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 AALA202205168566Element · overtempAIRCRAFT WAS GROUNDED: ON CLIMB OUT THE RIGHT WING-BODY OVERHEAT LIGHT ILLUMINATED INTERMITTENTLY SEVERAL TIMES. COMPLETED THE CHECKLIST TO THE POINT OF CLOSING THE ISO-VALVE. RIGHT PACK AND RIGHT BLEED VALVE, WING-BODY OVERHEAT LIGHT EXTINGUISHED FOR REMAINDESDR 2022FA0000225Fire Warning · no indicationDURING PREFLIGHT COCKPIT CHECKS THE RIGHT HAND ENGINE FIRE DETECT TEE HANDLE DIDN'T ILLUMINATE DURING TEST. FERRIED PLANE BACK TO HOME BASE.SDR AALA202202252748Pin · contaminatedAIRCRAFT WAS GROUNDED: LEFT ENGINE NACELLE TEMP FLASHING DURING CLIMB. 305-385 DEGREES. RIGHT ENGINE SHOWED 235 DEGREES. STOPPED FLASHING AS WE CLIMBED THROUGH ABOUT 25000 FEET. RETURNED AGAIN LATER IN FLIGHT, 325 DEGREES. AT 35000 FEET. RIGHT ENGINE 185 DEGRESDR AALA202202143371Detector · out of toleranceAIRCRAFT WAS GROUNDED: LEFT WING OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. PILOT DID NOT HAVE WING ANTI ICE ON. THE ENGINE ANTI ICE WAS ON. FOLLOWING THE CHECKLIST ISOLATED THE LEFT WING OVERHEAT. ISOLATED THE LEFT WING OVERHEAT AFTER APPROXIMATELY 5 MINUTES TSDR SWIA202264074None · fire warningAPU FAULT CAUTION FOLLOWED BY APU FIRE WARNING FOLLOWED BY APU ECU FAIL. (FILED - CLOSED) DEFERRED APU PER MEL 49-10-1A. ALL MX ACTIONS COMPLIED WITH.SDR CALA2022012400217Smoke Detector · warning lightSMOKE LAV EICAS 3R LAV RESET SMOKE DETECTOR, OPS CHECK OK. NO PREVIOUS HISTORY.SDR GTIA2022012036228None · noneSMOKE& FWD CARGO SMOKE ANN DURING DESCENT. EICAS COMPLETED W/ AND EMERGENCY DECLARED. UPON LANDING TAXIED A/C OFF THE RUNWAY AND HAD FIRE RESCUE CHECK A/C FOR HEAT SIGNATURES. AFTER RECEIVING ALL CLEAR CONTINUED TO GATE AND DEPLANED PAX PRIOR TO OPENING CARGO SDR IPXA2022010777616Warning Message · illuminatedEICAS MSG FIRE/ OVERHEAT SYS ON FINAL APPROACH. RAN CHECKLIST, MESSAGE CLEARED. NOTED MSG CLEARED WITH CHECKLIST, PERFORMED FIRE DETECTION TEST REF AMM 26-11-00-715-001. RT ENG OH LPI ALREADY ON DEFERRAL ITEM M768813. (OPEN)SDR IPXA2021110975823Warning Message · false activationENG 3 OVHT LP A.C/O T/S PER FIM TASK 31-98-00-810-801. CMC SHOWS NO CORRELATED PRESENT LEG FAULTS AND NO EXISTING FAULTS. ACCOMPLISHED OPS TEST FOR FIRE/OVHT DETECTION SYSTEMS PER AMM TASK 26-10-00-710-801 AT REL 36.02 WITH SATIS. A/C OK TO CONTINUE.SDR AALA202110254481Sensor · failedAIRCRAFT WAS GROUNDED: IN FLIGHT FLIGHT ATTENDANTS NOTICED SMELL OF BURNING RUBBER (ELECTRICAL FIRE). AFT CARGO COMPARTMENT INDICATED 218 DEGREES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MEM WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTSDR SWAA2021101126994None · failedSUPPLEMENTAL INFORMATION: ENGINE FIRE/ OVERHEAT DETECTOR FAULT LIGHT ILLUMINATED / UPON INSPECTION FOUND B LOOP TERMINAL LUG BROKEN ON LOWER FAN CASE FIRE LOOP. PERFORMED RESISTANCE CHECKS OF FAN AND ENGINE CORE LOOPS ALL WITHIN LIMITS PER FIM 26-10 TASK 810. SDR ASAA2021100536214Fire Detector · no testDURING CARGO FIRE TEST, THE FORWARD ARM LIGHT WOULD NOT ILLUMINATE AND THE DETECTOR FAULT LIGHT DID ILLUMINATE. GROUNDED - YES. REMOVED & REPLACED FWD CARGO A1 & A2 DETECTORS. OPS CK GOOD. REF B737-800 AMM 26-16-01.SDR NACA2021091200002Overheat Loop · warning messageDISCREPANCY: RH ENGINE OVERHEAT LOOP 2 EICAS MESSAGE. CORRECTIVE ACTION: REPLACED M690 CARD OPS CHECK PER AMM 26-11-00. GROUND VERIFICATION COMPLIED WITH, AC REMAINS ETOPS 180SDR UIEA2021090301942Circuit Card · malfunctionedL ENG OH LP 1 STATUS MESSAGE(<P>TRANSFERRED TO DMI #152929, CAT C, DUE DATE 12SEP21 IAW DDG 26-11-02-01.</P> / <P>03 SEP 21 - LP 1369067 ITEM 7 - CVG - T/S IAW FIM 26-11 FAULT TREE 804. FOUND L ENG OH LP CARD TO BE AT FAULT. REMOVED AND REPLACED L ENG OH LP1 CSDR UIEA2021082401860Circuit Card · faultedREPEATED, R BLD DUCT LEAK ON GROUND W/APU RUNNING, NO ENGINES RUNNING.(<P>REPLACED WHEEL WELL BLEED OVHT CARD IAW B767-300 AMM 36-21-00. RAN PACKS 30 + MIN WITH NO RECURRENT FAULTS.</P>)SDR ASAA2021080435664Wire Harness · brokenON PREFLIGHT ENG #1 OVERHEAT TEST FAILED, B LOOP A LOOP WORKS CURRENTLY. GROUNDED - YES. REPLACED #1 ENG CORE HARNESS P/N CA244-02 REF B737-900 AMM 26-11-02-401 OPS TEST PASSED.SDR 9WGA2021071125801Warning Message · illuminatedENGINE 4 OVERHEAT LOOP A (CLIMBOUT) (STATUS) EICASSDR AALA202107094364Overheat Loop · faultedAIRCRAFT WAS GROUNDED: WARNING MESSAGE FOR WING-TO-BODY OVERHEAT, FLIGHT DECLARED EMERGENCY AND RETURNED TO FIELD. REPLACED RH OUTBD OVERHEAT DETECTOR IAW TSM 26-18-00-810-802, OPS CHECK GOOD.SDR ASAA2021062435185Light · no testDURING FIRE/OVERHEAT TEST #1 ENGINE OVERHEAT AND DISCHARGE DOES NOT ILLUMINATE IN NORMAL. GROUNDED - YES. COULD NOT DUPLICATE FAULT, BOTH A & B LOOPS WORKING NORMALLY. DUE TO HISTORY OF INTERMITTENT FAULT, PERFORMED B737-800 FIM 26-10 TASK 805. ALL 4 A LOOP DESDR AALA202106219002Module · faultyAIRCRAFT WAS GROUNDED: AT APPROXIMATELY 10,000 FEET ENGINE 2 OVERHEAT LIGHT ILLUMINATED. ENGINE 1 FIRE LIGHT AND ENGINE 1 OVERHEAT DOES NOT TEST. RETURNED TO FIELD. REPLACED CHAFED HARNESS MW0325 (AALA202106189013) PER AMM 26-11-02 AND AMM 26-10-01. REPLACED SDR ASAA2021061635119Fire Detector · brokenFAULT LIGHT #1 ENGINE B LOOP. GROUNDED - YES. VERIFIED DISCREP FIRE DETECTION CONTROL UNIT SHOWS #1 ENG B LOOP UPPER FAN DETECTOR FAULT. UPON INSPECTION OF UPPER FAN DETECTOR ASSY. FOUND BROKEN B LOOP ELEMENT REF B737-800 AMM 26-11-01, REMOVED/REPLACED UPPER FSDR NACA2021061400002Warning Message · false activationINTERMITTENT RIGHT ENGINE OVERHEAT DETECTION LP2 STATUS IN FLIGHT. PERFORMED FIM 26-11 FAULT TREE 804. NO FAULTS FOUND. INSPECTION OF FIRE/OVHT LOOPS AND AND WIRING NO DISCREPANCIES NOTED. OPS CHECKED GOOD, ETOPS GROUND VERIFICATION CHECK OK.SDR AALA202106149014Wire Harness · faultedAIRCRAFT WAS GROUNDED: ENGINE 2 OVERHEAT INDICATION CLIMBING OUT OF 12000 MSL. REPLACED ENGINE 2 FIRE DETECTION HARNESS MW0326 PER AMM 26-11-00-710-801.SDR BKEA.CL600.5437Warning Message · illuminatedMLG BAY OVHT MASTER WARNING ACTIVATED SHORTLY AFTER RETRACTING THE GEAR ON TAKEOFF. THE CREW LEVELED OFF AT 7,000 FEET AND SLOWED TO 190 KNOTS AND THEN EXTENDED THE LANDING GEAR (AS PER THE CHECKLIST). THE WARNING LIGHT WENT OUT. THE CREW FLEW WITH THE LANDINSDR DXTA2021060743380Switch · defectiveBAG SMK RED CAS: BAGGAGE SMOKE WARNING CAME ON MOMENTARILY AT FL 370 WITH AURAL AND CAS MESSAGE. LANDED AND FOUND PASSENGER PROTEIN POWDER MIXTURE EXPLOADED COVERING ENTIRE AFT PORTION OF BAGGAGE COMPARTMENT. EMERGENCY FIRE CREWS NOTED NO ABNORMAL HEAT DETECTSDR ASAA2021060335031Overheat Loop · no test#1 ENGINE "A" OVHT LOOP WILL NOT PASS PREFLIGHT TEST. GROUNDED - YES. C/W ENG FIRE DETECTION OPERATIONAL TEST - ENG #1 A / B LOOPS TEST NORMAL. OPENED ENG #1 FAN COWLS AND THRUST REVERSERS. ACCOMPLISH VISUAL AND PHYSICAL INSPECTION OF ENG #1 LOOPS AND LUG CONNSDR ASAA2021052934979Overheat Sys · false activationENG 2 SYS B FIRE OVERHEAT HARD FAULT, SYS A OK. GROUNDED - YES. ENG #2 FIRE DETECTION OPERATIONAL TEST GOOD. CONTROL MODULE BIT SHOWS NO FAULTS. CONTROL MODULE REMOVED AND FIRE DETECTOR RANG OUT AT LOOPS B PINS 12 TO 2 AND 12 TO 10: BOTH WITHIN TOLERANCE (867 SDR N6WA2021052801Warning Message · illuminatedWING OVERHEAT WARNING MSG IN FLIGHT, R2 AILC IAW CRJ 550 AMM 30-12-12, OPS CHECK GOODSDR 2021F00104Overheat Sensor · dirtyIN FLIGHT, CREW HAD WHEEL WELL OVERHEAT LIGHT AS WELL AS MASTER FIRE WARNING LIGHTS ILLUMINATE. LIGHTS EXTINGUISHED WHEN LANDING GEAR WAS EXTENDED. UPON LANDING, MAINTENANCE INSPECTION DETERMINED OVERHEAT SENSING LOOP CONNECTION WAS DIRTY, CLEANED AND PERFORMESDR UIEA2021050301053Warning Message · false activationFWD EQPT OVHT UPON LANDING.(<P>TRANSFERRED TO DMI # 146288 MEL 21-58-03-02-01 CAT C DEFERRAL DUE DATE 12MAY21.</P><P>REF MDDR 146288 REF LOG PG # 1465089 ITEM M9 . TS PER FIM TASK 21-58 FT 991, NO FAULTS NOTED, UNABLE TO DUPLICATE FAULT. PERFORMED OPS CHECK OFSDR ASAA2021042334667Indicator · no indicationDURING OVHT/FIRE WARNING CHECK, ENGINE NO. 1 FIRE WARNING SWITCH DOES NOT ILLUMINATE IN 'B' CONFIGURATION. GROUNDED - YES. PERFORMED ENGINE FIRE DETECTION OPERATIONAL TEST PER B737-800 AMM 26-11-00-710-801. OPS CHECK GOOD AND BITE TEST ON THE ENGINE AND APU FISDR AALA202104209010Overheat Loop · false indicationAIRCRAFT WAS NOT GROUNDED: AUXILIARY POWER UNIT DISCHARGE LIGHT ON DURING CRUISE. OPERATIONS TEST OF AUXILIARY POWER UNIT FIRE AND OVERHEAT DETECTION SYSTEM, PER AMM 26-13-00-710-001-A. ACCOMPLISHED AUXILIARY POWER UNIT FIRE DETECTION UNIT TEST PER AMM 26-13-3SDR CALA2021032200363Overheat Loop · false activationWING-BODY OVERHEAT LIGHT LIGHT ON RIGHT SIDE REF FIM 26-18-00-810-810, OVERHEAT UNIT M237 SHOWS FAULT CODE 64. REMOVED AND REPLACED OVERHEAT DETECTOR M269 PER AMM 26-18-02-400-801 FAULT CLEARED. RAN RIGHT PACK ON HIGH FOR 30 MINUTES AND DRY MOTORED #2 ENG FOR SDR JJBA20210110039Sensor · false activationBRAKE OVERHEAR INDICATION ON EICAS DURING CLIMB OUT. LT INBOARD BRAKE TEMP IN MAX RANGE. REMOVED AND REPLACED LT INBOARD BRAKE TEMP SENSOR. OPERATIONS CHECK SATISFACTORY. RECONNECTED CANNON PLUG P1077.SDR 2021FA0000007Overheat Sensor · false indicationDURING CLIMB WITH MEL 36-05-02 THE LEFT WING BODY OVERHEAT LIGHT ILLUMINATED. DEVIATION TO DEPARTURE AIRPORT WAS NECESSARY. CORRECTIVE ACTION: INSPECTED DUCT LEAKAGE, REMOVED MOISTURE AND ISULATED TO GROUND IN THE AC PACK LT SENSORS, IAW AMM 26-18-00 LT WINGSDR ASAA2020120933665Overheat Sensor · failedUPON GEAR RETRACTION WE GOT A WHEEL WELL FIRE WARNING. WARNING CONTINUED FOR ABOUT 15- 30 SECONDS AFTER LANDING GEAR EXTENDED. NO OTHER ABNORMALITIES OR INDICATIONS. GROUNDED-YES. WHILE DEBRIEFING CREW, FIRE BELL CAME ON ALONG WITH WHEEL WELL FIRE LIGHT. SDR FDEA202011142842Sensing Element · failedDURNING CLIMBOUT ENGINE NO 1 BLEED LEAK, DIVERTED INTO TPA BECAUSE WE LOST PRESSURIZATION DUE TO DEFERRED NO 2 PACK, DECLARED EMERGENCY. FACT 15NOV20 16:06 TPA. R & R MANIFOLD OVERHEAT SENSING ELEMENT ON LT WING PYLON I/R/T MM 36-22-12-04, REMOVAL P/N 35518-SDR UIEA2020101802269Circuit Card · malfunctioned"FIRE/OVERHEAT SYSTEM" EICAS MESSAGE. ACCOMPLISHED QRH AND MESSAGE CLEARS BUT COMES BACK WITHIN 2-3 MINS. REMOVED/REPLACED AFOLT CARD M10224 ENGINE RT; PERFORMED FIRE/OVERHEAT ENGINE SYSTEM TEST OK, AMM 26-10-01.SDR ASAA2020100633290Overheat Sensor · faultedAPU DET INOPERABLE LIGHT ILLUMINATED MOMENTARILY IN FLIGHT. GROUNDED-YES. ACCOMPLISHED B737-800 FIM 26-10 TASK 802, NO FAULTS LOGGED. REPLACED M1925, REF B737-800 AMM 26-15-01-400-801. OPERATIONS NORMAL, REF B737-800 AMM 26-15-00-710-801. AIRCRAFT RETURNESDR DALA2020092803177Sensor · false indicationFLIGHT 8824; MSP-HNL PERFORMED AN AIR TURN BACK DUE TO 'FWD EQUIP OVERHEAT' WARNING. CORRECTIVE ACTION: REPLACED LOW FLOW SENSOR AT FORWARD RACK AND FLIGHT DECK LOW FLOW SENSOR TS0163. SYSTEM OPERATION IS NORMAL.SDR UIEA2020092102043Warning Light · inoperativeRT ENG OVHT DISCREET LIGHT ON THE CENTER CONSOLE IS INOP. FOUND DURING PRE-FLIGHT. PERFORMED FIRE TEST SYSTEM, OPERATE NORMAL, AS PER AMM 26-21-04.SDR SWIA2020090852309Overheat Loop · shortedMLG OVHT AFTER TO. COMPLIED WITH QRC, QRH AND RETURNED TO LAND. MSG EXTINGUISHED WITHIN APPX 30 SECONDS, FLIGHT 3287 - FILED CLOSED. PERFORMED INSPECTIONS OF THE MAIN WHEEL ASSEMBLIES AND THE BRAKE SYSTEM, WITH NO DISCREPANCIES FOUND. ALL BTMS INDICATIONS SDR P5CA2020083100293Overheat Sys · malfunctionedRIGHT ENGINE OH LP1; LEFT ENGINE OH LP2 STS MESSAGE DISPLAYED(PERFORMED CONVERSION FIRE DETECTION SYSTEM PER EO 6726A005 THEN FIRE/OVERHEAT SYSTEM OPERATIONS CHECKED NML AS PER AMM 26-10-01 WDM 26-11-22).SDR SROM020200718201I/O Module · malfunctionedRIGHT FUEL TANK TEMP INDICATED +99°C WITH FIRE BELL. REMOVED AND REPLACED THE RT FUEL HEATER THERMAL ACTUATOR INAW DHC-8-400 AMM 73-11-05 (FOR THE FUEL OVERHEAT). SWAPPED INPUT/OUTPUT MODULE (IOM) POSITIONS IAW Q400 AMM 31-41-11 (FOR TROUBLE SHOOTING THE FSDR R61A2020071500565Overheat Loop · faultyBLEED 1 LEAK ON EICAS. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R&R ODS LOOP 3.SDR N6WA20200708601Warning System · false activationMLG OVERHEAT WARNING MSG. NO SIGNS OF OVERHEAT OR FIRE, DEFERRED MLG OVERHEAT DETECTION SYSTEM ON OCN 70069499 PER MEL 26-14-01B CAT B.SDR JIKA20200624301Annunciator · false activationDURING CLIMB OUT, AT ABOUT 1400 FT AGL, RIGHT WING OVERHEAT ANNUNCIATOR LIGHT CAME ON STEADY. CREW COMPLETED THE MEMORY ITEMS FOR THAT ANNUNCIATION AND THE LIGHT REMAINED ON STEADY. ONCE AIRCRAFT REACHED 1500 FT AGL, CREW CONSULTED QRH AND INFORMED ATC REGARDSDR FDEA202006051136Detector Loop · failed17 MIN INTO FLT RECEIVED LEFT DUCT LEAK LIGHT ON OVERHEAD PANEL., NO EICAS. RAN CHECKLIST AND LIGHT WENT OUT FOR REMAINDER OF FLT. FLT CONDITION LEVEL CRUISE AT FL350. REMOVED AND REPLACED ELEMENT TS407 PER AMM 26-18-01-4-2. LOOP OPS CHECK IS GOOD. INSTASDR IPXA2020041554265Warning Message · false activationDIVERTED AND AN EMERGENCY WAS DECLARED, LANDED WITHOUT INCIDENT, WHEEL WELL FIRE EICAS MESSAGE AND BELL ACTIVATED. RAN QRH DROPPED GEAR, WHEEL WELL LIGHT WENT OUT. ACFT OPERATED NORMAL ON TAXI, DEPLOYED EVAS. REPLACED WHEEL WELL DUCT LEAK OVERHEAT POWER SDR ASAA2020040632615Overheat Sensor · faultyAPU DET INOP LIGHT ILLUMINATED UPON PUSHBACK. GROUNDED - YES. VERIFIED DISCREP - HARD FAIL. ENG/APU FIRE DET MODULE BITE PER B737-800 FIM 26-10 TASK 802 SHOWS APU TAILPIPE DET AT FAULT. RANG OUT SAME DETECTOR AND READ 160K OHMS - SHOULD BE 4K OHMS. REMOVED/REP
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