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 03FDEA01594Element · groundedLOWER AFT BODY HEAT LIGHT ILLUMINATED, FOLLOWED RED TAB PROCEDURES AND LIGHT EXTINGUISHED. LIGHT ILLUMINATED DURING CLIMB EPR AT 205. PER RED TAB ISOLATION PRODEDURE FAULT OCCURRED IN NR 3 ENG - RH PACK PNEU DUCTING. INSPECTED AFT AIRSTAIR AREA O/H LOOP ANSDR 2003F00617Warning System · malfunctionedTIL - FLT 6014 - LT WING OVERHEAT LIGHT CAME ON DURING CRUISE, CREW TURNED OFF BLEED AND GENERATOR, LIGHT WENT OUT AFTER 2 MIN, 55 SEC. CREW LANDED AT DESTINATION STATION WITHOUT INCIDENT. DESTINATION STATION WAS THE CLOSEST AIRPORT AT THIS TIME. NO FAULT WSDR EIA2003117Warning Light · intermittentDURING CLIMB RT WING OVERHEAT LIGHT FLICKER DIM TO BRIGHT, STAYED ON THE FLICKER, DID SAME THROUGHOUT PROCEDURE (FULL) ABNORMAL LIGHT WENT OUT AND STOPPED FLICKERING ON DECENT. UNABLE TO DUPLICATE FAULT ON GRD. CHECKED WING AND PYLON DUCTS FOR AIRLEAKS, NONESDR 03FDEA01467Switch · false indicationENGINE NR 3 OVERHEAT LIGHT ILLUMINATED ON CLIMB OUT REFRENCED JRH AND CLOSED THE RIGHT WING ANTI-ICE SWITCH. LIGHT WENT OUT AND STAYED OUT FOR REMAINDER OF FLIGHT. CHECKED DUCTS AND CLAMPS ON NR 3 ENGINE OPS CHECK SYSTEM USING APU POWER IAW SMP. COULD NOT SDR P5CA0300940Connector · disconnectedAFT 20 MINUTES INTO CRUISE RT WING L/E OVERHEAT LIGHT ILLUMINATED. REMAINED ON UNTIL BLOCK IN. FOUND NR 3 PYLON DETECTOR S1046 SHORTED. DISCONNECTED S1046. ITEM DEFERRED PER MEL 26-22-03A. SECOND LOOP OPS NRML PER MM 26-15-00SDR AWXA200301009Element · defectiveAFTER TAKEOFF AT PHX EN ROUTE FOR TUS RT WING TO BODY LIGHT ILLUMINATED CONTINUOUSLY, FOLLOWED QRH PROCEDURES AND TURNED BACK TO PHX. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE STRUT DETECTOR ELEMENT (M488) IAW BMM 26-18-11 PG 401. RAN ENGINE, APU AND RTSDR USAASB03152Accessory Unit · failedON APPROACH TO PHL FROM ALB, CREW REPORTED A STRONG ELECTRICAL ODOR IN THE CABIN. CREW PERFORMED ISOLATION PROCEDURES STARTING WITH GALLEY POWER THEN CABIN LIGHTS AND THOUGHT ODOR WAS FROM VICINITY OF SEAT ROWS 5 AND 6, RIGHT SIDE. CREW DECLARED AN EMERGENCYSDR MWEA030327Sensor · false indicationTHE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AND THEN WENT OUT. PERFORMED LEAK CHECKS OF ALL PNEUMATC DUCTS IN AFT ACCESSORY COMPARTMENT. NO LEAKS NOTED. PERFORMED ADJUSTMENT TEST OF TAIL COMPARTMENT TEMPERATURE HIGH SYSTEM. NO DEFECTS NOTED.SDR REXA03004Element · malfunctionedON CLIMB-OUT, RECEIVED 14TH STAGE LEFT DUCT WARNING MESSAGE. REMOVED AND REPLACED LEFT PYLON SENSING ELEMENT A59WK. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS. (M)SDR AWXA200300916Accessory Unit · malfunctionedPHX - AIR TURN BACK - FLT 0297 - ON CLIMB OUT OF PHX EN ROUTE FOR SJC THE RT WING TO BODY OVERHEAT LIGHT ILLUMINATED. TURNED BACK TO PHX, LIGHT REMAINED ILLUMINATED UNTIL AFTER LANDING. MAINTENANCE PERFORMED ENGINE RUN AT CLIMB POWER, FENWAL DIGITAL BOX 44 OVSDR 03224706Overheat Loop · unreliableDURING DESCENT CREW RECEIVED A 14TH STAGE WARNING MESSAGE AND SHUT DOWN THE LEFT ENGINE AS A PRECAUTION EMERGENCY WAS DECLARED FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LT ENGINE PYLON 14TH STAGE OVERHEAT DETECTION LOOP. ASDR 03FDEA01259Overheat Loop · intermittentAPPROX ONE HOUR INTO FLIGHT 28 DURING CRUISE NO TURBULENCE 29 EPR 27S 231 1.59 232 1.83 233 1.56_N2_231 86 25_232 86 25_ 233 85 25 LOWER AFT BODY OVERHEAT LIGHT FLICKERING. CHECKLIST ACCOMPLISHED-LT WENT OUT THEN BEGAN TO FLICKER AGAIN. LANDED GTF. REMOVEDSDR 03FDEA01251Overheat Loop · chafedDURING CRUISE FLIGHT AT FL 330 MACH .82, THE LOWER AFT BODY OVERHEAT LIGHT STARTED TO LIGHTLY FLICKER INTERMITTENTLY. LIGHT RARELY FLICKERED ON AND WAS MOSTLY COMPLETLEY OUT. SUSPECTED A SHORT IN THE IND SYSTEM. FURTHER DOWN LINE THE WARNING LIGHT FLICKERESDR 03FDEA01252Control Panel · malfunctionedIN CRZ FLT LOWER AFT BODY OVERHEAT LIGHT CAME ON BLINKING AT VARIOUS RATES. ACCOMPLISHED QRH L.A.B. OVERHEAT CHECKLIST TO INCLUDE CLOSING NR 3 ENG. BLEED. BLINKING SLOWED THEN STOPPED. SYSTEM TESTED GOOD. CONTINUED IN CRUISE WITH NR 3 BLEED CLOSED. R7R SDR USAASB03133Control Module · faultyORF - FLT 636 - EN ROUTE FROM CLT-PVD, AT FL330, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW REDUCED THE NR 1 ENGINE THROTTLE TO IDLE AND THE LIGHT EXTINGUISHED. CREW DECLARED AN EMERGENCY AND DIVERTED TO ORF. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MSDR AMTA200300984Overheat Loop · out of adjustRIGHT ENGINE OVERHEAT LOOP 2 INOPERATIVE, STATUS MESSAGE. VERIFIED SECURITY OF ALL RELATED CONNECTORS. PERFORMED ADJ/TEST OF OVERHEAT SYSTEM. SYSTEM CHECKS NORMAL PER MM 26-11-00-05. (M)SDR DHL2003754013Connector · dirtyLOWER AFT BODY OVERHEAT WILL NOT TEST. CLEANED AND RE-SEALED CONNECTOR PLUG ON LOWER AFT BODY OVERHEAT SENSOR, TESTED UNIT IAW M/M 26-14-01, OPS CHECKED NORMAL.SDR 03FDEA01131Warning Light · false activationDURING CRUISE GOT LOWER AFT BODY OVERHEAT LIGHT. ENGINE ANTI-ICE WAS OPEN. RED TABS COMPLETED DETERMINED NR 2 ENG ANTI-ICE WAS CAUSE OF OVERHEAT LIGHT. WHEN NR 2 ENGINE ANTI-ICE CLOSED DUCT TEMP DECREASED BELOW 50 DEGREES C OVERHEAT LIGHT WENT OUT. RAN ENSDR 03198637Connector · dirtyDURING APPROACH, THE CREW REPORTED A MLG BAY OVERHEAT WARNING WHEN THE GEAR WAS LOWERED. MAINTENANCE PERSONNEL CLEANED AND RESEATED THE LT AND RT GEAR BAY LOOP CONNECTORS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR AMTA200300933Warning Light · false activationLT STRUT OVERHEAT DET 1, STATUS MSG ILLUMINATED. PERFORMED BITE CHECK PER FIM 26-12-00 FIG 103. VISUALLY INSPECTED NR 1 ENGINE PYLON AREA, NO DEFECTS FOUND. RAN ENGINES 15 MINS, NO OVERHEAT DETECTED. (M)SDR AMTA200300930Warning Light · illuminatedLT ENGINE OVERHEAT EICAS MSG ILLUMINATED. ALL ATA PROCEDURES COMPLETED. LIGHT EXTINGUISHED. FLIGHT COMPLETED NORMALLY. PERFORMED BITE CHECK PER FIM 26-12-00 FIG 103. VISUALLY INSPECTED NR 1 ENGINE PYLON AREA, NO DEFECTS FOUND. RAN ENGINES 15 MINUTES, NO SDR DLM88030622Sensor · faultyIR: TAIL COMPARTMENT TEMP HI LIGHT CAME ON AT 400 FT. REPLACED TAIL TEMP HI SENSOR. RAN ENGINES TO TAKEOFF POWER. ALL INDICATIONS NORMAL.SDR SWIA200312171Switch · inoperative''CARGO BOTTLE LOW MSG'' DURING FLIGHT. FOLLOWED QRH AND LANDED AT NEAREST SUITABLE AIRPORT. REMOVED AND CLEANED SWITCHES ON FIRE PANEL. SYSTEM CHECKS GOOD.SDR A6WA200340101Warning Light · false indicationBLEED AIR DUCT MASTER WARNING ILLUMINATED ON TAKEOFF REMAINS ON EVEN AFTER LEFT ENGINE SHUTDOWN PER QRH COMPLIED WITH 14TH STAGE DUCT LEAK CHECK. NO LEAKS. OHMED OVERHEAT ELEMENTS. ALL CHECK GOOD. COMPLIED WITH CHECK FLIGHT, NO DEFECTS NOTED. (M)SDR A6WA200340100Wire · out of positionBLEED AIR DUCT MASTER WARNING WOULD COME ON INTERMITTENTLY AND REPEATEDLY IN FILGHT 31,000 FEET. COMPLIED WITH QRH MSS EXTINGUISHING 55 PERCENT N1 LEFT ENGINE. STRAIGHTENED WIRE AT 14TH STAGE BLEED AIR DUCT AND TIGHTENED CLAMP AT AIR SWITCH. RAN ENGINE, OPERSDR 2003UALA00525Warning Light · false indicationAIRCRAFT DIVERTED EN ROUTE DUE TO A WING-BODY OVERHEAT INDICATION. AIRCRAFT EXPERIENCED LEFT WING-BODY OVERHEAT WARNING INDICATION IN CRUISE FLIGHT WITH APU SUPPLYING AIR. WING-BODY OVERHEAT INDICATION LIGHT EXTINGUISHED PER THE IRREGULAR PROCEDURE. AIRCRAFSDR 03FDEA00993Control Unit · faultyREPEAT WRITEUP. ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED ON CLIMBOUT. COMPLIED WITH RED TABS AND LIGHT EXTINGUISHED WHEN NR 1 BLEED AIR SWITCH CLOSED AND LEFT, PACK TURNED OFF. REMAINED OFF FOR REST OF FLIGHT. INSPECTED NR 1 STRUT OVHT. DETECTOR SENSOR CSDR 03FDEA00969Warning Light · illuminatedWITH LEFT A/C PACK OPERATING THE LOWER AFT BODY OVERHEAT LIGHT ILLUM AFTER AT LEAST 30 MINS OF PACK OPS. AFTER TURNING OFF LT PACK, THE LIGHT EXTINGUISHED WITHIN 2 MINS. TURNED RT PACK ON, THE LIGHT CAME BACK ON AFTER 5 MINS. CHECKED AFT AIRSTAIR AREA FOR LSDR DHL2003749007Sensor · will not testLOWER AFT BODY OVERHEAT WILL NOT TEST. DEFERRED PER MEL 26-10-2. SP 26-10-2 COMPLIED WITH. DMI 13274 PLACARD INSTALLED. MAINTENANCE CONTROL NOTIFIED. REF DMI 13274; LOWER AFT BODY OVERHEAT WILL NOT TEST. TROUBLESHOT AND TESTED SYSTEM IAW BMM 26-14-00. NSDR DHL2003721006Connector · damagedLOWER AFT BODY HEAT HAS NO TEST FUNCTION. TRANSFERRED TO DMI 13272 MEL 26-10-2 CAT C. PLACARD INSTALLED SP 26-10-2 COMPLIED WITH. REF DMI 13272 LOWER AFT BODY HEAT. REMOVED AND CLEANED CONNECTORS ON BOTH ENDS OF DETECTOR. RE-INSTALLED, OPS CHECKED GOOD. SDR CX7A194J0349Detector · overheatedLT TAILPIPE HOT CWP ON.SDR DXTA200300045Sensor · faultySHORTLY AFTER T/O EMER PRESS LIGHT ILLUMINATED AND EMERGENCY PRESSURIZATION ACTIVATED W/SYSTEM IN NORMAL POSITION. AIRCRAFT RETURNED AFTER TAKEOFF AND LANDED OVERWEIGHT. COPILOTS WINDSHIED HAS DISTORTION LOCATED ON BOTTOM 3RD OF WINDSHIELD. REMOVED AND REPLSDR DL738030528Sensor · wornRIGHT ENGINE BLEED TRIP OFF. T/S PER FIM 36-10-TASK-801. HOOKED UP AIR SOURCE PER FIM. NO LEAKS NOTED. RECONNECTED MUSCLE LINE AT TEE. REPLACED HIGH PRESSURE BLEED 390 TEMP SENSOR AND 490 TEMP SWITCH PER M/M. PERFORMED PNEUMATIC CHECK OUT PER PFHB. OP CSDR AWXA200300680Thermocouple · faultyON TAKEOFF ROLL AT LAS EN ROUTE FOR PDX NR 2 BRAKE TRIGGERED HOT BRAKE ECAM MESSAGE, REJECTED TAKEOFF AT 85 KTS. NR 2 BRAKE INDICATED 580 CELSIUS MAXIMUM TEMPERATURE. MAINTENANCE PLACED SYSTEM ON MEL 32-47-01, COND 1 NR 2 BRAKE TEMP MONITORING UNIT INOP AND SDR CX7A194J0348Detector · malfunctionedLEFT TAILPIPE HOT LIGHT SHORTLY AFTER V1. LIGHT WENT OUT A FEW MINUTES AFTER POWER REDUCTION.SDR COMA0360255Element · false indicationFLIGHT 5313 MLG OVERHEAT MESSAGE. REPLACED THE LT MLG OVERHEAT SENSING ELEMENT.SDR CX7A194J0347Detector · malfunctionedLT TAIL PIPE HOT ILLUMINATED DURING T/O EXECUTED CHECKLIST. LIGHT EXTINGUISHED. RETURN TO AIRPORTSDR AMTA200300732Warning System · false indicationRT TURB OVERHEAT DETECTOR 2 STATUS MESSAGE. TROUBLESHOT PER FIM 26-13-00 FIG 104. NO FAULTS NOTED. OPS CHECK NORMAL. (M)SDR MEX2003197Switch · failedAFTER TAKEOFF ON CUU STATION TAIL COMP TEMP HIGH LIGHT COMES ON. DURING OVERNIGHT SERVICE, TAIL COMP OVERHEAT SENSORS WERE REPLACED IAW MM 36-20-02 AND WIRING SENSORS WERE VERIFIED IAW WDM 36-23-00, ALL TESTS CORRECT. (M)SDR CX7A194J0346Detector · malfunctionedTAILPIPE HOT LEFT ENGINE ON THE CLIMBOUT.SDR CA030530014Loop · failed(CAN) CREW EXPERIENCED A LT BLEED DUCT WARNING MSG ON CLIMB OUT THRU 23,000 FT. LT PACK WENT OFF LINE & APPROX. 30 SECONDS LATER, RT PACK WENT OFF LINE. CREW WERE UNABLE TO RESET THIS CONDITION IN AIR. AC DIVERTED. TROUBLESHOOTING, MAINT LT BLEED LOOP B HIGHSDR RAIA00305152Overheat Loop · false indicationRIGHT OVERHEAT INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 OVERHEAT LOOP.SDR ABXA030171Connector · damagedAFTER TAKEOFF, TAIL COMPARTMENT TEMP HIGH ILLUMINATED. ACCOMPLISHED EMERGENCY PROCEDURE CHECKLIST AND ANNUNCIATOR REMAINED ILLUMINATED. LANDED WITHOUT INCIDENT. REPLACED CONNECTOR P1-387, AFTER FINDING WIRES SHORTED AND TOUCHING EACH OTHER. TAIL COMPARTMENTSDR AMTA200300711Connector · defectiveLEFT ENGINE OVERHEAT LP2 INDICATION ON STATUS PAGE, INTERMITTENT. REMOVED AND REPLACED CONNECTOR D41162P IAW WDM 26-11-11 AND 26-11-12. OPS CHECK NORMAL. (M)SDR DXTA200300036Fire Loop · misroutedDURING FLIGHT 120124-1 FROM MIA TO CHS DIVERTED TO MCO DUE TO LT ENGINE FIRE LIGHT CAME ON AT FL240. REDUCED POWER TO HALF THROTTLE AND LIGHT EXTINGUISHED, NO EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED LT ENG COWLS AND RAN FOR LEAK CHECK. NO LEAKS SDR DHL2003754008Circuit Breaker · failedLOWER AFT BODY OVERHEAT WILL NOT TEST. LOWER AFT BODY OVERHEAT TEST FEATURE AT FLIGHT DECK DEFERRED PER MEL 26-10-2 CAT C. DMI 13038 SPECIAL PROCEDURE 26-10-2, COMPLIED WITH, PLACARD INSTALLED. REF DMI 13038 LOWER AFT BODY HEAT WILL NOT TEST. PER MEL REQUISDR DHL2003749006Switch · malfunctionedON PRE-DEPARTURE CHECK LOWER AFT BODY OVERHEAT WOULD NOT TEST. TRANSFERRED TO DMI CONTROL 13029 PER MEL 26-10-2. PLACARD INSTALLED. SPECIAL PROCEDURES 26-10-2 COMPLIED WITH TO VERIFY SYSTEM OPERATION. REF DMI 13029 ON PRE-DEPARTURE CHECK LOWER AFT BODY OVERSDR 187801Connector · dirtyAIRCRAFT 108CQ FROM HGR-PIT FLT 4535 ABORTED TAKE OFF DUE TO RIGHT TAIL PIPE HOT LIGHT. PIT MAINTENANCE DISPATCHED TO AIRCRAFT. MAINTENANCE CLEANED CONNECTORS ON TAIL PIPE HOT SYSTEM, GROUND RAN AIRCRAFT, OPS CHECK IAW 26-12-00, OPS CHECK GOOD. AIRCRAFT RETURNSDR CALA0300254Overheat Sensor · inoperativeTHE WHEEL WELL FIRE LIGHT ILLUMINATED WITH THE LANDING GEAR RETRACTED AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE OVERHEAT DETECTION UNIT WAS REMOVED AND REPLACED AND SDR 03FDEA00739Warning Light · illuminatedPASSING FL230, 330 KIAS, EPR 2.01/2.07/2.01, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. LEVELED OFF AT FL 260 AND PRIOR TO COMPLETING RED TABS , LOWER AFT BODY OVERHEAT LIGHT EXTINGGUISHED. RED TABS COMPLETED AND SYSTEM TEST GOOD. AT LEVEL OFF FL260 THRO
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