JASC 2613
Service difficulty reports · 1,796
Reports filed under 2613 · Overheat Detection, 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 = '2613' 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 = '2613' 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 NACA2024031000001Sensor · faultedFWD EQUIP OVHT LIGHT ON AND ALARM GOING OFF. BOTH EICAS AND OVERHEAD LIGHTS ON. ACCOMPLOSHED PROJECT WORKSHEET WO 123167, REPLACED TS104 SENSOR, TS 0041, VALVE COOLING MANIFOLD CONNECTOR, LEFT PACK LOW LIMIT VALVE. SYSTEM OPERATIONAL CHECK PER AMM 21-58-01SDR VNAA2024031311101Probe · faultedBRAKE OVHT WARNING MSG IN FLIGHT, L OUTBD SENSOR APPEARS ERRONEOUS AT 20 / PERFORMED TROUBLESHOOTING OF BRAKE OVHT WARNING MSG IAW FIM 32-46-01-810-802 A01. REMOVED LH OB THERMOCOUPLE SENSOR IAW 32-46-01-000-801 A01. REPLACED LH OB THERMOCOUPLE SENSOR IAW CRJSDR G1IA20240313060Warning Message · illuminatedWHILE CRUISING AT 41,000', WE HEARD 3 CHIMES AND OBSERVED A RED L ENG PYLON OVHT ILLUMINATION. I TOLD MY SIC TO GRAB THE QRH AND ADVISED HIM I WILL TAKE RADIO COMMUNICATION DUTY. FOLLOWING THE CHECKLIST, WE PULLED THE LEFT THROTTLE TO IDLE AND STARTED A DESCENSDR AALA202403074964Warning Message · false indicationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: RIGHT WING-BODY OVERHEAT LIGHT ILLUMINATED AROUND 1500 AND STAYED ON; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. ACCOMPLISHED WORK CARD 08C44126001. NO FAULTS NOTED. OPERTIONAL CHECK NORMSDR HALA20240304057Wire Harness · damagedETOPS - FOUND RAIL FOR FIRE DET. HARNESSES 32WD1, 31WD1, 42WD1, 41WD1 CLAMPS MISSING AND INCORRECT ROUTING. REPLACED MISSING CLAMPS FOR FIRE DET. HARNESSES 32WD1, 31WD1, 42WD1, 41WD1 AND CORRECTED ROUTING IAW MM 26-12-63-400-801-A. OPS CK GOOD. OK FOR SVC. DAMSDR NACA2024022800003Warning Message · false activationFWD EQUIP OVHT EICAS MESSAGE DURING DESCENT. PERFORMED FIM FAULT TREE TASK 912 NO DISCREPANCIES OPS CHECK NORMAL IAW AMM 21-50-00SDR 7P9A2024031900001Sensor · faultyDURING FLIGHT THE CREW EXPERIENCED INTERMITTENT L PYLON HOT CAS MESSAGE. ON ARRIVAL MX CREW CHECKED FOR BLEED LEAKS AND CONFIRMED THAT THERE WAS NO LEAK AND A FAULTY SENSOR. DETECTION SYSTEM MELED.SDR SWIA202402260001Warning Message · illuminatedAT ABOUT 800 FEET SHORT FINAL RECEIVED A MLG OVHT FAIL CAUTION. AS WE CONTINUED IT BECAME INTERMITTENT THEN TURNED INTO A MLG OVHT WARNING. AS WE ROLLED OUT THE WARNING WENT AWAY BUT WE NOTICED A BURNT RUBBER SMELL TAXING OFF THE RUNWAY. WE CALLED TOWER TO SENSDR SWIA202402210001Warning Message · illuminatedAT ABOUT 800 FEET SHORT FINAL RECEIVED A MLG OVHT FAIL CAUTION. AS WE CONTINUED IT BECAME INTERMITTENT THEN TURNED INTO A MLG OVHT WARNING. AS WE ROLLED OUT THE WARNING WENT AWAY BUT WE NOTICED A BURNT RUBBER SMELL TAXING OFF THE RUNWAY. WE CALLED TOWER TO SENSDR IPXA2024020627940Warning Message · illuminated*SDR FILED OPEN* *AIR TURN BACK* EQUIPMENT OVHT EICAS AND ANNUCIATOR RECEIVED AFTER T/O. THE CHECK LIST DID NOT FIX THE OVHT. RESULTED IN AIR TURNBACKSDR SWAA2024011741498Overheat Sensor · faultedDURING DESCENT RIGHT WING TO BODY OVERHEAT ILLUMINATED RAN QRH PROCEDURE. LIGHT EXTINGUISHED<[01] R/R M1763 & M1764 FWD AND AFT WING TO BODY STRUT ELEMENTS PER AMM 26-18-02. OPS CHECK OK.SDR CALA2023120103534Overheat Loop · looseOVERHEAT CIRCUIT L1 EICAS STATUS LEFT ENGINE OVERHEAT DETECTION CIRCUIT 1 FAILURE. FIM TASK REF : FIM TASK REFERENCE NOT FOUND CMC MSG# 2610131 FLIGHT STATUS: A INTERMITTENCE CODE: H PH: CRUISE NARRATIVE: ENGINE FIRE DETECTION C ARD (LEFT) CMC MSG# 2610141 FLISDR HALA20231124254Overheat Sensor · faultyETOPS - ENGINE 2 LOOP A FAULT ON ECAM FOUND DURING PDC WALKAROUND. PERFORMED TSM 26-12-00-710-002 FOUND LOOP 4002WD1 SHORTING. REMOVED & REPLACED ENG 2 LOOP A 4002WD1 IAW AMM 26-12-17 PB401. FDU TEST OKAY. NO FAULTS NOTED. A/C OK TO CONTINUE. MOC NOTIFIED.SDR AALA202311204645Overheat Sensor · dirtyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: RIGHT WING BODY OVERHEAT. AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. FOUND MULTIPLE SENSOR DIRTY. CLEANED SENSOR. PER SWPM 20-60-01. FUNCTIONAL CHECK GOOD.SDR ASAA2023110145977Module · faultedENG 2 OVERHEAT LIGHT ILLUMINATED ON SHORT FINAL. QRH FOLLOWED AFTER LANDING AND LIGHT EXTINGUISHED AT IDLE THRUST. GROUNDED - YES. REF AMM 26-00-1 FOUND NO WIRING ISSUE PER WDM 26-11-21, CONTINUE T/S FOUND WHILE PERFORM WING BODY OVER HEAT DET LOOP TEST, #2 ENSDR DALA2023103008902Unknown · unknownSHIP 3760 -ATB- DUE TO LEFT WING BODY OVERHEAT INDICATION. ICING CONDITIONS IN ORD. CORRECTIVE ACTION: FOUND M370 SENSOR BROKEN UNDER CLAMP. REPLACED SAME. OPS CHECKS GOOD. (LP 4277596)SDR SWAA2023090797779Overheat Sensor · intermittentFIRE WARNING LIGHT AND BELL ALONG WITH WHEEL WELL LIGHT ILLUMINATED; THEN WENT OUT. ON APPROACH; AFTER LANDING GEAR EXTENDED DOWN; HAPPENED AGAIN.<[01] REMOVED AND REPLACED INTERMITTENTLY SHORTINGWHEEL WELL OVERHEAT SENSING ELEMENT IAW AMM CHPT. 26-18-02.SDR AALA202309128554Overheat Sensor · false indicationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO ORD DUE TO LEFT ENGINE OVERHEAT DETECTOR LIGHT ILLUMINATED IN BOTH A AND B POSITIONS. FLIGHT LANDED SAFELY AT ORD WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT ENGINE UPPER FANSDR AALA202308221394Detector · false indicationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO ENGINE #1 OVERHEAT LIGHT ILLUMINATED ON INITIAL CLIMB. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202308214097: MAINTENANCE SDR AALA202308220767Detector · false indicationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO ENGINE #1 OVERHEAT LIGHT ILLUMINATED ON INITIAL CLIMB. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202308214097: MAINTENANCE SDR AALA202308221262Detector · false indicationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO ENGINE #1 OVERHEAT LIGHT ILLUMINATED ON INITIAL CLIMB. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202308214097: MAINTENANCE SDR AALA202308214097Unknown · unknownAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO ENGINE #1 OVERHEAT LIGHT ILLUMINATED ON INITIAL CLIMB. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)SDR ASAA2023081044515Overheat Sensor · faultyINTERMITTENT "APU DET INOP" CAUTION LIGHT ON FIRE CONTROL PANEL AND MASTER CAUTION. GROUNDED - YES. R/R APU TAILPIPE OVERHEAT DETECTOR ASSY M1925. REF B737-800 AMM 26-15-01. APU FIRE DETECTION OPS TEST GOOD.SDR 2023F00250Module · failedENGINE #1 OVERHEAT DURING CLIMB PHASE. CORRECTIVE ACTION: CHANGED OVERHEAT DETECTION CONTROL IAW AMM 26-18-01/401 AND TEST OK.SDR DXTA2022122777250Overheat Loop · false indicationDURING CRUISE FLIGHT THE RIGHT JET PIPE OVERHEAT ILLUMINATED NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED FOLLOWED THE CHECKLIST WHICH LED US TO A RIGHT ENGINE SHUT DOWN IN-FLIGHT. DISCONNECTED AND OHMED, READ 5,2 OHMS. CLEANED, RECONNECTED AND SAFETIED IAW SDR ASAA2022122441259Overheat Loop · false activationAPU DET INOP LIGHT ILLUMINATED. GROUNDED - YES. R/R APU OVERHEAT DETECTOR REF B737-800 AMM 26-15-01.SDR 9JLA2022122940057Overheat Sensor · defectiveTHE FLIGHT CREW REPORTED THAT PRIOR TO START OF ENGINES RECEIVING A LEFT HOT BATTERY INDICATION. THE BASE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE LEFT MAIN BATTERY TEMP SENSOR WAS DEFECTIVE. THE BATTERY TEMP SENSOR WAS REMOVED AND REPLACED WITH A NEWSDR AALA202212076857Module · faultedAIRCRAFT WAS GROUNDED: DURING CLIMB OUT CIRCUIT BREAKER A-19 ON P6-2 PANEL FOR OVERHEAT WHEEL WELL AND WING TO BODY POPPED. FLIGHT DIVERTED TO IND LANDING SAFELY. REPLACED OVERHEAT DETECTION CONTROL MODULE M00237 PER AMM 26-18-01. ACCOMPLISHED SATISFACTORY OPESDR AALA202212054972Overheat Loop · faultedAIRCRAFT WAS GROUNDED: PASSING 10000 ENGINE INDICATING AND CREW ALERTING SYSTEM MESSAGE ANTI-ICE LEAK ENGINE RIGHT CAME ON. AIR INTERRUPTING BACK TO EZE ACCOUNT MAINTENANCE ANTI-ICE ISSUE. REMOVED AND REPLACED RIGHT ENGINE FAN CASE OVERHEAT DETECTOR PER AMM 26SDR AALA202212023809Overheat Sensor · false activationAIRCRAFT WAS GROUNDED: AIR RETURNED TO DFW ACCOUNT RIGHT WING BODY OVERHEAT INDICATION. EMERGENCY WAS DECLARED. RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED DET M1764 (AALA202212023809) AND DET M1763 (AALA202212025735) IAW AMM 26-18-02.SDR AALA202212025735Overheat Sensor · false activationAIRCRAFT WAS GROUNDED: AIR RETURNED TO DFW ACCOUNT RIGHT WING BODY OVERHEAT INDICATION. EMERGENCY WAS DECLARED. RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED DET M1764 (AALA202212023809) AND DET M1763 (AALA202212025735) IAW AMM 26-18-02.SDR DXTA2022110373200Sensor · malfunctionedRIGHT JETPIPE OVHT RED CAS MESSAGE ILLUMINATED IN FLIGHT. FOLLOWED CHECKLIST WHICH HAD US SHUT THE RT ENG DOWN IN FLIGHT. CAS MESSAGE WAS STILL ILLUMINATED AFTER SHUTTING DOWN ON RAMP. REMOVED THE FAILED RT ENGINE EXHAUST NOZZLE SENSING ELEMENT. INSTALLED SDR ASAA2022102540522Overheat Loop · faultedENGINE #2 'B' LOOP ENGINE OVERHEAT INDICATES A FAULT LIGHT AND UNSATISFACTORY TEST WHEN OVERHEAT SWITCH IN THE NORMAL POSITION. ENGINE FIRE TEST SATISFACTORY WHEN OVERHEAT SWITCH IS PLACED IN THE A LOOP POSITION. GROUNDED - YES. PERFORMED ENGINE/APU FIRE DETECSDR 9JLA2022102832674Overheat Sensor · defectiveTHE FLIGHT CREW REPORTED THAT THE APU SHUTS DOWN WHEN BLEED AIR LOAD WAS APPLIED. THE MAINTENANCE TEAM VERIFIED DISCREPANCY AND FOUND THE APU INLET TEMP SENSOR DEFECTIVE. THE SENSOR WAS REMOVED AND REPLACED WITH A NEW UNIT. OPS CHECKS WERE SATISFACTORY, AND THSDR SWIA202266613None · failedD: CREW REPORTS APU FIRE FAIL CAUTION MESSAGE ON SHORT FINAL. DEFERRED APU FIRE DETECTION LOOPS PER MEL 26-12-1B. NO MX ACTION REQ'D & PLACARD INSTALLED. / C: MEL 26-12-1B / CAT C DUE 10/24/22 / SEE A/C MX LOG #1012872 / CREW REPORTS APU FIRE FAIL CAUTISDR SWIA202266589None · noneUPON STARTING THE APU, WE RECEIVED APU OVERTEMP WARNING MESSAGE FOLLOWED BY APU FIRE FAIL CAUTION MESSAGE. (FLIGHT #5130 FILED CLOSED) PERFORMED OPS CHECK OF APU IN REFERENCE TO AMM 49-10-00 AND OPS CHECK OF APU FIRE DETECTION IN REFERENCE TO AMM 26-12-00.SDR SWAA2022092930452Sensor · false activationON START OF TAKEOFF ROLL; GOT A RIGHT WING TO BODY OVERHEAT INDICATION. REJECTED TAKEOFF. WING/ BODY OVERHEAT INDICATION FLICKERED ON INTERMITTENTLY ON TAXI BACK WITH BLEED AIR SYSTEM OFF/ ISOLATED / [01] OK TO CONTINUE PER MEL 26-13-01 SP#1 AUTH#91958;[02] RESDR 2022FA0000539Switch · false activationDURING CLIMB THRU FL220 THE R ENG OVHT CAS ILLUMINATED. WE RAN THE APPROPRIATE CHECKLIST AND RETURNED FOR A SINGLE ENGINE LANDING. DURING THE DESCENT THE LIGHT WOULD COME ON EVEN WITH THE ENGINE SHUT DOWN. WE WOULD CLEAR THE CAUTION AND IT WOULD RETURN A FEW MSDR ASAA2022091939999Overheat Sensor · warning lightAPU DET INOP LIGHT ILLUMINATED IN FLIGHT. GROUNDED - YES. REMOVED AND REPLACED APU OVERHEAT DETECTOR ASSEMBLY (TAILCONE) REF B737-800 AMM 26-15-01.SDR FDEA202209132318Overheat Loop · failedDURING CLIMBOUT, GOT AN ECAM MESSAGE GREEN RSVR OVHT . COMPLETED THE ECAM AND QRH, OVHT LIGHT INTERMITTENT. CONTINUED FLIGHT. DURING DESCENT, OVHT LIGHT EXTINGUISHED, DECIDED TO RESTORE SYS USING EDP. DECLARED AN EMERGENCY & LANDED WITHOUT ISSUES. IAW MMSDR 2022FA0000506Overheat Sys · false activationDURING CLIMB OUT, GOT A RIGHT ENGINE PYLON OVERHEAT CAS MESSAGE. REDUCED POWER WITH NO AFFECT. DIVERTED TO CVG AIRPORT.SDR SWAA2022091251933None · overheated#2 ENGINE OVERHEAT DURING START HAS TONS OF HISTORYPLEASE CHECK PNEUMATIC PLUMBING AND CONNECTIONS FOR ENG START SYSTEM REF FIM 26-10 TASK 811 IF NO FAULTS FOUND ACCOMPLISH ENGINE FIRE DETECTION LOOP RESISTANCE SYSTEM TEST REF AMM 26-11-00-730-801 / [01] VERIFSDR AALA202209065104Sensor · false indicationAIRCRAFT WAS GROUNDED: LEFT WING TO BODY OVERHEAT LIGHT ON DESCENT INTO DCA. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. REPLACED DETECTORS M268 (AALA202209065104), M1761 (AALA202209067061), AND M1762 (AALA202209064772) PER AMM 26-18-02. ACCOMPLISHED SATISFACTORSDR AALA202209067061Element · false indicationAIRCRAFT WAS GROUNDED: LEFT WING TO BODY OVERHEAT LIGHT ON DESCENT INTO DCA. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. REPLACED DETECTORS M268 (AALA202209065104), M1761 (AALA202209067061), AND M1762 (AALA202209064772) PER AMM 26-18-02. ACCOMPLISHED SATISFACTORSDR AALA202209064772Element · false indicationAIRCRAFT WAS GROUNDED: LEFT WING TO BODY OVERHEAT LIGHT ON DESCENT INTO DCA. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. REPLACED DETECTORS M268 (AALA202209065104), M1761 (AALA202209067061), AND M1762 (AALA202209064772) PER AMM 26-18-02. ACCOMPLISHED SATISFACTORSDR ASAA2022082339639Detector · inoperativeAPU DET INOP CAUTION LIGHT ILLUMINATED IN CRUISE. GROUNDED - YES. REMOVED AND REPLACED APU TAILPIPE OVHT DET M1925 IAW B737-800 AMM 26-15-01/401.SDR AALA202208010880Module · inoperativeAIRCRAFT WAS NOT GROUNDED: OVERHEAT DETECTOR LOOP A ENGINE #2 INOPERATIVE. REPLACED ENGINE AND APU FIRE CONTROL MODULE P8-1, PER AMM 26-00-01. OPERATIONAL CHECK GOOD.SDR SWIA202266138None · fire warningAPU FIRE WARNING MESSAGE IMMEDIATELY AFTER LANDING. APU AUTO SHUTDOWN AND BLEW FIRE BOTTLE. FIRE WARNING WENT AWAY IMMEDIATELY. (FLIGHT #4039 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25172039 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVSDR UIEA2022062200645Fire Detector · damagedPRIOR TO DEPARTURE, ENG 4 FIRE DET LOOP B WAS DEFERRED. SHORTLY AFTER TAKEOFF, LOOP A ON THE SAME ENGINE BEGAN FLAGGING IN AHM. QRH PROCEDURES FOR DUAL LOOP FAILURE INDICATES FIRE DETECTION AND OVERHEAT DETECTION MAY BE INOP FOR THAT ENGINE. DUE TO CLOSE PROXISDR AJXA2022060600017Overheat Sensor · intermittentDURING TAKEOFF PILOT RECEIVED A TAIL CONE BLEED LEAK INDICATION. HE REPORTED THAT THE INDICATION WAS INTERMITTENT. WE REMOVED AND REPLACED A FAILING RTD SENSOR, PERFORMED FUNCTIONAL CHECK WITH NO FURTHER DEFECTS
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