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 97UAL900887Overheat Light · illuminatedLEFT WING BODY OVERHEAT LIGHT CAME ON AFTER TAKEOFF. NR 1 ENGINE BLEED AIR AND ISOLATION VALVE WERE SHUT OFF. LEFT PACK LIGHT STAYED ON UNTIL TOUCHDOWN. *S/D* APU WAS NOT RUNNING DURING THE EVENT. RAN NUMBER ONE ENGINE AND FOUND NO LEAKS. A RESISTANCE CHSDR UPS97225349Overheat Light · intermittentINSPECTION TYPE-N/A, DURING FLIGHT ENG NR 1 STRUT OVERHEAT LIGHT INTERMITTENTLY BEGIN FLUCTUATING ON AND OFF. INSPECTED NR 1 ENG STRUT FOUND OVERHEAT DETECTOR LOOP INSULATION MISSING. REINSTALLED SAME AND TIGHTEND LOOSE CONNECTOR, RUN NR 1 ENG AND FOUND NO FSDR C2XA97CL100Sensor · failedCLE - FLT 3283 - CREW REPORTED A DUCT LEAK ON RIGHT SIDE, PERFORMED QRH ITEMS AND LIGHT EXTINGUISHED AT 3 MINUTES AFTER BLEED WAS CLOSED. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED A DUCT LEAK SENSOR AND ALL OTHER SSDR 97UAL900877Overheat Det · shortedRIGHT HAND WING BODY OVERHEAT LIGHT CAME ON INTERMITTENTLY ONE MINUTE AFTER TAKEOFF. *S/D* TROUBLESHOOTING INDICATED THAT RIGHT-HAND WING LEADING EDGE OVERHEAT DETECTOR ELEMENT WAS SHORTED TO GROUND. REPLACED DETECTOR AND PERFORMED ENGINE RUN. SYSTEM CHECKSDR UPS97225337Overheat Sensor · malfunctionedINSPECTION TYPE-N/A, NR 1 STRUT OVERHEAT IN CLIMB. ACCOMP ENG SHUTDOWN. *S/D* REMOVED AND REPLACED BOTH NR 1 PYLON SENSING ELEMENTS, RAN ENGINE, NO AIR LEAKS NOTED. NO OVERHEAT NOTED, OPS CK SYS IAW MM 26-14-00.SDR UPS97225087Overheat Loop · out of positionINSPECTION TYPE-N/A, ON TAKEOFF ENG 1 STRUT OVERHEAT LIGHT ILLUMINATED. PER CHECK LIST, NR 1 THRUST LEVER RETARDED TO IDLE AND LIGHT WENT OUT. WHEN THRUST LEVER ADVANCED AGAIN, LIGHT RE-ILLUMINATED. LEFT THRUST IN IDLE AND RETURNED TO JAX. REMOVED NR 1 STRSDR DL757972369Overheat Switch · malfunctionedPASSING FL 260, RT BLEED, RT PACK AND RT BLEED VALVE LIGHT CAME ON. FOLLOWED CHECKLIST, RESET VALVE AND OPERATED NORMAL FOR A FEW SECONDS AND THEN ALL 3 LIGHTS RE-ILLUM. FOLLOWED PROCEDURE FOR ICING CONDITIONS, LEAVING RT SIDE OFF AND OPENED ISOLATION VALVE.SDR RRXA97311Smoke Detector · failedCARGO SMOKE WARNING LIGHT CAME ON IN FLIGHT, NO EVIDENCE OF SMOKE. FOUND NR 3 SMOKE DETECTOR STUCK IN TEST. REMOVED AND REPLACED NR 3 SMOKE DETECTOR, OPS CHECK NORMAL.SDR 97FDEA00807Overheat Light · malfunctionWHILE CONDUCTING THE PRESSURIZATION DISCREPANCY SHEET THE NR 1 STRUT OVERHEAT LIGHT BEGAN TO FLICKER. NR 1 BLEED OFF, LEFT PACK OFF, NR 2 BLEED CLOSED, NR 3 BLEED AND RIGHT PACK ON. RAN ALL 3 ENGINES, AND APU AND PACKS, UNABLE TO DUPLICATE. SYSTEM FUNCTIONASDR PLGA971025CConnector · contaminatedALB - FLT 4763 - TWENTY MINUTES AFTER TAKEOFF, THE RIGHT TAILPIPE HOT WARNING LIGHT ILLUMINATED. CREW FOLLOWED PROCEDURES AND SHUT DOWN THE RIGHT ENGINE. AIRCRAFT DIVERTED TO ALB AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED WATER FROM SYSTEM CONNECTOR ASDR SRAA971009Overheat Det · defectiveDURING FLIGHT, NR 1 TURBINE OVERHEAT LIGHT CAME ON, RETARDED THROTTLE TO 977 AND LIGHT WENT OUT. AIRCRAFT ARRIVE AT DESTINATION WITHOUT INCIDENT. INSPECTED OVERHEAT DETECTORS AND FOUND ELEMENTS DEFECTIVE. REPLACED DETECTORS AND OPS CHECKED GOOD PER MM CH 26SDR CA971106006Loop · failed(CAN) LEFT ENGINE 14TH STAGE OVERHEAT WARNING DISPLAYED, THROTTLE RETARDED AND MESSAGE REMAINED, ENG SHUT DOWN AND AIRCRAFT RETURNED TO BLOCKS. 14TH STAGE LOOP SHORTED TO GROUND. LOOP REPLACED.SDR 97UAL900769Overheat Light · illuminatedLANDED DFW UNDER AMBER ALERT WITH NR 1 ENGINE SHUT DOWN DUE TO STRUT OVERHEAT LIGHT.SDR SRAA971002Wire · looseON APPROACH, MASTER NACELLE OVERHEAT WARNING LIGHT CAME ON WHEN LANDING GEAR HANDLE WAS PLACED IN THE DOWN POSITION. FOUND NACELLE MASTER WARNING LIGHT WIRING LOOSE. REPAIRED WIRING TO SWITCH AND REFORMED OPS CHECK PER MM CH 26.SDR COMA9710419Wire · shortedAVIONICS BAY OVERHEAT WARNING ON. REPAIRED OVERTEMP SENSOR WIRING (P/N W012-0203-20).SDR VTZA97506Overheat Light · illuminatedFLT 6150 - IAD-EWR - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO LEFT DUCT OVERTEMP LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND FREED PACK. OPS CHECK OK, COULD NOT DUPLICATE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE (M)SDR P5CA9701591Wire · chafedCHAFED WIRE CAUSED RIGHT WING OVERHEAT WARNING LIGHT TO ILLUMINATE AFTER TAKEOFF. FOLLOWED PROCEDURES PER CHECKLIST AND LIGHT REMAINED ON. RETURNED TO DEPARTURE STATION. WIRE CHAFED DUE TO RUBBING ON CLAMP, REPAIRED PER BAC WDM 26-18-11 AND TESTED OK PER BASDR 97FDEA00652Sensing Element · malfunction97-0178 4 MINUTES 30 SECONDS AFTER SWITCHING BLEEDS AT FLIGHT LEVEL 180 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. BLEED SWITCHED BACK (NR 1 BACK ON, NR 2 OFF) AND LIGHT WENT OUT AFTER 4 MINUTES.RAN ALL 3 ENGINE PER JET RUN HANDBOOK AND COULD NOT DUPLICATE PRSDR USAASB97251Overheat Loop · failedPHL - FL 1268 - FLIGHT RETURNED TO FIELD AT PHL DUE TO A RIGHT WING BODY OVERHEAT LIGHT ILLUMINATING. CREW COULD NOT GET THE LIGHT TO EXTINGUISH, INDICATING CONDITION STILL EXISTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OVERHEAT DETECTSDR AALA971749Sensor · defectiveMCO - FLT 0060 - AFTER TAKEOFF DFW DURING CLIMB-OUT, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED FOR APPROXIMATELY ONE MINUTE AND THEN EXTINGUISHED WHEN HIGH PRESSURE BLEED SELECTED CLOSED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO MCO,SDR 97UAL900679Overheat Warn · activatedEICAS EQUIPMENT OVERHEAT AND STATUS MESSAGES, SUPPLY FAN AND OVERBOARD EXHAUST VALVE DISPLAYED IN NORMAL. ALTERNATE EQUIPMENT COOLING DOES NOT CLEAR MESSAGES PER CREW. A/C DIVERTED TO ORD UNDER AMBER ALERT.SDR 97ZZZX4289Switch · failedAIRCRAFT DEPARTED. EN ROUTE EXPERIENCED RT ENGINE ALTERNATOR OVERHEAT MESSAGE ON EICAS. PIC TOOK CORRECTIVE ACTION AND RETURNED. TROUBLESHOOTING REVEALED RT ALT OVERHEAT SWITCH FAILED IN TRIPPED CONDITION. REMOVED AND REPLACED WITH NEW SWITCH. OPS CHECK AOSDR 97FDEA00596Overheat Light · wrong bulbLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED 5 MINUTES AFTER SWITCHING LEFT AIR CONDITIONING PACK FROM NR 1 TO NR 2 ENGINE. CHECKLIST COMPLIED WITH LIGHT WENT OUT AFTER CLOSING NR 1 START LEVER. RAN ALL 3 ENGINES WITH ALL BLEEDS OPEN AND BOTH PACKS ON COULD NOTSDR AALA971599Detector · defectiveMIA - FLT 2103 - AFTER TAKEOFF MIA DURING CLIMB-OUT, NR 1 ENGINE STRUT OVERHEAT INDICATION FLICKERED. ACCOMPLISHED ABNORMAL PROCEDURE AND PRECAUTIONARY SHUTDOWN NR 1 ENGINE. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE STRUT OVSDR REXA97232Spot Detectors · failedRIGHT TAIL PIPE HOT LIGHT AFTER TAKEOFF. REMOVED AND REPLACED ALL THREE SPOT DETECTORS ON RIGHT ENGINE. (M)SDR 97FDEA00533Overheat Light · illuminatedSHORTLY AFTER SWITCHING BLEEDS FOR THE RIGHT PACK FROM THE NR 3 ENGINE TO THE NR 2 ENGINE DURING CLIMB ABOVE FLIGHT LEVEL 180 THE LOWER AFT BODY OVERHEAT WARN LIGHT ILLUM. WE PERFORMED THE STEPS AS PER THE EMERGENCY CK LIST PROC FOR THE LWR AFT BODY OVERHEAT.SDR P5CA9701401Overheat Wire · shortedINTERMITTENT LEFT WING OVERHEAT LIGHT ON. ISOLATION VALVE AND ENGINES 1 AND 2 BLEED VALVES CLOSED. FOUND WIRE W640-1W728-18R SHORTED, REPAIRED WIRING PER BAC WDM AND OPS CHECK PERFORMED IN CONJUNCTION WITH HIGH POWER ENGINE RUN OPS NOW NORMAL. CLEARED DEFERSDR P5CA9701389Overheat Wire · shortedOVERHEAT WARNING LIGHT FOR LEFT WING ON IN FLIGHT, LEFT WING ISOLATION VALVE AND ENGINES 1 AND 2 BLEED VALVES CLOSED AND LIGHT OFF. FOUND WING OVERHEAT SENSOR S1052 DAMAGED. DEACTIVATED AND DEFERED S 1052 PER MEL 26-22-1A.SDR REXA97220Probes · dirtyTAIL PIPE HOT LIGHT ON AFTER TAKEOFF. REMOVED MOISTURE AND CLEANED PROBES. (M)SDR USAASB97219Connector · brokenLAX - FL428 - DURING CLIMB-OUT AFTER DEPARTURE, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED (FLICKERING). INITIALLY MASTER CAUTION DID NOT ILLUMINATE. WHEN OVERHEAT ILLUMINATED STEADY, MASTER CAUTION ALSO ILLUMINATED. WHEN THRUST LOWERED LIGHT WENT OUT. RETURNESDR 97FDEA00503Overheat Light · illuminatedDURING CLIMBOUT AT FLIGHT LEVEL 200, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH ABNORMAL CHECKLIST. LOWER AFT BODY OVERHEAT LIGHT EXTINGUISHED WITH LEFT PACK OFF AND NR 1 THROTTLE RETARDED. CHECKED AFT STAIRS AREA, NO LEAKS. REMOVED AFT FOSDR 97UAL900602Overheat Light · illuminatedAT TAKEOFF AND HIGH POWER SETTINGS NR 1 STRUT OVERHEAT LIGHT ON. WITH THROTTLE PULLED BACK LIGHT WOULD GO OUT. RETURNED TO ORD. *S/D* REPLACED DUCT DUE TO WEAR.SDR COMA9760145Overheat Loop · failedLT 14TH STAGE BLEED AIR DUCT WARNING. FALSE WARNING, REPLACED PYLON DETECTION LOOP.SDR P5CA9701378Overheat Switch · out of positionLEFT WING LEADING EDGE OVERHEAT LIGHT FLICKERED INTERMITTENTLY, WING BLEED ISOLATED, LIGHT CONTINUED TO FLICKER. FOUND S-898 LEADING EDGE OVERHEAT SWITCH TOUCHING STRUCTURE CORRECTED SWITCH POSITION TO NORMAL TESTED PER M/M 26-18-00. ALSO, CHECKED FOR PNEUMASDR DLM88971467Temp Sensor · failedTAIL COMPARTMENT TEMP HI LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABORTED AT 1OO KIAS 136,000 LBS. REPLACED RIGHT TAIL COMPARTMENT TEMP SENSOR. RAN RIGHT ENGINE AND PACK PER PFHB. ALL SYS CHECK GOOD PER 36-20-02.SDR 9714699861Overheat Sensor · failedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED INTERMITTENTLY DURING CLIMB-OUT OF MSP. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED BOTH OVERHEAT SENSORS IN TAIL COMPARTMENT. OPERATIONAL CHECK OK.SDR 97FDEA00472Detection Unit · malfunctionedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN CRUISE FLIGHT. (NO ANTI-ICE ON AT ALL). NR 2 ENGINE LEFT BLEED ON NR 3 BLEED ON, LEFT AND RIGHT PACKS ON. FOLLOWED RED TABS PROCEDURES. LIGHT WENT OUT AFTER NR 1 ENGINE BLEED TURNED OFF FOR SEVERAL MINUTES. RANSDR DLM90971427Temp Sensor · malfunctionedRT TAIL HIGH TEMP ILLUM AFTER T/O. REPLACED RT HI TEMP SENSOR RAN ENGS W/PYLON PLATES OPENED. NO LEAKS NOTED RAN ENG TO T/O PWR FOR 4 MINS ALL IND NRML.SDR 9713899953Temp Sensor · failedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TEMPERATURE SENSOR, OPERATIONAL CHECK NORMAL.SDR 98UAL900323Overheat Det · failedRIGHT BODY OVERHEAT LIGHT CAME ON IN FLIGHT, SHUT OFF PNEUMATICS AND THE PACK LIGHT STAYED ON. *S/D* REPLACED LOOP M1204 PER MM 26-18-11 AND OPS CHECKED OK PER MM 26-18-00.SDR 97ZZZM773Overheat Loop · failedFCO - FL 3 - AFTER TAKEOFF, CREW RECEIVED EICAS MESSAGES 'R ENG FIRE LP' AND 'R ENG OVHT LP', FOLLOWED BY THE RIGHT FIRE LIGHT AND FIRE BELL. THE CREW REDUCED POWER ON THE RIGHT ENGINE, AND THE INDICATIONS CEASED. FLIGHT RETURNED TO FCO AND LANDED WITH NO FUSDR 97FDEA00415Overheat Sensor · out of position97-0125 REPEAT ITEM (SEE AIRCRAFT MAINTENANCE LOG # 51863). LOWER AFT BODY LIGHT ILLUMINATED DURING CLIMB. FOLLOWED CHECK LIST PROCEDURE. SHUTDOWN LEFT PACK AND ENGINE NR 2 BLEED VALVE RETARDED NR 1 THROTTLE AND LIGHT WENT OUT. RESTORED NR 1 THROTTLE ANDSDR PLGA970704AOvertemp Warn · illuminatedLGA - FLT 4720 - ON TAKEOFF, THE RIGHT ENGINE OVERTEMP WARNING ILLUMINATED FOR APPROXIMATELY ONE SECOND. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. TRANSCIENT ITT SPIKE FOR ONE SECOND IS WITHIN LIMITS PER GE MM SPECIAL PROCEDURES. ENGINE WAS PLASDR 9712989862Overheat Sensor · malfunctionedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ACCOMPANIED BY MASTER WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. CREW ABORTED TAKEOFF AT 110 KNOTS AND AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE INSPECTED SYSTEM AND NO LEAK OR PROBLEMS WERE FOUND. REPLACED TSDR P5CA9701216Wire · brokenRIGHT WING OVERHEAT LIGHT ON. ISOLATED RIGHT WING IAW CHECKLIST LIGHT DID NOT GO OUT WITH EITHER NR 3 OR NR 4 ENGINE AT IDLE. WITH NR 3 ENGINE OF AND NR 4 ENGINE AT IDLE LIGHT WENT STEADY ON. FOUND WIRES TO AFT OVERHEAT SENSOR IN NR 4 PYLON BROKEN FROM SENSSDR AALA971149Overheat Loop · dirtyLAX - FLT 0032 - DURING DEPARTURE FROM LAX, LEFT ENGINE OVERHEAT EICAS MESSAGE APPEARED, THROTTLE WAS RETARDED. WHEN THROTTLE WAS ADVANCED, THE MESSAGE APPEARED ONCE AGAIN. AIR INTERRUPTED AND RETURNED TO LAX, LANDED WITHOUT FURTHER INCIDENT. CHECKED RESISTSDR CA970626002Clamp · worn(CAN) ECIAS MESSAGE "DETECT FIRE/OHT 2". AIRCRAFT RETURNED. LOWER AFT LPB ELEMENT OPEN, REPLACED. FIVE CLAMPS WORN ON LOOP A WEARING INTO WIRE REPAIRED.SDR 9712279884Temp Sensor · failedAFTER TAKEOFF, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. LIGHT WENT OUT WITH POWER REDUCTION. FLIGHT RETURNED TO TPA AND LANDED WITHOUT INCIDENT. INSPECTED FOR TAIL COMPARTMENT AIR LEAKS AND REPLACED THE LEFT TEMPERATURE SENSOR, OPERATIONAL CHECKSDR EISA08138Connector · dirtyLOWER AFT BODY OVERHEAT LIGHT ON. CLEANED LOOP CONNECTORS. (X)SDR 97FDEA00341Overheat Wire · looseLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AT FL 250 REFERRED TO RED TAB OK LIST PG 2-/-14. LIGHT EXTINGUISHED AFTER STEP 14. A CHECKLIST INDICATES LEAK BETWEEN BLEED VALVE AND PACK VALVE. FOUND SENSING ELEMENT DISCONNECTED FROM SUPPORT CLAMP AND DROPPING DO
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