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 2002UALA01638Controller · malfunctionedLT ENGINE HIGH STAGE CAUTION ON EICAS AND HIGH STAGE LIGHT ILLUMINATED AT APPROX 40 KTS. REPLACED LT ENGINE HIGH STAGE CONTROLLER.Oct 30, 2002 · N548UA · Boeing 757222SDR 000214Warning Light · illuminatedCREW RECEIVED A BLEED NR 2 LEAK ON EICAS ON CLIMBOUTOct 25, 2002 · N293 · Emb EMB145SDR C2XA02IA226Sensor · leakingIAH- FLIGHT 3498, THE CREW NOTED THAT #2 BLEED LEAK INFLIGHT,(FOLLOWED QRH, MX CONTROL ADVISED RETURN TO IAH), THE CREW RETURNED THE AIRCRAFT TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE SECURED RIGHT WING ANTI ICE VALVE SENSOR LINE,PERFORMED A LEOct 24, 2002 · N14939 · Emb EMB145ERSDR IXXA0200090ODuct · damagedAFTER TAKE OFF FROM ANC, THE FIRE WARNING LIGHT ILLUMINATED AND THE AUDIO WARNING SOUNDED FOR THE NUMBER THREE ENGINE. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND SECURED THE ENGINE. THE FLIGHT RETURNED TO ANC FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPEOct 23, 2002 · N827BX · Doug DC871FSDR VJ32003F00016Pump · failedDURING GROUND RUN UP OUTPUT OF ENGNE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. DRY AIR PUMP SHAFT SHEARED.Oct 22, 2002 · N8101C · Beech F33ASDR BAQA081165Valve · leakingAIR VALVE LEAKS. REPLACED WITH SERVICEABLE UNIT.Oct 17, 2002 · N213AE · Bolkms BK117B1SDR COMA0260588Bleed Valve · inoperativeFLIGHT 5973 R/H 10TH STAGE BLEED VALVE INOP.REPLACED BLEED AIR SHUT OFF VALVEOct 17, 2002 · N987CA · Cndair CL6002B19SDR 2002UALA01588Valve · failedNR 2 RIGHT HAND THRUST REVERSER TRANSLATING SLEEVE COWL DELAMINATED ON FORWARD ACOUSTIC SKIN. CAUSED BY HEAT OF FAILED VALVE IN THE OPEN POSITION FOR 10TH STAGE BLEED VALVE. ENGINE VIBRATION SURVEY ACCOMPLISHED ON GROUND, WITH FAILED VALVE, LEADING TO UNUSUAOct 14, 2002 · N827UA · Airbus A319131SDR VJ32002F00093Pump · 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. PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.Oct 14, 2002 · N1565A · Beech F33ASDR VJ32002F00083Pump · 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. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.Oct 4, 2002 · N5609S · Beech F33ASDR MALA020596Periseal · wornDURING FLIGHT NR 3522 RT ZONE HIGH TEMP LIGHT ILLUMINATED DURING FLIGHT. WING AND TAIL ANTI-ICE WAS ON. AIR RETURN TO MSP. MAINTENANCE FOUND WORN OUT NR 4 PYLON AFT OF HEAT EXCHANGER PERISEALS. REPLACED SEALS. LEAK CHECK GOOD REFER AMM 36-11-00.Oct 4, 2002 · N518XJ · Bac AVRO146RJ85ASDR 02FDEA00692Clamp · out of positionFL290 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, COMPLETED QRH PROCEDURES LIGHT WENT OUT. REMAINDER OF FLIGHT CONDUCTED WITH NR 3 BLEED OFF, NR 2 PACK OFF NORMAL POWER ON NR 3 ENGINE. CHECKED AFT AIRSTAIR AND FOUND RT PURGE VALVE V BAND CLAMP OPENING LESS THSep 27, 2002 · N268FE · Boeing 727200SDR DL757021140Circuit Card · faultyFL 310 LT ENG BLEED OFF, A/I VALVE, LT ENG WING LT VALVE ON. REINSTATED A/I THROUGH ISOL VALVE. RT BLEED OFF. NO PRESS SOURCE. CABIN CLIMBED TO 8000FT REINSTATED LT BLEED. SAME SEQ OF EVENTS OCCURRED AT FL 240 DIVERTED TO DFW. R&R LT AND RT ENG BLEED CONSep 25, 2002 · N639DL · Boeing 757232SDR 2002F00941Duct · leakingFLIGHT NUMBER 504. EICAS STATUS MESSAGE R STRUT OH DET 1 DISPLAYED DURING TAXI. MAINTENANCE REMOVED AND REPLACED ENGINE SUPPLY DUCT INACCORDANCE WITH M.M. 36-11-01. RAN ENGINE AND PERFORMED HIGH POWER TEST AND LEAK CHECK. AIRCRAFT RETURNED TO SERIVE.Sep 25, 2002 · N521AT · Boeing 75728ASDR 2002F00924Valve · intermittentOUT OF SVMC, DURING CLIMB AT 26,000 FEET, THE CABIN STARTED TO CLIMB AT MAXIMUM RATE THE CABIN WAS UNCONTROLLABLE, FOLLOWED THE CHECKLIST AND RETURNED TO SVMC WITHOUT INCIDENT. AIRCRAFT WAS PRESSURIZED USING ENGINE 1 AND 3 BLEEDS. THE PROBLEM WAS THE NR 3 ENSep 22, 2002 · N64346 · Boeing 727231SDR GAIA02108OPClamp · looseFLT 778 - FWA-BOS - DURING CRUISE, THE NR 1 ENGINE STRUT LIGHT ILLUMINATED. ACCOMPLISHED AOM PROCEDURE AND THE LIGHT EXTINGUISHED. THE AIRCRAFT CONTINUED TO BOS AND LANDED WITHOUT FURTHER OCCURRENCE. FOUND A LOOSE CLAMP AT THE SIXTH STAGE CHECK VALVE IN THESep 19, 2002 · N77780 · Boeing 727232SDR 2003F00043Valve · malfunctionedAFTER DEPARTURE FROM PIE-20 MINUTE INTO FLIGHT TO SFB, THE CREW GOT A TAILCONE OVERHEAT LIGHT AND DID A RETURN TO FIELD PIE. REMOVED AND INSTALLED AUGMENTATION VALVE IAW MD80 MM 36-10-01. OPS CHECK GOOD IAW MD80 MM 36-10-00. (M)Sep 16, 2002 · N12FQ · Doug MD88SDR A4J2002F00003Valve · inoperativeAFTER DEPARTURE, 20 MINUTES INTO FLIGHT, THE CREW GOT A TAILCONE OVERHEAT LIGHT AND DID A RETURN TO FIELD. REMOVED AND INSTALLED AUGMENTATION VALVE IAW MM. OCK GOOD IAW MM.Sep 16, 2002 · N12FQ · Doug MD88SDR VJ32002F00074Pump · 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. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.Sep 3, 2002 · N8112T · Beech F33ASDR VJ32002F00073Pump · 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. PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.Sep 3, 2002 · N5519A · Beech F33ASDR VJ32002F00072Pump · 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. PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP. RECOMMENDATION FOR CORRECTIVE ASep 3, 2002 · N1569A · Beech F33ASDR VJ32002F00071Pump · 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. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.Sep 3, 2002 · N5599P · Beech F33ASDR GLBA2002135Plug · missingRT BLEED FAIL ON TAKE OFF, REPLACED EVA TUBE PLUG OPS CHECK OK.Aug 26, 2002 · N211GL · Beech 1900DSDR QXEA0201280Valve · carbonedSEA- NR 1 ENGINE BLEED AIR PRODUCES BLUE HAZE WHEN FIRST TURNING ON AFTER ENGINE START. HAZE AND ACCOMPANYING SMELL LAST ONLY 2-4 MINUTES. CLEANED CARBON BUILDUP ON NR 1 P2.5-3 SWITCHING VALVE. NO SMOKE OR SMELL NOTED. NO PARTS REPLACED, OPERATIONAL CHECKSAug 25, 2002 · N367PH · Dhav DHC8202SDR F3LA200200250Shutoff Valve · failedAIR TURNBACK. FLIGHT CREW REPORTED WING/BODY OVERHEAT ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST AND LIGHT REMAINED ILLUMINATED. PRESSURE IN RT DUCT 10 PSI, WHICH DECREASED TO 5 PSI WHEN THRUST LEVER REDUCED IN POWER. SHUT DOWN NR 2 ENGINE AND MONITOREAug 21, 2002 · N306FL · Boeing 73736NSDR 02FDEA00593Cooler · leakingENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. NO PACK TAKEOFF, ALL BLEED AIR SWITCHES CLOSED, 0 PSI MANIFOLD PRESSURE PRIOR TO TAKEOFF. LIGHT WENT OUT AS THRUST LEVERS RETARDED AND NR 1 BLEED AIR VALVE WAS OPENED. OVERHEAT SYSTEM TESTEAug 16, 2002 · N492FE · Boeing 727200SDR UPS02439076Odor · detectedINSPECTION TYPE:N/A OIL SMELL AND HAZE IN COCKPIT AT TOP OF DESCENT WHEN THROTTLES RETARDED. VERIFIED SOURCE OF OIL SMELL FROM NR 3 ENGINE PNEUMATICS. LOCKED OUT NR 3 ENGINE PYLON VALVE TO ISOLATE PNEUMATICS FROM AIRFRAME.Aug 15, 2002 · N521UP · Boeing 747200SDR ASOA02448Regulator Valve · leakingWHILE PERFORMING A GO AROUND PROCEDURE, CLIMBING TO 4000 FEET, THE FLIGHT CREW RECEIVED A DUCT LEAK WARNING FOR THE RT ENGINE. THE APPROPRIATE CHECKLIST WAS COMPLIED WITH, BUT THE LIGHT DID NOT EXTINGUISH. IAW THE CHECKLIST THE CAPTAIN SECURED THE RT ENGINE,Aug 12, 2002 · N638AS · Emb EMB120ERSDR GLBA2002119Printed Ckt Board · malfunctionedDUAL ENVIRO FAIL AFTER TAKEOFF, RESET BLEED AIR MANAGEMENT PCB.Aug 11, 2002 · N226GL · Beech 1900DSDR DLM11020923Computer · malfunctionedAIR SYS 02 PRESS LO LIGHT ILLUMINATED IN FLT 5 PSI, FOLLOWED BY AIR SYS 2/3 PRESS LO LIGHTS, RESULTING IN TOTAL PRESSURIZATION FAILURE. RECOVERED AIR SYS 01/03 IN MANUAL MODE. REVIEWED CFDS, SYS SHOWS NO CURRENT FAULTS. PERF RTS OF ACC, ALL TEST PASSED. PEAug 8, 2002 · N809DE · Doug MD11SDR SWIA200211109Shutoff Valve · malfunctionedAFTER TAKEOFF, SET 10TH STAGE VALVES PER SOP AND LEFT 10TH ARM OPEN APPEARED ON EICAS NR 2. FIRST OFFICER'S SYNOPTIC SHOWED LEFT 10TH VALVE WAS CLOSED, BUT LEFT 10TH SWITCH WAS PUSHED IN. RETURNED TO SLC. LANDED OVERWEIGHT BY 70 LBS. REPLACED LEFT 10TH STAAug 4, 2002 · N597SW · Cndair CL6002B19SDR ZW0A0208203B-Nut · looseDURING TAKEOFF HIGH TEMP LIGHT IN TAIL COMPARTMENT RESULT IN UNSCHEDULED LANDING/RETURN TO STL. PNEUMATIC PRESS REGULATOR RELIEF LINE LOOSE HEAT EXCHANGE VENTING TO TAIL COMPARTMENT RT HEAT EXCHANGE PERRY SEAL LEAKING. TIGHTENED B-NUT ON LT PRESS REGULATOR RAug 3, 2002 · N914TW · Doug DC982SDR VNAA0207046Drain Line · brokenDURING TAKEOFF, THE CREW RECEIVED A LEFT HAND BLEED SHUT OFF VALVE FAIL MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND FOUND A BROKEN DRAIN TUBE ON THE PACK. MAINTENANCE REPLACED THE DRAIN TUBE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. Jul 30, 2002 · N461PS · Dorner DO328100SDR DLM88020854Packing · leakingTHE TAIL COMPARTMENT TEMP HI LIGHT ON DURING CLIMB. EXTINGUISHED TEMPORARILY WITH HP BLEED OFF, THEN RE-ILLUMINATED. COMPLIED WITH CHECK LIST, PULLED LEFT THROTTLE TO IDLE AND LIGHT EXTINGUISHED, LEFT PACK OFF AND LEFT THROTTLE BACK TO NORMAL. POWER AND LIGJul 22, 2002 · N987DL · Doug MD88SDR 072242002Tee Fitting · crackedUNABLE TO MAINTAIN CABIN PRESSURIZATION IN SIGNAL SOURCE. REPLACED SEVERAL VALVES PARTIALLY CORRECTED PROBLEM FURTHER INSPECTION REVEALED BLEED AIR T-FITTINGS ON RIGHT HAND PRECOOLER INBOARD AND OUTBOARD SIDES CRACKED. REPLACED BOTH T-FITTINGS, PERFORMED OPEJul 22, 2002 · N385CW · Cessna 650SDR 02FDEA00501Clamp · looseLOWER AFT BODY OVERHEAT LIGHT CAME ON 30 MIN INTO FLIGHT. WHILE RUNNING THE QRH AND WITH BOTH PACKS NR 1 AND NR 3 BLEEDS ON, THROTTLE WAS MOVED TO IDLE. OVERHEAT LIGHT THEN EXTINGUISHED. REPEAT WRITEUP. RETURNED TO NORMAL CONFIGURATION WITH NO REPEAT OCCURJul 19, 2002 · N281FE · Boeing 727200SDR 02FDEA00500Clamp · brokenLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CRUISE AT FL 310, 20 MINUTES AFTER TAKEOFF. ACCOMPLISHED CHECK LIST PROCEDURES AND LIGHT EXTINGUISHED IAW CHECK LIST LEAK WAS BETWEEN BLEED VALVE AND PACK VALVE. REPLACED BROKEN SUPPORT CLAMP SET BLEED DUCT ONJul 18, 2002 · N282FE · Boeing 727200SDR 02FDEA00496Sleeve · deterioratedLOWER AFT BODY OVERHEAT LIGHT CAME ON 30 MIN INTO FLIGHT. COMPLIED WITH QRH & SECURED RIGHT PACK NR 3 ENG BLEED. LIGHT STAYED ON IAW QRH, MOVED NR 3 THROTTLE TO IDLE, AND OVERHEAT LIGHT IMMEDIATELY WENT OUT. QRH INDICATES LEAK IS BETWEEN NR 3 BLEED VALVE ANJul 17, 2002 · N281FE · Boeing 727200SDR 2002F00803Duct · damagedFLIGHT NUMBER 579, DURING CLIMB RECEIVED R STRUT OH DET 1 FOLLOWED BY R ENG OVERHEAT. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE HP6 DUCT IN ACCORDANCE WITH MM 36-11-01.Jul 15, 2002 · N517AT · Boeing 75723NSDR VJ32002F00055Pump · failedDURING FLIGHT OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE. CHECKED SYSTEM FOR LEAKS AND CHECKED REGULATOR FOR PROPER OPERATION, ALL CHECKED WELL. SUSPECT PROBABLE CAUSE IS HEAT. NO RECOMMENDATION FOR CORRECTIVE ACTION AT THIS TIMEJul 11, 2002 · N9299B · Piper PA28181SDR AWXA200200589Filter · contaminatedPHX - AIR TURNBACK - FLT 0256 - WHILE CLIMBING OUT OF PHX EN ROUTE FOR PHL RECEIVED ECAM CAUTION AIR ENGINE NR 1 BLEED FAULT, BLEED TEMPERATURE EXCEEDED 300 DEGREES, TURNED BACK TO PHX DUE TO POSSIBLE ICING CONDITIONS. MAINTENANCE REMOVED AND REPLACED THE NR Jul 9, 2002 · N660AW · Airbus A319132SDR GLBA2002099Tube · damagedRIGHT BLEED AIR FAIL ON TAKEOFF. REPAIRED EVA TUBING, OPS CHECKED SYSTEM SATISFACTORY.Jul 3, 2002 · N261GL · Beech 1900DSDR RAIA00207205O-Ring · leaking5251-RIC- CREW REPORTED NR 2 BLEED LEAK WARNING. MAINTENANCE REMOVED AND REPLACED NR 2 BLEED DUCT SEAL, LEAK AND OPS CHECK OK.Jul 3, 2002 · N809HK · Emb EMB145SDR MALA020386Control Valve · malfunctionedSYSTEM INDICATES LT ENGINE BLEED LEAK, QRH CPMPLETED, INDICATION CLEARED WITH HP & LP BLEED VALVES CLOSED. R & R TEMP CONTROL VALVE AFTER INSTALLING NEW O-RINGS AT DUCTING FLANGES.Jun 30, 2002 · N425XJ · Saab 340BSDR GLBA2002093Tube · damagedLEFT BLEED AIR FAIL ANNUNCIATION ILLUMINATED. REPAIRED EVA TUBING, OPS CHECKED SATISFACTORY.Jun 27, 2002 · N195GL · Beech 1900DSDR USA2002F00065Valve · inoperativeENROUTE, CREW RECEIVED THE EICAS MESSAGES (RT ENGINE PRV) AND (RT ENG BLD OVHT). SHORTLY THEREAFTER, THE RIGHT PACK BECAME INOPERATIVE. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE SHAFT AND BUTTERFLY OF THE RIGHT PRV DISCRJun 27, 2002 · N656US · Boeing 7672B7SDR USAASB02124Regulator · failedCLT - FLT 1664 - AFTER T/O FROM CLT TO MDT, A/C EXPERIENCED A DUAL PACK FAILURE. LT PACK TRIPPED, THEN THE RT. FLT RETURNED TO CLT AND LANDED INCIDENT. MAINTENANCE R&R THE RT ENGINE HIGH STAGE REGULATOR PER MM 36-11-86 FOR THE RT PACK. OPS CHECK GOOD. LT Jun 25, 2002 · N356US · Boeing 737301SDR SWIA200210964Duct · leakingAT ABOUT 50 KTS ON TAKEOFF ROLL, TRIPLE CHIME DUCT LEAK RED LIGHT ON MAP AND DUCT LEAKAGE ON LEFT SIDE OVERHEAD. ABORTED TAKEOFF. LIGHTS REMAINED ON FOR ONLY 10-15 SECONDS, THEN WENT OUT. INSTALLED SERVICEABLE LEFT WING BLEED LINE. OPS CHECK GOOD.Jun 25, 2002 · N269UE · Emb EMB120RTSDR ABXA020005Sensor · defectiveLt eng hi stage displayed. Lt hi stage light illuminated. Per non-normal check list the left pneumatic switch was cycled on/off with oily fumes coming into the cabin. Note: The remainder of the flight was operated with left engine bleed and left A/C pack off. Jun 25, 2002 · N788AX · Boeing 767281SDR 02FDEA00424Clamp · looseLOWER AFT BODY OVERHEAT LIGHT CAME ON FOLLOWED RED TAB PROCEDURES. LIGHT EXTINGUISHED 1 MINUTE AFTER NR 3 BLEED AND RIGHT PACK VALVES WERE CLOSED. RAN NR 3 ENG PER JRH CHAPTER 5A, COULD NOT DUPLICATE. FAULT ON LEAK CHECK FOUND CLAMP LOOSE DOWN STREAM OF NR Jun 22, 2002 · N281FE · Boeing 727200
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