DETECTION SYSTEM TO ILLUMINATE.Feb 2, 2003 · N273MG · Lear 55LEARSDR 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 AIRCRJan 21, 2003 · N920DC · Gulstm GULFSTREAMGVSDR 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 RJan 18, 2003 · N804MA · Boeing 727225SDR 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 MINJan 18, 2003 · N257FE · Boeing 727200SDR DL78K030072Thermostat · leakingON TAKEOFF RIGHT DUCT PRESSURE DROPS TO 10 PSI. REPLACED 450 DEGREE THERMOSTAT.Jan 17, 2003 · N3735D · Boeing 737832SDR 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 VANEJan 15, 2003 · N8173C · Beech F33ASDR 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 VANEJan 14, 2003 · N5540P · Beech F33ASDR 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.Jan 12, 2003 · N589UA · Boeing 757222SDR 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)Jan 5, 2003 · N972AS · Doug DC983SDR COMA0360006CouplingFLIGHT 5239 LEFT 14TH STAGE BLEED AIR DUCT WARNING.TIGHTENED LOOSE BLEED AIR COUPLING AT THE T/R PDUJan 4, 2003 · N712CA · Cndair CL6002B19SDR 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.Jan 3, 2003 · N14940 · Emb EMB145ERSDR 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 VANEDec 31, 2002 · N5530A · Beech F33ASDR 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.Dec 23, 2002 · N103DA · Boeing 767232SDR 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 INCDec 13, 2002 · N414TE · Raythn 390SDR 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.Dec 12, 2002 · N5582X · Beech F33ASDR BAQA081603Shutoff Valve · intermittentSHUTOFF VALVE INTERMITTENT. REPLACED WITH SERVICEABLE UNIT.Dec 9, 2002 · N9024Z · Bolkms BK117A4SDR 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 Dec 7, 2002 · N508MC · Boeing 747230BSDR GLBA2002193Splice · damagedLEFT BLEED AIR FAIL ANNUCIATOR ILLUMINATED, REPAIRED EVA TUBE SPLICEDec 6, 2002 · N261GL · Beech 1900DSDR 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 Dec 5, 2002 · N860DA · Boeing 777232SDR 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.Dec 3, 2002 · N244WA · Boeing 737247SDR 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.Nov 27, 2002 · N1565A · Beech F33ASDR 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.Nov 25, 2002 · N8251C · Beech F33ASDR 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. Nov 21, 2002 · N354MC · Boeing 747300SDR 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.Nov 19, 2002 · N131UP · Airbus A300F4622RSDR 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 Nov 16, 2002 · N615AE · Emb EMB145LRSDR 2002F01060Valve · inoperativeDURING CRUISE, RT ENGINE BLEED OFF DISPLAYED. MAINTENANCE REMOVED AND REPLACED FAN AIR MODULATING VALVE IAW MM 36-11-16. OPERATIONAL CHECKS NORMAL.Nov 13, 2002 · N515AT · Boeing 75723NSDR 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. INSPECTNov 12, 2002 · N6810 · Boeing 727223SDR 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.Nov 12, 2002 · N435UA · Airbus A320232SDR RAIA00211314Gasket · leaking5538-STL- RIGHT ENGINE DID NOT MAKE TORQUE, MAINTENANCE REMOVED AND REPLACED A GASKET IN THE HP BLEED LINE, OPS CK OK.Nov 8, 2002 · N570HK · Jetair JETSTM4101SDR 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 TIGHNov 7, 2002 · N620AE · Emb EMB145LRSDR 000222Clamp · looseBLEED 2 LEAK TIGHTENED BOTH U CLAMPS AT THE LINE AND REPLACED BOTH UPPER AND LOWER BLEED O'RINGS IN CARGO COMPTNov 5, 2002 · N260 · Emb EMB145SDR 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 SNov 4, 2002 · N7520A · Doug DC982SDR 000221Warning System · false indicationBLEED 2 LEAK. PERFORMED GROUND RUN FOR BLEED LEAKS NO LOCK NOTED AND NO EICAS MSG FOR BLEED LEAK NOTED,Nov 4, 2002 · N260 · Emb EMB145SDR 000220Warning System · false indicationBLEED 2 LEAK. PERFORMED GROUND RUN FOR BLEED LEAKS NO LOCK NOTED AND NO EICAS MSG FOR BLEED LEAK NOTEDNov 4, 2002 · N260 · Emb EMB145SDR 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 DISCNov 2, 2002 · N127NK · Doug DC921SDR 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. MAINTENNov 2, 2002 · N127NK · Doug DC921SDR 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 36-11Oct 31, 2002 · N8887Z · Boeing 727225SDR 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)Oct 30, 2002 · N8887Z · Boeing 727225
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