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 5TNA2015F00027Warning Switch · reversedIN CRUISE, LT BLEED AIR FAIL LIGHT ILLUMINATED. CREW SWITCHED OFF LT BLEED PACK. SIMULTANEOUSLY, THE RT BLEED AIR OFF LIGHT ILLUMINATED. THE PLANE DESCENDED TO AN APPROPRIATE ALTITUDE AND LANDED AT THE DESTINATION. IT WAS DISCOVERED THAT THE RT EVA TUBE HADSDR ASMF201501027Unknown · malfunctionedAIRCRAFT RETURNED FROM FLIGHT, DURING CLIMB, THE LT PNEUMATIC SYS INDICATOR SHOWED 5 PSI AT 1,000 FEET & IT WAS SHOWED 0 PSI AT 26,000 FEET WITH OSCILLATIONS. ACCOMPLISHED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE. DEFERRED THE LT PNEUMATIC SYS IAW MEL 3SDR ASAA2014123010108Packing · leakingLEAK CHECKED PRE-COOLER CONTROL VLAVE SENSOR AND FOUND THE 450 DEGREE SENSOR LEAKING. ACFT GROUNDED. REMOVED 450 SENSOR. REPLACED PACKING AND REINSTALLED 450 SENSOR IAW AMM 36-11-05. LEAK CHECKED GOOD.SDR VNAA2015010100002Clamp · leakingCREW REPORTED RT 14TH DUCT MESSAGE DURING CLIMB. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND BLEED AIR DUCT CLAMP LEAKING. MAINTENANCE R & R CLAMP AS REQUIRED AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.SDR AALA20141230007Shutoff Valve · failedDURING CLIMB OUT, LT BLEED TRIP ACCOMPANIED WITH LT PACK OFF LIGHT ILLUMINATED. EMERGENCY DECLARED, RETURNED TO DEPARTURE, AND LANDED UNEVENTFULLY. R & R THE LEFT PRSOV IAW AMM. ACCOMPLISHED HIGH POWER RUNS. OPS CHECKED GOOD.SDR CHQA20141229362Switch · faultyTHE CREW REPORTED THAT THEY RECEIVED A BLEED 2 VLV CLOSED MSG IN FLIGHT. THE CREW DIVERTED THE ACFT & LANDED WITHOUT INCIDENT. REPLACED THE BLEED SYS 2 PUSHBUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20141228002Coupling · failedON CLIMB OUT HEARD A LOUD BANG THEN BLEED 2 LEAK. COMPLIED WITH AOM 1 PROCEDURE, MSG EXTINGUISHED WITHIN 2 MINUTES 30 SECONDS. RETURNED FOR NORMAL LANDING. REPLACED COUPLING IAW AMM 36-11-10. LEAK CHECKED GOOD.SDR HALA2014122400220Shutoff Valve · malfunctionedRT ENG HPSOV EICAS MESSAGE, ENGINE HIGH STAGE BLEED VALVES. ACFT DIVERTED AND LANDING WAS MADE. RESTORED HPSOV TO NORMAL CONFIGURATION. ACCOMPLISHED AMM-36-002.SDR HALA2014122400219Warning Message · false activationON APPROACH INTERMITTENT EICAS MESSAGE RT ENGINE HPSOV. TROUBLESHOT IAW FIM 36-10, BITE CHECKED AIR SYS PANEL, NO FAULTS. RAN NR 2 ENGINE, NO MESSAGES DURING ENGINE RUN. AIR SHIFT NORMAL. OK TO CONT SERVICE.SDR CHQA20141223361Filter · dirtyTHE CREW REPORTED THAT THEY RECEIVED A BLEED 2 OVER TEMP MSG DURING CLIMB. THE CREW UTILIZED THE QRH & RETURNED TO FIELD. THE ACFT LANDED WITHOUT FURTHER INCIDENT. CLEANED THE FAN AIR VLV FILTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR UIEA2014122600664Shutoff Valve · malfunctionedRIGHT ENG BLEED SWITCH LIGHT OFF, LIGHT FAILS TO ILLUMINATE ON SHUTDOWN. LIGHT IS OK, MULTIPLE OCCASIONS. R & R PRSOV. RUN OPERATIONS CHECKED GOOD IAW AMM 36-11-09.SDR SIMA20141223005Thermostat · malfunctionedBLEED 1 OVER TEMP WARNING DURING CLIMB THROUGH 8000 FT ICING CONDITIONS, BLEED TEMP POINTER WAS IN RED RANGE SAT-10 TAT-1C. R & R NR 1 FAN AIR THERMOSTAT IAW AMM 36-11-06. OPERATIONS CHECKED GOOD.SDR ASAA2014121910023Regulator · failedNR 1 ENGINE HIGH STAGE REGULATOR FAILED REVERSE FLOW DIAPHRAM TEST DURING ENGINE BLEED AIR HEALTH CHECK TASK CARD. ACFT GROUNDED. REPLACED NR 1 ENGINE HIGH STAGE REGULATOR. LEAK/OPS CHECK OK, REF MM 36-11-07.SDR SIMA20141219002Shutoff Valve · faultyAFTER TAKEOFF LT ENG BLEED CAUTION PRESENTED ON EICAS. R & R LT ENG PRSOV IAW AMM 36-12-01. OPERATIONS CHECKED GOOD.SDR ASAA2014121909998Regulator · no testNR 1 ENGINE HIGH STAGE REGULATOR FAILED REVERSE FLOW DIAPHRAM TEST DURING ENGINE BLEED AIR HEALTH CHECK TASK CARD. ACFT GROUNDED. REPLACED NR 1 ENGINE HIGH STAGE REGULATOR. LEAK, OPS CHECK OK, REF MM 36-11-07.SDR CALA2014121801541Shutoff Valve · failedON TAKEOFF ROLL, LT ENG BLEED OFF, EICAS MSG. AFTER DEPARTURE RAN QRH V LIST, LIGHT REMAINED ILLUMINATED. NOTICED RESIDUAL BLEED AIR OF 15 PSI ON LT SIDE WITH LT ENG BLEED OFF. ALSO LT BLEED HPSOV STATUS MSG. ACCOMPLISHED ASCTU BITE PROCEDURE IAW MM 36-23-SDR USAA2014121800003Regulator Valve · faultyNUMBER 1 ENG SURGED AFTER TAKEOFF TURNED PACK OFF & SURGE STOPPED. REPLACED NR 1 ENG PRESS REGULATING VLV.SDR ASAA2014121609949Regulator · failedDUCT PRESSURE SPLIT EXCEEDS 20 PSI, LT SIDE 25 PSI, RT SIDE 47 PSI AT CRUISE FLIGHT F340. ACFT GROUNDED. ACCOMPLISHED T/C NG-36WC-00001. NR 1 ENG PCCV AND HSR FAILED THE SYS HEATH CHECK. REPLACED PCCV AND HSR REF AMM 36-12-02/401 AND AMM 36-11-07. OPS AND SDR ASAA2014121609948Shutoff Valve · failedDURING TAKEOFF, DUCT SPLIT NOTED PALT N1, N2 LT DUCT, RT DUCT SAT 2000 88.9 95.1 43-26 +5 302 KTS, 10000 91.4 96.1 45-27-0 M.79, 25000 96.4 97.3 45 30 -31 M.77, 37000 88.8 90.8 45-33-62. ACFT GROUNDED. PERFORMED NR 2 ENGINE BLEED AIR SYS HEALTH CHECK IAW T/C SDR CA141217014Duct · ruptured(CAN) LT ENGINE ANTI-ICE DUCT RUPTURE. DURING REPOSITION FLIGHT, LH ENGINE ANTI-ICE DUCT RUPTURED. THEY HAD IN FLIGHT "L COWL A/ICE" MESSAGE, SO THEY SWITCHED OFF ENG ANTI ICE AND DIVERTED TO AERODIENST. THE AIRCRAFT LANDED SAFELY BUT THE LEFT THRUST REVERSESDR AALA20141215001Regulator Valve · failedAIR INTERRUPT, DIVERTED, EMER NOT DECLARED & LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. DURING CRUISE A NR 1 ENG BLEED FAULT ECAM MSG WAS RECEIVED WITH LOSS OF BLEED AIR. POST FLIGHT REPORT SHOWED NR 1 ENG PRESS REGULATING VLV FAULT. R & R NR 1 ENG PRESS REGSDR SIMA20141213004Valve · failedREF ITEM NR 1 LOG PAGE 3653889 IAW REPEAT DESK NR 2 FAN AIR VLV NEEDS TO BE REPLACED. BLEED 2 OVER TEMP EICAS MSG & BLEED 2 POINTER IN RED RANGE. R & R NR 2 FAN AIR VLV IAW AMM 36-11-03, DID NOT FIX. SEE PIREP NR 1 LOG PAGE 3653889.SDR YENA20141209273Shutoff Valve · failedACFT DIVERTED DUE TO BLEED 2 FAILED INFLIGHT WITH BLEED 1 ON MEL. R & R NR 2 ENG NAPRSOV VALVE IAW AMM 36-11-03. FAILURE SUSPECTED OVERLOAD ON SINGLE BLEED OPERATION. OPS CHECK GOOD.SDR V0XD201412100267Attach Fitting · crackedENGINE START GND AIR SUPPLY ADAPTOR PULLED THROUGH ITS ATTACHMENT BOX HOUSING. R & R CONNECTOR BOX IAW AMM 36-17-03 & SRM 51-42-06.SDR SIMA20141207001Clamp · failedNR 2 BLEED LEAK CLIMBING OUT OF FL 20,000. FOUND AIR CONDITIONING DUCT BLOWN OFF. REPLACED CLAMP AT HEAT EXCHANGER IAW AMM 21-51-025. LEAK CHECKED GOOD.SDR YENA20141205269Valve · failedACFT DIVERTED DUE TO PRESSURIZATION ISSUE. CREW PERFORMED AN EMERGENCY DESCENT AFTER NOTING LOW PACK PERFORMANCE ON OUR REMAINING PACK BUT NORMAL CAB PRESSURE 6700 AT FL 300. WE RECEIVED CAB ALT WARNING W/CAB PRESS CLIMBING THRU 9600, INITIATED EMERGENCY DESDR SWIA2014120540291Valve · failedLEFT ENGINE BLEED CYCLED ON AND OFF. COULD NOT MAINTAIN PRESSURE. REPLACED THE LT PRSOV AND RT SAFETY VALVE. SYSTEM OPERATES NORMAL.SDR CA141204012Shutoff Valve · failed(CAN) DUAL BLEED HOT CAUTION LIGHT WHEN POWER WAS ADVANCED FOR TAKE-OFF. TAKEOFF REJECTED AT APPROXIMATELY 60 KTS. NO.2 ENGINE NACELLE PRESSURE SHUT-OFF VALVE REPLACED. NO FURTHER FAULT INDICATION ON ENGINE RUN UP.SDR YENA20141130268Bleed Air Sys · unknownAIRCRAFT DIVERTED DUE TO BLEED 2 PRESSURE FLUCTUATED RAPIDLY BETWEEN 9-70 PSI AT CLIMB AND CRUISE, THRUST SETTINGS RESET UNSUCCESSFUL. T/S SYS IAW FIM 36-14-00, CHECK TORQUE MOTOR SERVO LINES FOR LEAKS NO FAULT FOUND. R & R NR 2 ENG TORQUE CONTROL MOTOR 36-1SDR CA150421006Gasket · broken(CAN) DURING TROUBLESHOOTING AN AVIONICS/BLEED AIR PROBLEM, TEST AIR PRESSURE WAS INTRODUCED TO THE SYSTEM. A VERY LOUD RUSHING OF AIR WAS NOTED COMING FROM THE ENGINE AREA. IT WAS DISCOVERED THAT THE GASKET HAD BLOWN OUT OF THE BLEED AIR FLOW CONTROL VALVE.SDR CA141202028Clamp · broken(CAN) THERE ARE 4 V BAND SEGMENTS SPOT WELDED ON CLAMP. ONE V BAND SEGMENT BROKE OFF DUE TO SPOT WELD FAILURE FROM V BAND SEGMENT TO CLAMP STRAP.SDR UIEA2014112900619Valve · faultyLEFT ENG PRV EICAS & STATUS MSG ON TAKEOFF. R & R THE LT ENG PRV VLV IAW MM 36-11-18 IAW DMI 53104.SDR LOMA2014FA0000688Valve · leakingRIGHT 10TH STAGE WARNING LIGHT CAM ON DURING DECENT.SDR SWAA2014120134573Control Valve · faultyDIVERSION, DECLARED EMER DUAL BLEED TRIP, WOULD NOT RESET UNTIL 13,000'. PRESSURIZATION EVENT, MASKS DROPPED, EMER DESCENT. R & R LT ENG PRE COOLER CONTROL VLV IAW MM.SDR DXTA2014112405936Valve · failedBLEED AIR OVERHEAT LIGHT CAME ON AFTER TAKEOFF WITH A STRONG BURNING ODOR. PERFORMED HIGH POWER RUNS WITH NO DEFECTS NOTED IAW AMM 21-21-00. FOUND LEFT ENGINE SUPPLYING INSUFFICIENT AIR AT HIGH POWER. SELECTED THE BLEED AIR SOURCE FROM LT TO RT MULTIPLE TIMSDR SIMA20141123001Clamp · looseBLEED 2 LEAK ON CLIMB OUT, POWER WAS IN THE NOTCH IN CLIMB , ICING SYSTEMS WERE OFF. TIGHTENED CLAMP FOR STAB SUPPLY DUCT NEAR CROSS BLEED VLV. LEAK CHECKED GOOD IAW AMM CH 36-11-09.SDR CA141124006Shutoff Valve · failed(CAN) ON TAKEOFF, NR 1 AND 2 BLEED HOT CAUTION LIGHTS ILLUMINATED SIMULTANEOUSLY. TAKEOFF WAS ABORTED AT LOW SPEED AND THE AIRCRAFT RETURNED TO THE RAMP. APU BLEED AIR WAS ALSO NOT FUNCTIONING. MAINTENANCE REPLACED THE FLOW CONTROL SOV AND THE AIRCRAFT WAS SUBSDR SIMA20141122007O-Ring · damagedON CLIMB OUT IN CLB POWER RECEIVED AN ENG 2 BLEED LEAK WARNING, WOULD NOT EXTINGUISH. AFTER FOLLOWING ASSOCIATED CHECKLIST ENG 2 WAS SHUTDOWN IN FLIGHT IAW THE AOM 1 CHECKLIST. BLEED LEAK WARNING REMAINED ON EVEN AFTER THE ENG WAS SHUTDOWN. R & R O RINGS ATSDR UIEA2014112500608Shutoff Valve · malfunctionedDURING ENG RUN UP EICAS MSG LT ENG HPSOV. R & R LT HPSOV IAW AMM 36-11-07. OPERATIONS CHECKED NORMAL.SDR SIMA20141119002Shutoff Valve · failedABORTED TAKEOFF, LT ENG BLEED CAUTION APPEARED AS TAKING RNWY. R & R NR 1 ENG PRSOV IAW AMM 36-12-01. LEAK CHECKED, OPERATIONS CHECKED GOOD.SDR CA141124004Valve · defective(CAN) RT BLEED OVERHEAT LIGHT ON DURING TAKEOFF.SDR YENA20141116246Solenoid · leakingAIR RETURN DUE TO ENG 1 BLEED LEAK. ACCOMPLISHED TSM 36-22-00-810-803-A. FOUND THERMOSTAT SOLENOID 10HA1 LEAKING. R & R THE SOLENOID IAW AMM 36-11-55. LEAK AND OPS CHECKED NORMAL.SDR COEA2014111307801Switch · failedAIR TURN BACK. ON REACHING CRUISE ALTITUDE, THE ACFT LOST PRESSURIZATION. ELECTED TO RETURN. NO EMERGENCY WAS DECLARED. ACFT LANDED WITHOUT INCIDENT. AFTER TROUBLESHOOTING, IT WAS DETERMINED THAT THE CABIN PRESSURIZATION WORKED NORMALLY WHEN NR 1 ENGINE SDR RAIA201411120001Duct · disconnectedLOUD CLUNK NOISE FROM FLOOR BEHIND COCKPIT DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND FOUND BLEED DUCT DISCONNECTED. MAINTENANCE REPLACED NR 2 BLEED DUCT LINES FROM TAIL TO WING BOX. OPS AND LEAK CHECK GOOD.SDR SOKF20141113Bleed Air Sys · malfunctionedDURING CLIMB, THE ACFT RETURNED DUE BLEED 2 OVER PRESS MSG DISPLAYED ON CAS, STATION WAS ENTERED BLEED SYS AS DMI MEL IAW 36.00.00.1. THE ACFT RETURN TO NORMAL OPERATION.SDR VQI2014F00033Regulator Valve · failedCREW REPORTED A FOUL ODOR IN THE MID CABIN AREA. TECHS ACCOMPLISHED TSM 71-00-00-810-802 WITH NO FINDINGS AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE ACFT FLEW ITS NEXT LEG WITHOUT ANY REPORTED ODORS, ON THE FLIGHT, THE IN-FLIGHT CREW ONCE AGAIN REPORTED ASDR AALA20141111011Duct · crackedRETURNED, EMER WAS DECLARED & LANDING WAS UNEVENTFUL. ACFT WAS OVERWEIGHT. DURING CRUISE AT FL 310 FLIGHT ATTENDANT REPORTED EXCESSIVE & ABNORMAL VIBRATION FROM ROW 24 REARWARD TO THE AFT OF THE ACFT. NO ENG INDICATIONS, VARIED POWER SETTINGS TO ISOLATE VIBSDR HALA2014111000188Warning Message · activatedAFTER ENGINE SHUTDOWN, RECEIVED AN ECAM MESSAGE FOR AIR ENGINE 2 BLEED NOT CLOSED. SWITCHED ENGINE BLEED TO OFF AND INOPERATIVE, SYS ENG 2 BLEED REMAINED. RESET CIRCUIT BREAKER FOR BMC NR 2 AND AIRBLEED ENG 2. PERFORMED BITE BMC NR 2 IAW AMM 36-11-00-740-8SDR HALA2014111000187Line · unsecureAFTER ENGINE SHUTDOWN: ENG 2, BLEED FAULT. SECURED LINE TO FAN AIR VALVE IAW TSM 36-21-00-810-926-A. GROUND RUN NR 2 ENG FAULT DID NOT RETURN.SDR FDEA201411093595Duct · damagedDURING CLIMB OUT GOT EICAS RT ENG OVERHEAT. REFERENCE QRH. WHEN THROTTLE WAS RETARDED THROUGH 1.30 EPR, LIGHT WENT OUT WITH BLEED OFF. THIS WAS THE RT ENG. LIGHT REMAINED OFF THE REMAINDER OF FLIGHT. RETURNED TO BASE. R & R HP 2 DUCT ASSEMBLY 2 PC WITH N
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