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 AALA202610100389Sensing Element · defectiveAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING THAT WHILE IN CLIMB, PASSING APPROX FL180, ECAM READ AIR ENG 1 BLEED LEAK - THE FLIGHT CREW EXECUTED ECAM ACTIONS THE AIRCRAFT LANDED SAFELY AT DSDR CALA2026092119567Control Module · damagedLEFT WING BODY OVHT LIGHT AFTER TAKE OFF, LIGHT REMAINED ON AFTER CHECKLI ST IAW FIM 26-18 TASK 801 PERFORMED BITE OF WHEEL WELL FIRE, WING & BODY OVERHEAT DETECTION CONTROL MODULE. FOUND MAINT MSG 14 (LEFT WING LE - ALARM). R & R WHEEL WELL FIRE WING & BOSDR SWAA2026091866830Sensing Element · faultedLEFT WING-BODY OVERHEAT ILLUMINATED, R & R LEFT PYLON FWD SENSING ELEMENT IAW AMM 26-18-02 OPS CHECK GOODSDR ABXA20260912402Overheat Sys · false activationFIRE/OVHT SYS ON FINAL APPROACH. AC LANDED AND MTX GROUNDED A/C. PERFORMED OPERATIONAL CHECK I.A.W A.M.M B767 26-11-00. ALL FOUND NORMAL. UNABLE TO DUPLICATE FAULT, NO STATUS MESSAGE. AIRCRAFT REMAINS NO ETOPS AND RETURNED A/C TO SERVICE.SDR SWAA2026090918056Overheat Sensor · false activationNR 1 ENGINE OVERHEAT LIGHT CAME ON, STARTED QRH & THEN WENT OUT. PERFORMED FIM 26-10 TASK 811. NO DEFECTS FOUND AT THIS TIME. PERFORMED ENGINE FIRE DETECTION LOOP RESISTANCE CHECK. FOUND TO BE WITHIN LIMITS IAW AMM 26-11-00. REMOVED AND REPLACED UPPER FAN FSDR AALA202609061485Sensing Element · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO RDU DUE TO THE FLIGHT CREW REPORTING AN AIR ENG 1 BLEED LEAK. THE FLIGHT CREW REPORTED THAT AFTER PERFORMING THE ECAM ACTIONS THE FAULT LIGHT REMAINED. THE AIRCRAFT LANDED SAFELY ASDR SWAA2026082716808Overheat Loop · faultedLEFT WTB OVERHEAT LIGHT ILLUMINATED ON TAXI OUT WITH LEFT PACK RUNNING ON APU BLEED SOURCE. PERFORMED QRH, LIGHT EXTINGUISHED WITH PACK OFF_ OK TO CONTINUE PER MEL 26-12-01 SP1 PERFORMED FIM 26-18 TASK 809 FOUND OPEN AT LOOP M1911. REMOVED AND REPLACED SENSE LSDR SWAA2026081961064Control Unit · intermittentRIGHT WING TO BODY OVERHEAT INOPERATIVE & ALL DETECTOR UNITS FAILING ON THE RT SIDE. OVERHEAT DETECTION CONTROL UNIT SHOWS INTERNAL FAULT. R & R WTB COMPT OVERHEAT DETECTION CONTROL UNIT IAW AMM 26-18-01. OPS CHKD GOOD.SDR K11A2026081300384Elec Connector · intermittentRIGHT WING BODY OVERHEAT ILLUMINATED WHILE CLIMBING THROUGH FL185 AND REMAINED ON EVEN WITH BLEED AIR OFF. LEFT WING BODY OVERHEAT ILLUMINATED WHILE TAXING IN WITH ALL TEMPS SET TO AUTO. REMOVED AND REPLACED OVERHEAT DETECTION SENSING ELEMENT M273 IAW B737 AMSDR IPXA2026080420489Controller · unserviceableAIR TURN BACK, ENG 1 BLEED LEAK RESULTING IN AIR TURN BACK FOUND LT WING MFA ILLUMINATED ON MX PANEL. INSPECTED WING PNEUMATIC JOINTS FROM PACK BAY OUT TO LT WING TIP. NO LEAKS NOTED IAW TSM 36-22-00/401. RAN NR 1 ENGINE, NO LEAK INDICATIONS. CHANGED NR 2 OVESDR SWAA2026082106267Overheat Loop · false indicationLEFT WING BODY OVERHEAT LIGHT ILLUMINATED AFTER NR 2 ENGINE START, WITH APU BLEED SWITCH ON. BITE SHOWS CODE 44 WITH ALARM LIGHT ILLUMINATED. CHECKED AFT CARGO, FOUND FULLY LOADED. UNABLE TO CHECK FOR HOT AREAS. TROUBLESHOT IAW FIM 26-18 TASK 802, AND 8SDR SWAA2026080451397Overheat Loop · false activationENGINE FIRE/OVERHEAT DETECTOR FAULT LIGHT ILLUMINATED.INTERMITTENTLY ACCOMPLISHED OPS CHECK OF ENGINE FIRE/OVERHEAT DETECTOR SYS. NO DEFECTS NOTEDSDR ABXA20260730340Warning Message · false activationSTATUS MSG "L ENG OH LP2 "KEEPS COMING ON AND OFF DURING THE FLIGHT. PER MCC REQUEST, PERFORMED LEAK CHECK AT L ENG PYLON HEAT EXCHANGER AND PRSOV DUCTS PER AMM 36-00-00. NO LEAKS NOTED. PLACED ON MEL 26-11-2-1. PLACARD INSTALLED, MX PROCEDURES C/W. A/C REMAINSDR SWAA2026073145069Overheat Sys · illuminatedENG 2 OVERHEAT LIGHT ILLUMINATED ON START, R & R NR 2 ENGINE CORE RT & LT FIRE DETECTOR IAW MM 26-11-01. R & R NR 2 ENGINE FAN UPPER AND LOWER FIRE DETECTOR IAW MM 26-11-01. R & R ENGINE AND APU FIRE DETECTION CONTROL MODULE (M279) IAW MM 26-10-01.SDR SCNA20260723323Bottle · illuminatedAFTER START ENG 1 OVERHEAT LIGHT ILLUMINATED RAN QRH AND DID ESP ON GROUND. QRH THEN DICTATED TO DISCHARGE A BOTTLE. AFTER BOTTLE DISCHARGE OVERHEAT LIGHT WENT AWAY. PERFORMED AMM TASK 71-00-00-800-803, NO EVIDENCE OF FIRE. PERFORMED FIM 26-10 TASK 801, NO FSDR ABXA20260721329Overheat Loop · warning messageDURING TAKEOFF, STATUS MSG: L ENG OH LP 2. DEFERRED IAW MEL 26-11-2-1 MX PROCEDURES COMPLIED WITH MBCB 7/31/26 PLACARD INSTALLED. A/C RETURNED TO SERVICESDR K11A2026071600383Overheat Sensor · dirtyWHEEL WELL FIRE LIGHT IN FLIGHT. CLEANED WHEEL WELL OVERHEAT DETECTOR ELEMENT IAW AMM 26-17-11. PERFORMED OPERATIONAL CHECK OF WHEEL WELL OVERHEAT DETECTION ELEMENT IAW B737 AMM 26-17-00, OPS CHECK GOODSDR CALA2026070617559Sensor · faultedBRAKE 3 TEMP SENSOR ROSE TO 995C AND CAUSED HOT BRK ECAM IN FLT BRIEFED INBOUD CREW, STATED 5 MILES OUT NR 3 BRAKE TEMP SENSOR READS 900 PLUS C, AFTER LANDING TEMP SENSOR READ NORMAL IN THE GREEN RANGE, FIRE DEPT MET PLANE & INSPECTED FOR FIRE & GLOWING BRAKESDR N6WA2026070207Overheat Loop · faultedL BLEED DUCT WARNING MSG. R & R CERAMIC INSERT AT LOOP MT202 IAW AMM 36-21-00.SDR SCNA20260702375Overheat Loop · faultedNR 1 OVHT DET LOOP B INOPERATIVE. ON TEST ENG 1 OVERHEAT LIGHT DOES NOT ILLUMINATE AND FAULT LIGHT ILLUMINATED. ENGINE OVERHEAT AND FIRE DETECTION SYSTEMS; DUAL LOOP ). PERFORMED NR 1 ENG FIRE DETECTION TEST OPS CHECKS GOOD.SDR ABXA20260624282Overheat Loop · faultedL ENG OH-LP 2 MESSAGE. PERFORMED T/S IAW B767 FIM 26-11 F/T 804 AND AMM 26-10-01. SWAPPED CARDS M688 AND M690. FAULT DID NOT FOLLOW AND IT'S STILL FAULTY. REPOSITIONED CARDS TO THEIR ORIGINAL POSITIONS. ITEM DEFERRED IAW MEL 26-11-2-1. NO MX PROCEDURES APPLIESDR CALA2026062617367Overheat Loop · faultedDIVERSION TO GJT. RT WING BODY OVERHEAT. PERFORMED INSPECTION IN RT WING LE AREA & RT PACK BAY. NO BLEED LEAKS NOTED. DEFERRED RHWING-BODY OVERHEAT DETECTOR SYSTEM PER MEL 2613C. FIM 36-18 / 801 HAD FAULT CIDE 64 RT WING LE & ACFT PACK BAY, ALARM. PERF INSPSDR SCNA20260522213Overheat Sys · activatedDURING CLIMBOUT RIGHT SIDE WING BODY OVERHEAT LIGHT ILLUMINATED. RAN QRH & NOTIFIED MX CONTROL JB 7665. MX US RETURN TO MSP (EMERGENCY DECLARED)SDR REXA2026041300284Overheat Sensor · inoperativeAT FL250 MLG BAY OVHT WARN RAN QRH WARN MSG DID NOT EXTINGUISH BTMS ALL 0000 LANDED W/O ISSUE WARN MSG PERSISTS AT GATE. R/R FIRE DETECTION CONTROL IAW AMM 26-14-01. MESSAGE DID NOT CLEAR. R/R L & R MLG BAY TEMPATURE SENSING ELEMENT IAW AMM 26-14-04. OPS TESDR IPXA2026040311723Overheat Sys · false activationEMERGENCY DECLARED, EQUIP OVRHT MSG @ FL 390. DID QRH CHECKLIST YET MSG REMAINED. WENT AWAY @ 1200" AGL. ALSO REF 21-58-00-710-802-011 STEP D. AND STEP E. NO OVER HEAT NOTED. INSTALLED FWD AIR FILTER REF AMM 21-58-21-201 OPS CHECK GOOD SEE ATTACHED PICTURE FSDR AALA202604029753Overheat Loop · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. REPLACED DETECTOR ELEMENT (RIGHT WING) M1763 AND TESTED GOOD. PER AMM 26-18-00.SDR AALA202603257925Overheat Loop · faultyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: WING BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. **SUPPLEMENTAL REPORT FOR (AALA202603197925) SUBMITTED 03/19/2026 BY DFW: REMOVED AND REPLACSDR AALA202603197925Light · illuminatedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: WING BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. (OPEN).SDR CALA2026022013934Overheat Loop · faultedRT WING-BODY OVERHEAT DURING CLIMB & CRUISE. PERFORMED CHECKLIST, NO HELP. DIVERTED BACK. PER FLIGHT CREW: RT WING - BODY OVERHEAT CAME ON & STAYED ON, AFTER QRH PERFORMED. DID NOT EXTINGUISH UNTIL THROTTLES RETARDED FOR DESCENT. LIGHT REMAINED OFF FORSDR IPXA2026021866915Warning Message · illuminatedDIVERSION, EMERGENCY DECLARED, RT ENG OVHT AT CRUISE 4512 MSG WENT OUT AFTER 2 MIN AND ENGINE AT IDLE THRUST. ALL ENGINE INDICATIONS WERE NORMAL.SDR CALA2026020513601Sensor · faultedDUCT PX SPLIT ON DPT LEFT 10PSI RIGHT 40PSI REMOVED AND REPLACED PRECOOLER CONTROL VALVE REF AMM 36-12-03, AND 450 SENSOR REF AMM 36-11-05. RAN ENGINES OPS CHECKS NORMAL, REF FIM 35-10-00-3 FIG 305.SDR LR7A2026020103801Overheat Sensor · illuminatedMOMENTARY ILLUMINATION OF MASTER FIRE WARNING LIGHT, NO TEE HANDLE LIGHT INDICATION. REMOVED AND REPLACED THE NR 2 TURBINE OVERHEAT WARNING SENSOR. OPS CHECKED GOOD IAW LAC 382 WDM 26-10.SDR DALA2026012200476Overheat Sensor · faultedRETURNED TO ATL DUE TO RT WING BODY OVERHEAT. REPLACED M371 AND M1763 OVERHEAT ELEMENTS AND OVERHEAT DETECTION MODULE. CHECKED FOR BLEED AIR LEAKS, NONE FOUND. OPS CHECK GOOD. (LP 7725874)SDR SWIA2026012000013Overheat Loop · faultedANTI ICE DUCT WARNING ON CLIMB OUT OF DEN. QHR CLEARED THE MSG AND WE DIDN€™T NEED TO USE THE ANTI ICE AFTER THAT. (FLIGHT 5366) INTERROGATED MDC AND FOUND B1 CODES 007309 (L WING LOOP B) AND 007180 (L BLEED LOOP A). TROUBLESHOT L BLEED LOOP A PER FIM 36-2SDR AALA202512269331Sensing Element · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MIA DUE TO THE FLIGHT CREW REPORTING A RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED THE QRH PROCEDURES AND THE LIGHT STAYED ON. THE AIRCRAFT LANDED SAFELY SDR AALA202512264340Sensing Element · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MIA DUE TO THE FLIGHT CREW REPORTING A RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED THE QRH PROCEDURES AND THE LIGHT STAYED ON. THE AIRCRAFT LANDED SAFELY SDR AALA202512261255Sensing Element · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MIA DUE TO THE FLIGHT CREW REPORTING A RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED THE QRH PROCEDURES AND THE LIGHT STAYED ON. THE AIRCRAFT LANDED SAFELY SDR ABXA20251212330Overheat Loop · false indicationINTERMITENT MN CARGO LP 1 AND 2 STATUS MESSAGE W/FIRE WARNING.MTX GROUNDED A/C AND PERFORM MAIN CARGO/ENG/APU/FIRE/OVHT TEST. IAW AMM 26-14-00. OPS CHECKED NORMAL. NO MSG. RETURNED ACFT TO SERVICE.SDR N6WA2025110401Overheat Loop · out of positionANTI ICE DUCT WARNING MSG. INSPECTED AND FOUND LOOP MT173 TOUCHING PICCOLO TUBE. REPOSITIONED LOOP IAW CRJ AMM 36-21-15. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. OPS CHECK GOOD IAW CRJ AMM 36-21-00SDR 6CBA2025101625001Overheat Sensor · faultedDURING A ROUTINE REPOSITIONING FLIGHT FROM KCHS TO KBCT, THE CREW REPORTED A "BATTERY 1 HOT CAS" MESSAGE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO KVRB, LANDING WITHOUT ANY FURTHER INCIDENT. TECHNICIANS REPLACED THE #1 BATTERY P/N 31406-002 S/N 1190124SDR AALA202510010010Overheat Sys · no testAIRCRAFT IN BASE MAINTENANCE: WHEEL WELL FIRE OVERHEAT DETECTION BOX FAILED. CLEARED FAULT AND RESET DETECTION MODULE, PERFORMED SELF TEST, TEST COMPLETE NO FAULTS. PER AMM 26-18-01-740-801.SDR I5PA2025090519301Switch · faultyRIGHT TURB OVHR DET 1 STATUS MSG. R & R RT ENG OVHT DET 1 SWITCH PER AMM, OPS CHECK NORMAL.SDR CALA2025081907936Pcb · faultedR OVHT DET STATUS MSG FOLLOWED BY R ENG OVHT CAUTION. COMPLIED W ITH QRH. WENT AWAY WITH IDLE DEBRIEFED FLIGHT CREW, ADVANCED THROTTLES AT LANDING, MSG DID NOT REAPPEAR. HAS HISTORY REF LP 5883831. PERFORMED FLOWCHART 26-11 FAULT TREE 803. VERIFIED NO PRESSURESDR SWIA2025081800015Warning Message · illuminatedD:AFTER TAKE OFF RECEIVED GEAR OVHT FOLLOWED BY BRAKE OVHT. BOTH EXTINGUISHED AND RE ILLUMINATED. (BELIEVE TO BE ERRONEOUS BECAUSE OF HISTORY AND AFTER RUNNING QRH BTMS OFFENDING #4 ONLY SHOWED TEMP OF 1). RETURN TO DENVER EXTENDING GEAR BRAKE OVHT WARNING TRSDR SWAA2025081299948Control Unit · faultedLEFT WING TO BODY OVERHEAT LIGHT ILLUMINATED TWICE ON TAXI OUT. R & R COMPARTMENT OVERHEAT DETECTION CONTROL UNIT IN REF TO AMM 26-18-01. NO CURRENT FAULTSSDR SWAA2025080697783Overheat Sensor · faultedRIGHT WING-BODY OVERHEAT LIGHT ILLUMINATED AT 2 HOURS INTO FLIGHT. LIGHT NEVER EXTINGUISHED EVEN AFTER QRH AND ENGINE SHUTDOWN. FOUND FAULT: RT SIDE OVHT; RIGHT SIDE; LOOP 6 2ND GND AT 588; REMOVED R FWD STRUT OVERHEAT SENSOR ELEMENT (M1763) PER AMM 26-18-02SDR SWIA202507030624Warning Message · false activationIN SLN, GOT ANTI-ICE DUCT WARNING, RAN QRH. DIVERTED TO SLN TO AVOID CLOUDS (FLIGHT 5824 - FILED CLOSED)AFTER BRIEF INVESTIGATION WITH FLIGHT CREW, IT WAS REPORTED THE LEFT WING WAS INDICATING RED ANTI ICE DUCT WARNING ON EICAS. INSPECTED LEFT WING THERMAL SENSDR SWIA202506160011Detector · faultedL SIDE FUSELAGE ANTI ICE DUCT WARNING MESSAGE IN ICING WITH WINGS/COWLS SELECTED ON. ACCOMPLISHED QRH WHICH REMOVED MESSAGE. (FLIGHT 5435 - FILED CLOSED)PLEASE REFERENCE AML 1627651 AND AML 1627747 FOR HEAT SENSING ELEMENTS A41WK AND A47WK REPLACEMENT. PERFORSDR VNAA2025052311101Overheat Loop · faultedL BLEED DUCT WARNING MSG ON CLIMB, FL260. / REMOVED AND REPLACED LOOP MT141 IAW CRJ 700 AMM 36-21-01-000/400-806-A04. OPS CHECK GOOD AT THIS TIME. PERFORMED UNATE SCAN OF AILC. AILC OPS CHECKS GOOD AT THIS TIME.SDR U5QA2025052340152Detector · faultedRED PACK LEAK CAS B3-007406 LEAK DETECTED IN DUCT RUNNING FROM THE LEFT FLOW CONTROL VALVE TO THE PACK INLET AND PRECOOLER CROSS VALVE. PERFORMED OPERATIONAL CHECK OF THE AC SYSTEM. NO LEAK DETECTS AND SYSTEM OPERATES NORMALLY. PERFORMED BLEED LEAK DETECTION
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