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 AALA20150618027Clamp · leakingAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB, PACK TRIPPED OFF & THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. REMOVED & REPOSITIONED DUCT. REPLACED LOWER CLAMP & UPPER SHIMS IAW AMM 20-10-11. PERFORMED OPERATIONSDR WX0A2015061972671Clamp · unsecureTAIL COMPARTMENT TEMP HI ON AT 200 AFTER TAKEOFF. APU WAS RUNNING WITH AIR OFF. COMPLIED WITH QRH 21.4, LIGHT WENT OUT AFTER 1:15 DURING STEP 5. REFERENCE WO 00258905, PERFORMED TASK CARD 21-059-005, FOUND CLAMP LT HEAT EXCHANGER CLAMP LEAK RE-SECURED.SDR AALA20150613002Duct · leakingAIR INTERRUPT, RETURNED, EMER LANDING WAS DECLARED. LANDING WAS UNEVENTFUL & ACFT WAS OVERWEIGHT. CREW REPORTED THAT THE RT ENG OVERHEAT LIGHT ILLUMINATED. FOUND HP6 DUCT SEALING SURFACE DAMAGED & LEAKING. REPLACED DUCT. AN OPERATIONAL & LEAK CHECK WAS ACSDR WX0A2015061572661Clamp · looseTAIL COMPARTMENT TEMP HIGH ON TAKEOFF RIGHT AFTER V1. COMPLIED WITH QRH 21.4 DURING STEP 5, LIGHT WENT OUT AFTER 90 SECONDS. APU HAD BEEN RUNNING WITH APU AIR OFF. COMPLIED WITH TC 21-059-010 & 21-059-005, FOUND LEAKING CLAMP FROM DUCT TO INLET OF PRIMARY HSDR SIMA20150613002Damper · dirtyDURING PNEUMATIC ICE TEST, GOT WING ANTI-ICE FAIL. VLV SHOWED OPEN. CLEANED NR 2 WING BLEED AIR DAMPER IAW AMM TASK 36-11-11-100-801A. OPERATIONS CHECKED GOOD IAW AMM TASK 30-00-00-70802A.SDR ASAA2015061212079Valve · failedDUCT PRESSURE SPLIT RIGHT WAS 36 PSI, LEFT FLUCTUATED 16-20 PSI AT FL 39000. ACFT GROUNDED. ACCOMPLISHED TASK CARD NG-36WC-00001, ENGINE BLEED AIR SYS HEALTH CHECK. FOUND PRSOV & PRE-COOLER CONTROL VALVE TO HAVE FAILED. REPLACED PRSOV IAW AMM 36-11-04-000-8SDR HALA201506100106Filter · dirtyAPU BLEED FAULT, ECAM MESSAGE. OPS CHECKED BAD, RESISTANCE CHECK OK IAW TSM 49-62-00-810-841-A. REMOVED, CLEANED AND REINSTALLED APU BLEED VALVE FILTER ELEMENT IAW AMM 49-51-51-960-801A. OPS CHECKED GOOD.SDR AALA20150608012Valve · leakingAIR INTERRUPT, EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, TAIL COMPARTMENT HIGH TEMP INDICATION ILLUMINATED. INSPECTED TAIL COMPARTMENT & FOUND LT PRESS REGULATING VLV LEAKING. R & R VLV IAW AMM 21-31-01. ACCOMPLISHED CARD 36-95-14SDR WC72015060800003Sleeve · failedAFTER RE-INSTALLING THE LT AND RT HEAT EXCHANGERS THAT WERE REMOVED FOR CLEANING THE COUPLINGS WERE INSTALLED TO CONNECT THE DUCTWORK BETWEEN THE HEAT EXCHANGER AND THE ACFT. DURING THE LEAK CHECK OF THE HEAT EXCHANGERS WITH BLEED AIR APPLIED IT WAS FOUND THASDR ASAA2015060712014Regulator · failedDURING CLIMBOUT, OBSERVED RT PACK PRESSURE INDICATION FLUCTUATIONS, WITH THE LT PACK INDICATION STABLE AT 32 PSI. THE RT PACK NEEDLE WAS OCCILATING BETWEEN APPROXIMATELY 37 TO 46 PSI IN CYCLES OF APPROXIMATELY 1 TO 2 SECONDS. THIS OBSERVATION STAYED CONSISTENSDR ASAA2015060511999Regulator · failedAFTER NR 2 ENGINE START, TURNED ON RT PACK & AIR CONDITIONER BLEED AIR VALVE RT CIRCUIT BREAKER OPENED. ACFT GROUNDED. REPLACED NR 2 ENGINE BLEED AIR REGULATOR REF AMM 36-11-03-400-801. OPS AND LEAK CHECKED GOOD.SDR ASAA2015060411998Valve · failedRIGHT DUCT PRESSURE READS 5 PSI IN FLIGHT GROUNDED. RETURNED TO DEPARTURE. DIVERSION TIME - 38 MINUTES. PERFORMED ENGINE BLEED HEALTH CHECK REF. T/C NG-36WC-00001 IAW STEP .04, HIGH STAGE VALVE FAILED WRENCH CHECK. REPLACED NR 2 ENGINE HIGH STAGE VALVE IAWSDR AALA20150604007Regulator Valve · leakingAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. RETURNED, ACFT TAIL COMPARTMENT TEMP HIGH LIGHT. DURING TAKEOFF CREW NOTED A TAIL COMPARTMENT TEMP HIGH INDICATION. ACCOMPLISHED TAIL COMPARTMENT LEAK CHECK IAW MCM 36-95-14. R & R PRESS RSDR FDEA201505271637Pressure Switch · malfunctionedCRUISING AT FL370 RECEIVED AIR SYS OFF LEVEL 1, FOLLOWED BY AIR MAN NR 3 FAIL LEVEL 3. COMPLIED WITH CHECKLIST & LAND AT NEAREST SUITABLE. RELEASED FOR SERVICE IAW MEL 36-10-02-A. PERFORMED NR 3 PNEU SYS DECAY CHECK IAW AMM 36-00-04-5. 13 SECONDS FROM 30-2SDR HALA2015052600096Clamp · looseRIGHT WING LEAK ECAM UPON LANDING. FOUND RT PACK EXHAUST CLAMPS AND SLEEVES LOOSE, BLOWING HOT AIR ON O/H LOOP. 121HF. RESECURED RT PACK EXHAUST CLAMPS AND SLEEVES AT PACK EXHAUST PLEUM REF AMM 21-52-22. LEAK CHECK GOOD. RAN RT PACK FOR 20 MINUTES ON GROUND. SDR CALA2015052600452Line · brokenAFTER TAKEOFF NOTICED LEFT DUCT PRESS GAUGE CLOSE TO ZERO. FLIGHT DECK FELT VERY WARM, NO MASTER CAUTION OR FAILURE LIGHTS. AIR RETURN & TROUBLE SHOT ENG BLD REF 36-10-00. FOUND LINE TO PRSOV BROKEN. REPLACED SAME NR 1 ENG BLD. OPERATIONS CHECKED GOOD. ASDR CA150525013Bellows · cracked(CAN) DURING 125 HOUR INSPECTION, IT WAS NOTED THAT THE NR 1 ENG FIRE BOTTLE HAD BEEN ACTIVATED. UPON FURTHER INSPECTION, THE CAUSE WAS FOUND TO BE A CRACKED BELLOWS IN THE C6VW1026-3 BLEED AIR DUCT. DUCT WAS REPLACED & ACFT RETURNED TO SERVICE.SDR ASAA2015052011788Valve · malfunctionedFOLLOW-UP TO RECENT HISTORY OF DUCT PRESSURE SPLIT WITH LT PRESSURE LOW. ACFT GROUNDED. ACCOMPLISHED TC NG-36WC-00001, NR 1 ENG BLEED AIR HEALTH CHECK, NO DEFECTS NOTED. REPLACED PRECOOLER VALVE REF MM 36-12-02-400-801. REPLACED 390 DEGREE SENSOR REF MM 36-SDR AALA20150520001Check Valve · stuckAIR INTERRUPT, EMER NOT DECLARED. DURING CLIMB, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED WC 36-95-14 & FOUND RT TAIL COMPARTMENT OVERHEAT SENSOR DUCT CHECK VLV STUCK CLOSED. R & R CHECK VLV ASSEMBLY & RT & LT TAIL COMPARTMENT OVERHESDR SWAA2015052039855Valve · faultyDIVERSION, DECLARED EMER. CABIN ALTITUDE ABOVE 10,000 MSL WHILE CLIMBING THROUGH FL 350. R & R NR 1 ENG HIGH STAGE VLV IAW MM.SDR YENA20150516120Controller · failedDURING FLIGHT BLEED NR 1 EICAS MESSAGE, AFTER QRH WAS RUN THE MSG DID NOT EXTINGUISH. AN EMERGENCY WAS DECLARED. REPLACED AMS CONTROLLER 1 AND 2 AND PERFORMED APPLICABLE CK IAW 21-00-01-000-801A. ENG 1 AND 2 RUN AND NO DEFECT NOTED.SDR YENA20150516119Controller · failedDURING FLIGHT, BLEED NR 1 EICAS MESSAGE, AFTER QRH WAS RUN THE MSG DID NOT EXTINGUISH. AN EMERGENCY WAS DECLARED. REPLACED AMS CONTROLLER 1 AND 2 AND PERFORMED APPLICABLE CK IAW 21-00-01-000-801A. ENGINE 1 AND 2 RUN AND NO DEFECT NOTED.SDR FDEA201505161524Valve · faultyAT 340 NR 1 MANIFOLD FAIL LEVEL 3 ALERT WITH ASSOCIATED HIGH TEMPERATURE. CHECKED FAULT BALLS IN CAC AND NO FAULTS SHOWING OR LATCHED. PERFORMED RTS OFPSC1 AND NO FAULTS. PERFORMED DECAY CHECK PER AMM 36-00-05-5 AND DECAY CHECK GOOD. REMOVED AND REPLACED SDR ASAA2015051611749Valve · failedFOLLOW-UP TO RECENT HISTORY OF DUCT PRESSURE SPLIT WITH RT PRESSURE LOW. ACFT GROUNDED. WHILE ACCOMPLISHING NR 2 ENGINE BLEED AIR SYS HEALTH CHECK, TASK CARD NG-36WC-00001, FOUND PRE-COOLER CONTROL VALVE FAILED STEP F AND HIGH STAGE VALVE FAILED IAW STEPS J ASDR CALA2015051593791Duct · disconnectedDIVERT DUE TO RT BLEED DUCT LEAK EICAS MSG. FOUND AIR DUCT DISCONNECTED AT R2. ADOMG EDGE FLAP PDU. R & R SEAL & SECURED DUCT IAW AMM 27-81-03 201. LE FLAP OPERATIONS CHECKED OK.SDR SIMA20150511002Duct · leakingBLEED 1 LK ON CLIMB OUT. COMPLIED WITH EPC & AOM 1. REPAIRED ALL BLEED LEAKS IN CARGO COMPARTMENT, LT ENG PYLON & SERVICE MANIFOLD AREA IAW AMM 36-11-09 & 36-11-10. OPERATIONS CHECKED BLEED NR 1 SYS IAW AMM 36-00-00 & NO LEAKS OR FAULTS NOTED AT THIS TIMESDR ASAA2015050711655Valve · failedDUCT SPLIT OBSERVED AT FL380 RT DUCT 40PSI LT DUCT 20PSI. ACFT GROUNDED. ACCOMPLISHED T/C: NG-36WC-00001, STEPS 1 THRU 5 ON ENG 1. REPLACED PRE-COOLER VALVE REF MM 36-12-02. REPLACED HIGH STAGE VALVE REF MM 36-11-06. COMPLIED W/ TC: NG-36WV-00001, STEP 6. OPSDR DJSA20150506001O-Ring · failedFIRE WARNING AUDIBLE TONE ENGAGES WITH NO ANNUNCIATOR LIGHT VERIFYING FIRE. FOUND BLEED AIR LEAK AT RT FUEL HEATER IN PYLON. RE-PACKED AFT FUEL HEATER WIGGINS FITTING.SDR P5CA2015050700038Controller · faultedLEFT ENGINE PRV STATUS MESSAGE. FIM PROCEDURE 36-10, FAULT TREE 847, CARRIED OUT. LEFT ENGINE PRV CONTROLLER REPLACED & AMP; TESTED IAW AMM 36-11-19 P 401, LEFT BLEED SYSTEM SERVICEABLE.SDR UIEA2015050600263Unknown · malfunctionedAT TOP, FL 370 DUCT PRESS SUDLING DROP TO 7 PSI WHEN THROTTLES RETARTED TO IDLE. CABIN ALTITUDE ROSE TO 9300 FT & STABILIZED. WITHIN 5 - 10 SECONDS PRESSURIZATION OF CABIN BEGAN TO RETURN TO NORMAL, NO OTHER NON-NORMAL NOTED. PERFORMED BITE TEST OF SYS, BITSDR RU3A20150505011Tube · looseRIGHT BLEED AIR FAIL LIGHT ILLUMINATED IN FLIGHT. EVA TUBING COMING LOOSE, CONNECTED SUPPLY LINE AT DISTRIBUTION MANIFOLD & REPLACED CLAMP.SDR CALA2015050400368Clamp · brokenSHORTLY AFTER TAKEOFF FLIGHT ATTENDANT CALLED COMPLAINING ABOUT A VERY LOUD NOISE UNDER THE FLOORBOARDS IN THE AFT GALLEY. FLIGHT CREW NOTICED EAR POPPING & HIGHER THAN NORMAL CABIN DIFFERENTIAL. FLIGHT BURNED OFF FUEL & DIVERTED. TROUBLE SHOT TO BROKEN CLASDR ASAA2015050311617Valve · failedON CLIMBOUT, RT DUCT PRESSURE VARIED BETWEEN 38-44, PSI AT 8000', 90.4 N1 SAME AT 13000 FEET 95 PERCENT N1. AT FL 290 RT DUCT PRESSURE STEADY AT 42 PSI 98 PERCENT, N1. ACFT GROUNDED. ACCOMPLISHED T/C NG-36WC-00001 HEALTH CHECK ON NR 2 ENGINE. FOUND HIGH STAGESDR ASAA2015050211608Valve · failedDURING CLIMBOUT, LT DUCT PRESSURE READ 41, RT DUCT PRESSURE 22, AT TOP OF CLIMB AND POWER IN CRUISE SETTING RT PACK 21, LT PACK 44, 2 HOURS INTO FLIGHT RT 40, LT PACK 42. ACFT GROUNDED. TASK CARD COMPLIED WITH. REPLACED NR 2 ENGINE PRECOOLER CONTROL VALVE REFSDR CA150501001Clamp · failed(CAN) DURING THE CLIMB, CREW REPORTED AN ANTI-ICE DUCT WARNING MESSAGE AND A DUCT FAIL LIGHT ON THEIR ICE PROTECT PANEL. THE DECISION WAS MADE TO RETURN TO DEPARTURE POINT FOR MAINTENANCE ACTION. MAINTENANCE ACTION FOUND SUBSTANTIAL LEAK NOTED DURING ENGINESDR AALA20150505011Thermostat · failedDURING CLIMB THE RT PACK BLEED FAULTED & WOULDN`T RESET. EMERGENCY DECLARED & FLIGHT LANDED WITHOUT INCIDENT. R & R RT ENGINE 450 DEGREE THERMOSTAT IAW AMM 36-11-05.SDR CA150427013Control Unit · failed(CAN) SHORTLY AFTER TAKEOFF FROM POINT A, CREW RECEIVED LT WING ANTI-ICE DUCT WARNING MSG. DISPATCH & MOC WERE CONTACTED & THE QRH WAS FOLLOWED. AFTER WEIGHING, AVAILABLE OPTIONS, DIVERSION INTO POINT B WAS DEEMED SAFEST OPTION AS THE ACFTT WOULD NOT BE ABLESDR CALA2015041600289Valve · unserviceableRIGHT ENG OVERHEAT PERFORMED CHECKLIST & LIGHT WENT OUT. HAD A PNEUMATIC DUCT SURGE PRIOR TO THIS MSG & THE STATUS STRUT OVERHEAT MSG. TROUBLE SHOT IAW FIM26-12-00, FOUND POSSIBLE LEAK DOWNSTREAM OF HPSOV. LOCKED HPSOV IN CLOSED POSITION IAW MEL 3611R. REFSDR HALA2015041400059Circuit Card · damagedRT ENGINE BLEED PSI AT 5 PSI DURING CLIMB. IT WAS NORMAL DURING GROUND OPERATIONS. R & R RT ENGINE BLEED AIR CONTROL CARD M860 IAW AMM 36-11-12-404-026. OPS CHECKS GOOD.SDR F3LA2015041501130Duct · failedDISCREPANCY, ENG 2 FIRE, AIR TURN BACK 1839 Z. ENG 2 FIRE INDICATION ON TAKEOFF AFTER THRUST REDUCTION ON ENG 2 IAW ECAM. FIRE INDICATION CHANGED TO AMBER, ENG 2 SHUTDOWN. ENG 2 SHUTDOWN COMPLETED. FOUND HIGH PRESS BLEED DUCT BROKEN CAUSING ENG 2 FIRE INDISDR DXTA201504136005Sleeve · leakingWHILE CLIMBING THROUGH 15,000', BOTH RED MWS LIGHTS STARTED FLASHING FOLLOWED BY REAR BAY OVERHEAT LIGHT. INITIALLY REDUCED CLIMB & REDUCED POWER. AS POWER REDUCED, REAR BAY OVERHEAT LIGHT EXTINGUISHED. NO VISIBLE SMOKE OR ODOR IN COCKPIT OR CABIN. PERFORMSDR AALA20150411005Valve · faultyDURING CLIMB LT ENGINE BLEED OFF & HOT BURNING ODOR IN COCKPIT & CABIN. DIVERTED. R & R LT ENG HIGH STAGE PILOT VALVE IAW MM 36-11-08. PERFORMED OPERATIONAL & LEAK CHECKS. ACCOMPLISHED SHED HIGH POWER RUN. NOTED NO BURNING SMELLS THROUGHOUT THE CABIN.SDR CA150413003Duct · leaking(CAN) AFTER GETTING AIRBORNE, THE ACFT ENCOUNTERED AN AIR WING LEAK IN CRUISE. IN CONSULTATION WITH MAINTENANCE, THE FLIGHT CREW RETURNED THE ACFT. THE LANDING WAS UNEVENTFUL WITH NO ADVERSE PASSENGER REACTION. THE ACFT WAS TAKEN OFFLINE AND A NEW ACFT WAS USDR ASAA2015041011296Valve · failedNR 1 BLEED TRIP OFF LIGHT ILLUMINATED DESCENDING THROUGH 380. ACCOMPLISHED BLEED TRIP OFF CHECKLIST. LIGHT REMAINED ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED T/C NG-36WC-00001. FOUND PCU VALVE & PRSOV FAILED. R & R PRECOOLER CONTROL VALVE REF AMM 36-12-02 OSDR CA150409007Duct · cracked(CAN) BLEED HOT CAUTION LIGHT INFLIGHT. RT FIREBOX DUCT PN 14400-115 FOUND CRACKED. EARLIER DUCT LEAK SWITCH WAS REPLACED FOR TROUBLESHOOTING.SDR QXEA2015040800189Duct · damagedNR 2 BLEED HOT CAUTION IN FLIGHT. RESET UNSUCCESSFUL. CAME BACK ON AFTER ABOUT 15 MINUTES. IT CAME BACK ON, WITH NR 2 BLEED SWITCH OFF, FOR APPROX 70 PERCENT TRQ. EXTINGUISHED AGAIN WHEN POWER PULLED BACK. RETURNED TO FIELD, LANDING UNEVENTFUL. REPLACED NRSDR RJEF20150410001Selector Switch · faultyDURING ENG START, PREVIOUS TO DEPART AS FLIGHT TAI 409, THE FLIGHT CREW REPORTED AIR CROSS BLEED FAULT, DUE TO FAILURE THE ACFT REMAINED ON GND FOR MX. PERFORMED FAULT ANALYSIS IAW TSM 36-12-00-810-802-A. REPLACED THE CROSS BLEED VLV SELECTOR SWITCH 3HV IAW SDR QXEA2015040700183Shutoff Valve · malfunctionedNR 2 BLEED HOT CAUTION, RAN CHECKLIST, LIGHT STAYED ON, DIVERTED, UNEVENTFUL LANDING. INTERROGATED CDS AND FOUND FAULTS 1007, 7006, 4105, 4108. C/W FIM TASK 36-10-00-810-801. R & R NR 2 NACELLE SHUTOFF VALVE IAW AMM 36-11-19, TASK 36-11-19-000-801, 36-11-19-SDR CA150406005Seal · leaking(CAN) FLIGHT DIVERT DUE BLEED SNAG. A TECH STOP WOULD BE REQUIRED AS THE CREW ADVISED THEY WOULD BE AT FL300 THE ENTIRE FLIGHT. THE ACFT WOULD BE GROUNDED ONCE IT LANDED. THE DECISION WAS MADE TO DIVERT. FLIGHT LANDED OVERWEIGHT BY 8.6 KGS. FOUND DUCT LEASDR CA150406002Duct Seal · failed(CAN) DURING THE FLIGHT THE CREW REPORTED A WING ANTI-ICE FAULT AND ELECTED TO DIVERT DUE TO POSSIBLE ICING CONDITIONS. RESOLUTION LT WING ANTI-ICE DUCT SEAL AT RIB NR 9 REPLACED IAW AMM 30-11-42 & 30-11-51. LEAK CHECK AND FUNCTIONAL TEST C/O, NO FAULT FOUND.
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