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 MALA976375Connector · dirtyRIGHT TAIL PIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF FROM ELM. AFTER PERFORMING MEMORY ITEMS AND REDUCING POWER ON RIGHT ENGINE THE LIGHT EXTINGUISHED. PER THE QRH, OPERATED THE RIGHT ENGINE AT REDUCED POWER AND RETURNED TO ELM. MAINTENANCE REMOVED RIGHT ENGSDR COMA9960092Overheat Syst · malfunctionedAIRCRAFT MADE UNSCHEDULED LANDING WHEN ENCOUNTERING ICING CONDITIONS WITH GEAR DOWN WHILE MLG OVERHEAT SYSTEM WAS DEFERRED. REPAIRED MLG OVERHEAT WARNING SYSTEM.SDR 99FDEA00076Overheat Loop · out of positionENGINE NR 3 STRUT OVERHEAT MOMENTARILY FLICKERED FOR 1 SEC ON APPROACH. INSP NR 3 ENGINE STRUT FOR LOOSE CLAMPS AND ADEQUATE CLEARANCE OF DETECTOR LOOP. TIGHTENED SEV CLAMPS PER MM 26-14-1. RAN ENG PER JET RUN HDBK, NO STRUT OVERHEAT LIGHT ILLUM. ALL INDICSDR SWAA990322Overheat Loop · malfunctionedWING BODY OVERHEAT CAME ON DURING PUSHBACK. COMPLIED WITH QRH AND RETURNED TO GATE. LIGHT REMAINED ON, CONTINUED PER MEL 26-12. REMOVED AND REPLACED APU O/H LOOP AND WINGBODY O/H LOOP PER M/M. OPS CK OK PER M/M.SDR 99UAL900094Overheat Element · malfunctionedRIGHT HAND WING-BODY OVERHEAT WARNING. *S/D* REPLACED THE RIGHT WING LEADING EDGE DETECTOR ELEMENT ITEM M1204, REFERENCE MM 26-18-11 PG 401, OPS CHECK OK.SDR DL733990219Overheat Light · illuminatedON APPROACH COS, NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW DISCHARGED BOTH BOTTLES, LIGHT REMAINED ILLUMINATED EVEN AFTER ENGINE SHUTDOWN. PARTS ARRIVING FROM SLC AND DFW. REPLACED BOTH FIRE BOTTLES, FIRE TEST MODULE AND LOWER LOOP.SDR MALA976312Hot Light · illuminatedRIGHT TAIL PIPE HOT INDICATION ON CLIMBOUT. RETURNED TO SBN. MAINTENANCE PERFORMED GROUND RUNS WITH CREW, COULD NOT DUPLICATE.SDR C2XA99CL010Sensor · failedGSO - FLT 3346 - CREW REPORTED THAT IN-FLIGHT, THEY RECEIVED A LEFT DUCT LEAK AURAL WARNING, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED A DUCT TEMP SENSOR IAW EMB-120 MM 20-21-00, OPERATIONAL CHECKS WERE SATISFACTORYSDR F3LA99003Warning System · illuminatedLAS - FLT 772 - AIR TURN BACK, FLIGHT CREW REPORTED NR 2 ENGINE OVERHEAT LIGHT ILLUMINATE INFLIGHT. NR 2 ENGINE WAS SHUT DOWN AND BOTH FIRE EXTINGUISHER BOTTLES WERE DISCHARGED. AIRCAFT RETURNED TO LAS WITHOUT INCIDENT. MAINTENANCE REPLACED ENGINE/APU FIRE SDR MALA976304Hot Light · illuminatedRIGHT TAIL PIPE HOT CWP CAME ON INTERMITTENTLY. REDUCED POWER AND LIGHT NEVER CAME ON AGAIN. AIRCRAFT RETURNED TO DTW. MAINTENANCE RAN ENGINES AT TAKEOFF POWER AND VISUALLY CHECKED WIRES. COULD NOT DUPLICATE THE PROBLEM. ALL CHECKS GOOD AT THIS TIME.SDR 98UAL900599Overheat Light · illuminatedDUCT OVERHEAT INDICATION. RAN LEFT PACK ON GROUND PER MAINTENANCE MANUAL SERVICE TIP 21-61-99-PG200 SYSTEM CHECK'S OKAY, NO FAULTS FOUND.SDR EISA98284Overheat Light · illuminatedSHORTLY AFTER SELECTING WING ANTI-ICE ON, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, EXTINGUISHED AFTER TURNING OFF ENGINE NR 3 ANTI-ICE. ENGINE NR 1 OPENED NORMAL. OPS CHECKED IN AIR AND GROUND MODES, OPS CHECKED NORMAL IAW MM CHAPTER 26. (M)SDR SWIA971329Warning · activatedRIGHT DUCT LEAK WARNING OCCURRED DURING TAKEOFF. RETURNED TO AIRPORT MEL 75-32-2. OPS CHECKS GOOD WITH NO DEFECTS NOTED.SDR EISA98251Detector · inoperativeNR 3 ENGINE STRUT OVERHEAT LIGHT ON, ISOLATED TO BLEED. GENERATED FROM PILOT REPORT. REPLACED FIRE OVERHEAT DETECTOR ACCESSORY BOX IAW MM 20-10-17, OPS CHECK NORMAL MM 26-14-11. (M)SDR 98UAL900520Element · failedAPU FIRE LIGHT CAME ON. NO EXTERIOR INDICATIONS. REPLACED APU TAIL PIPE OVER HEAT SENSING ELEMENT AND WIRE HARNESS FOR OVER HEAT ELEMENT, REF MM 26-15-14. TESTED OK.SDR 98FDEA00675Connector · dirtyDURING CLIMB WITH ENG ANTI-ICE ON, ENG NR 3 STRUT OVERHEAT LIGHT ILLUM. ALL ITEM IN EMERGENCY CHECKLIST ACCOMP. LIGHT WENT OUT AND REMAINED OUT WHEN THRUST WAS RESTORED. REPEAT WRITEUP. CONNECTION TO STRUT OVERHEAT DETECTOR REMOVED. CLEANED AND REFITTED. SDR COMA9860299Overheat Loop · malfunctionedRIGHT 14TH STAGE DUCT MESSAGE DURING FLIGHT. REPLACED THE RIGHT 14TH STAGE DUCT LOOP.SDR 98FDEA00639Loop · out of position98-244 WITH RT PACK ON, RT NR 2 BLD OPEN, LT PK OFF AND ALL OTHER BLDS CLOSED. THE LWR AFT BODY O/H LIGHT CAME ON PER RED TABS. LIGHT WENT OUT WHEN NR 1 ENG BLD AND LT PK WERE OPEN/TURN ON RESPECTIVELY. FOUND LOOP PUSH DOWN CLOSE TO RT DUCT WORK. REPOSITISDR COMA9860291Wire · out of positionJET PIPE OVERHEAT FAIL WARNING. WIRING TERMINALS SHORTING TO ENGINE COWLING. INSULATED TERMINALS FROM COWLING.SDR USAASB98253Overheat Loop · failedCLT - FLT 835 - DURING CLIMB-OUT FROM CLT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. AFTER ACCOMPLISHING APPROPRIATE CHECKLIST, LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND THE ENGISDR COMA9860261Detector · malfunctionedLEFT 14TH STAGE BLEED AIR LEAK WARNING. REPLACED THE PYLON LEAK DETECTOR LOOP.SDR 98FDEA00530Overheat Light · malfunctionedCLIMBING THRU 16,000 LWR AFT BODY OVERHEAT LIGHT CAME ON. CLOSED NR 1 BLD AND LT PACK, WENT TO IDLE PWR ON NR 1 ENG. RAN BOTH PACK WITH APU AND WITH NR 1 AND 3 ENG, COULDN'T DUP. CK TEMP GUN FOR HOT SPOT, NONE FOUND. LEAK CHK GOOD AT HIGH POWER CW (144405).SDR UPS98227428Overheat Loop · looseENGINE STRUT OVERHEAT LIGHT ILLUMINATED DURING FLT. ENGINE WAS SHUTDOWN FOR REMAINDER OF FLIGHT. FOUND BACKSHELL LOOSE ON OVERHEAT LOOP AT STATION NR 48. RAN ENGINE AND OPS CKS OK.SDR ORJA98193Overheat Loop · malfunctionedFROM RENO, AIR TURNBACK TO RENO, TAIL COMPT TEMP HIGH LIGHT CAME ON AFTER TAKEOFF. STAYED ON FOR 3 MINUTES. WENT OUT ON FIRST POWER REDUCTION. RAN ENGINES NR 1 AND NR 2 AND APU AT TAKEOFF POWER 3 TIMES. COULD NOT DUPLICATE TAIL TEMP HIGH LIGHT AT THIS TIMESDR DHL98741003Overheat Loop · out of positionDURING CLIMB LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. ABNORMAL CHECKILIST ACCOMPLISHED AND AT ONE MINUTE WITH NR 1 ENG BLEED CLOSED, LIGHT EXTIGUISHED. TROUBLE SHOT SYSTEM PER 26-14-00. FOUND AFT LEFT LOOP TOUCHING STRUTURE. REPOSITIONED LOOP, RAN AIRCRASDR AALA981462Sensors · malfunctionedDFW - FLT T0071 - SHORTLY AFTER TAKEOFF, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. APU WAS NOT RUNNING. DURING PERFORMANCE OF CHECK LIST, THE LIGHT EXTINGUISHED. REPLACED LEFT AND RIGHT HIGH TEMPERATURE SENSORS IN TAIL. RAN ENGINES AT POWER FOR SDR COMA9860209Overheat Element · malfunctionedLEFT HAND STAGE BLEED DUCT LEAK WARNING. REPLACED THE BLEED LEAK SENSING ELEMENT IN LEFT HAND ENGINE PYLON.SDR USAASB98199Harness · failedIAH - FLT 1934 - SHORTLY AFTER TAKEOFF, THE NR 2 ENGINE OVERHEAT LIGHT AND THE MASTER CAUTION LIGHT ILLUMINATED. CREW WENT THROUGH EMERGENCY PROCEDURES, DISCHARGED BOTH ENGINE FIRE BOTTLES AND SHUT DOWN THE NR 2 ENGINE. FLIGHT RETURNED TO FIELD AT IAH AND LASDR 9809859620Sensor · failedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT WAS RETURNED TO OKC. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT TAIL COMPARTMENT TEMPERATURE SENSOR. OPERATIONAL CHECK NORMAL.SDR ORJA98194Detector · malfunctionedRETURN TO RENO, TAIL COMPT TEMP HI LIGHT CAME ON FOR 2 MINUTES AFTER TAKEOFF. OPERATING WITH LEFT THROTTLE RETARDED FOR 2 MINUTES, LIGHT WENT OUT. RESTORED THROTTLE AND TURNED LT PACK OFF. LIGHT CAME ON, THEN WENT OUT. PERFORMED MAINTENANCE ENGINE RUN PER SDR EIAA980232Engine · overtempJFK - LOG PAGE: F73265 - EN ROUTE FROM KLCK TO KJFK, NR 1 ENGINE NACELLE TEMP WENT TO 720 DURING CLIMB, INCREASED TO 820. ACCOMPLISHED NAC OVERTEMP PROCEDURE, NO HELP. ACCOMPLISHED IN-FLIGHT SHUT DOWN CHECK LIST. WINDMILL TIME, 1 HOUR NAC TEMP, WENT TO ZERSDR 98UAL900334Detector · out of positionON TAKEOFF, NR 2 ENGINE LOWER AFT BODY OVERHEAT LIGHT CAME ON. REDUCED POWER AND LIGHT WENT OUT. BY KEEPING REDUCED POWER, LIGHT STAYED OUT. RETURNED TO DEN. *S/D* MAINTENANCE RAN ENGINE, APU AND OPERATED A/C PACKS, NO LEAKS FOUND. REPOSITIONED EMPENNAGESDR 98UAL900336Clamp · looseLEFT WING BODY OVERHEAT WARNING LIGHT ILLUMINATED DURING CLIMB. *S/D* ADJUSTED CLAMP ON THERMOCOUPLES AND LIGHT DID NOT ILLUMINATE.SDR ORJA98169Sensor · malfunctionedTAIL COMPARTMENT TEMP HIGH, LIGHT ILLUMINATED AFTER TAKEOFF. QRH PROCEDURE ACCOMPLISHED. LIGHT EXTINGUISHED. MAINTENANCE REMOVED SIDE PANELS. INSPECTED DUCTS WITH PACKS RUNNING. NO LEAKS NOTED. INSPECTED TEMP SENSOR AND AIR OUTLET. COULD NOT DUPLICATE ASDR AALA981371Sensors · malfunctionedDFW - FLT 1676 - AFTER TAKEOFF DFW, THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. STAYED ON STEADY FOR ABOUT 30 SECONDS. ACCOMPLISHED EMERGENCY PROCEDURES CHECK LIST. THE LIGHT FLICKERED ON AND OFF FOR ABOUT 2 MINUTES. DECISION TO LAND BACK AT DSDR 98UAL900322Overheat Det · failedRIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. *S/D* FOUND RIGHT WING LEADING EDGE OVERHEAT DETECTOR (M1204) SHORTED. REPLACED THE DETECTOR AND OPS CHECKED OK.SDR BJNA980701Sensor · malfunctionedLEFT WING BODY OVERHEAT LIGHT ILLUMINATED. AIRCRAFT RELEASED PER MEL 26-12, DMI 701, ITEM TRANSFERRED TO DMI LOG AND PLACARDED. REF: DMI 701, REMOVED AND REPLACED OVERHEAT LOOP IN APU COMPARTMENT IAW 26-18. OPS CHECKS NORMAL. (LOG PAGE 10721). (X)SDR SPAA9800003Sensor · out of positionEN ROUTE BETWEEN DLH AND JAX, THE NR 1 ENGINE WAS SHUT DOWN DUE TO AN OVERHEAT WARNING. BOTH ENGINE FIRE EXTINGUISHER CYLINDERS WERE DISCHARGED. AIRCRAFT DIVERTED TO SAV AND LANDED WITHOUT INCIDENT. UPON INSPECTION, THE NR 1 ENGINE LOWER OVERHEAT SENSING ELSDR BJNA980604Insulator · mislocatedON GROUND LEFT WING BODY OVERHEAT ILLUMINATED. IN THE APU COMPARTMENT, THE OVERHEAT LOOP ELEMENT IS POSITIONED A FEW INCHES ABOVE THE BLEED AIR SUPPLY DUCT. THIS ELEMENT IS HELD IN POSITION BY NUMEROUS CLAMPS WITH INSULATORS DURING TROUBLESHOOTING, AN INSULASDR BJNA980603Detector · out of positionNR 1 WING BODY OVERHEAT ILLUMINATED INTERMITTENTLY AFTER TAKEOFF AT BFF WITH BLEEDS OFF, APU ON TAKEOFF, REMAINED OFF AFTER BLEEDS RECONFIGURED. DISCOVERED OVERHEAT DETECTOR AGAINST APU BLEED SUPPLY DUCT, RELOCATED AND RAN APU AT MAX TEMP FOR 40 MIN, NO DISCRSDR UPS98227040Overheat Det · malfunctionedPASSING 10,000 FT ON CLIMB-OUT, WHEEL WELL LIGHT FLASHED AND BELL RANG MOMENTARILY. PASSING 7,000 FT ON DESCENT, CAME ON AND STAYED ON UNTIL GEAR WAS EXTENDED. MEASURED BRAKE TEMPERATURE AT BLOCK-IN AND NO HOT BRAKE WAS NOTED. INSPECTED ALL WHEEL WELLS WITHSDR 98UAL900275Wire · looseNUMBER TWO ENGINE OVER TEMPERATURE INDICATION. *S/D* HEAT DAMAGE NEAR FRONT OF FUEL CONTROL CAUSED WIRE TO BE PULLED LOOSE. REPLACED CONNECTOR.SDR 98UAL900238Overheat Light · illuminatedLOWER AFT BODY OVER HEAT LIGHT ON. AFTER TURNING APU OFF LIGHT FLICKERS.SDR BJNA980506Overheat Light · illuminatedLEFT WING BODY OVERHEAT LIGHT ILLUMINATED DURING THE DESCENT INTO KEKO. AIRCRAFT RELEASED PER MEL 26-12, DMI 10508, ITEM PLACARDED AND TRANSFERRED TO DMI LOG. (M)SDR BJNA980503Connector · dirtyLEFT WING BODY OVERHEAT ILLUMINATES INTERMITTENTLY. CLEANED CONNECTORS ON FORWARD AND AFT KEEL BEAM SENSOR, OPS CHECK NORMAL. OK FOR SERVICE. (M)SDR CA980602025Sensor · failed(CAN) AIRCRAFT TURNED BACK DUE TO L/H WING OVERHEAT LIGHT ON AND MASTER CAUTION LIGHT FLICKERING ON. FOUND SENSOR TOUCHING BLEED DUCT AND A LOOSE GROUND WIRE TO SENSOR. REPOSITIONED SENSOR AND CHECKED CONNECTIONS. ENGINE RUN OK.SDR BJNA980502Connector · dirtyLEFT WING BODY OVERHEAT LIGHT CAME ON DURING DESCENT. CLEANED CONNECTORS OF SENSING ELEMENT ON LEFT ENGINE STRUT CAVITY TESTED WING AND LOWER AFT BODY OVERHEAT DETECTION SYSTEM PER BMM 26-18-0, PAGE 501, TO 502, TEST OK. (M)SDR COMA9860113Overheat Loop · malfunctionedRT 14TH STAGE BLEED AIR DUCT LEAK WARNING IFSD. REPLACED THE PYLON BLEED AIR LEAK DETECTION LOOP.SDR BJNA980501Overheat Light · illuminatedLEFT WING BODY OVERHEAT LIGHT CAME ON EN ROUTE. REMOVED AND REPLACED COMP OVERHEAT UNIT PER BMM 26-17-0, OPS TEST PERFORMED PER BMM 26-18-0, TEST OK. (M)SDR 98FDEA00361Overheat Light · illuminatedLOWER AFT BODY OVERHEAT LIGHT CAME ON JUST AFTER FIRST LEVEL OFF. NR 2 AND NR 3 BLEEDS OPEN BOTH PACKS ON, LIGHT WENT OUT AFTER ONE MINUTE BUT CAME BACK ON DURING CLIMB. STARTED RED TAB PROCEDURE, LIGHT WENT OUT WHEN NR 1 BLEED AND LEFT PACK TURNED OFF REMAI
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