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 WX0A2015040872520Gasket · leakingTAIL COMPARTMENT HIGH MSG ILLUMINATED WHILE CLIMBING THROUGH FL 280 INTERMITTENT UNTIL LEVEL OFF WITH SUBSEQUENT THROTTLE DECREASE FOLLOWED QRH & CONTINUED FLIGHT. ACCOMPLISHED WO 251051 FOUND LT THERMOSTAT BASE GSKT LEAKING REPLACED BASE GASKET REF 36-00-00 SDR AALA20150331006Shutoff Valve · inoperativeAIR INTERRUPT, DIVERTED & EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. LT BLEED OFF LIGHT ILLUMINATED CLIMBING THROUGH 10,000 FEET. COMPLETED QRH SINGLE PACK. REPLACED NR 1 ENG PRSOV IAW AMM 36-11-09.SDR ASAA2015033011154Regulator · failedLT DUCT PRESS LOW ON CLIMBOUT AND CRUISE. ACFT GROUNDED. ACCOMPLISHED NR 1 ENGINE BLEED AIR SYSTEM HEALTH CHECK REFERENCE TC NG 36WC-00001. R & R NR 1 ENGINE BLEED AIR REGULATOR IAW AMM 36-11-03-400-801. PERFORMED GROUND VERIFICATION IAW AMM TASK 36-11-00-SDR FDEA201503281121Regulator Valve · faultyDURING DESCENT AT APPROX 12,000 FEET TURNED ON ENG & WING ANTI-ICE. IMMEDIATELY NR 1 AIR SYS SHOWED A NR 1 ENG MANIFOLD FAILURE. NR 1 AIR SYS INDICATED RED & NR 1BLEED AIR INDICATED CLOSED. WITH NR 1THROTTLE IDLE, NR 1 AIR SYS REMAINED RED UNTIL TAXI TO GASDR YENA20150327063Pressure Switch · malfunctionedAIR RETURN DUE TO BLEED 1 OVER PRESSURE. COULD NOT RESET VIA QRH. CMC FAULT CODE 36146225AM1. PERFORMED FIM TASK 36-14-00-810-817-A. FAILURE OF THE OVER PRESSURE SWITCH. R & R 1 BLEED OVER PRESSURE SWITCH IAW AMM 36-14-01-000-801-A & 36-14-01-400-801-A. OPS SDR CA150324005Duct · cracked(CAN) CREW REPORTED A RT ENVIRO FAIL LIGHT. THE ENVIOR FAIL LIGHT SNAG WAS RECTIFIED, BUT DURING THE TROUBLESHOOTING OF THIS SNAG MAINTENANCE FOUND A DUCT ASSEMBLY CRACKED FROM THE FLANGE. ALSO, A HOLE WAS ALSO DISCOVERED IN THE EVA TUBING ADJACENT TO THE CRASDR SWAA2015032337733Shutoff Valve · faultyDECLARED EMER, CABIN ALTITUDE WARNING HORN SOUNDED AT 370. CABIN ALTITUDE INDICATION 10,500' & CLIMBING AT 700' PER MIN. EMER DECLARED WITH EMER DESCENT. NO DEGRADED SYS INDICATIONS WERE INDICATED ON PRESS CONTROLLER. CABIN CONTINUED UP TO 13,800' DURING DSDR DJFA20150319001Controller · failedDURING FLIGHT, A BLEED 1 LEAK CAS MESSAGE ILLUMINATED. DIVERTED & FOLLOWING THE CHECK LIST, SHUTDOWN THE NR 1 ENGINE. AN EMERGENCY WAS DECLARED & THE ACFT LANDED WITHOUT INCIDENT. THE AMS, AIR MANAGEMENT SYS, CONTROLLER WAS REPLACED. OPS CHECKED GOOD & THESDR ASAA2015031711045Tube · looseAT TOP OF CLIMB, AT 350, LT DUCT PRESSURE WAS 22, RT WAS 46PSI. AT TOP OF DESCENT THEY READ LT=31, RT=46PSI. ACFT GROUNDED. ACCOMPLISHED TASK 36-00-00-860-807 NR 1 ENGINE BLEED AIR SYS ABBREVIATED TROUBLESHOOTING FOUND CONTROL LINE FROM HIGH STAGE REGULATORSDR FDEA201503170981Duct · leakingAIR SYS MANUAL MODE, 2000 AGL NR 3 PACK SHUTDOWN, MANIFOLD NR 3 DEPRESSURIZED. AIR SYS OFF ALERT. ON DECAY CHECK , FOUND PNEUMATIC LEAK FROM RT FWD LOWER CARGO COMPARTMENT, AFT OF NR 3 AC FLOW CONTROL VLV, BETWEEN BULKHEAD. R & R DUCT ASSEMBLY IAW AMM 36-23SDR SIMA20150317006Thermostat · faultyBLEED 2 OVER TEMP DURING CLIMB THRU 10000 FT IN ICING CONDITIONS, REF FIM 36-11-00-810-804. PERFORMED INSPECTION GVI OF PRE COOLER REGION IAW AMM 36-11-04. CLEANED FAN AIR VLV FILTER AMM 36-11-03. R & R FAN AIR THERMOSTAT IAW AMM 36-11-06. OPERATIONS CHECSDR HALA2015031805007Valve · malfunctionedAIRCRAFT RETURNED TO DEPARTURE DUE TO AIR NR 1 ENGINE BLEED FAULT PRIOR TO ENTERING ETOPS AIR SPACE. REPLACED NR 1 ENGINE PRV.SDR CA150313002Valve · failed(CAN) NR 1 AND NR 2 BLEED HOT CAUTION LIGHTS ILLUMINATED ON TAKEOFF ROLL. T/O ABORTED. BLEED WERE ON/MIN FOR T/O. WHEN BLEEDS WERE TURNED OFF IAW CHECKLIST, BOTH LIGHTS EXTINGUISHED. CDS INDICATED LT, RT FCV, LHPSOV, LT NAPRSOV IN PRESENT FAULTS. VERIFIED FCSDR AALA20150313003Controller · faultyAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. PASSING 6000 FEET ON CLIMB OUT, LT ENG BLEED & LT PACK OFF EICAS MSGS WITH LT PACK OFF LIGHT ALSO ON. REPLACED LT ENG 450 DEGREE TEMP SENSOR IAW AMM 36-11-13. REPLACED REVERSE FLOW CHECSDR HALA2015031000033Regulator Valve · unknownETOPS SIGNIFICANT EVENT, LT ENGINE PRV EICAS ILLUMINATED ON CLIMBOUT. R & R LT ENGINE PRESSURE REGULATING VALVE IAW AMM 36-11-18-004-001-002, AND AMM 36-11-18-404-017-002. LEAK AND OPS CK OK. RAN ENGINE IAW AMM 71-00-00. BLEED OPS NORMAL. LT ENGINE PRV DSDR SIMA20150309002O-Ring · damagedBLEED 1 LEAK CLIMBING THRU 13000. IAW AOM VOL 1, IT EXTINGUISHED. FOLLOWING DUCT LINES INSPECTION IAW AMM 36-11-09 FOUND O RING 21 LEAKING. R & R O RING, LEAK CHECKED GOOD, RAN PAX K1 FOR 2 HRS, NO BLEED LEAK.SDR ASOA2015030412316Duct · leakingWHILE CLIMBING THRU FL250, RECEIVED LT BLEED DUCT WARNING MSG FOLLOWED BY TOTAL PRESSURIZATION FAILURE, EXECUTED EMERGENCY DESCENT TO 10K, FOLLOWED QRH AND DIVERTED. ENROUTE, ACFT DIVERTED DUE TO MAINTENANCE. WING ANTI-ICE DUCT OPS AND LEAK CHK GIID IAW AMM SDR RAIA201503010004Control Valve · inoperativeBLEED 1 OVERTEMP EICAS MSG IN ICING CONDITION DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND REPLACED NR 1 ENGINGE FAN AIR CONTROL VALVE, OPS CHECK GOOD.SDR ASAA2015022610809Shutoff Valve · failedWITH NR 1 ENGINE RUNNING, TRYING TO START NR 2 ENG THE APU AIR DOES NOT RISE ABOVE 20 PSI - WITH ISOLATION VALVE SWITCH IN AUTO OR OPEN, DOES NOT AFFECT THE PRESSURE, STILL 20 PSI, MAKING NR 2 ENG SLOW TO SPOOL. ACFT GROUNDED. FOUND PRSOV ON NR 1 ENG DEFECTIVSDR SIMA20150224005Duct · crackedNUMBER 2 ENG 14TH STAGE DUCT FROM CUSTOMER SERVICE PANEL CRACKED AT ANTI-ICE VLV END. R & R 14TH STAGE DUCT AT NR 2 ENG CUSTOMER SERVICE PANEL TO ANTI-ICE VLV IAW AMM 36-11-09. LEAK CHECKED GOOD.SDR SIMA20150224003O-Ring · damagedWHILE CLIMBING THROUGH FL220 BLD 2 LEAK MSG ON EICAS, EPC & AOM 1 PROCEDURE COMPLIED WITH. R & R O RINGS AT JOINT 12 IAW MM 36-11-10. PERFORMED LEAK CHECK OF BLD SYS IAW MM 36-00-00. NO LEAKS NOTED.SDR COZA20150226047Sensor · defectiveON DECENT, RT DUCT PRESSURE INDICATED 15 PSI WITH LT PRESSURE AT 40 PSI. BLEED TRIP LIGHT ILLUMINATED. REPLACED PRE-COOLER CONTROL VALVE SENSOR AND BLEED SYSTEM OPERATED NORMALLY.SDR COZA20150226046Control Valve · inoperativeON DECENT, RT DUCT PRESSURE INDICATED 15 PSI WITH LT PRESSURE AT 40 PSI. BLEED TRIP LIGHT ILLUMINATED. REPLACED PRE-COOLER CONTROL VALVE AND BLEED SYSTEM OPERATED NORMALLY.SDR USAA2015022300009Valve · stuckRETURNED, ON CLIMB OUT INTERMITTENT ENG 1 NAC TEMP 300 DEGREES. ENG 1 HP AIR VLV STUCK OPEN.SDR USAA2015022300008Relief Valve · stuckRETURNED, ON CLIMB OUT INTERMITTENT ENG 1 NAC TEMP 300 DEGREES. ENG 1 HP AIR VLV STUCK OPEN. REPLACED ENG 1 OVER PRESS VLV. SDR SUBMITTED IN CONJUNCTION WITH SDR USAA2015022300009.SDR SIMA20150221005Clamp · failedDURING PNEUMATIC ICE TEST IN AIR BLD 2 LEAK WITH ASSOCIATED LOUD BANG HEARD IN COCKPIT & IN CABIN. FOUND RT BLEED DUCT JOINT 9 SEPARATED. INSTALLED NEW O RINGS & CLAMP IAW AMM 36-11-00. LEAK & OPERATIONS CHECKED GOOD IAW AMM 36-00-00.SDR CA150220001Bleed Valve · failed(CAN) THE FLIGHT DEPARTED WITH 1 ENG. BLEED INOP UNDER MEL. AFTER DEPARTURE, THE REAMING ENGINE BLEED BECAME UNSERVICEABLE. THE FLIGHT LANDED BACK WITHOUT FURTHER INCIDENT. NR 1 NAPRSOV REPLACED 36-11-03 PB401. ENG RUN CARRIED OUT - CK`D SERV.SDR FDEA201502190548Line · failedRECEIVED AIR MANIFOLD ONE FAIL ALERT. BLEED ONE TURNED OFF & ALERT WENT AWAY. RETURN TO FIELD. TEMP COMING OUT OF BLEED ONE AT THE TIME WAS 210 C. FOUND SENSE LINE TO NR 1 FAN AIR VALVE BAD. R & R SENSE LINE.SDR SIMA20150216006O-Ring · damagedON DEPARTURE, CLIMBING THROUGH 10,000 FEET, WE RECEIVED EICAS INDICATION BLD 1 - 2 LEAK. LEAK LIGHT IN RED, BLD BUTTONS DID NOT LIGHT. FOLLOWED AOM PROCEDURES & MADE AN EMER LANDING, INDICATION REMAINED AFTER ENG SHUTDOWN. AT JOINT 14 FOUND THERMAL SWITCH WISDR IPXA2015021685969Shutoff Valve · inoperativeINSPECTION TYPE: E, TOP WAN NR 2253636, ACCOMPLISHED SEE LP 823263, ITEM 2.SDR CA150213003Hose · failed(CAN) AT TOP OF DESCENT THE PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED FOLLOWED BY THE ALTERNATE LIGHT. THE QRC DIRECTED THE FLIGHT CREW TO SWITCH TO ALTERNATE MODE. APPROXIMATELY 30 SECONDS LATER THE AUTO FAIL LIGHT ILLUMINATED AGAIN. THE CREW HAD TO CONTROL SDR RAIA201502110001Seal · failedLOUD POP, BLEED 1 LEAK, APU BLEED LEAK, BAGGAGE SMOKE LIGHT AND PRESSED BAG EXT BUTTON, RETURN TO BLOCK. MAINTENANCE INSPECTED AND REPLACED BLEED DUCT SEALS AT NR 2 LOCATION, REPLACED THERMAL SWITCH, OPS AND LEAK CHECK GOOD, REPLACED BOTH BAGGAGE FIRE BOTTLESSDR SIMA20150210007Clamp · looseBLEED 2 OVERTEMP AFTER EXITING ICING. COMPLIED WITH FIM 36-11-00-810-804-A BLOCK 1. PERFORMED VISUAL INSPECTION OF PRE COOLER AREA & FOUND LOOSE CLAMP AT ENG SIDE TUBE ASSEMBLY. REPOSITIONED & TIGHTENED IAW AMM 36-11-04 & REMOVED & INSTALLED FAN AIR VLV FILSDR SIMA20150207002Control Panel · failedBLEED 2 LEAK WARNING MSG ON CLIMB OUT. MSG EXTINGUISHED AFTER COMPLYING WITH EMER PROCEDURES HOWEVER, ACFT STARTED DEPRESSURIZING AFTER COMPLYING WITH PROCEDURES. R & R PNEUMATIC CONTROL PANEL IAW AMM 20-13-10. COMPLIED WITH TEST OF BLEED SYS IAW AMM 36-00-SDR SIMA20150206001O-Ring · damagedBLEED LEAK 2 WARNING MSG ON CLIMB OUT ABOVE FL200. MSG EXTINGUISHED AFTER COMPLYING WITH EMER PROCEDURE. RETURNED NOT OVER WEIGHT LANDING. LANDING WEIGHT 39,000 LBS. FOUND LEAK AT JOINT 10. R & R ORINGS & SLEEVE IAW AMM 36-11-09. R & R BLEED SYS FOR AN HSDR DXTA2015020605975Hose · meltedELECTRICAL INSULATION ODOR WAS SMELLED IN CABIN AREA APPROX 30 MINUTES INTO FLIGHT. DECLARED EMER, RAN QRC & QRH CHECKLISTS. THERE WAS NO SMOKE. UPON LANDING, ALONG WITH FIRE INSPECTORS DID NOT SMELL ANYTHING BUT THEY INDICATED OUTLETS WERE STILL WARM. APSDR SIMA20150130009Duct · crackedPNEUMATIC DUCT BETWEEN LT SIDE FUSELAGE BLEED AIR JOINT 9 & 11 IS CRACKED. R & R IAW AMM 36-11-09.SDR UIEA2015012700038Seal · leakingBLEED AIR DUCT LEAKING, LT WING LE INBD OF NR 1 PYLON. REMOVED & REINSTALLED NR 1 PYLON BLEED AIR DUCT INBD LT IAW AMM 36-11-01. LEAK CHECKED, NO LEAKS NOTED.SDR ASAA2015012510417Control Valve · failedTAKE OFF POWER APPLIED SUDDEN AIR SURGE FROM ACFT, DURATION 5 SEC, AT ALTITUDE SAME THING, DURATION CONTINUOUS. DUCT PSI: CLIMBOUT L35, R20. LEVEL FLIGHT 30, 28 AFTER THAT 38, 42. ACFT GROUNDED. PERFORMED FIM TASK 36-10, TASK 804 ON NR 1 ENGINE STEPS E. (16SDR SWAA2015012636108Control Valve · failedDIVERSION, RT BLEED TRIP OFF LIGHT ILLUMINATED. RESET IAW QRH A-7, IMMEDIATELY CAME ON AGAIN. RT PACK SWITCH SELECTED OFF IAW QRH. FOUND PRE COOLER CONTROL VLV FAILED. R & R PRE COOLER CONTROL VLV IAW MM.SDR GRTA2015012900001Tube · rupturedRIGHT BLEED FAIL LIGHT ILLUMINATED IN FLIGHT. POST FLIGHT VISUAL INSPECTION REVEALED A RUPTURED BLEED-AIR-WARNING TUBE LOCATED IN THE RT WING JUST INBD OF THE NACELLE. NO EVIDENCE OF A BLEED AIR LEAK IN THE RT BLEED AIR SUPPLY LINE WAS EVIDENT.SDR CA150121006Shaft · failed(CAN) DURING A STUDENT IFR FLIGHT IN VFR CONDITIONS THE INSTRUCTOR NOTED THAT THERE WASN`T ANY INSTRUMENT PRESSURE FROM EITHER ENGINE. UPON INSPECTION WE NOTICED THAT BOTH PRESSURE PUMPS HAD SHEARED THEIR SHAFTS. WE COULD NOT FINE ANY OBSTRUCTIONS. ALL LINES WSDR AALA20150120006Shutoff Valve · deactivatedAIR INTERRUPT, DIVERTED & EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE THE RT BLEED VLV INOPERATIVE LIGHT ILLUMINATED. UPON INSPECTION THE RT PRSOV WAS FOUND DEACTIVATED & THE RT HPSOV ACTIVATED WITH MEL36-3A APPLIED. DEACTIVATED THE SDR SIMA20150120001Valve · failedWING ANTI-ICE FAIL & STAB ANTI-ICE FAIL DURING SINGLE BLEED OPERATION IN ICING CONDITION, FOLLOWED BY ICE CONDITION ANTI-ICE INOPERATIVE WARNING. PERFORMED OPERATIONAL TEST IAW MM 30-00-00. OPERATIONS CHECK GOOD. BLEED 1 OVER TEMP WARNING DURING CLIMB, TROUSDR CWQR20150119001Tube · crackedDURING A SCHEDULED INSPECTION WE FOUND THE BLEED AIR, AIR TUBE MOUNTING FLANGE CRACKED 1/3 THE WAY AROUND THE BLEED AIR TUBE ASSEMBLY. ABOUT 2.5 INCHES LONG. THIS CRACKED FLANGE ATTACHES TO THE APU CONTAINMENT BOX & IS THE PASS THROUGH FOR THE BLEED AIR TUBISDR YENA20150117006Controller · failedAT FL 270, NR 1 BLEED FAIL EICAS MESSAGE WITH AMBER X OVER NR 1 BLEED THIS OCCURRED AFTER ENTERING ICE CONDITION WITH EQUIPMENT ON. NR 1 BLEED WAS RESET, BLEED NR 1 FAILED MSG REMAINED. AMBER X OVER THE VALVE CLEARED AND BLEED PRESSURE RETURNED TO 40 PSI. CSDR CA150114008Duct · ruptured(CAN) DURING CLIMB OUT NR 3 ENGINE FIRE INDICATION APPEARED, AFTER FOLLOWING CHECKLIST PROCEDURE NR 3 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO EWR AIRPORT. FIRE INDICATION WENT AWAY AS THROTTLE WAS RETARDED TO IDLE AS PART OF ENGINE SHUT-DOWN PROCEDURE. MSDR SWAA2015011535747Control Valve · faultyDECLARED EMER DUAL BLEED TRIPPED. R & R NR 2 PRECOOLER CONTROL VLV IAW MM.SDR SWAA2015011535746Control Valve · faultyDECLARED EMER DUAL BLEED TRIPPED. R & R NR 1 PRECOOLER CONTROL VLV IAW MM.SDR AALA20150106020Duct · crackedAIR INTERRUPT, DIVERTED & EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE TAIL COMPARTMENT OVER TEMP WARNING ILLUMINATED. ACCOMPLISHED TAIL COMPARTMENT LEAKS MCM 36-95-14 FOUND CRACKED DUCT. R & R DUCT & PERFORMED MCM CARD 36-95-14.
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