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 QXEA2009121101033Switch · malfunctionedNR 1 BLEED HOT CAUTION MESSAGE ON APPROACH , AT 5,000 FEET. ABORTED APPROACH AND RETURNED TO DEPARTURE. LANDING UNEVENTFUL. INTERROGATED CDS AND FOUND FAULT CODES 7001- L BLD OVR TEMP AND 7005- L BLD AND OT, C/W FIM TASK 36-046, REMOVED AND REPLACED NR 1 BLEEDSDR DL76G091905Shutoff Valve · malfunctionedDURING INTITIAL T/O ROLL LT ENG BLEED AND MESSAGE ILLUMINATED FWD TO MCO PLACARDED HPSOV IAW MEL 36-11-02. DISP GRANTED. FWD TO MCO PLACARDED HPSOV IAW MEL 36-11-04 AND LT ENGINE THRUST REVERSER DEACTIVATED IAW MEL 36-11-02 DISP DISP GRANTED. ETOPS CATEGORY 'SDR UALA2009120303735Duct · crackedAPU AIR SUPPLY DUCT LOCATED IN LT WHEEL WELL IS CRACKED. REPLACED DUCT ASSEMBLY. LEAKED CHECK GOOD.SDR SIMA200933701Thermostat · inoperativeDURING FLIGHT 3489 THE CREW REPORTED A NUMBER 2 BLEED LOW TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CREW DECLARED AND EMERGENCY AND DUE TO THE WEATHER DIVERTED TO XNA. THE AIRCRAFT LANDED WITHOUT INCIDENT. NO OTHER PROBLEMS WERE NOTED BY THE CREW. REMOVSDR DL76G091939Shutoff Valve · malfunctionedDURING INITIAL T/O ROLL L ENG BLEED AND MSG ILLUM FWD TO MCO PLACARDED HPSOV IAW MEL 36-11-04 AND LT ENG THRUST REVERSER DEACTIVATED IAW MEL 36-11-02 DISP GRANTED. R & R LT ENG PRV IAW AMM PERFORMED HIGH PWR ENG RUN DUCT PRESS FOR LT ENG LOW. NO MESSAGES NOTSDR RAIA2009120200004Valve · malfunctionedDURING CLIMB, THE CREW REPORTED RECEIVING A BLEED 1 OVERTEMP MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 1 FAN AIR VALVE FOLLOWED BY AN OPERATIONAL CHECK OF THE BLEED SYSTEMS. NO DEFECTS NOTED.SDR C2XA09IA295O-Ring · blownIAH - FLIGHT 3033, DURING CLIMB THE CREW REPORTED A NUMBER ONE BLEED LEAK. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BLOWN O-RINGS AT JOINT NUMBER 21 LEFT, LEAK CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS SDR UALA2009113003700Controller · faultyL HPSOV FLUCTUATES WITH THROTTLES AT IDLE IN DESCENT. DURING PNEUMATIC HEALTH CHECK FOUND HPSOV SLUGGISH AND CONTROLLER FAILING TO COMMAND VALVE CLOSURE. REPLACED VALVE AND CONTROLLER. ALL CHECKS NORMAL.SDR SIMA200933403Clamp · defectiveON FLIGHT 4113 THE CREW REPORTED ENCOUNTERED ICE ON CLIMBOUT AT 8000 FEET AND RECEIVED BLEED 1-2 LEAK WARNING ON EICAS. THE CREW ALSO REPORTED A FOUL SMELL IN THE COCKPIT AND CABIN. THE CREW ELECTED TO RETURN TO CHM AT A NORMAL DESCENT RATE. LANDING WEIGHT SDR CHQA200900251Clamp · leakingDURING CRUISE THE CREW REPORTED A BLEED 1 LEAK MESSAGE WHILE AT 17,000FT. THE AIRCRAFT DIVERTED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LEAKING V-BAND CLAMP DOWN-STREAM FROM THE HIGH STAGE VALVE. THE CLAMP WAS TIGHTENED AND ENGINE RUNS WERE SDR RAIA2009113000002O-Ring · wornCREW REPORTED RECEIVING A NR 1 BLEED LEAK MESSAGE ON THE EICAS. MAINTENANCE REPLACED THE LEFT ENGINE PRE COOLER DUCT TY-WRAPS AND BLEED O-RINGS IN THE CARGO BAY UNDERNEATH THE FLOOR PANELS. OPS CHECKED AND LEAK CHECKED GOOD.SDR RAIA2009113000007Clamp · out of positionTHE CREW REPORTED RECEIVING A NR 2 BLEED LEAK MESSAGE ON THE EICAS IN FLIGHT. MAINTENANCE PERFORMED AN INSPECTION OF THE BLEED SYSTEM AND FOUND THE CLAMP OFF AND THE DUCT SEPARATED BEHIND THE WING ON THE BOTTOM OF THE FUSELAGE. THE PACKINGS WERE REPLACED ALOSDR QXEA200901006Warning Light · illuminatedON T/O ROLL AT 70KTS, GOT THE NR 1 AND NR 2 BLEED HOT CAUTION LIGHT, AFTER FOLLOWING ABNORMAL CHECKLIST, BLEED, PRESSURIZATION ALL WORKING NORMALLY. INTERIGATED CDS, NO FAULTS FOUND, C/W OPS TEST OF THE BLEED AIR SYS IAW AMM TASK 36-11-00-710-802, OPS TEST GSDR QXEA200911301008Shutoff Valve · malfunctionedFLIGHT CREW NOTICED "HOT' ODOR, SHORTLY AFTERWARD LAVATORY SMOKE DETECTOR BEGAN SOUNDING. NO SMOKE WAS OBSERVED BY CABIN CREW, ONLY HAZE. CABIN REPORTED CONDITIONS IMPROVED BY LANDING. RETURNED TO FIELD. LANDING UNEVENTFUL. PERFORMED FIM TASK 71-00-00-810-81SDR UALA2009112303653Controller · malfunctionedRT ENG BLEED LIGHT & RT ENG HPSOV EICAS MSG DURING CRZ, WITH ENG BLEED SWITCH ON, & ENG RUNNING. CREW COMMENTS: DUCT PRESS=17. CREW REPORTS 'BLEED' LIGHT AND EICAS INTERMITTENTLY APPEAR AND DISAPPEAR WITH VLV LOCKED OUT PER MEL. REPLACED NR 2 ENG HIGH STAGSDR UALA2009112303647Controller · malfunctionedRIGHT BLEED LOSES PRESS WHENEVER THROTTLE IS IN LOW THRUST CONDITION. REPLACED PRESSURE REGULATING VALVE CONTROLLER. RAN ENG PNEU PRESSURE NORMAL.SDR UALA2009112003629Shutoff Valve · malfunctionedAFTER ENG START R ENG HPSOV & ASSOCIATED BLEED VALVE ILLUMINATED. REPLACED HPSOV VALVE RT, RAN ENG; NO MESSAGES.SDR UALA2009112003621Controller · faultyNR 2 ENG PRSOV VLV CONTROLLER EXCEEDS UPPER LIMIT DURING HEALTH CHECK. REMOVED AND INSTALLED NEW CONTROLLER. PRSOVC TEST PASSED.SDR UALA2009111803597Shutoff Valve · faultyCREW REPORTS AFTER ENG START, THE LEFT BLEED WOULD NOT CLOSE. SHUTDOWN NR 1 ENG, CYCLED LT BLEED CONTROL CB AND RESTARTED ENG, NO HELP. OPERATED ENGINE AND FOUND THAT LEFT PRSOV WOULD OPEN WITH SWITCH SELECTED TO OFF. REPLACED LEFT PRSOV. OPERATED ENGINE, SDR UALA2009111803602Shutoff Valve · malfunctionedLT & RT DUCT PRESSURE SPLIT DURING CRUISE, WITH ENGS RUNNING, LT & RT ISOL VLVS CLSD & BLEED SW ON. ACCOMPLISHED PNEU HEALTH CHECK. PRV & PRV CONTROLLER CHECKS GOOD, FAN AIR VALVE CHECKED GOOD, PRSOV FAILED. REPLACED PRSOV. NO HELP. REPLACED HPSV VALVE ANSDR UALA2009111603572Thermostat · faultyBLEED AIR LOSS, FLT DIVERTED. RE-ACTIVATED NR 2 ENG PRV AND DE-ACTIVATED HP VALVE. REPLACED NR 1 ENG FAN AIR VALVE CONTROL THERMOSTAT. REPLACED SOLENOID. BLEED CHECK COMPLETED ALL RUNS COMPLETED SATISFACTORY. ACCOMPLISHED HEALTH CHECK FROM PAGE 1 TO 14 ALSDR PCSA2009111501Modulating Valve · leakingDURING CLIMBOUT PASSING 28000 FEET ENGINE 1 ENG STRUT OVERHEAT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURE, NO FURTHER OCCURRENCE. MAINTENANCE FOUND ENGINE 1 HIGH PRESSURE MODULATING VALVE LEAKING, REPLACED THE VALVE IAW THE B727 AMM, PERFORMED A LEAK CHECKSDR UALA2009111603547Precooler · crackedNR 1 ENG FAILED DUCT LEAK TEST. FOUND LARGE CRACK ON NR 1 ENG PRECOOLER. REPLACED PRECOOLER. AFT PRECOOLER CLAMP LEAKING AT HINGE POINTS. RE-SECURED, SECURED ENGINE COWLS.SDR C2XA09IA289O-Ring · blownIAH, FLIGHT 2012, THE CREW REPORTED A BLEED ONE LEAK MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE O-RINGS AT LOCATIONS 3 AND 1 ON THE BLEED AIR SYSTEM, OPERATIONALLY AND LEAK CHECKED WISDR C2XA09CL148Valve · faultyCLE FLT NR 153, THE CREW REPORTED A BLEED NR 2 OVERTEMP MESSAGE WHEN THE ANTI-ICE WAS SELECTED ON. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FAN AIR VALVE. OPERATIONAL CHECKS WERE GOOD.SDR DL76P091744Valve · malfunctionedLT BLEED OFF LIGHT ILLUMINATED AT ENG START AND WOULD NOT EXTINGUISH. CLEANED PRSOV C/P. CYCLED VALVE AND RESET LT BLEED CARD. RAN ENGINE, CHECKS GOOD. OK FOR SERVICE.SDR PCSA2009110601Clamp · looseDURING INITIAL CLIMB, ENGINE 3 STRUT OVERHEAT LIGHT ILLUMINATED. MAINTENANCE REPLACED THE AFT CLAMP ON 3 ENGINE BLEED AIR SHUTOFF VALVE. THE CLAMP WAS REPLACED AND LEAK CHECKED GOOD IN AN ENGINE OPERATIONAL CHECK.SDR ASAA0956954Control Valve · stuckAS DESCENT WAS INITIATED AT FL 400 NR 1 ENG BLEED TRIPPED OFF WITH A CORRESPONDING DROP IN LEFT DUCT PRESSURE. QRH OPERATED AND BLEED TRIP LIGHT EXTINGUISHED NO ENG OR WING A/I OF FLIGHT MIG 2C 237137 INITIATED. WHILE PERFORMING FIM TASK 36 10 00 810 801 FOUSDR UALA2009110403419Shutoff Valve · failedLEFT DUCT PRESSURE FLUCTUATES BETWEEN 25 TO 40 PSI ON DESCENT. FOUND PRSOV FAILED HEALTH CHECK. REPLACED PRSOV, OPS CHECKS GOOD.SDR SWIA200923049Duct · blownRIGHT ENGINE OVERTORQUED ON CLIMB OUT DUE TO BLOWN DUCT. (FLT 6847)REPLACED BLEED DUCT AND RIGHT ENGINE PROP.SDR UALA2009110403413Shutoff Valve · faultyLEFT ENG BLEED WILL NOT CLOSE. REPLACED LEFT ENG PRSOV. OPS NORMAL.SDR C2XA09CL141O-Ring · faultyEWR FLT 2940 - THE CREW REPORTED A BLD 2 LEAK ON CLIMBOUT. MAINTENANCE INSPECTED AND REPLACED THE O-RINGS ON THE NR 2 BLEED DUCT IN THE CARGO COMPARTMENT JOINT NR 20. OPERATIONAL CHECKS WERE GOOD.SDR UALA2009110403415Shutoff Valve · malfunctionedEICAS "R ENG HPSOV". FOUND WIRE CHAFING ON HPSOV ACTUATOR ARM RT ENG. MAYBE CAUSING EICAS MESSAGE. REPLACED RIGHT ENGINE HPSOV. OPS OK, NO EICAS MSGS DISPLAYED.SDR Q2SA760001Flex Duct · crackedON TAKEOFF CLIMBOUT OF EBLG ENGINE FIRE WARNING CAME ON FOR ENGINE NR 2, CREW ELECTED TO SHUTDOWN ENGINE NR 2, DUMPED 77,000 LBS OF FUEL, RETURNED TO AND LANDED SAFELY AT EBLG. AFTER LANDING MAINTENANCE CREW IN EBLG INSPECTED ENGINE NR 2 AND FOUND A CRACKED PSDR C2XA09IA276O-Ring · blownIAH - FLIGHT 2617 THE CREW REPORTED A BLEED ONE LEAK IN CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLEED O-RINGS IN THE LEFT CARGO WALL AT LOCATION 19, OPERATIONALLY AND LEAK CHECKED WITH NO DEFESDR ASAA0956876Precooler · failedENG NR 2 BLEED TRIP OFF LIGHT ILLUMINATED DURING CLIMB PASSING FL310 WHEN ENGINE AND WING ANTI ICE TURNED ON. SAT WAS 35C LIGHT RESET USING QRC AND DID NOT COME ON AGAIN. FOUND NR 2 ENG PRECOOLER VALVE BAD PER 36 12 00MM. REMOVED BAD NR 2 ENG PRECOOLER VALVSDR AWKA7561028Seal · leakingTHE FLIGHT CREW RECEIVED A RT ENG FIRE LIGHT AND ASSOCIATED EICAS MESSAGE ON TAKEOFF ROLL AT 75 KIAS. LIGHTS WENT OUT WHEN PWR WAS REDUCED TO IDLE. ENG FIRE EXTINGUISHING SYS WAS NOT ACTIVATED. THE ACFT WAS INSPECTED BY MX AND WORN HIGH PRESSURE BLEED AIR DSDR C2XA09CL139Switch · inoperativeCLE FLT 2580 - THE CREW REPORTED A BLEED 1 VALVE CLOSED MESSAGE AFTER TAKEOFF. COULD NOT GET THE NR 1 BLEED VALVE TO OPEN. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BLEED VALVE PUSH BUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD.SDR FDEA200910243659Pilot Valve · inoperativeON TAKE OFF BLEED AIR 2 OFF ALERT. TRIED MANUAL AND 2ND AUTO CHANNEL COULD NOT RESTORE (BLEED AIR 3 PREVIOUSLY DEFERRED) AIR TURNBACK PHNL 90,000 LBS FUEL DUMPED. REPLACED NR 2 PRESSURE REGULATOR PILOT VALVE IAW AMM 36-12-20-4. RAN NR 2 ENG IAW JRH. NR 2 PSDR CHQA200900226Clamp · defectiveTHE FLIGHT CREW RECEIVED A BLEED 1 LEAK MESSAGE AFTER TAKEOFF AT APPROXIMATELY 500FT AGL AND RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND OPS CHECKED THE NR 1 BLEED SYSTEM AND FOUND THE CLAMPS ON THE NR 1 FAN AIR VALVE TO BE BAD ANSDR DL76L091698Shaft · looseRT PACK OFF LT ILLUMINATED RT ENG BLEED LT ILLUMINATED. T/S PER AMM R/R RT ENG PRV CONT FOUND RT ENG PRV VLV SHAF LOOSE R/R RT ENG PRV. PRV CONT AND VALVE NEEDS OPS CHECK. PERFORMED OPS CHECK PER AMM RT ENG RAN OPS CHECK NORMAL. ETOPS CATEGORY 'E': PROBLEMSDR DL76G091671Controller · malfunctionedDURING TAXI NO RT ENG BLEED AIR AVAILABLE, RTB. PRV CONTROLLER REPLACED BUT FOUND INOP ON FIT. LOAN ITEM OBTAINED FROM LUFTHANSA. FITTED IAW AMM 36-11-19-404-016-001, ENGINE RUN. PERFORMED AND OPS OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO SDR UALA2009102203299Regulator · faultyL ENG BLEED WILL NOT CLOSE. REPLACED LEFT ENGINE PRSOV WITH ENGINE HIGH STAGE VALVE. NO HELP. REPLACED HIGH STAGE VALVE WITH PRSOV VALVE. SUSPECT LEFT ENGINE PRSOV REGULATOR. LEFT ENG PRSOV REGULATOR REMOVED. REPLACED PRSOV REGULATOR. ACCOMPLISHED IDLE RUN, CSDR DL76L091662Valve · unserviceableRT PACK OFF LT ILLUMINATED RT ENG BLEED LT ILLUMINATED. T/S PER AMM R/R RT ENG PRV CONT. FOUND RT ENG PRV SHAFT LOOSE R/R RT ENG PRV. PRV AND CONT AND VALVE NEEDS OPS CK. PERFORMED OPS CK PER AMM RT ENG RAN OPS CHECK NORMAL. ETOPS CATEGORY 'B': DIVERSION SDR CHQA200900223Unknown · malfunctionedSHORTLY AFTER TAKEOFF THE CREW RECEIVED A BLEED VALVE 2 CLOSED MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE BLEED VALVE WOULD NOT OPEN. THE AIRCRAFT LEVELED OFF AT FL230 AND ENCOUNTERED ICING CONDITIONS. THE AIRCRAFT DESCENDED TO 15,000FT AT WHICH TIME A SDR C2XA09IA266Filter · dirtyIAH - FLIGHT 2160, DURING CLIMB THE CREW REPORTED A BLEED ONE OVERTEMP. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE FAN AIR VALVE FILTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFSDR PCSA2009102101Clamp · looseNUMBER 3 STRUT OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT. MAINTENANCE DISCOVERED A LOOSE CLAMP ON THE NUMBER 3 PRECOOLER. THE CLAMP WAS RETORQUED AND LEAK CHECKED GOOD IN AN ENGINE OPERATIONAL CHECK.SDR A6WA200940685Isolation Valve · malfunctionedISOLATION VALVE WOULD NOT OPERATE IN FLIGHT, RESULTED IN UNPRESSURIZED LANDING. REMOVED AND REPLACED ISOLATION VALVE IAW AMM 36-11-07. OPS CHECK GOOD. (K)SDR ASAA0956815Shutoff Valve · malfunctionedDUCT PRESSURE INDICATES: L R, AFTER T/O (CLIMB) 15 45 CRUISE 15 42 AFTER T.O.D. (IDLE) 12 16. AFTER T.O.D. BOTH DUCT PRESSURE NEEDLES WERE MATCHED THRU LANDING. REPLACED NR 1 PRSOV. FOUND A LEAKING DIAPHRAM REF AMM 36 11 04 000 801. REPLACED NR 1 450 THERMOSDR C2XA09CL143Precooler · faultyCLE FLIGHT 2875 - THE CREW REPORTED A BLD 1 OVERTEMP MESSAGE ON CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BLEED SYSTEM PRECOOLER. OPERATIONAL CHECKS WERE GOOD.
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