JASC 3150
Service difficulty reports · 3,981
Reports filed under 3150 · Central Warning, 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 = '3150' 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 = '3150' 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 HALA2019022100058Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 FUEL FILTER CLOG ECAM AMBER CLOG ILLUMINATED UNDER F.USED. REMOVED INSPECTED AND REINSTALLED RT ENGINE FUEL FILTER ELEMENT PER AMM 73-11-41. NO DEBRIS NOTED ON FILTER. ACCOMPLISHED TSM 73-21-79 FOR FUEL FILTER CLOGGED MESSAGESDR ASMF2019042309Warning Message · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE MESSAGE IN EICAS AND STATUS ELEC WERE SHOWN. MAINTENANCE PERSONNEL PERFORMED FIM DMC-B787-A-24-20-F8-64A-421A-A PROCEDURE, SHOWING FAILURE CODE 24-13412; SO THE FIM DMC-B787-A-24-20-F8-64A-421A-A PROCEDURSDR AALA2019021109009Computer · faultyMASTER WARNING LIGHT ILLUMINATED FOUR DIFFERENT TIMES IN FLT, NO CHIME, IT RESETS ITSELF AFTER 4-6 FLASHES. THE AIRCRAFT WAS GROUNDED. REPLACED THE NR 1 AND 2 FWCS, OPERATIONAL TESTED IAW 31-53-34 ACCOMPLISHED LAND CAT 3 CAPABILITY TEST REF; 22-97-00-710SDR HNAA2019020400033Relay · malfunctionedPDIS 603 31-50 1983712 01FEB19 PHL CLOSE
NO TAKE OFF CONFIG WARNING DURING TAKE OFF.
FACT 01FEB19 15:23 PHL
T/S IAW EMB FIM 31-51-00-810-804A BLOCK 1. R/R RELAY
K0212 IASDR DXTA2019011501913Warning System · false activationSWPS FAULT YELLOW CAS ILLUMINATED - DURING INITIAL DESCENT FROM CRUISE FLIGHT, WE HAD MULTIPLE CAS FAIL AND FAULTS LIGHTS INCLUDING PTRIM BKP FAIL, SWPS FAULT, TRIM FAIL, SPOILER FAULT. AS WELL, NO MATTER THE SPEED, THE AIRCRAFT WAS INDICATING A FLASHING MAXSPSDR ASMF2019042301Warning Message · false activationAIRCRAFT RETURN TO PLATFORM DUE TO DURING TAKEOFF, IT WAS ACTIVE “TAKE OFF CONFIGURATION ALARM”; FLIGHT CREW ACCOMPLISHED THE QRH 15.2 PROCEDURES; MAINTENANCE PERSONNEL PERFORMED TAKE OFF WARNING SYSTEM TEST IAW FIM 31-51 TASK 803 , NO FAILURE WAS FOUND, TEST SDR ASMF201901017Warning System · false activationAIRCRAFT RETURN TO PLATFORM DUE TO DURING TAKEOFF, IT WAS ACTIVE “TAKE OFF CONFIGURATION ALARM”; FLIGHT CREW ACCOMPLISHED THE QRH 15.2 PROCEDURES; MAINTENANCE PERSONNEL PERFORMED TAKE OFF WARNING SYSTEM TEST IAW FIM 31-51 TASK 803 , NO FAILURE WAS FOUND, TEST SDR UIEA2018123102967Status Message · false activationSTATUS MSG AFT EQ EXAST FAN 2(<P>PERFORMED FIM 21-26- FAULT TREE 808 SYSTEM CHECK NORMAL AT THIS TIME </P>)SDR QXEA2018122600471Warning Message · false activationREJECTED T.O. AFTER RECIVING A ENG TLA NOT TOGA EICAS CAUTION NEAR 60 KTS VERIFIED THRUST LEVERS IN TOGA MESSAGE REMAINED UNTIL EXITING RUNWAY. REMOVED FROM SERVICE. INTEROGATED CMC IAW AMM TASK 45-45-00-970-801-A NO FAULTS NOTED NO FURTHER DEFECTS NOTED C/W FSDR ASAA2018122417519Warning Light · false activationUPON ARRIVAL AT GATE, NOTICED "ELEC" ANNUNCIATOR ILLUMINATED. GROUNDED - YES. RAN FIM TASK 24-31 #801 SPCU INOP MESSAGE. RAN B737-900 FIM 24-34 #802 SPCU POWER CYCLED, TEST PASSED. RESET ELECT LIGHT. OK FOR SERVICE.SDR HNAA2018122100325Warning Message · illuminatedEICAS MESSAGE ON CLIMB OUT...AIRCRAFT CURRENTLY DOWN IN PHL FOR REPAIRSSDR ASAA2018122097479Warning Light · false activation#2 PACK LIGHT ILLUMINATED. GROUNDED - YES. FOUND RIGHT PACK TRIP. ACCOMPLISHED B737-900 FIM 21-53 TASK 802. RIGHT PACK LIGHT RESET & OPS CHECK NORMAL.SDR HALA2018121900665Fault Message · false activationETOPS SIGNIFICANT SYSTEM - ENGINE 1 REV. FAULT. // OPS TEST #1 ENG REV PER A330 AMM 78-31-00-740-802-A, OPERATION NORMAL. A/C, OK FOR SERVICE.SDR HALA2018121900664Warning Message · false activationETOPS SIGNIFICANT SYSTEM - AFTER TAKEOFF ENG 2 BLEED VALVE INOP. PER MX PERFORMED RESET OF BLEED OPERATION RETURNED TO NORMAL OPS. // T/S PER A330 TSM 36-11-00-740-804 NO BMS #2 FAULTS NOTED RAN #2 ENG AS PER A330 AMM 71-00-00 INDICATIONS SHOW NORMAL / OPEN ASDR UIEA2018121982877Warning Message · false activationSTATUS MSG CABIN ALT AUTO 1 (<P>PERFORMED CABIN PRESSURE CONTROLLER BITE TEST NO FAULT NOTED I.A.W FIM 21-31 FT 809 CABIN PRESSURE SYSTEM 1 WORKS GOOD </P>)SDR UIEA2018121972864Warning Message · false activationAPU BAT CHARGE STATUS MESSAGE (<P>PERFORMED FIM 24-31 FT 805 MESAGE CLEARED APU BATTERY 28V </P>)SDR UIEA2018121982878Warning Message · false activationSTATUS MSG AFT EQ EXH FAN 2 (<P>PERFORMED OPS CHECK OF AFT EQ EXH FAN 2 I.A.W AMM 21-58-41 MSG CLEARED OPS CHECKED OK </P>)SDR VNAA2018121871101Warning Message · false activationTHE CREW RECEIVED A SLATS FAIL MESSAGE AT ZERO. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHUR INCIDENT. MAINTENANCE JCLEARED INHIGITS AND SLATS OPS CHECKED GOOD.SDR ASAA2018121427364Warning Message · false activationAUTO FLT FCU 1 FAULT. GROUNDED - YES. ACCOMPLISHED FCU 1 RESET PER AMM 22-81-00. NO FAULTS FOUND. ACCOMPLISHED CAT III CAPABILITY TEST PER AMM 22-97-00. AND AFS TEST PER AMM 22-96-00. ALL CKS OK.SDR P5CA2018121320379Warning Message · false activationAFTER STARTING LEFT ENGINE WE RECEIVED L GEN OFF CAUTION MESSAGE MESSAGE CLEARED WITH QRH PROCEDURE THIS IS THE 4TH WRITE UP WITH REGARDS TO THIS ISSUE(<P>PERFORMED BPCU TEST CARRIED OUT AS PER FIM 24-20 TASK ACRD 801 FOUND LEFT GEN OVER FREQUENCY FOUND IDG SDR IPXA2018121036781Lamp · inoperativeFIRST OFFICER`S MASTER CAUTION LAMP INOPERATIVE. REPLACED THE LAMP.SDR IXXA20181130043Socket · fodPRE-DEPARTURE CHECK FINDING, RH ENGINE #2 SQUIB LIGHT WILL NOT ILLUMINATE DURING TEST. CLEANED CONTAMINANTS FROM LAMP SOCKET IAW B757 AMM 20-00-00. INITIATED DEFERRAL MAINTENANCE ITEM IAW ATI MEL 26-20-02-01 CAT C NO FLY DATE 12/7/2018. GENERAL VISUAL INSPECTISDR U5QA2018112950088Pseu · unknownFROM RMN TO BCT, DIVERT TO FLL AND EMERGENCY LANDING DECLARED. AML #98 - MULTIPLE INFLIGHT FAILURES AND CAS MESSAGES. LOST AUTOPILOT, FLT SPOILERS, BRAKE FAULT, L & R ENGINE FAULTS, RUDDER TRIMFAULT, FLAP FAULT, STAB TRIM FAULT, L & R TR'S FAULT, XPDC STBY FASDR HALA2018112760613Warning Light · false activationETOPS SIGNIFICANT SYSTEM - BTB ENG 1 OIL CHIP DETECTED. DURING ENG START.// PERFORMED TSM 79-35-00-810-806-A FOR RELATED GROUND REPORT ENG1A-0571- LOSS OF ODM. PERFORMED TSM 77-31-00-810-807-A FOR RELATED GROUND REPORT ENG1D-0730 PHMU INTERNAL SNSR INTERFACE. SDR HALA2018112760611Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ENG 1- AIR EXCHANGER FAULT MINOR FAULT.// PERFORMED ENG 1 EEC CHAN"A" AND CHAN"B" TEST PASSED TAW AMM 73-21-00-710-812 AND "AIR/OIL HEAT EXCHANGER"CONNECTORS CLEANED AND RESECURED.SDR ASAA2018112627055Warning Light · false activationMACH TRIM LIGHT ILLUMINATED IN FLIGHT. DOES NOT EXTINGUISH ON MASTER CAUTION RECALL/RESET. AFTER A SHORT DELAY AND MULTIPLE RESET ATTEMPTS, THE MACH TRIM LIGHT DID EXTINGUISH. OPERATES AS EXPECTED NOW WITH MEL 22-5C. SUSPECT MASTER RECALL/RESET ISSUE. GROUNDEDSDR ASAA2018112617053Warning Message · false activationSINGLE CHANNEL MACH SPEED TRIM FAIL. GROUNDED - YES. NO FAULTS LOGGED IN FCC-A . ONLY FAULTS LOGGED IN FCC-B ARE THREE LEGS OF MACH TRIM INPUT POWER INVALID THAT WERE INDUCED BY CONFIGURATION CHANGE. NO PRIOR FAULTS WERE LOGGED. CONFIGURATION CHANGE REVERSED. SDR SIMA201811260002Relay · inoperativeABORTED TAKEOFF. BREAKS DID NOT OVERHEAT DUE TO MASTERWARNING NO TO CONFIG TRANSFERRED TO NRWC 918-ORD-03868 -C/A-CREW DEBRIEF INDICATED "NO TAKEOFF CONFIG" MESSAGE HAPPENED WITH NO AURAL MESSAGE. TROUBLESHOT IAW FIM TASK 31-51-00-810-804-A. REMOVED AND REPLACSDR HALA2018112000604Warning Light · false activationETOPS SIGNIFICANT SYSTEM - UPON ENGINE START ENG 1 OIL CHIP DETECTED ECAM DISPLAYED.// INSPECTED ALL CHIP DETECTORS PER AMM 79-00-00-281-802-A. ALL CHECK OK. RAN #1 ENGINE AND NO ECAM MESSAGES, NO LEAKS NOTED. OK FOR SVC.SDR AALA201811199035Lens · detachedAFT EXIT WARNING LIGHT DETACHED. REPLACED THE LENS IAW AMM 52-73-22-420-055-A.SDR ASAA2018111986899Status Message · false activationSTATUS MSG- CLASS II SMOKE . GROUNDED - YES. RESET SDCU SYSTEMS. OPS CHECK GOOD REF AMM 26-16-00.SDR ASAA2018111966897Warning Message · false indicationCIDS 2 MESSAGE ON ECAM. GROUNDED - YES. PERFORMED RESET IAW AMM 23-73-00-740-005, CHECK GOOD.SDR HALA2018111500586Fault Message · false activationETOPS SIGNIFICANT SYSTEM - "ENG. 1 MINOR FAULT". // PERFORMED BITE CHECK OF BOTH EEC'S. NO FAULTS DETECTED. COULD
NOT DUPLICATE FAULT. OK FOR SVC.SDR UIEA2018111402618Status Message · false activationRIGHT ENGINE PRV STATUS MESSAGE (<P>CLEARED MESSAGE, BITE CHECK OF AIR SUPPLY INDICATION SYSTEM PASSED. NO OTHER FAULTS NOTED IAW AMM 36-10-00</P>)SDR UIEA2018111652624Warning Light · illuminatedWITH R ENG BLEED SELECTED ON AND PACK SELECTED ON IN ANY MODE, "R ENG BLEED AIR OFF" LIGHT ILLUMINATED AT ALL POWER SETTINGS, CONTRARY TO DDG.(<P>PER DDG 36-11-02 UNDER OPERATION LIGHT ILLUMINATING IS NORMAL.</P>)SDR HALA2018111400580Warning Message · false activationETOPS SIGNIFICANT SYSTEM - UPON PLACING ENGINE MODE SELECTOR TO IGN/START, ENG 2 OIL CHIP DETECTED ECAM DISPLAYED. MAINTENANCE ADVISED TO START ENG 2, ENG HAD A NORMAL START AND CAM DISAPPEARED WHEN ENG 2 MASTER SWITCH WAS PLACED TO ON.// PERFORMED AMM 79-00-0SDR UIEA2018111432597Warning Message · false activationIDLE DISAGREE MESSAGE DURING ENTIRE DESCENT PHASE. PERFORMED A BITE TASK L AND R PIMU IAW AMM 77-35-00. TESTED GOOD.SDR RJEF20181113001Warning Light · false activationDURING CRUISE PHASE OF FLIGHT TAI523 FROM LAX TO SAL, THE AIRCRAFT DIVERTED TO MEX DUE TO A MEDICAL EMERGENCY WITH A PASSENGER. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED THE FOLLOWING 6 ITEMS: 1) APU LOW OIL LEVEL INDICATION. MAINTENANCE PERSONNEL VERIFIESDR QXEA2018111300414Warning Light · false activationMULTIPLE NO AIII LIGHTS, CONFIGURATION CHECKED OUT AND LIGHTS RESOLVED THEMSELVES. AT MINS, APCH WARN ILLUMINATED. A/C AVIONICS WERE PROPERLY CONFIGURED. CONDUCTED MISSED APPROACH. LIMITATIONS DID NOT APPEAR TO HAVE BEEN EXCEEDED. ( HGS INOP-UNUSABLE ). PLACEDSDR ASAA2018110976783Warning Message · false activationRIGHT "RAM DOOR FULL OPEN" LIGHT REMAINS ON IN CRUISE. GROUNDED - YES. PERFORMED PACK TEMPERATURE CONTROL BITE PROCEDURE ON BOTH PZTCS REF B737-900 FIM 21-62 TASK 801. NO CURRENT OR PREVIOUS FLIGHT FAULTS LOGGED. ALSO, ACCOMPLISHED RAM AIR SYSTEM OPERATIONAL TSDR HALA2018110500365Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ON LANDING. ENG 1 AIR EXCHANGER FAULT. ENG 1 MINOR FAULT.// PERFORMED TROUBLE SHOOT PER TSM 79-20-00-810-809-A. VISUAL INSPECTED AIR OIL/HEAT EXCHANGER, NO DAMAGE FOUND. PERFORMED FADEC SYSTEM TEST PER AMM 73-21-00. SYSTEM TEST OK. SDR RJEF20181105001Warning Message · false activationAFTER ENGINE START OF FLIGHT TAI423 FROM MCO TO SAL THE PILOT REPORTED: "F/CTL ELEV SERVO FAULT CAME ON E/WD AND ALSO ON FLIGHT CONTROL PAGE IT SHOWED THE BLUE SERVO FAULT", THE AIRCRAFT RETURNED TO THE GATE FOR MAINTENANCE. MAINTENANCE PERSONNEL PERFORMED FAUSDR UIEA2018110502519Warning Message · false activationLEFT ENGINE VALVE LIGHT AND LEFT VALVE EICAS MESSAGE ILLUMINATED. CYCLED THE CIRCUIT BREAKER IAW AMM 26-60-01. NO DEFECT NOTED. OPS CHECKED GOOD.SDR UIEA201811022471Warning Message · false activationSTATUS MESSAGE IN FLIGHT FOR THE CABIN ALTITUDE AUTO 2. THE CABIN PRESSURE CONTROLLER 2 BITE TEST CARRIED OUT IAW AMM 21-31-02, TEST PASSED , NO ACTIVE MESSAGE.SDR HALA2018110100556Warning Message · false activationDURING NR 2 ENGINE START, ECAM FOR NR 1 ENGINE OIL CHIP DETECTOR. DURING NR 2 ENGINE CRANKING, MESSAGE DISAPPEARED. STARTED NR 1 ENGINE, ALL INDICATIONS NORMAL.. PERFORMED TSM 79-35-00-810-808-A, NR 1 ENGINE OIL CHIP DETECTOR ECAM REPORTED BY CREW WITH SDR ASMF20190109005Warning System · false activationAIRCRAFT RETURN TO PLATFORM DUE TO BEFORE TO TAKEOFF, THE TAKEOFF CONFIGURATION ALARM AND LIGHT, PSEU LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO PSEU IAW AMM 31-51-00, SHOWING MESSAGES AND FAILURE CODES STAB TRM NOT GRN, STAB TRM GREEN AND TAKEOFSDR 2018FA0000434Relay · failedCUSTOMER REPORTED THAT THE CREW ALERTING SYSTEM (CAS) MESSAGE ECU1FAIL ILLUMINATES ON THE RELATED DISPLAY AND THAT THE ENGINE CONTROL (ECU) REVERTS THE ENGINE FROM ECU CONTROL TO THE MANUAL MODE OF CONTROL. AFTER EXTENSIVE TROUBLE SHOOTING AND RECOMMENDATIONSSDR DJFA2018111208001Warning Message · false activationDIVERTED DUE TO SWPS FAULT AND SPOILER FAULT. WITH THE AUTO PILOT/FLIGHT DIRECTOR ENGAGED THE AUTO PILOT WOULD ONLY HOLD ALTITUDE AND NAV IT WOULD NOT CLIMB OR DESCEND. USING VNAV PROMPTED MAX SPEED WARNING AT ALL SPEEDS. AIRCRAFT LANDED WITHOUT INCIDENT. PESDR ASAA2018092726292Warning Message · false activationENG 2- MINOR FAULT ONLANDING. GROUNDED - YES. PERFORMED ENG 2 FADEC TEST. TEST OK NO FAULTS AT THIS TIME REF AMM 73-29-00SDR ASAA2018092876286Warning Message · illuminatedON ENG SHUTDOWN CLASS 2 ENG 2 FADEC MESSAGE. GROUNDED - YES. ON DEFERRAL
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