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 AALA20060119Valve · inoperativeLHR - RIGHT ENGINE HIGH PRESSURE SHUT OFF VALVE MESSAGE WITH ASSOCIATED OVERHEAD PANEL LIGHT. FOUND BROKEN WIRE ON RIGHT HAND HIGH PRESSURE SHUT OFF VALVE. REPAIRED WIRE, SYSTEM GROUND CHECKED NORMAL OPERATION.Feb 25, 2006 · N194AA · Boeing 757223SDR DXTA200601258Control Valve · failedSHORTLY AFTER SELECTING BLEED AIR ON THE FLOW OF BLEED AIR TO THE COCKPIT WAS ABNORMALLY HIGH FOLLOWED BY ILLUMINATION OF THE AIR DUCT O'HEAT, CKPT ANNUNCIATOR AND THE COCKPIT BEGAN TO FILL WITH SMOKE. ABNORMAL CHECKLIST COMPLETED. REPLACED ECU TEMP CONTROL Feb 22, 2006 · N625QS · Cessna 560XLSDR 06FDEA0721Duct · failedPASSING FL 220 PILOTS BOTH HEARD A LOUD BANG UNDERNEATH OUR SEATS. PRESSURIZATION WENT ERRATIC FOR ABOUT 10 SECONDS, SHORTLY FOLLOWED BY A LEVEL 2 AIR SYS 1-2 OFF LIGHT. FOLLOWED QRH, ISOLATED NR 1 MANIFOLD WHICH SUSPECT WAS THE PROBLEM. DIVERTED TO ATL. Feb 17, 2006 · N388FE · Doug MD1010FSDR 06FDEA0719Warning Light · unknownAPPROACHING LEVEL AT F330 ENTERED ICING CONDITION, TURNED ON ALL ANTI-ICE AND GOT THE FOLLOWING ALERTS, LEVEL TWO BLEED AIR 2 FAULT LEVEL ONE BLEED AIR 1 OFF", PACK 1 OFF", PACK 3 OFF "AVIONICS FAN OVRD", "BLEED AIR 3 OFF. SYNOPTIC CONFIRMED ONLY NR 2 SYSTFeb 17, 2006 · N624FE · Doug MD11SDR AMTA200600139Line · looseRT DUCT PRESSURE DROPS FROM 35 PSI TO 15 PSI SERVER AT TIMES IN FLIGHT. FOUND LOOSE SENSE AIR LINE ON BLEED AIR REGULATOR. TIGHTENED LINE. PERFORMED FIM 36-10-00 810-807 OPS CHECK NORMAL. RAN ENG AT 80 PERCENT FOR 5 MINUTES, NO FLUCTUATIONS. (K)Feb 13, 2006 · N318TZ · Boeing 73783NSDR 2006UALA00280Precooler · damagedRIGHT ENGINE PNEUMATIC STRUT PRECOOLER HAS A 5 INCH BY 1-4 INCH GAP AT BOTTOM LEFT SIDE. REPLACED RIGHT ENGINE PRECOOLER. OP CHECKS OK. THE DAMAGE FOUND WAS TYPICAL FOR THIS UNIT. THE CYCLING OF THE HPSOV AND THE ASSOCIATED PRESSURE SPIKES CAUSE FATIGUE CRFeb 12, 2006 · N796UA · Boeing 777222SDR DL777060120Valve · leakingAFTER T/O, LEFT ENG BLEED OFF EICAS MESSAGE. A/C RETURN TO ATL. MTC REPLACED HPSOV AND PNEU PRESSURE LINE FROM BRACKET DISCO, HPSOV NEED LEAK CHECK AND OP CHECK. PERFORMED LEAK CHECK, ENGINE AIR SUPPLY OP TEST PER MM 36-10-00-700-801. FOUND PNEUMATIC LINE Feb 11, 2006 · N865DA · Boeing 777232SDR EIA2006023Controller · malfunctionedPRESSURE RELIEF VALVE OPENS IN FLIGHT. UNABLE TO CONTROL OVER PRESSURE CONDITION RESULTING IN AN AIR TURN BACK. PRELIMINARY REVIEW ON GROUND REVEALED NO FINDINGS SO FAR. REPLACED AUTO PRESS CONTROLLER PER MM 21-31-02, OPS CHK OK, PITOT STATIC TEST C/W PER 3Feb 10, 2006 · N477EV · Boeing 747SR46SDR DJFA2006194Coupling · leakingCREW REPORTED THAT ON CLIMBOUT AT APPROX 23,500 FT THE BLEED AIR DUCT FAIL ANNUNCIATOR ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO KPBI AFTER THE CREW TRIED UNSUCCESSFULLY TO GET THE LIGHT TO EXTINGUISH. AN UNEVENTFUL LANDING WAS COMPLETED IN KPBI. MAINTENANCFeb 10, 2006 · N743TA · Beech 400ASDR PCSA02090603Thermal Switch · intermittentCREW PREPARED FOR TAKEOFF, CREW REPORTED NR 1 ENGINE BLEED TRIPPED WHEN TAKEOFF POWER SET. AIRCRAFT RETURNED TO BLOCK WITHOUT INCIDENT. MX TROUBLESHOT & ACCOMPLISHED OPERATIONAL CHECKS OF THE BLEED SYSTEM AND COULD NOT DUPLICATE THE PROBLEM, THE AMERIJET FLIFeb 9, 2006 · N495AJ · Boeing 727233SDR MALA060053Heater · failedFLIGHT RETURNED TO MSP DUE TO STATIC AIR TEMP SAT PROBE HEATER FAULT AND ENROUTE ICING CONDITIONS. NO FURTHER INFORMATION AT THIS TIME.Feb 7, 2006 · N442XJ · Saab 340BSDR DLM8K060103Duct · crackedDURING CLIMBOUT AT 22K FT A TAIL COMPT TEMP HIGH MSG ILLUM. RAN PROCEDURE VIA THE QRH AND LIGHT EXTINGUISHED WHEN HP BLEED OFF. DISPATCH RECOMMEND DIVERT TO ATL DUE TO ICING IN NY AREA. FOUND RT SPIDER DUCT CRACKED. DUCT REPLACED, LEAK CHECK OK.Feb 4, 2006 · N914DE · Doug MD88SDR NACA20060006Duct · crackedNR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, RETURN TO ANCHORAGE. REPLACED CRACKED 13TH STAGE BLEED DUCT IN THE NR 1 ENGINE PYLON. REF BMM 36-00-1 PG 201.Jan 25, 2006 · N792A · Boeing 72722CSDR COMA0560826Warning System · malfunctionedFLIGHT 5846 - ANTI-ICE DUCT WARNING. OPERATIONAL CHECKS OF ANTI-ICE AND LEAK DETECTION SYSTEM WERE NORMAL.Jan 23, 2006 · N914CA · Cndair CL6002B19SDR 2006FA0000104Coupling · failedWITH APU RUNNING AND BLEED AIR SELECTED ON, COUPLING FAILED CAUSING DUCT TO SEPARATE. PROBABLE CAUSE UNKNOWN. SUGGEST MORE AGGRESSIVE LOCKING MECHANISM. (K)Jan 21, 2006 · N327TL · Gulstm GIVSDR 2006FA0000136Line · chafedDURING A ENGINE CHANGE A PYLON INSPECTION WAS BEING PERFORMED. SPIRAL WRAP WAS NOTICED WORN. FURTHER INVESTIGATION REVEALED CHAFF ON HIGH TEMPERATURE BLEED AIR LINE MORE THAN 50 PERCENT THROUGH. (K)Jan 20, 2006 · N780E · Gulstm GIVSDR MASA200600076Element · malfunctionedASH 6112 PHX - DECLARED AN EMERGENCY DUE TO THE LEFT 14TH STAGE DUCT WARNING. CREW SHUTDOWN THE ENGINE. MAINTENANCE REMOVED AND REPLACED THE LT 14TH STAGE SENSE ELEMENTS.Jan 17, 2006 · N7305V · Cndair CL6002B19SDR RAIA00601016Seal · leakingFLT 5479-STL- BLEED NR 1 LEAK IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE BLEED DUCT SEALS.Jan 13, 2006 · N821HK · Emb EMB145SDR RAIA00601013O-Ring · leakingFLT 5488-STL- NR 1 BLEED LEAK. MAINTENANCE REMOVED AND REPLACED THE O-RINGS IN JOINT NR 14.Jan 10, 2006 · N821HK · Emb EMB145SDR RAIA00601012Check Valve · leakingFLT 5567-STL- BLEED 1 LEAK IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE CHECK VALVE AND SEALS FORWARD OF POSITION NR 2.Jan 10, 2006 · N821HK · Emb EMB145SDR RAIA00601008Seal · damagedFLT 5579 - STL - BLEED 2 LEAK DISPLAYED ON EICAS. MAINTENANCE SECURED A LOOSE DUCT AND REPLACED THE SEALS.Jan 5, 2006 · N821HK · Emb EMB145SDR JBGA200600001Control Unit · failedBOTH BLEED AIR WARNING LIGHTS CAME ON, UNABLE TO EXTINGUISH USING CHECK LIST. A/C WAS EN ROUTE TO SUN, DIVERTED TO BIL, LANDED SAFELY. AIRCRAFT WAS REPARED. REPLACED PN 310-32 SEALS AND PN 35009-20 CONTROL BOX.Jan 4, 2006 · N460AN · Lear 60LEARSDR CA060129015Line · fractured(CAN) FOLLOWING TAKEOFF, THE ENGINE FIRE WARNING ANNUNCIATED AND THE ENGINE WAS REPORTED TO BE (TRAILING SMOKE). THE ENGINE WAS SHUTDOWN IN FLIGHT, AN EMERGENCY DECLARED AND THE FLIGHT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED NO EVIDENSJan 3, 2006 · Braero BAE1251000SDR SWAA054136Shutoff Valve · faultyDIVERSION/INFLIGHT SHUTDOWN/DECLARED EMERGENCY, LT WING TO BODY OVERHEAT LIGHT ILLUMINATED. LT DUCT PRESSURE DID NOT DROP. SHUTDOWN NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE PRSOV, LOW STAGE REGULATOR AND ENGINE BLEED AIR SOLENOID PER MM.Dec 24, 2005 · N713SW · Boeing 7377H4SDR ASOA051136Clamp · looseDURING CLIMB OUT, THE CREW RECEIVED A LT JET OVERHEAT MESSAGE. THE CREW COMPLIED WITH THE QRH WHEN THEY RECEIVED A LT 10TH DUCT WARNING MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DEPARTURE, WHERE IT LANDED SAFDec 21, 2005 · N820AS · Cndair CL6002B19SDR 2006FA0000054Duct · crackedDURING SCHEDULED NR 2 ENGINE CHANGE INSPECTION NOTICED HP BLEED AIR DUCT WAS CRACKED AT CENTER BLEED AIR TAP. CRACK APPEARED TO ORIGINALS AT THE WELD AND PROGRESSED RADIALLY, APPROX 2.25 INCH TOWARDS THE BRAIDED FLEX COUPLING. NEW DUCT WAS ORDERED AND INSTALDec 15, 2005 · N39WP · Amd FALCON50MYSTSDR DL76L050793Controller · failedLEFT ENGINE PNEUMATIC SUPPLY PULSES TO 0 PSI ON THROTTLE RETARD THEN CATCHES UP. PRESSURIZATION OK BUT PULSES ALSO. REPLACED LT ENG HP S/O VLV PER MM. REPLACED HP CONTROLLER. NDS CK OUT. NO HELP. REPLACED LT ENG BLEED AIR CARD AND PRV CONTROLLER PER MM. Dec 15, 2005 · N181DN · Boeing 767332SDR AU510002220Valve · faultyNR 2 ENGINE BLEED SYSTEM FAN AIR VALVE SUSPECT FAULTY.Dec 12, 2005 · Airbus A320232SDR AU510002162Valve · faultyRT ENGINE PRESSURE REDUCING VALVE (PRV) SUSPECT FAULTY.Dec 12, 2005 · Boeing 767338SDR AU510002107Shutoff Valve · faultyRT BLEED AIR PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) FAULTY.Dec 12, 2005 · Fokker F28MK0100SDR AU510001910Pressure Valve · faulty(AUS) RT ENGINE BLEED AIR SYSTEM PRESSURE REGULATING VALVE (PRV) FAILED. INVESTIGATION FOUND EXCESSIVE BUTTERFLY SHAFT PLAY DUE TO WORN CARBON SHAFT BUSHINGS. (CASA NR 510001910)Dec 12, 2005 · Boeing 767338SDR F3LA200500047Controller · malfunctionedBLOCK TURNBACK. FLIGHT CREW REPORTED LOW PRESSURE BOTH ENGINES DURING START WITH FUMES INTO CABIN. REPLACED BMC NR1. LOW BLEED PRESSURE OPS CHECKED GOOD IAW AMM 36-11-34, PAGE 401. FOUND DE-ICE FLUID IN APU AIR INTAKE WHICH WAS CAUSING FUMES. CLEANED APU Dec 12, 2005 · N924FR · Airbus A319111SDR 200512101Bleed Valve · failedCREW REPORTED ENGINE 1 AND ENGINE 2 BLEED LEAK MESSAGE. VERIFIED THAT ENGINE BLEED VALVE FAILED OPEN DURING TAKEOFF.Dec 10, 2005 · N651RW · Emb ERJ170100SDR MASA200501009Control Panel · malfunctionedASH 6424 PHX - 10TH STAGE ISOLATION VALVE WOULD NOT CLOSE. MAINTENANCE REMOVED AND REPLACED BLEED CONTROL PANEL.Dec 8, 2005 · N77302 · Cndair CL6002B19SDR AU510001579Shutoff Valve · faulty(AUS) PNEUMATIC SYSTEM PRESSURE REGULATING SHUTOFF VALVE (PRSOV) FAULTY. (CASA NR 510001579)Dec 7, 2005 · Fokker F28MK0100SDR AU510001446Ring · dislodged(AUS) NR 1 ENGINE BLEED AIR SYSTEM HIGH STAGE VALVE GATE SEALING RING DISLODGED, PREVENTING VALVE FROM FULLY CLOSING. INVESTIGATION FOUND THE HIGH STAGE VALVE BUTTERFLY PLATE SEALING RING CLIP FAILED ALLOWING THE SEALING RING TO JAM THE THE VALVE IN THE SLIGHTDec 6, 2005 · Boeing 737800*SDR A6WA200560020Seal · leakingRT ZONE HI TEMP CAPTAIN ILLUMINATED ENROUTE IN ICING CONDITIONS. REPLACED SEALS AT NR 4 PYLON LEADING EDGE AND LEAK CHECKED WING ANTI-ICE. OPS CHECKED GOOD. (K)Dec 3, 2005 · N290UE · Bag BAE146200ASDR 2005FA0001582Pneumatic System · contaminatedPNEUMATIC SYSTEM INSPECTED AND TRACES OF WATER WERE FOUND IN THE EJECTOR VALVE AND AREA BELOW THE VALVE. FURTHER INSPECTION REVEALED WATER IN THE PNEUMATIC MANIFOLD VALVE AND ASSOCIATED PLUMBING. APPROXIMATELY .5 OZ OF WATER WAS REMOVED FROM THE SYSTEM. THENov 30, 2005 · N202P · Beech 58SDR 2005FA0001574Pneumatic System · contaminatedDURING PROLONGED PERIODS OF OPERATION IN HEAVY PRECIPITATION CONSIDERABLE AMOUNTS OF WATER INTO THE PNEUMATIC SYSTEM. INSP OF PNEUMATIC SYS REVEALED LARGE AMOUNTS OF WATER BEING PASSED THROUGH DEICE BOOT EJECTOR, FURTHER DISASSEMBLY INSP REVEALED SEVERAL OUNCNov 23, 2005 · N3214H · Beech 58SDR 2005F00110Pneumatic System · contaminatedDURING PROLINGED PERIODS OF OPERATION IN HEAVY PRECIPITATION CONSIDERABLE AMOUNTS OF WATER ENTER INTO THE PNEUMATIC SYSTEM. INSP OF PNEUMATIC SYS REVEALED LARGE AMOUNTS OF WATER BEING PASSED THROUGH DEICE BOOT EJECTOR, FURTHER DISASSEMBLY INSP REVEALED SEVERANov 23, 2005 · N401BC · Beech 58SDR 2005FA0001573Pneumatic System · contaminatedDURING PROLONGED PERIODS OF OPERATION IN HEAVY PRECIPITATION CONSIDERABLE AMOUNTS OF WATER ENTER INTO THE PNEUMATIC SYSTEM. INSP OF PNEUMATIC SYS REVEALED LARGE AMOUNTS OF WATER BEING PASSED THROUGH DEICE BOOT EJECTOR, FURTHER DISASSEMBLY INSP REVEALED SEVERANov 23, 2005 · N1065B · Beech 58SDR 2005FA0001572Pneumatic System · contaminatedDURING PROLONGED PERIODS OF OPERATION IN HEAVY PRECIPITATION CONSIDERABLE AMOUNTS OF WATER ENTER INTO THE PNEUMATIC SYSTEM. INSP OF PNEUMATIC SYS REVEALED LG AMOUNTS OF WATER BEING PASSED THROUGH DEICE BOOT EJECTOR, FURTHER DISASSEMBLY INSP REVEALED SEVERAL ONov 23, 2005 · N3267N · Beech 58SDR RAIA00511028Valve · overtempFLT 7989 - DAY - ON CLIMBOUT, DID 2ND PART OF F/O'S ICE TEST AND RECEIVED AN EICAS MESSAGE OF BLEED 2 OVERTEMP. MAINTENANCE REMOVED AND REPLACED THE FAN AIR VALVE THERMOSTAT.Nov 21, 2005 · N839HK · Emb EMB145LRSDR SA05117Precooler · damagedCLT FLT 1130 WHILE EN ROUTE, THE NR 1 ENGINE BLEED SYSTEM INDICATED INOPERATIVE WHEN ECAM MESSAGE -AIR L WING LEAK-, GENERATED. WITH THE NR 2 ENGINE BLEED SYSTEM ON MEL, THE AIRCRAFT DID NOT HAVE SOURCE AIR TO MAINTAIN CABIN PRESSURE, CAUSING BOTH AIR CONDITNov 19, 2005 · N118US · Airbus A320214SDR QXEA200501545Warning Light · illuminatedPDX FLIGHT 2450: NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED (EXT ONCE NR 1 BLEED SELECTED OFF PER CHECKLIST AFTER ABOUT 45 SPC TO 1 MINUTE). MAINTENANCE COMPLIED WITH OPS TEST OF BLEED AIR SYSTEM PER 36-11-00. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RNov 17, 2005 · N402QX · Bombdr DHC8402SDR RAIA00511018O-Ring · leakingFLT 5535 - STL - BLEED 2 LEAK WITH ASSOCIATED STRONG ODOR. MAINTENANCE REMOVED AND REPLACED BLEED O-RINGS.Nov 14, 2005 · N817HK · Emb EMB145LRSDR AU510002125Clamp · fractured(AUS) APU BLEED AIR DUCT FRACTURED. BLEED AIR SUPPLY DUCT SEPARATED IN HORIZONTAL STABILISER COMPARTMENT. (CASA# 510002125)Nov 11, 2005 · Boeing 737800*SDR AU510002041Pneumatic System · faultyLT ENGINE PRV WARNING WHEN TAKEOFF THRUST SET. MESSAGE CLEARS WHEN THRUST REDUCED. INVESTIGATION CONTINUING.Nov 10, 2005 · Boeing 767338SDR 2005UALA01243Switch · failedFLIGHT DIVERTED DUE TO LOST RIGHT PACK. FOUR UNITS WERE REMOVED DUE TO THIS EVENT: HIGH PRESSURE SHUTOFF VALVE AND PRESSURE REGULATING VALVE (HPSOV/PRV, P/N: 790270-4/-14), HIGH PRESSURE CONTROLLER (HPC, P/N: 773289-15) AND PRESSURE REGULATING VALVE CONTROLLNov 6, 2005 · N672UA · Boeing 767322SDR DHL2005805003Regulator Valve · malfunctionedON TAKEOFF NR 2 ENGINE OVERPRESS LIGHT ILLUMINATED. REJECTED T/O A/C WEIGHT 252000 IAS 20KTS OAT 13C PA 1000FT. DEFFERRED NR 2 HIGH PRESS 9TH STAGE REG & SO VALVE IAW MEL 36-1-5 SPEC PROC C/W NR 2 HS PRESS 9TH STAGE REG & SO CLOSED. DMI NR 23103 PLACARDS INSNov 4, 2005 · N805DH · Doug DC873F
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