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 UIEA2017091701679Fire Loop · malfunctionedDURING A TRANSIT CHECK, FOUND RIGHT ENGINE FIRE LOOP 2 STATUS MESSAGE. REMOVED AND REPLACED RIGHT ENGINE UPPER AFT FIREWALL FIRE DETECTOR IAW AMM 26-11-00. OP CHECKED GOOD.SDR BJNA20170911008Warning Light · illuminatedLEFT WING BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT & WOULD NOT EXTINGUISH.SDR AALA20170903009Warning System · false activationTHE AIRCRAFT WAS GROUNDED. AIRCRAFT RETURNED TO THE GATE ACCOUNT LEFT ENGINE OVER HEAT WITH BOTH FIRE BOTTLES USED. FIRE DEPARTMENT MET AIRCRAFT WITH NO EVIDENCE OF OVER HEAT. PERFORMED ENG. EXCEEDANCE CK PER AMM 71-00-00-740-801 NO EXCEEDANCES. PERF ACT TESSDR HALA2017081800228Thermocouple · failedAIR TURN BACK. RT ENGINE SYSTEM FAILED, LT ENGINE SYSTEM FAILED ON CLIMB. PERFORMED FIM TASK 77-22-801, NR 1 ENGINE NO DEFECTS, NR 2 ENGINE TURBINE OVERHEAT CHN A/B DISAGREE, R & R TURBINE BEARING OVERHEAT DETECTOR THERMOCOUPLE IAW AMM 77-23-01, OPS GOOD, NSDR UIEA2017080901446Warning Message · false activationFWD EQUIPMENT OVERHEAT EICAS LIGHT ILLUMINATED. PERFORMED QRH PROCEDURES. OAT WAS 46 C. MESSAGE EXT IAW QRH PROCEDURES, OPS CHECKED EQUIPMENT COOLING SYSTEM IAW 21-58-00/501. NO FAULTS FOUND.SDR REXA2017080400856Element · inoperativeRT 14TH STAGE BLEED WARNING AT FL 280 PERFORMED QRHM MESSAGE DID NOT GO OUT, CLOSED 4 14TH STAGE BLEED, OPENED ISOLATION VALVE REDUCED RT THRUST TO IDLE. LANDED FLAPS 20.
R & R PYLON SENSING ELEMENT ON RT SIDE LOOP A58WK IAW AMM 36-21-04. OPS CHECKED GOOD.SDR UIEA2017073001387Warning Light · false activationAFTER TAKEOFF, THE FWD EQUIPMENT OVERHEAT ILLUMINATED. ACCOMPLISHED QRH NON NORMAL PROCEDURE. EICAS MESSAGE OUT AFTER PROCEDURE COMPLETE. PERFORMED FIM 21-58 FT 815, NO DEFECTS NOTED. SYS OPS NORMAL.SDR DALA2017072505680Warning System · false activationL DUCT LEAK LP1 STATUS/MTC MSG. INSPECTED PACK DUCTING. RAN PACKS. NO MSG'S - CHECKS GOOD.SDR AALA201707249033Overheat Sensor · false indicationBULK CARGO HEAT INDICATION. EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE. LANDING UNEVENTUL. ACCOMPLISHED AN AFT AND BULK CARGO HEAT TEST IAW FIM DMC-B787-A-21-40-F0-01A-421A-A. NO FAULTS FOUND. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.SDR UIEA2017072401282Warning Message · false activationAFTER TAKE OFF, FWD EQPT OVERHEAT DISPLAYED COMPLIED WITH QRH AND WAS ABLE TO CLEAR MESSAGE. PERFORMED EQUIP COOLING TEST IAW MM 21-58-00. SYSTEM CHECKED NORMAL NO FAULTS NOTED.SDR UIEA2017071801237Warning Light · false activationFWD EQUIPMENT OVERHEAT EICAS ON TAKEOFF RAN QRH CHECKLIST AFTER 35 MINUTES LIGHT EXTINGUISHED, GROUND TEMP 47C EQUIPMENT COOLING SYS OPS TESTED NORMAL IAW AMM 21-58-00/705-120-006.SDR SWAA2017071715103Module · malfunctionedINFLIGHT SHUTDOWN/AIR TURNBACK/DECLARED EMERGENCY, AT CRUISE 22K, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. R&R ENGINE APU FIRE OVERHEAT MODULE PER MM.SDR AALA20170713001Warning Message · false activationRIGHT AFT WING BODY OVERHEAT INDICATION. EMERGENCY DECLARED, FLIGHT RETURNED TO DEPARTURE. LANDING UNEVENTFUL. ACCOMPLISHED WING TO BODY HEAT DETECTOR FAULT ISOLATION IAW 26-18-00-810-802, CONTROL MODULE BITE IAW AMM 26-18-00, AND HIGH POWER ENGINE RUN IASDR AALA201706309021Overheat Sensor · malfunctionedDURING DESCENT, MASTER CAUTION LIGHT, OVERHEAT DETECTOR, SIX PACK AND APU DETECTOR INOPERATIVE LIGHTS ILLUMINATED INTERMITTENTLY THREE DIFFERENT TIMES OVER 20 MINUTES. APU WAS NOT STARTED. ACCOMPLISHED APU FIRE DETECTION OPS TEST, TESTED GOOD IAW AMM 26-15-00SDR RU3A20170627013Line · leakingRT BLEED AIR FAIL ILLUMINATED IN CRUISE FLIGHT. DISCOVERED A PINHOLE LEAK IN EVA LINE FORWARD AND OUTBOARD OF RT WING JACK POINT. LINE WAS REPLACED. NO FURTHER ACTION REQUIRED.SDR REXA2017062600726Sensing Element · inoperative14TH DUCT CAUTION DURING CLIMBOUT, RETURNED TO FIELD IAW QRH. REMOVED AND REPLACED THE SENSING ELEMENT IAW AMM 36-21-04. OPS CHECKED GOOD IAW AMM 36-21-00.SDR REXA2017060500651Sensor · inoperativeWHILE CLIMBING OUT THROUGH 150' BRAKE OVERHEAT WARNING ILLUMINATED. COMPLETED QRH. BRAKE TEMP ON LEFT OUTBOARD WAS RED AT 18 AND VERY IRRATIC NUMBERS.AFTER COMPLETION OF QRH WARNING WENT AWAY ALL INDICATIONS NORMAL. CONTINUED CLIMB THROUGH FL210' AND BRAKE OVHSDR SWAA2017060114089Module · faultyRIGHT WING - BODY OVERHEAT LIGHT INDICATION. R&R WING BODY OVERHEAT MODULE IAW MM.SDR UIEA2017052000824Warning Message · false activationDURING CLIMB OUT, THE FWD EQUIPMENT OVERHEAT EICAS MESSAGE ACTIVATED. COMPLETED QRH, MESSAGE DID NOT ILLUMINATE AGAIN. RETURNED EQUIPMENT COOLING SWITCH TO AUTO AND COMPLIED WITH SYSTEM OPS CHECK IAW AMM 21-58-00, NO FAULTS INDICATED.SDR AALA20170517011Overheat Loop · malfunctionedCREW REPORTED RT WING TO BODY OVERHEAT LIGHT ILLUMINATED INTERMITTENTLY DURING CRUISE. DECLARED AN EMERGENCY AND DIVERTED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT. MAINTENANCE ACCOMPLISHED FIM 26-18-00-810-803, FOUND OVERHEAT DETECTOR TO BE WITHIN LSDR AALA201705059052Overheat Loop · faultyAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DURING DESCENT THE RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED INTERMITTENTLY AT LOW AND HIGH POWER SETTINGS. FOUND OVERHEAT LOOP M269 BAD. REMOVED AND REPLACED LOOP IAW AMM REF 26-18-02. SYSTEM CHECKS NORMAL.SDR AALA20170502007Sensor · faultyAFTER TAKE-OFF, THE TAIL COMP TEMP HIGH OVERHEAT LIGHT CAME ON. THE LIGHT WENT OUT AFTER MEMORY ITEMS. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DFW WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LT TAIL COMP OVERTEMP SENSOR IAW AMM 36-20-02. OPS AND LESDR AALA201704259007Sensing Element · shortedFIRE/OVERHEAT INDICATION RECEIVED DURING CLIMB. ACCOMPLISHED CHECKLIST AND LIGHT EXTINGUISHED. NORMAL FLIGHT CONTINUED. INSPECTED RIGHT ENGINE FIRE/OVERHEAT DETECTION SYSTEM AND FOUND SENSING ELEMENT GROUNDING TO SUPPORT TUBE ON UPPER AFT ENGINE FIRE LOOP. SDR DALA2017032802484Test Panel · defectiveON CLIMB OUT EICAS STATUS MESSAGE R DUCT LEAK LP 1 APPEARED. REPLACED DUCT LEAK TEST PANEL. SYSTEM OPERATION IS NORMAL.SDR AALA20170322001Sensor · faultyTAIL COMP OVERHEAT LIGHT CAME ON INFLIGHT. LIGHT EXTINGUISHED WHEN PNEUMATIC CROSS FEEDS CLOSED, AIRFOIL ANTI ICE OFF AND A/C SUPPLY HP BLEED OFF. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. ACCOMPLISHED MCM 36-95-14. REMOVED &SDR AALA201703179035Detector · faultyAIRCRAFT WAS GROUNDED. RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED RIGHT AFT STRUT DETECTOR M1764 IAW AMM 26-18-02-000-801. OPERATIONAL CHECK GOOD.SDR A6WA201744844Overheat Loop · chafedDURING CLIMB FL240, RECEIVED AN MLG BAY OVERHEAT WARNING. COMPLIED WITH THE QRH. BTMS WAS 1-1-1-1 ON ALL BRAKES. WARNING WAS INTERMITTENT AND WENT OUT AFTER LANDING. PERFORMED GENERAL VISUAL INSPECTION OF AIRCRAFT AND MLG BAYS NO DEFECTS NOTED. FOUND RT MLG SDR AALA201703099008Overheat Sensor · faultyAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DCA-DFW FLIGHT. LEFT ENGINE WING TO BODY OVERHEAT INDICATION DURING DESCENT. LANDING UNEVENTFUL. INSPECTION FOUND NO INDICATION OF HEAT. REMOVED AND REPLACED LEFT FORWARD STRUT CAVITY OVERHEAT DETECTOR M1671 IAW AMM SDR ASAA2017022719958Overheat Loop · failedAPU OVERHEAT DETECTOR INOPERATIVE CAUTION LIGHT ILLUMINATED. ACFT GROUNDED. REMOVED AND REPLACED M1925 APU TAILPIPE OVERHEAT DETECTOR IAW AMM 26-15-01-000-802 & AMM 26-15-00-400-802. PERFORMED APU FIRE DETECTION OPERATIONAL TEST IAW AMM 26-15-00-710-801, ALLSDR UIEA2017022200229Circuit Card · malfunctionedRIGHT ENGINE OVERHEAT LOOP 1 ILLUMINATED. REMOVED AND REPLACED ALFOLTS CARD IAW FIM 26-11 TASK 804 AND SWPM 20-82-13. OPS CHECKED NORMAL.SDR UIEA2017022200232Detector · malfunctionedSTATUS MESSAGE FOR THE RT ENGINE OVERHEAT LOOP 1. REMOVED AND REPLACED THE RT ENGINE UPPER FWD OVERHEAT DETECTOR IAW AMM 26-11-02. OPS CHECKED NORMALSDR LR7A2017020800962Detector · inoperativeDURING SCHEDULED A-1 CHECK, FOUND THE MASTER CAUTION FIRE LIGHT DIMLY FLASHING. REPAIR BY REPLACEMENT OF TURBINE OVERHEAT KEYER IAW SMP581 CH26-10.SDR UIEA2017020700152Circuit Card · failedRT ENGINE OVERHEAT LOOP 1 STATUS MESSAGE DURING FLIGHT. REMOVED AND REPLACED THE RT OVERHEAT LOOP 1 DETECTOR CARD M689 IAW AMM 26-10-01 , OPS CHECKED OK.SDR F2PA201701310001Sensor · failedAFTER TAKE OFF CREW RECEIVED A CAS WARNING "WING STAB" LEAK. AIRCRAFT RETURNED TO STARTING POINT AND MAINTENANCE CREWS WERE DISPATCHED FROM KFLL TO INVESTIGATE SOURCE OF THE CAS MESSAGE. IT IS BELIEVED AT THIS TIME THAT THE LEAK SENSOR ITSELF FAILED, AND NO LESDR T17A201701208015Overheat Sensor · defectiveDURING CLIMB OUT AT APPROXIMATELY 13,000 FT, THE REAR BAY OVERHEAT ANNUNCIATOR ILLUMINATED. CREW RAN CHECKLIST AND REQUESTED TO RETURN TO DEPARTURE. NO BLEED LEAKS WERE DETECTED. WHEN THE SENSORS WERE BENCH CHECKED, THREE WERE FOUND DEFECTIVE. MX REPLACED SDR AALA20161220012Valve · faultyFLIGHT RETURNED TO DEPARTURE FOR A TAIL COMPARTMENT OVERHEAT INDICATION WARNING. EMERGENCY DECLARED. UNEVENTFUL LANDING. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED RIGHT AUGMENTATION VALVE IAW MCM CARD 5770-20. LEAK CHECK IAW MCM CARD 5770-20 AND MCM CARD 5SDR AALA20161214033Warning System · false activationDURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH WARING ILLUMINATED ACCOMPANIED BY FIRE AGENT 2 LOW LIGHT ILLUMINATION. EMERGENCY DECLARED. RETURNED TO FIELD. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED HIGH PRESSURE LEAK CHECK IAW TASK CARD 5461. OPERATIONAL CHSDR UIEA2016121200998Circuit Card · malfunctionedSTATUS MESSAGE FOR RT ENG OVERHEAT LOOP 1. REMOVED AND REPLACED THE OVERHEAT DETECTOR IAW AMM 26-11-02-424-033, AND REMOVED AND REPLACED M689 FIRE DETECTOR CARD IAW AMM TASK 26-10-01-024-024. OPS CHECK GOOD.SDR AALA20161201009Control Module · faultyAIRCRAFT GROUNDED. WHEEL WELL FIRE LIGHT ON CENTER PEDESTAL WILL NOT EXTINGUISH. REMOVED AND REPLACED M237 COMPARTMENT OVERHEAT DETECTION CONTROL MODULE ASSEMBLY IAW AMM 26-18-01. OPERATIONAL CHECK GOOD.SDR CALA2016112600974Control Unit · faultyWHEEL WELL FIRE INDICATION ON FINAL. OCCURRED WHEN FLAPS PLACED TO 5. REMAINED ON THROUGH LANDING FOUND FAULT CODE 84 ON CTRL UNIT, PER FIM26-18-00-810-802 VOLTAGE CHECKS & RESISTANCE CHECKS GOOD. CODE WOULD NOT RESET. RPL OVERHEAT CTRL UNIT REF MM 26-18-0SDR UIEA2016111400840Overheat Loop · false indicationSTATUS MESSAGE RT ENGINE OVERHEAT LOOP 1. COMPLIED WITH FIRE DETECTION BITE PROCEDURE, FIM 26-11 FT 808, MESSAGE CLEARED, SYS OK.SDR ASOA20161008013Warning Message · false activationPILOT REPORTED THE RT JET OVERHEAT FAIL CAUTION MESSAGE IN FLIGHT. CAME ON AND DISAPPEARED TWICE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY IAW AMM 26-11-00, OPS CHECKED GOOD WITH NO DEFECTS NOTED. THE DISCREPANCY HAS NOT REPEATED.SDR A6WA201644414Warning Message · false activationENROUTE, RECIEVED MLG BAY OVERHEAT WARNING MESSAGE, COMPLIED WITH THE QRH. BTMS INDICATIONS WERE ALL AT 1. LANDED WITHOUT INCIDENTSDR CALA2016092900702Overheat Loop · failedRIGHT WING TO BODY OVERHEAT LIGHT INFLIGHT DID NOT EXTINGUISH. TROUBLESHOT IAW FIM 28-18-00-810-802. FOUND LOOP FAILED M1764 PER STEPS H (4) (D) 3. REPLACED M1763 AND M1764 IAW AMM 26-18-02. TESTED OKSDR MASA2016092612418Insulator · looseACFT RETURNED TO FIELD & EMERGENCY WAS DECLARED DUE TO, LEFT BLEED DUCT WARNING IN FLIGHT. MX SECURED LOOP INSULATOR AT M225L.SDR CALA2016092600683Warning Light · illuminatedAT FL 380 THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED, DID NOT GO OUT WITH THRUST LEVER CLOSED. RAN ENGINE FIRE, ENGINE SEVERE DAMAGE OR SEPARATION CHECK LIST. SHUTDOWN THE NR 1 ENGINE. DISCHARGE LEFT AND RIGHT EXTINGUISHER BOTTLES.SDR AALA20160921005Overheat Sensor · faultyDURING CLIMB, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED WORK CARD 36-95-14. REMOVED AND REPLACED LEFT AND RIGHT TAIL COMPARTMENT HIGH TEMPERATURE SENSORS IAW AMSDR AALA20160921004Overheat Sensor · faultyDURING CLIMB, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED WORK CARD 36-95-14. REMOVED AND REPLACED LEFT AND RIGHT TAIL COMPARTMENT HIGH TEMPERATURE SENSORS IAW AMSDR AALA20160912009Module · faultyRIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED DURING CRUISE AT FL 360. QRH PROCEDURE ACCOMPLISHED. LIGHT EXTINGUISHED WHEN RIGHT PACK WAS TURNED OFF. AN EMERGENCY WAS DECLARED, DESCENDED TO FL 240. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. SDR QXEA2016090700572Switch · malfunctionedNR 2 BLEED HOT CAUTION DURING CLIMB AT APPROXIMATELY 15000 FT MSL. REPLACED NACELLE DUCT LEAK OVERTEMP SWITCH. NR 2 BLEED HOT CAUTION DID NOT APPEAR DURING OPS TEST. RETURNED TO SERVICE.
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