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 UALA2008121106841Detector · faultySTATUS MSG R ENG OH LP2 DISPLAYED. REPLACED SUSPECT HEAT DETECTOR.SDR VNAA2008120400010Overheat Sensor · failedDURING TAXI WITH WING HEAT ON, CREW RECEIVED MOMENTARY RIGHT WING OVERHEAT RED WARNING MSG. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED SYSTEM. AIRCRAFT WAS RELEASED FOR SERVICE. AIRCRAFT LEFT THE GATE AND DURING TAXI, CRSDR DUFA20080003Overheat Sensor · false activationWHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE RT WING OVERHEAT LIGHT ILLUMINATED. THE RT GENERATOR WAS SHUT DOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND PROCEDURES CALL OUT FOR ENGINE SHUT DOWSDR A6WA200840609Sensor · shortedRECEIVED LT STAGE DUCT MSG INFLIGHT. MSG STAYED ON AFTER RETARDING THRUST LEVER TO IDLE. C/W GVI OF LT 10TH STAGE DUCTING WITH ENGINE RUNNING. NO LEAKS DETECTED. LT 10TH STAGE WARN MSG OCCURRED AGAIN WITH ENGINES SHUTDOWN. CONFIRMED BAD INDICATION. REF 1SDR NSVA2008042Warning Light · false activationDURING TAKE-OFF ROLL LEFT ENGINE TAIL-PIPE HOT LIGHT ILLUMINATED AND SUBSEQUENTLY ABORTED TAKE-OFF. OPS CHECK IAW AMM 26-11-00-05, PROCEDURE 1, NO DEFECTS NOTED.SDR 2008UALA06359Warning System · activatedWING BODY OVERHEAT LIGHT. RTFL DUE TO INCLEMENT WEATHER AT PLANNED DESTINATION. FAULT RECURRED ON NEXT FLIGHT OUT.SDR CHQA200800210Overheat Loop · malfunctionedFLIGHT 5601, IAH TO JAX. DURING CLIMB THE FLIGHT CREW RECEIVED AN L JETPIPE OVHT FAIL CAUTION MESSAGE. THE MESSAGE APPEARED AND EXTINGUISHED SEVERAL TIMES. THE QRH CHECKLISTS WERE FOLLOWED AND A L JETPIPE OVERHEAT MESSAGE APPEARED ALONG WITH THE TRIPLE CHIMSDR MAL2008F00051Pump · malfunctionedFLIGHT CALLED AROUND THE MBS AREA WITH A MAIN HYDRAULIC PUMP PROBLEM. MAIN HYDRAULIC ACCUMULATOR PRESSURE DROPS FROM 3000 TO 2000 PSI EVERY 35 SECONDS IN FLIGHT. CREW TALKED TO DISPATCH MXC AND RETURNED TO DTW. WORKED UP NRS FOR FLIGHT TO RETURN TO DTW. THSDR COMA0860396Sensing Element · failedFLIGHT NR 6264 ON CLIMBOUT FROM GSO TO CVG RECEIVED RT ENGINE 14TH STAGE DUCT MSG. PERFORMED QRH, EMERGENCY DECLARED. A/C DIVERTED TO ROA AND LANDED SAFELY. R&R RT PYLON SENSING ELEMENT A58WK.SDR 08FDEA03956Engine · false indicationDURING CLIMB PASSING FL180 EICAS MESSAGE DISPLAYS L ENG OVHT ALL OTHER ENG INDICATIONS WERE NORMAL. RETARDED L THROTTLE AND TURNED OFF L BLEED AIR. AFTER APPROXIMATELY 2 MIN THE EICAS MESSAGE WENT AWAY. DECLARED EMERGENCY AND LANDED WITH L ENG AT IDLE. COMPSDR A6WA200840584Element · malfunctionedLT 14TH DUCT WARNING MESSAGE EN ROUTE. COMPLIED WITH QRH. R&R LT PYLON 14TH STAGE SENSE ELEMENT IAW 36-21-00. OPS CHECK GOOD.SDR MAS2008F00039Control Unit · malfunctionedASH 2648 SAT-CLT. NR 2 MLG BRAKE OVERHEAT WARNING AFTER LANDING. MAINTENANCE REMOVED AND REPLACED ASCU. (S)SDR GLB2008F00009Sensor · wornINFLIGHT SHUTDOWN - AIR RETURN - AC N108UX - FLT5136 ENROUTE, PILOTS REPORTED A NR1 ENG DUCT LEAK, WAITED FOR THE ANNUNCIATOR TO EXTINGUISH WITHOUT LUCK. PILOTS SHUTDOWN THE NR1 ENG AND RETURNED TO DEPARTURE CITY "LBF". MAINT REMOVED AND REPLACED THE LT DUCSDR 08FDEA02901Warning System · malfunctionedINFLIGHT, LOWER AFT BODY OVERHEAT LT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES AND DETERMINED THAT THE LEAK IS BETWEEN NR 3 BLEED VLV AND PACK VALVE. HAD TO DESCEND TO FL250 TO CONTROL CABIN ALTITUDE AT 10000 FT. RAN ENGINES AT H/P. NO OVERHEAT LIGHT CHECKESDR DXTA200803159Sensor · illuminatedAFTER TAKEOFF WE BROUGHT THE THRUST LEVERS TO CLIMB POWER. AT THAT TIME RECEIVED A RED CAS "PYLON BLEED LEAK L" MESSAGE. EMERGENCY DECLARED. TURNING OFF THE BLEED FOR THAT ENGINE AND REDUCING THROTTLE TO IDLE REMOVED THE CAS MESSAGE. PERFORMED GROUND ENGINE SDR AALA200801700Clamp · defectiveORD INFLIGHT T1345/25JUN. CREW REPORTED TAIL COMPARTMENT OVERHEAT INDICATION DURING CLIMB. INDICATION EXTINGUISHED WHEN LT AIR CONDITIONING SWITCH PLACED TO OFF POSITION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED CLAMP AND SHIM AT LT HEAT EXCHASDR PNS2008F00002Detector · malfunctionedON JUNE 22, 2008, THE FLIGHT CREW HAD A LEFT TAIL PIPE HOT LIGHT, AN INFLIGHT ENGINE SHUTDOWN WAS MADE, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT DEPARTURE AIRPORT. THE LIGHT WENT OUT A FEW MINUTES BEFORE LANDING, AND THE TOTAL SDR F3LA200800381Relay · damagedDURING C-CHECK INSP NOTED OPS TEST OF APU AUTO FIRE EXTINGUISHING EXITING CIRCUIT AND THE APU LOW PRESSURE VALVE OPERATION USING EACH INDIVIDUAL MOTOR IN TURN AND TEST APU EMERGENCY SHUTDOWN CIRCUIT FAILS. MAINT REMOVED AND REPLACED RELAY 39WF AND OPS CHECKED SDR SWIA200819788Controller · no testFLT 5990 - MAIN LANDING GEAR BAY OVERHEAT WOULD NOT TEST CORRECTLY. REPLACED MAIN LANDING GEAR OVERHEAT CONTROLLER AS REQUIRED. OPS CHECKS GOOD.
SDR C2XA08CL068Thermostat · faultyEWR FLIGHT 2373. THE CREW REPORTED A BLEED 1/2 OVERTEMP MESSAGE IN ICING CONDITIONS. THE ACFT DIVERTED INTO CLE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BLEED THERMOSTAT. OPERATIONAL CHECKS WERE GOOD. (S)SDR 2008UALA03279Overheat Loop · faultyFOUND WING OVERHEAT LOOP M1204 BAD. SUSPECT IMPROPERLY INSTALLED. REPLACED RT OVERHEAT LOOP ENGINE PYLON IAW MM26-18-11. OP CHECKED GOOD. AC OK FOR SERVICE.SDR TRAX200800723Detector · malfunctionedHOT BRAKE TEMP IN CRUISE. FLT 4216 DEL 31 MINS. (BRAKE TEMP LIGHT SYSTEM) REMOVED AND REPLACED LT O/B AND I/B COMPENSATORS IAW ATR 72 JIC 32-42-56. OPS CHECK GOOD. DEFER CLEARED. PLACARD REMOVED. (B)SDR UPS08652348Thermal Switch · inoperativeINSPECTION TYPE:ETOP ATB - DUCT LEAK LIGHT ILLUM. EICAS MSG: LEFT BLEED DUCT LEAK DISPLAYED. FUEL DUMPED. REPLACED M691 CONTROL CARD PER MM 26-10-01-4. REPLACED S236 THERMAL SWITCH PER MM 26-18-01-4. REMOVED AND REPLACED S237 THERMAL SWITCH PER MM 26-18-SDR NSVA2008030Seal · leakingAIR RETURN FOR RT TAILPIPE HOT ON CLIMB-OUT FROM LGA. EMERGENCY DECLARED, LIGHT WENT OUT ON IT'S OWN SHORTLY AFTER. WEATHER ON THE GROUND WAS HEAVY RAIN PRIOR TO DEPARTURE. CW WORKCARD FOR TAILPIPE SENSOR SEALING. ONCE DONE, OPS CHECKED GOOD.SDR ABXA080153Control Panel · defectiveAFTER TAKEOFF FROM STA JFK, RIGHT ENGINE OVERHEAT LIGHT AND EICAS MESSAGE. PERFORMED NON NORMAL - SECURED RIGHT ENGINE. LIGHT DID NOT GO OUT AFTER THRUST LEVER RETARDED. AN EMERGENCY WAS DECLARED AND AN AIR TURNBACK TO JFK WAS PERFORMED. TROUBLESHOT PER FISDR 2008UALA02764Warning System · activatedRTFL DUE TO A WING/BODY OVERHEAT INDICATION. NORMAL LANDING.
SDR NSVA2008025Connector · dirtyTAIL PIPE HOT LIGHT IN FLIGHT. CLEANED CONNECTIONS ON TAILPIPE HOT LIGHT SENSORS, OPS CHECK GOOD IAW SAAB MM 26-12-00.SDR TRAX200800610Overheat Loop · malfunctionedON CLIMBOUT RECEIVED A 14TH STAGE BLEED DUCT MSG FOLLOWING THE QRH THE MSG WENT AWAY THEN CAME BACK ABOUT 30SEC LATER. RETARDED THE LEFT ENGINE LANDING SINGLE ENGINE CONFIGURATION. LANDING WEIGHT WAS APPROX 48,500 LBS. ALSO NOTED HYD 1 PRESSURE READOUT WAS SDR COMA0880007Loop · out of positionFLIGHT 5056- ON CLIMB-OUT FROM AUS TO ATL, RECEIVED LEFT BLEED DUCT WARNING MESSAGE. EMERGENCY DECLARED AND A/C RETURNED BACK TO AUS AND LANDED SAFELY. REPOSITIONED INSULATION AND LOOPS AT HP GROUND DUCT. OPS CHECK GOOD.SDR 2008UALA02669Module · failedNR 1 OVERHEAT LIGHT FAILS TO COME ON DURING TEST. REPLACED THE ENGINE AND APU FIRE CONTROL MODULE PER MM26-21-51. AC OK FOR SERVICE.SDR NSVA2008024Seal · missingRT TAIL PIPE HOT LIGHT ILLUMINATED ON CLIMB-OUT. SEALED TAIL PIPE SENSOR IAW SB 340-26-029, AFTER FINDING THE BACK OF THE SENSORS EXPOSED TO THE ELEMENTS. OPS CHECK GOOD.SDR DXTA200803018Sensor · inoperativeBLEED OVERHEAT LIGHT CAME ON 2 MIN AFTER TAKEOFF. CHECKLIST ACCOMPLISHED AND CREW WAS UNABLE TO ISOLATE THE MALFUNCTION. FAULT CODE 404 AND 428. BLEED OVERHEAT COMES ON WITH APU BLEED ON AND ENGINE OFF. REMOVED & REINSTALLED TEMP SENSOR L70HU. OPS & LEAK CHSDR 2008UALA02284Overheat Loop · worn"L ENG OVHT LOOP 1" STATUS MESSAGE ON EICAS. FOUND OVER HEAT LOOP 1 WORN. REPLACED OVERHEAT LOOP 1, OPS CHECKED OK.SDR 08FDEA01446Hose · leakingENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT COMPLIED WITH QRH. AIRCRAFT INCURRED A MAINTENANCE FLIGHT DIVERSION INTO ATL. FLIGHT CREW ADVISED, THAT, THE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED AT APPROXIMATELY 10,000 FT, DURING CLIMB-OUT WITH AN EPRSDR DL738080593Overheat Loop · inoperativeAFTER TAKEOFF CLIMBING THROUGH 300 FT AGL LT WING-BODY OVERHEAT LIGHT ILLUM. DID QRH PROCEDURE. LIGHT STILL ILLUM, RETURNED TO LAND SLC. LANDED OVERWEIGHT. AT GATE, LIGHT STILL ILLUM. REPLACED DETECTORS M347 AND M1147. TESTS OK.SDR C8GA20080013Overheat Loop · faultedCLT TO BNA - DURING CLIMB OPERATION, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED TO TOL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 3 STRUT OVERHEAT DETECTOR LOOP AT FAULT. REMOVED AND REPLACED NSDR MALA080052Seal · looseR TAILPIPE HOT INDICATION ON TAKEOFF CLIMB-OUT. RESEALED DETECTOR IAW SAAB MM 26-00-00, ALL CKS GOOD.SDR HALA0800441Circuit Card · faultyETOPS SIGNIFICANT SYSTEM, RT DUCT LEAK LT ON AND EICAS R BLD DUCT LEAK. PERFORMED FIM 26-18-00, NO DEFECT NOTED. REMOVED AND REPLACED WHEEL WELL OVERHEAT DUCT LEAK DETECTION CARD PER AMM 26-10-01.SDR HALA0800425Circuit Card · faultyETOPS SIGNIFICANT SYSTEM, EICAS STATUS MSG, R ENG OH LPW DISPLAYED. REPLACED RT OVERHEAT DETECTION CARD PER AMM 26-11-02. OPS CK OK.SDR 2008UALA01583Switch · faultyLEFT ENGINE FIRE HANDLE AND L ENGINE FUEL CONTROL FIRE LIGHTS CAME ON, ENG NOT RUNNING AND IN. SUSPECT APU CARGO OVERHEAT SWITCH. REPLACED ENGINE APU CARGO OVERHEAT TEST SWITCH. GROUND CHECK NORMAL. AC OK FOR SERVICE.SDR UPS08651895Element · defectiveINSPECTION TYPE:ETOP DIVERSION - DURING CLIMBOUT A LEFT ENGINE DUCT LIGHT ILLUMINATED THE CREW RAN THE CHECKLIST CONTACTED DISPATCH, BUT WERE UNABLE TO CONTINUE TO BFI DUE TO ICING CONDITIONS. FLIGHT LANDED WITHOUT INCIDENT IN RFD. REMOVED AND REPLACED LEFT SDR HALA0800420Overheat Loop · malfunctionedETOPS SIGNIFICANT SYSTEM, INTERMITTENT EICAS STATUS MSG, R ENG OH LP2 DISPLAYED. REPLACED NR 2 ENG FWD UPPER LOOP PER AMM 26-11-02. OPS CHK PER AMM 26-11-00. ENGINE HIGH PWR RUN, NO DEFECTS NOTED.
SDR A6WA200840160Element · malfunctionedFOUND LT WING ANTI-ICE DUCT WARNING MESSAGE. REMOVED AND REPLACED HEAT SENSE ELEMENT A41WK REF AMM 36-21-04, OPS CHECK GOOD. (M)SDR AALA200800662Gasket · blownPBI INFLIGHT T862/17MAR - CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. RETURNED TO PBI AND LANDED WITHOUT INCIDENT. FOUND THE LEFT HAND PACK HIGH THERMOSTAT GASKET BLOWN. REPLACED THERMOSTAT, GASKET AND RIGHT PACK TEMPERATURE CONTROL VALVE. SDR COMA0860177Sensing Element · faultyFLIGHT 5664 - RECEIVED LEFT ANTI-ICE DUCT WARNING MESSAGE ON CLIMBOUT FROM CVG. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. REMOVED AND REPLACED AFT BAY HEAT SENSING ELEMENT (A47WK).SDR SMIA200807305Overheat Sensor · malfunctionedON FLIGHT 3306, CREW REPORTED ON THE GROUND THEY GOT A LEFT ENGINE TAIL PIPE HOT LIGHT DURING CLIMB-OUT FOLLOWED AOM. LIGHT DID NOT GO OUT THEY THEN SHUT DOWN ENGINE 1 AS A PRECAUTIONARY PROCEDURE AND RETURNED TO ACT. AIRCRAFT REMOVED FROM SERVICE. REMOVED SDR 2008UALA01316Circuit Card · overheatedL ENG OH LP 1 STATUS MESSAGE WILL NOT ERASE. FOUND OVERHEAT DETECTION CARD. RESEATED OVERHEAT CARD FOR NR 1 ENGINE MESSAGE CLEARED, FIRE-TEST CHECKS GOOD. AC OK FOR SERVICE.SDR MALA080035Overheat Sensor · malfunctionedTAIL PIPE HOT WARNING LIGHT ILLUMINATED IN FLIGHT, QRH COMPLETED. REMOVED AND REPLACED TAILPIPE OVERTEMP DETECTOR RDI CODE 30WG, P/N OFF/ON 17343-62-450 IAW AMM 26-12-05-04. OPS CHECK GOOD.SDR A6WA200840148Element · malfunctionedRT 14TH DUCT FAIL MESSAGE ILLUMINATED AT 15,000 FT AFTER DEPARTURE. PERFORMED QRH, MESSAGE DID NOT EXTINGUISH FOR APPROX 12 MINUTES. AIR DIVERSION DECLARED EMERGENCY LANDING. (K) REMOVED AND REPLACED FUSELAGE SENSING ELEMENT A46WK (RT SIDE) IAW AMM 36-21-04SDR COMA0860148Sensing Element · failedFLIGHT 5104- EN ROUTE FROM BNA TO JFK RECEIVED ANTI-ICE DUCT WARNING MESSAGE. PERFORMED QRH, MESSAGE PERSISTED. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO GSO AND LANDED SAFELY. REMOVED AND REPLACED RIGHT SIDE FUSELAGE SENSING ELEMENT (A18WK).
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