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 9617709886Overheat Sensor · malfunctionedUPON APPLYING TAKEOFF POWER, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACFT RETURNED TO THE GATE. AT GATE WITH APU ON AND LEFT PACK ON LIGHT CAME ON AGAIN. LIGHT WENT OUT WHEN LEFT PACK WAS SECURED. REPLACED BOTH LEFT AND RIGHT TAIL COMPARTMENT SDR UPS96220810Connector · wetON CLIMB-OUT FROM PHL, NR 1 ENGINE STRUT OVERHEAT LIGHT BEGAN FLICKERING. LIGHT BECAME STEADY UPON LEVEL OFF AT FL 280. ACCOMPLISHED ENGINE STRUT OVERHEAT QF CHECKLIST. LIGHT WENT OUT WHEN NR 1 THROTTLE RETARDED TO NEAR IDLE. AFTER ABOUT 5 MINS, LIGHT RE-ISDR 96FDEA01330Overheat Light · illuminatedAFTER T/O ON CLIMBOUT, ENG NR 1 STRUT OVERHEAT LITE ON. RAN CHKLST. ENG AT IDLE FOR 3 MIN LITE REMAINED ON. SHUTDOWN ENG PER CHKLST. AFTER 5 MIN LITE STILL ON. PULLED FIRE HANDLE AS PRECAUT. 2 MIN LATER LITE OFF. WINDMILL 20 MIN OIL PRESS 43. REMD PNLS TSDR VSTA9608001Overheat Element · brokenNR 2 ENG OVERHEAT LIGHT CAME ON. PULLED BACK POWER AND THE LIGHT STAYED ON. FIRED BOTH EXTINGUISHERS AND LIGHT STAYED ON. SHUT DOWN ENGINE, INSP, FOUND LOWER FWD ELEMENT BELOW G/BOX BROKEN. REMOVED AND REPLACED, OPS CHECK GOOD.SDR P5CA9600426Overheat Loop · crimpedCRIMPED OVER HEAT LOOP LEFT BODY GEAR WHEEL WELL PRESSURE DECK INBOARD, FOUND ON BLOWN TIRE INSPECTION. REPLACED LOOP AND TESTED PER BOEING MAINT MANUAL 26-17-02.SDR UPS96220664Sense Wires · chafedNR 1 ENGINE STRUT OVERHEAT FLICKERED TWICE DURING CRUISE. FOUND STRUT DETECTOR WIRES WITH MINOR SIGNS OF CHAFING. CORRECTED ALL CHAFING AREAS. SYSTEM CHECKS NORMAL. OK FOR SERVICE.SDR 96FDEA01266Overheat Light · illuminatedDISCREPANCY: (MOCC 96-137) NR 1 ENGINE STRUT OVERHEAT ILLUMINATED MOMENTARILY ON TAKEOFF. EXTINGUISHED WHEN POWER WAS REDUCED TO QUIET EPR. SYSTEM TESTED OK. CORRECTIVE ACTION: INSPECTED NR 1 ENGINE STUB WING DUCTING FOR LEAKS, NO DEFECTS NOTED, OK FOR SESDR USAAD96104Temp Sensors · failedFLT NR 1665 - PIT-FLL - 'TAIL COMPT TEMP HIGH' LIGHT ILLUMINATED DURING CLIMB. RETURNED TO FIELD. REPLACED WIRING BETWEEN TAIL COMPARTMENT TEMPERATURE SENSORS AND AFT PRESSURE BULKHEAD. (M)SDR UPS96220599Connector · chafedINSPECTION TYPE N/A, ENG 3 STRUT OVERHEAT LIGHT CAME ON JUST PRIOR TO LANDING. EXTINGUISHED AFTER ENGINE WAS SHUT DOWN. ENGINE SHUTDOWN DURING LANDING ROLL. *S/D* REPAIRED CHAFED WIRE AT FIRE WALL. REMOVED AND REPLACED CONNECTOR ON START STRUT, CONNECTOR SDR 96UAL900513Overheat Light · illuminatedBODY OVERHEAT LIGHT CAME ON, RETURNED TO SMF.SDR AALA961018Detector · defectiveDFW - FLT 544 - DURING MAX POWER TAKEOFF WITH OAT 104 DEGREES, TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED FOR APPROXIMATELY 1 MINUTE AND THEN ILLUMINATED AGAIN. AIRCRAFT RETURNED TO DFW AND PRIOR TO SDR USAASB96121Overheat Light · illuminatedBDA - FL 1459 - WHILE CLIMBING OUT OF DBA AT 24,000 FEET, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. REDUCED THRUST TO IDLE, HOWEVER, LIGHT REMAINED ON. CAPTAIN SHUT DOWN THE NR 1 ENGINE AND RETURN TO BDA. TOTAL SINGLE ENGINE TIME WAS 16 MINUTES. MAINTENASDR UPS96220583Overheat Detect · defectiveINSPECTION TYPE NA, NR 1 ENG FIRE DETECTION GROUND FAULT LIGHT STEADY IN FLIGHT, FIRE WARNING BELL SOUNDED. GROUND FAULT WAS EXTINGUISHED. REMOVED AND REPLACED NR 1 ENG FIRE OVERHEAT DETECTOR, OPS CHK GOOD PER M/M 26-11-00.SDR P5CA9600302Overheat Sensor · bare wireDURING TAXI OUT, LEFT WING OVERHEAT LIGHT ILLUMINATED. RETURNED TO BLOCKS. FOUND NR 4 LED GROUP WITH AN AIR LEAK, REPLACED SEAL IAW MM 36-11-01. FOUND SENSOR NR 2 INBOARD OF NR 2 PYLON WITH A BARE WIRE. REPAIRED SAME IAW MM 26-18-02. L/E OVERHEAT SYSTEM CSDR USAAD96085Circuit Breaker · failedFLT 765 - CLT-MSY - ON CLIMB, WHEEL WELL OVERHEAT CIRCUIT BREAKER POPPED. RETURNED TO FIELD. REPLACED CIRCUIT BREAKER. (M)SDR 9613716601Overheat Wire · failedDURING CLIMB, THE NR 3 HYDRAULIC SYSTEM OVERHEAT LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPAIRED WIRE FOR OVERHEAT INDICATION IN THE NR 3 HYDRAULISDR CA960711016Temp Switch · faulty(CAN) PILOT REPORT INDICATED THE ENGINE OVERHEAT LIGHT ILLUMINATED IN FLIGHT, BUT ALL OTHER PARAMETERS WERE NORMAL. STANDARD EMERGENCY PROCEDURES WERE FOLLOWED AND THE ENGINE WAS SHUTDOWN. MAINTENANCE CHECKED OUT THE SYSTEM AND REPLACED THE OVERHEAT DETECTOR. SDR AU960920Connector · faulty(AUS) NO1 ENGINE OVERHEAT WARNING SYSTEM FAULTY - LOOP A AND B CORE DETECTOR, CONNECTORS D3088 AND D3096 AND ASSOCIATED WIRING REPLACEDSDR AALA960920Control Unit · defectiveRDU - FLT 1880 - EN ROUTE MIA/DTW DURING CRUISE, LOWER AFT BODY OVERHEAT LIGHT BEGAN TO FLICKER. SHORTLY AFTER BEGINNING QRH PROCEDURE, LIGHTS STOPPED FLICKERING AND SYSTEM WOULD NOT TEST. AIRCRAFT DIVERTED TO RDU AND LANDED WITHOUT INCIDENT. REPLACED FIRE SDR 96UAL900433Overheat Element · failedAFTER TAKEOFF, LEFT WING/BODY OVERHEAT LIGHT CAME ON. ACCOMPLISHED IRREGULAR PROCEDURE, BUT LIGHT STAYED ON. RETURNED TO DEN. *S/D* FOUND OVERHEAT ELEMENT BAD. REPLACED M487 ELEMENT, CHECKS OK.SDR 96ZZZM1085Temp Sensor · air leakON FT 396 - ATL-RDU - THE TAIL COMPARTMENT HIGH LIGHT CAME ON APPROXIMATELY 4-5 MINUTES AFTER TAKEOFF. FOUND A/C TEMP HIGH SENSOR LEAKING AIR, REMOVED AND REPLACED THE TEMP SENSOR AND SEAL PER MM 36-00. OPS CHECK AND LEAK CHECK OK. (M)SDR 96FDEA01072Overheat Unit · malfunctionedDISCREPANCY: ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED WHEN NR 1 THROTTLE WAS RETARDED, LIGHT WENT OUT. FINISHED CHECK LIST RESULTING IN RIGHT PACK AND NR 3 BLEED ONLY USABLE. CORRECTIVE ACTION: RAN ENGINE NR 1 AT IDLE POWER, CHECKED PYLON AREA FOR ANYSDR 96UAL900413Overheat Det · inoperativeLOWER BODY OVERHEAT DOES NOT TEST. SUPPLEMENTAL DATA UPDATE: REPLACED FIRE AND OVERHEAT DETECTOR.SDR PLGA9606031Connector · dirtyJFK - FLT 4960 - ON CLIMB-OUT OF JFK, THE LT TAIL PIPE HOT LIGHT ILLUMINATED. THE CREW SECURED THE ENGINE AND RETURNED TO JFK LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND MOISTURE IN THE CANNON PLUG (RAINING AT THE TIME) TO SDR AALA960824Temp Sensor · defectiveDFW - FLT 2016 - ON ROTATION OUT OF DFW, THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RETURNED TO LAND DFW AND LIGHT EXTINGUISHED WITH POWER REDUCTION. LIGHT ILLUMINATED AGAIN WITH POWER INCREASE. LANDED DFW WITHOUT INCIDENT AND NORMAL WEIGHT. SDR 9610899943Temp Sensors · malfunctionedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB-OUT. FLIGHT RETURNED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH TEMPERATURE SENSORS. LEAK AND OPERATIONAL CHECK NORMAL.SDR 9610909943Temp Sensor · malfunctionedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB-OUT. FLIGHT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT TEMPERATURE SENSOR. LEAK CHECK WAS PERFORMED ON ALL PNEUMATIC DUCTING IN THE TAIL COMPARTMENT. NO LEAKSSDR 96ZZZM993High Temp Light · illuminatedTHE TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON IN FLIGHT.SDR 96ZZZM1084High Temp Light · illuminatedTHE TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON IN FLIGHT. (M)SDR 9610619987Overheat Sensor · failedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMBOUT. FLIGHT RETURNED TO SLC AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH THE LEFT AND RIGHT TAIL COMPARTMENT OVERHEAT SENSORS AND RIGHT CHECK VALVE. OPERATIONAL CHECK NORMAL.SDR GTIA96NK155Thermo Switch · malfunctionedTAIL COMPARTMENT TEMP HI-LIGHT ILLUMINATED AFTER TAKEOFF PRIOR TO 1000 FEET AGL. WARNING EXTINGUISHED WITH BOTH HP BLEED SWITCHES OFF. REPLACED TAIL COMPARTMENT TEMP SENSORS. OPS CHECKED GOOD. (M)SDR COMA9630104Hot Warning · activatedRIGHT TAILPIPE HOT WARNING CAME ON DURING CLIMB. RETURNED POWER LEVER AND WARNING EXTINGUISHED. AIRCRAFT RETURNED TO CVG. COULD NOT DUPLICATE DISCREPANCY. FALSE WARNING CAUSED BY RAIN.SDR 9608896634Overheat Sensor · failedDURING CRUISE, THE LEFT WING OVERHEAT LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO SEA AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT WING OVERHEAT SENSOR, OPERATIONAL CHECK GOOD.SDR P5CA9600208Overheat Sw · malfunctionedLEFT WING LEADING EDGE OVERHEAT LIGHT CAME ON AFTER ENGINE START. REPLACED OVERHEAT SWITCH INBOARD OF NR 2 ENGINE STA 388 IAW MM 26-18-02.SDR REXA96013Connector · broken wireLEFT TAIL PIPE 'HOT' LIGHT (CAPTION) ON DURING CLIMB-OUT. SHUT ENGINE DOWN AND RETURNED RAMP. LIGHT WAS ON WHOLE WAY BACK. REPLACED BROKEN WIRE ON LEFT ENGINE TAIL PIPE SPOT DETECTOR CANNON PLUG. AIRCRAFT OK FOR SERVICE. (M)SDR COMA9630093Overheat Det · dirtyRIGHT ENGINE TAIL PIPE H0T WARNING CAME ON. WARNING REMAINED AT REDUCED POWER. CLEANED AND SEALED WIRING CONNECTIONS ON RT TAIL PIPE HEAT SENSORS.SDR DL72S960659Overheat Sensor · out of positionLOWER AFT BODY OVERHEAT LIGHT ILLUM. C/W PROM LIGHT WENT OUT WHEN LT PACK AND BLEED TURNED OFF. REPOS OVERHEAT SENSOR IN 48 SECTION. RAN ENGINE WITH NO OVERHEAT IND.SDR USAASB96043Connector · failedFLT NR 311 - PHL - DURING TAKEOFF ROLL, LEFT WING BODY OVERHEAT LIGHT CAME ON. FLIGHT RETURNED TO FIELD. REPLACED CONNECTOR D886. OPS CHECKS SATISFACTORY. (M)SDR COMA9630054Overheat Light · illuminatedLEFT ENGINE TAIL PIPE HOT WARNING LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. FOUND NO DEFECTS WITH AIRCRAFT OR TAIL PIPE HOT WARNING SYSTEM. SUBMITTER STATED CAUSE OF FALSE WARNING IS MOISTURE. ACFT RETURNED TO SERVICE.SDR COMA9630052Overheat Warning · activatedRIGHT ENGINE TAIL PIPE HOT WARNING CAME ON SHORTLY AFTER TAKEOFF. FOUND NO DEFECTS WITH FIRE DETECTION SYSTEM. AIRCRAFT WAS IN HEAVY RAIN. MOISTURE WAS SUSPSECTED CAUSE OF FALSE WARNING.SDR QXEA9600094Connector · dirtyNR 2 ENGINE OVERHEAT LIGHT ILLUMINATED IN FLIGHT WITH ASSOCIATED MASTER WARNING LIGHT. NR 2 ENGINE SHUTDOWN PER CHECKLIST PROCEDURES AND WARNING LIGHT REMAINED ON AFTER ENGINE SHUTDOWN. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBLEM. CANNON PSDR COMA9630047Heat Sensor · wetRT TAIL PIPE HOT WARNING ILLUMINATED DURING TAKEOFF. DRIED MOISTURE ON THE TAIL PIPE HEAT SENSORS. ACFT RETURNED TO SERVICE.SDR USAASB96033Overheat Light · illuminatedFLT NR 800 - MCI - DURING CLIMB AT APPROXIMATELY 10,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT CAME ON. THE CAPTAIN REDUCED POWER AND THE LIGHT WENT OUT. PULLED NR 2 ENGINE BACK TO IDLE AND RETURNED TO MCI. (M)SDR 96FDEA00305Overheat Det · shortedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT WITH ENG ANTI-ICE ON. FOLLOWED PUBLISHED ABNORMAL PROCEDURES AND DETERMINED ENG NR 2 INLET ANTI-ICE SYS TO BE THE SOURCE OF THE OVERHEAT TEMP ON ENG NR 2 INLET. LEFT ENG NR 3 ANTI-ICE OFF FOR REMAINDESDR USAASB96030Overheat Det · malfunctionedFLT 771 - PIT - DIVERTED TO PIT DUE TO RIGHT WING AND BODY OVERHEAT. RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. WENT OUT SHORTLY AFTER RIGHT ENGINE BLEED VALVE WAS CLOSED ACCORDING TO FLIGHT MANUAL PROCEDURE. MAINTENANCE CHECKED WIRING RESISTANCESDR SRAA29601Detector · malfunctionedFLT ADT07 - ON TAKEOFF ROLL FROM MHZ, MASTER TURBINE OVERHEAT ILLUMINATED, ABORTED TAKEOFF AND RETURNED TO BLOCK. FOUND NR 3 ENGINE AT 7 O'CLOCK OVERHEAT DETECTOR DID NOT FUNCTION PROPERLY, REPLACED NR 7 DETECTOR. SYSTEM OPS CHECKED GOOD PER MM, CHAPTER 26. SDR DL72S960255Wire · brokenON CLIMBOUT, NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON, WING ANTI-ICE NOT ON, BUT DUCT TEMP SHOWED 200 DEGREES. FOUND STRUT WING ANTI-ICE VALVE STUCK OPEN. REMOVED AND REPLACED RELAY R32 AND FOUND BROKEN WIRES IN CANNON PLUG ON STRUT VALVE. REMOVED AND REPLASDR COMA9630018Weu · malfunctionedDURING TAKEOFF, LEFT ENGINE TAIL PIPE HOT WARNING CAME ON. REPLACED THE WARNING ELECTRONIC UNIT.SDR COMA9660007Element · defectiveLEFT 14TH STAGE DUCT OVERHEAT WARNING IS ON INTERMITTENTLY DURING FLIGHT. REPLACED THE PYLON SECTION OF THE 14TH STAGE BLEED LEAK DETECTION SYSTEM.SDR USAASB96001Element · shortedFLT NR 1244 - CLT - LEFT WING BODY OVERHEAT ILLUMINATED IN FLT. ISOLATED LEFT BLEED AIR DUCT BUT OVERHEAT LIGHT REMAINED ON. MAINTENANCE FOUND OVERHEAT ELEMENT SHORTED. REPLACED ELEMENT. OPS CHECKS SAT. (M)
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