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 08FDEA02820Fitting · looseON CLIMB-OUT PASSING 15000 FT GOT NR 2 BLEED FAULT. COMPLIED WITH ECAM, RETURNED TO DFW. FOUND SENSE LINE FOR NUMBER 2 ENG PNEU PRESSURE REGULATOR LOOSE AT PYLON FITTING SECURED FITTING. PERFORMED FUNCTIONAL CHECK OF THE NUMBER 2 ENG BLEED REF MM 36-11-00-6SDR 2008UALA03725Precooler · leakingLEFT ENGINE PRECOOLER LEAKING AIR. *S/D* FOUND PRECOOLER LEAKING. REPLACED LEFT ENGINE PRECOOLER ASSEMBLY IAW MM 36-11-15, LEAK AND RUN CHECK GOOD. AC OK FOR SERVICE.SDR 2008FA0000442Coupling · missingDURING GROUND RUN AFTER INSTALLATION, HOT AIR ESCAPED FROM THE NOSE COWL ANTI-ICE DUCT AT THE 12 O`CLOCK POSITION CAUSING THERMAL DAMAGE TO THE C-DUCT THERMAL BLANKETS AND TRUST LINK TEFLON WASHERS. INVESTIGATION FOUND DUCT COUPLING PN AS1895-4-175 MISSING. SDR USAASB08043Valve · faultyFLT 1835 - DURING CRUISE AT FL270, A PRESSURIZATION FAILURE AS CABIN ALTITUDE WARNING HORN SOUNDED. DECLARED AN EMERGENCY & DESCENDED TO 10,000 FT. ACCOMPLISHED QUICK REFERENCE PROCEDURES & REGAINED CABIN PRESSURE. FLT CONTINUED & LANDED AT RSW WITHOUT FURSDR 2008UALA03497Controller · failedNR 1 ENG PRSOV CONTROLLER FAILED. *S/D* NR 1 ENGINE PRSOV CONTROLLER FAILED. INSTALLED NEW PRSOV CONTROLLER, OPS CHECK GOOD. AC OK FOR SERVICE.SDR 2008UALA03496Valve · failedNR 2 ENGINE PRSOV FAILED HEALTH CHECK. *S/D* NR 2 ENGINE PRSOV FAILED HEALTH CHECK. REPLACED PRSOV PER MM 36- 11-18 401, OPS TEST GOOD. AC OK FOR SERVICE.SDR USAABB08106Bellows · blownCUN - FLT 808 EN-ROUTE CUN TO CLT. ON CLIMBOUT, AT FL290, THE RIGHT ENGINE INDICATED AN OVERHEAT CONDITION. THE CREW REDUCED THE THRUST SETTING. HOWEVER, THE INDICATION DID NOT GO OUT. THE CREW SHUT DOWN THE RIGHT ENGINE AS REQUIRED PER PROCEDURES, AND RESDR 2008UALA03414Valve · faultyBLEED OFF ENG L - EICAS MSG ON TAXIOUT. SUSPECT FAULTY HIGH PRESSURE SHUT OFF VALVE. REPLACED NR 1 ENGINE HPSOV REF AMM 36-11-07. AC OK FOR SERVICE.SDR 2008F00017Valve · malfunctionedAT FL400 ENROUTE, RAT ABOUT -38 C AND NOT IN ICING CONDITIONS. DURING DESCENT, NOTED ABNORMALLY HIGH N1 AND ITT INDICATIONS FOR DESCENDING FLT AT IDLE. FOUND COULD ADD POWER, BUT NOT REDUCE IT. ACTIVATED NAC HEAT ON BOTH ENGINES IN AN ATTEMPT TO RESTORE NORMALSDR 2008UALA03363Controller · faultyNR 2 ENGINE PRSOV CONTROLLER FAILED HEALTH CHECK. *S/D* SUSPECT FAULTY CONTROLLER. REPLACED CONTROLLER PER MM 36-11-18-401. OPS CHECKED GOOD. AC OK FOR SERVICE.SDR CHQA200800108O-Ring · leakingFLIGHT 7803, IAD TO IND. WHILE CLIMBING THROUGH 8,000 FT THE FLIGHT CREW RECEIVED A BLEED 1 LEAK MESSAGE, RETURNED TO IAD, AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DURING INSPECTION THAT THE BAGGAGE COMPARTMENT FLOOR WAS WARM, AND AFTER REMOVING THE FLSDR 2008UALA03312Precooler · crackedLEFT ENGINE PRECOOLER LEAKING BEYOND LIMITS. *S/D* SUSPECT FAULTY PRE COOLER. REPLACED PRE COOLER LEAK CHECKED GOOD. AC OK FOR SERVICE.SDR 772AFCheck Valve · defectiveFLAPPERS IN BLEED AIR INLET CHECK VALVE CAME LOOSE AND CHAFED THE INSIDE OF THE HOUSING. ONE FLAPPER CHAFED A HOLE THROUGH THE HOUSING.SDR 2008UALA03206Modulating Valve · faultyBLEED FAMV R RIGHT ENGINE BLEED FAN AIR MODULATING VALVE (FAMV) FAILED OPEN OR CLOSED, OR RIGHT AIR SUPPLY AND CABIN PRESSURE CONTROLLER FAILURE. STATUS MSG-3610320 LATCH DC MODE. SUSPECT FAN AIR MODULATING VALVE. REPLACED NR 2 ENGINE FAMV IAW MM 36-11-16. SDR DL76G080818Valve · malfunctionedABORTED TAKEOFF FOR L ENG PRV LT AT 60 KTS FWD TO MCO PER MEL 36-11-08C. TESTED LT ENG PRVC PER HEALTH CK JIC 6119. TESTED BAD. REPLACED WITH FLEX MUSCLE LINE. TESTED PRV VALVE. NOTED LEAKAGE REPLACED PER AMM. ALL TESTS NOW OK PER AJIC 6119 HEALTH CK. ASDR CWQR200805Air Duct · crackedDURING A PHASE 1-4 INSPECTION THE PRECOOLER EXHAUST DUCT WELD ASSEMBLIES WERE FOUND TO BE CRACKED IN THE LEFT AND RIGHT PYLON. THE LEFT HAD TWO CRACKS AND THE RIGHT HAD THREE CRACKS. A SERVICE CONDITION REPORT HAS BEEN SENT TO CESSNA UNDER #362539 FOR THE LESDR 08FDEA02022Bleed Valve · failedNR 1 PACK FAULT, XFEED WOULD NOT OPEN, RESET BREAKERS STILL INOP. THE NR 1 HP BLEED VALVE IS ON MEL 36-11-03. REPLACED THE PNEUMATIC CROSSBLEED VALVE 16HV PER AB MM 36-12-11-4, OPS CK OK, ALL ACCESS PANELS IN WHEEL WELL CLOSED UP. REMOVAL/INSTALLATION, OFF SDR 2008UALA03064Controller · shortedTHE "AIR SPLY L HTR" C-B ON P110 POS M16 WILL NOT RESET. SUSPECT HIGH PRESSURE CONTROLLER/FAN AIR SHORTED. REPLACED LT FAN HP CONTROLLER. RAN BOTH ENGINES. OPS OK. AC OK FOR SERVICE.SDR HALA0800588Bleed Air Sys · warning lightATB - RT AIR SYS FAULT DURING CLIMB AND INTERMITTENT LT AIR SYS PRESSURE LOW. REPAIR IN WORK.SDR COMA0870019Shutoff Valve · malfunctionedFLIGHT 5249 - LEFT AND RIGHT PRSOV'S AS WELL AS ISOLATED VALVE BEGAN CYCLING OPEN AND CLOSED. RAPID PRESSURIZATION LOSS OCCURRED. DECLARED EMERGENCY, FOLLOWED QRH, ISOLATION FAULT MESSAGE DISPLAYED. LANDED WITHOUT INCIDENT. OPS CHECKED PRSOV'S BOTH SIDES, SDR RAIA00805018Bleed Air Sys · leakingFLT 8068 - IAD - BLEED NR 2 LEAK MESSAGE ON THE EICAS. MAINTENANCE DEFERRED THE NR 2 BLEED SYSTEM IAW MEL PROCEDURES.SDR UALA2008111302764Clamp · leakingRTFL DUE TO A WING/BODY OVERHEAT INDICATION. NORMAL LANDING. FOUND PNEUMATIC LEAK JUST INBOARD OF NR 1 ENG PYLON AT CLAMP. REPLACED CLAMP, NO LEAK NOTED. RUNUP CREW RAN BOTH ENGS AT HIGH THRUST SETTINGS FOR SEVERAL MINUTES WITH NO OVERHEAT WARNING. A/C OKSDR YENA2008047Valve · leakingFLT NR 303, IAD-FLL, AIR ENG 1 BLEED ABNORMAL PRESSURE (SUBSEQUENT PACK 1/PACK 2-FAULT). FOUND AIR LEAK ON PRESSURE REG VALVE CLAMP JOINT. CLAMP WAS REMOVED AND JOINT RE-ALIGNED WITH VALVE. NO FURTHER AIR LEAK NOTED FAN AIR VALVE THERMOSTAT SEAL WAS REPLACESDR 2008UALA02706Clamp · looseRTFL DUE TO WING BODY OVERHEAT WARNING. FOUND PNEUMATIC LEAK JUST INBOARD OF NR 1 ENGINE PYLON AT CLAMP. REPLACED CLAMP.SDR ASAA0852935Bellows · leakingON CLIMBOUT DUCT PRESS SPLIT WITH RT DUCT CYCLING APPROX 60 CYCLES PER MIN. 10 000 N1 91.6 LT DUCT 40 PSI N2 94.7 RT DUCT40 50 PSI. 18 000 N1 96.7 LT DUCT 42 DUCT N2 96.7 RT DUCT 42 45 PSI 39 000 N1 90.7 LT DUCT 40 PSI. N2 93.8 RT DUCT 40 PSI. CYCLING STOPPEDSDR 2008UALA02665Isolation Valve · unknownRIGHT ENGINE ISOLATION ISLN VALVE WON`T OPEN.SDR DL757080833Duct · crackedAT FLT LVL 240 WITH ENGINE AND WING ANTI-ICE ON LEFT ENG BLEED LIGHT ILLUMINATED. FOLLOWED QRH SHUT BLEED SW OFF. OPENED ISOLATION VLV AT FLT LVL 260 RIGHT ENGINE BLEED LIGHT ILLUM. CABIN PRESSURE CLIMBED THROUGH 10K DEPLOYED MASKS. DECLARED EMERGENCY INTOSDR NOCA03408Controller · malfunctionedA/C HAD REJECTED TAKEOFF IN FRU. ON TAKEOFF ROLL L ENG PRV MESSAGE CAME ON. ACCOMPLISHED AIR SUPPLY BITE PROCEDURE PER MM 36-20-00, NO FAULTS FOUND. ACCOMPLISHED NR 1 ENG PRV VALVE AND CONTROLLER SENSE LINE CHECK, ALL LINES SECURED. INSPECTED AND CLEANED CSDR UIEA200800163Regulator Valve · leakingNR 1 ENGINE FULL POWER TAKEOFF ON CLIMB-OUT BOTH A/B LOOPS REACHED 3.0. AFTER POWER REDUCTION BOTH LOOPS CAME BACK DOWN TO 2.0. REST OF FLIGHT WAS OK. OPENED COWL AND FOUND LEAKING PRV. REPLACED THE PRV IAW AMM 36-11-13. OPS AND LEAK CHECKED OK.SDR HALA0800549Shutoff Valve · malfunctionedETOPS SIGNIFICANT SYSTEM, ATO, LT HPSOV EICAS MSG UPON SPOOL-UP FOR TAKEOFF, ABORTED TAKEOFF, AT 60-80 KNOTS AIRSPEED. LOCKED-OUT HPSOV VALVE PER MEL MPCW, ALSO ACCOMPLISHED HIGH ENERGY STOP INSPECTION, FOR ABORTED T/O PER TASK 05-51-14-212-089. OK TO CONTINSDR 2008UALA02486Shutoff Valve · malfunctionedRESET AIR SUPPLY MODULE, RAN NR 1 ENGINE, NO DUCT PRESSURE INDICATED, BOX FAULTED PRSOV VALVE.SDR RAIA00804020Seal · wornFLT 5484 - STL - BLEED 1 LEAK MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED BLEED DUCT SEALS UNDER THE CARGO BAY FLOORBOARDS. SYSTEM CHECKED GOOD.SDR ASAA0852829Control Valve · faultyRIGHT BLEED TRIP OFF LIGHT ILLUMINATED FOLLOWING A BLEEDS OFF TAKEOFF FROM LAS THE LIGHT ILLUMINATED APPROXIMATELY 60 SECS AFTER RE-ESTABLISHING THE BLEEDS ON BOTH ENGINES. BLEED RE-ESTABLISHED WITH TRIP RESET PER QRH. PRECOOLER CNTL VLV PASSED HEALTH CHECK.SDR GUUA04190801Regulator · malfunctionedFLIGHT 9205, AFTER TAKEOFF, STRONG SCENT OF BURNED RUBBER IN COCKPIT. (NO SMOKE) THE PNEUMATIC PRESSURE GAUGE PEGGED OVER THE RED LINE AND VACUUM PRESSURE GAUGE PEGGED AT ZERO, WHEN TRYING TO ADD HEAT, USE DEICE BOOTS ON ANY OTHER ENVIRONMENTAL PRESSURE FUNCTISDR ASAA0852821Valve · trippedRIGHTHAND ENGINE BLEED TRIPPED DURING CLIMB AT 2000 MSL. REPLACED HIGH STAGE VALVE.SDR RAIA00804014Valve · malfunctionedFLT 5497 - STL - BLEED NR 1 OVERTEMP MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 1 BLEED FAN AIR VALVE. SYSTEM OPS CHECKED GOOD.SDR RAIA00804015O-Ring · wornFLT 5468 - STL - BLEED NR 1 & 2 LEAK MESSAGE ON THE EICAS FOLLOWED BY A BURNING SMELL IN THE COCKPIT. MAINTENANCE REMOVED AND REPLACED THE O-RINGS AND CLAMP ON THE BLEED DUCT FOLLOWED BY SUCCESSFUL OPERATION OF THE BLEED AIR SYSTEM.SDR 2008UALA02140Valve · failedRIGHT ENG PRV EICAS CAME ON IN DESCENT. FOUND FAULTY PRESSURE REGULATING VALVE AND CONTROLLER REPLACED PRV PER MM36-11-18 & CONTROLLER PER MM36-11-08. OP CHECKED GOOD. AC OK FOR SERVICE.
SDR AALA200800890Boot · splitDFW INFLIGHT T852/09APR - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH AND DUCT PRESSURE ANOMALY. REDUCED POWER FOR DESCENT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION AND REPAIR. FOUND BLOWN DUCT BOOT ON SDR ASAA0852812Control Valve · failedPNEUMATIC DUCT PRESSURE SPLIT BETWEEN LEFT AND RIGHT SYSTEMS NOTED DURING CLIMB. REPLACED RIGHTHAND ENGINE PRECOOLER CONTROL VALVE.SDR HALA0800522Isolation Valve · malfunctionedETOPS SIGNIFICANT SYSTEM DURING TAXI RIGHT BLEED ISOLATION VALVE EICAS MESSAGE RECEIVED. UNABLE TO RESET. REPLACED RIGHT ISOLATION VALVE PER AMMM 36-11-04, OPS CHECK LEAK CHECK OK.SDR HALA0800485Spring · brokenETOPS SIGNIFICANT SYSTEM, FOUND LT ISOLATION BYPASS CHECK VALVE SPRING BROKEN. REMOVED AND REPLACED LT ISOLATION BYPASS CHECK VALVE PER AMM 36-11-04. OPS AND LEAK CK OK.
SDR DL76G080517Shutoff Valve · malfunctionedRT HPSOV CAUTION LIGHT ILLUMINATED AT CRZ APPROX 2 HRS INTO FLT. DEACTIVATED RT ENG HPSOV IN CLOSED POSITION PER MEL 36-11-02 AND ALSO DEACTIVATED RT ENG THRUST REVERSER PER MEL 78-31-01, FWD TO MCO AND PLAC PER MEL 36-11-02.SDR HALA0800480Controller · malfunctionedETOPS SIGNIFICANT SYSTEM, ATB A/C DIVERTED TO HNL. EICAS MESSAGE: L ENG BLEED OFF DISPLAYED ENG BLEED AIR VALVE OFF LIGHT ILLUM WITH SWT ON AND ENG RUNNING. DUCT PRESS 0 PSI. ACCOMPLISHED AMM 36-11-705-115. 2A TO 2I (4) 4/1/08, 2I (5) TO 2K PENDING. ACCOMPSDR C2XA08ON109Duct Clamp · missingFLT 0412 - SAN - FLIGHT CREW ABORTED T/O DUE TO NR 1 ENG EXCEEDANCE ON TAKEOFF ROLL. MX INSPECTED BLEED DUCTS AND COMPRESSOR BLEED AIR DUCTING ON ENGINE AND FOUND CLAMP MISSING ON COMPRESSOR DISCHARGE TUBE. INSTALLED NEW CLAMP OPERATIONALLY AND LEAK CHECKED SDR UPS08551946Sense Line · leakingINSPECTION TYPE:N/A ATB - DURING CLIMB LT ENGINE OVERHEAT LIGHT CAME ON. REDUCED POWER, LIGHT WENT OUT. RE-APPLIED POWER, LIGHT CAME BACK ON. REDUCED POWER, RETURNED TO MIA. ACCOMPLISHED 757 FIM 26-11-00 FIG 103A FOUND LEFT ENG HPSOV SENSE LINE AND UNION LSDR CHQA200800065O-Ring · blownFLIGHT 5984 -JAX TO CLE - DURING CLIMB, THE FLIGHT CREW RECEIVED A BLEED 1 LEAK MESSAGE AND RETURNED TO JAX AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SEVERAL PANELS IN THE CARGO COMPARTMENT THAT WERE ABNORMALLY WARM, AND THE SOURCE WAS FOUND TO BE THE O-SDR CHQA200800058O-Ring · leakingCVG TO GSP - DURING CLIMB, THE CREW RECEIVED A BLEED 2 LEAK MESSAGE ON EICAS. THE AIRCRAFT THEN RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN THE BLEEDS AND INSPECTED FOR LEAKS. A LEAK WAS FOUND AT JOINT 4 AND AFTER REPLACING THE O-RINGS ATSDR C2XA08IA090Bleed Air Sys · contaminatedIAH - FLIGHT 2127, THE CREW REPORTED A LAV SMOKE INDICATION DURING DEPARTURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND DETERMINED THE CAUSE TO BE RESIDUAL OIL IN THE BLEED AIR SYSTEM FROM PREVIOUSSDR ASAA0852760Sensor · malfunctionedLEVEL AT FL370, IN CRUISE LT BLEED TRIP OFF LIGHT ILLUMINATED. FOLLOWED QRH, PRESSED TRIP RESET BUTTON. LIGHT EXTINGUISHED FOR ABOUT 20 SECONDS AND RE ILLUMINATED. SELECTED LT PACK OFF AND DUCT PRESSURES RETURNED TO NORMAL. CHANGED NR 1 ENGINE 450 DEGREE T
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