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 ASAA2016090417916Overheat Sensor · failedB-SIDE FAULT IN NR 2 ENGINE OVERHEAT DETECTOR. ACFT GROUNDED. REMOVED AND INSTALLED NEW UPPER FAN DETECTOR ELEMENT REF AMM 26-11-01-000-801. PERFORMED NR 2 ENGINE FIRE DETECTION. OPS TEST, TASK 26-11-00-710-801. SYS CHECKS NORMAL.SDR SWAA2016082455081Overheat Sys · malfunctionedRIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. DIVERTED. R & R THE WING TO BODY OVERHEAT UNIT IAW AMM.SDR AALA20160814001Sensor · faultyDURING CRUISE, THE AFT CARGO TEMPERATURE STEADILY ROSE FROM 100 DEGREES F TO 122 DEGREES F. EMERGENCY DECLARED, AND LANDING UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE AFT CARGO BAY TEMPERATURE SENSOR 14HC IAW AMM 21-43-15. OPS CHECKED NORMAL.SDR ASMF201610002Module · intermittentAIRCRAFT RETURNED TO PLATFORM DURING TAXING, THE RIGHT SIDE WING BODY OVERHEATS LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO WHEEL WELL FIRE, WING AND BODY OVERHEAT DETECTION CONTROL MODULE IAW FIM 26-18 TASKS 801 AND 802, SHOWING FAILURE CODE 64 “SDR P5CA2016080200180Relay · faultyBULK CARGO OVERHEAT LIGHT ILLUMINATED. DEFER BULK CARGO OVERHEAT LIGHT ILLUMINATED MDDR 68835. FOUND RELAY K729 FAULTY , RELAY REPLACED IAW SWPM 20-81-00.SDR UIEA2016072600631Warning Message · false activationFWD EQUIPMENT OVERHEAT EICAS MESSAGE RECEIVED DURING CLIMB. CHECKLIST PERFORMED, EICAS MESSAGE CLEARED IAW CHECKLIST T/S IAW FIM 21-58-F/T 912, NO DEFECTS NOTED.SDR ASAA2016072217467Switch · malfunctionedFIRE, OVERHEAT TEST SHOWS FAULT LIGHT AND NO LIGHTS IN NR 2 ENGINE FIRE HANDLE. ACFT GROUNDED. REPLACED BROKEN TERMINAL IAW SWPM 20-30-11 AND WDM 26-11-21. OPS CHECKED OK. NR 2 ENGINE OVERHEAT DETECTOR SWITCH PLACED IN BOTH POSITION.SDR VNAA2016071800018Control Unit · malfunctionedLEFT JET OVERHEAT FAIL MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R FIRE AND OVERHEAT CONTROL UNIT AND PERFORMED CHECKS IAW AMM.SDR VNAA2016071800017Overheat Sensor · out of positionLEFT JET OVERHEAT FAIL MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED JETPIPE SENSING ELEMENTS AND FOUND LOOP-A SENSING ELEMENT TOUCHING A CLAMP. MAINTENANCE REPOSITIONED LOOP AND PERFORMED CHECKS IAW AMM.SDR UIEA2016070700568Warning Message · false activationEQUIPMENT OVERHEAT MESSAGE. ACCOMPLISHED QRH SELECRTOR TO STBY FOR 5 MIN THEN OVRD FOR 30 MIN. SELECTOR BACK TO AUTO . OVERHEAT LIGHT EXTINGUISHED . CONT FLIGHT NORMAL. PERFORMED EQUIPMENT COOLING TEST IAW AMM 21-58-00. NO FAULTS FOUND AT THIS STATION.SDR AALA20160630019Overheat Loop · malfunctionedDURING CRUISE A RIGHT WING BODY OVERHEAT MESSAGE DISPLAYED. EMERGENCY DECLARED. LANDING UNEVENTFUL AND AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED RIGHT FORWARD OVERHEAT DETECTION ELEMENT M1763 IAW AMM 26-18-02. OPS CHECKED GOOD.SDR PCSA2016062701Warning System · activatedEICAS MESSAGE: LT STRUT DUCT LEAK. THE PRV CLOSED AUTOMATICALLY BECAUSE THE STRUT TEMPERATURE IS TOO HIGH.SDR AALA20160620019Warning System · activatedAIRCRAFT WAS GROUNDED. AIR INTERRUPT, EMERGENCY WAS DECLARED, LANDING UNEVENTFUL. DURING CLIMB, THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. MAINTENANCE ACCOMPLISHED MCM 36-95-14. REPAIRED ALL LEAKS.SDR WX0A2016062073171Sensor · dirtyAFTER TAKEOFF, TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. SINCE APU OPERATION WAS REQUIRED BY MEL, IT REMAINED RUNNING. ENGINES WERE RETARDED IAW THE GRH. THE LIGHT EXTINGUISHED WHEN THE RT ENGINE WAS RETARDED TO IDLE. A LANDING WAS MADE WITH THE RT ENGSDR AALA20160526006Switch · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER WAS DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED MCM 36-95-14 & MCM 0930. R & R LT & RT TEMPERATURE SWITCHED. SYS CHECKED NORSDR AALA20160525003Switch · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER WAS DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED MCM 36-95-14 & MCM 0930. R & R LT & RT TEMPERATURE SWITCH. SYS CHECKED NORMASDR AALA20160518011Control Unit · malfunctionedDURING CLIMB, RECEIVED A WHEEL WELL FIRE WARNING FOR THREE SECONDS. EMERGENCY DECLARED. DIVERTED AND LANDING UNEVENTFUL. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF OVERHEAT OR FIRE. REMOVED AND REPLACED WHEEL WELL OVERHEAT DETECTION CONTROL UNIT M237 IASDR SWAA2016051051675Overheat Sys · faultyDIVERSION RT WING BODY OVERHEAT ILLUMINATED IN FLIGHT AFTER ABOUT 30 MINUTES FROM TAKEOFF. R & R M237 WING BODY O/H UNIT IAW MM.SDR OZCA20160504111Sensor · faultyLEFT TAIL PIPE HOT LIGHT ILLUMINATED. R & R LT TAIL PIPE HOT SENSORS. INSPECTED ALL TERMINALS & WIRES WITH NO DEFECTS NOTED. OPERATIONAL CHECKED OK AT THIS TIME.SDR P5CA2016042500086Circuit Card · inoperativeFWD EQUIPMENT OVERHEAT EICAS ; COMPLIED WITH QRH PROCEDURE. MSG EXTINGUISHED AFTER SELECTING OVERHEAD AUTO AFTER 30 MINUTES. R & R IN EC5 CONTROL CARD IAW AMM 21-58-42.SDR SWAA2016042951438Overheat Loop · faultyAIR TURN BACK. LT WING BODY OVERHEAT CAME ON CLIMB OUT & WOULD NOT EXTINGUISH. R & R LOOP IAW WDM.SDR IPXA2016042002382Warning Light · false activationEMERGENCY DECLARED ON SHORT FINAL DUE TO WHEEL WELL FIRE INDICATION. R & R DUCT LEAK DETECTION CARD IAW FIM 27-17-00-815 IAW BLOCK NR 1, 2, 3, 10, 11, 12, 13 & 24 R & R IAW MM 26-10-01-024-001 & 26-10-01-0424-006. PERFORMED ADJ/TEST AS REQIRED, NO FAULT AT TSDR AALA20160408006Switch · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB, RECEIVED TAIL COMPARTMENT HIGH TEMP INDICATION. ACCOMPLISHED MCM CARD TAIL COMPARTMENT LEAKS CHECK WITH NO LEAKS NOTED. R & R TEMP SWITCHES IAW MCM 36SDR AALA20160406014Switch · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB, RECEIVED TAIL COMPARTMENT HIGH TEMP INDICATION. ACCOMPLISHED MCM CARD TAIL COMPARTMENT LEAKS CHECK WITH NO LEAKS NOTED. R & R TEMP SWITCHES IAW MCM 36SDR RU3A20160330007Control Unit · failedBOTH BLEED AIR LIGHTS ILLUMINATED 17 MINS INTO FLIGHT. REPLACEMENT OF THE TAIL CONE OVERHEAT CONTROL UNIT SOLVED THE ISSUE.SDR AALA20160329013Module · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING TAKEOFF, MASTER CAUTION ILLUMINATED WITH, APU DETECTOR INOPERATIVE LIGHT. DURING CLIMB, MASTER CAUTION ILLUMINATED WITH ALL FIRE WARNING DETECTION LIGHTS. FOSDR YENA20160325266Overheat Sensor · faultedAIR RETURN BACK TO DEPARTURE. BLEED 1 LEAK DURING FLIGHT; R & R BLEED 1 OVERHEAT DETECTOR SYS, ODS, LOOP 3, A IAW AMM 36-21-02. OPS CHECKS GOOD. OK FOR SERVICE.SDR AALA201602159003Detector · defectiveRETURNED, ACFT WAS GNDED. CREW NOTED A STATUS MSG, RT ENG OH LP1, RESULTING IN THE ACFT RETURNING WHERE IT LANDED SAFELY WITH NO INCIDENTS REPORTED. NO EMER WAS DECLARED & THE ACFT DID NOT LAND OVERWEIGHT. REPLACED THE NR 2 ENG NACELLE OVERHEAT DETECTOR IAWSDR SWIA201641807Warning Message · false activationLEFT 14TH DUCT MESSAGE OVERTEMP ON CLIMBOUT. CREW FOLLOWED QRH AND TOOK ENGINE TO IDLE. CREW DECLARED EMERGENCY. R & R BLEED DUCT INSIDE PYLON, OPS CHECKED GOOD. R & R LT PYLON SENSING ELEMENT IAW AMM. OPS CHECK GOOD.SDR QXEA2016011700028Warning Light · false activationNR 1 BLEED HOT ILLUMINATED IN FLIGHT, DIVERTED, UNEVENTFUL LANDING. ACCOMPLISHED FSM BLEED HOT RESET PROCUDURE RESET SUCCESSFULL BLEED HOT CAUTION DID NOT ILLUMINATE. RETURNED TO SERVICE.SDR S9BA20160001Element · chafedBLEED AIR LEAK CAUTION LIGHT ILLUMINATED DURING FLIGHT, PROCEED TO QRH AND LIGHT REMAINED ILLUMINATED, PROCEEDED WITH ENGINE SHUTDOWN. PRELIMINARY INSPECTION FOUND SENSING ELEMENT CHAFING AGAINST DUCT CLAMP. SENSING ELEMENT REPOSITION AND SECURED, OPS CHECK SDR AALA20151226001Sensor · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB RT WING BODY OVERHEAT AMBER LIGHTS & MASTER CAUTION ILLUMINATED. QRH PROCEDURES COMPLETED & LIGHTS EXTINGUISHED. NGAR FOR TROUBLESHOOTING. ACCOMPLISHESDR AALA20151212004Detector · shortedAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB RT WING BODY OVERHEAT LIGHT ILLUMINATED. FOUND THE RT FWD STRUT CAVITY OVERHEAT DETECTOR M1763 SHORTED. R & R DETECTOR IAW AMM 26-18-02. OPERATIONAL CHECKED OK. ACCOMPLISHED HSDR ASAA2015111713827Warning Light · false activationLEFT WING BODY OVERHEAT LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH IAW QRH. NO PASSENGER CABIN SMELL OR SMOKE INDICATIONS. AFTER DIVERT SMELL LIKE A DUSTY FURNACE ROWS 18ABC AND AFT. ACFT GROUNDED. DIVERSION TIME-43 MINUTES. PERFORMED OVERHEAT DETECTION MSDR HNAA2015101900305Warning Light · false activationELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED ON ROTATION, WOW CAUTION LIGHT ILLUMINATED AFTER GEAR SELECTED UP, NOSE GEAR DOOR CAUTION LIGHT ILLUMINATED AFTER GEAR RETRACTED. SELF CLEARED AFTER CHECK LIST COMPLIED WITH.SDR CALA2015100600824Overheat Loop · defectiveDURING TAXI OUT NR 1 ENG START, THE OVERHEAT DETECTOR ANNUNCIATOR LIGHT CAME ON. SHORTLY AFTER THE NR 1 ENG FIRE SWITCH LIGHT ALSO ILLUMINATED, NO BELL. ENG WAS SHUT DOWN, QRH FOLLOWED. BOTH FIRE BOTTLES USED. FOUND HIGH RESISTANCE LOOP M1759, REPLACED SAMSDR ASAA2015100413319Lug · failedNR 1 ENGINE OVERHEAT LOOP-A INOPERATIVE. ACFT GROUNDED. BROKEN TERMINAL LUG AT UPPER FAN DETECTOR FOR A-LOOP. INSTALLED NEW TERMINAL LUG, REF SWMP 20-30-00 & WDM 26-11-11. ENGINE FIRE TEST NORMAL.SDR RU3A20150918019Sense Line · damagedRIGHT BLEED AIR FAIL & MC ILLUMINATED. A HOLE WAS DISCOVERED IN THE EVA SENSE LINE IN RT NACELLE LE. LINE WAS REPLACED WITH NO DEFECTS NOTED.SDR CALA2015090394265Overheat Loop · dirtyBLEED LOOP 1 BODY FAILURE OF BODY DUCT LEAK DETECTION LOOP OR LT DUCT LEAK OVERHEAT DETECTION SYS, DLODS, CARD. CLEANED & RESEATED LOOP 1 M26144 TO RESISTOR M26111 CONNECTOR & RESEATED P85A5 DLODS CARD, FAULT NOT ACTIVE. BLEED LOOP 1 BODY LOOP SYS OKAY FOR SSDR ASOA2015083013647Overheat Loop · shortedMLG OVERHEAT WARNING AFTER TAKE OFF. DECLARED AN EMERGENCY AND COMPLIED WITH QRH AND LANDED AT 66.7K LBS. ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED AS A PRECAUTION. UPON FURTHER INSPECTION, FOUND RT ELEMENT TO HAVE LOW RESISTANCE FROM INNER SDR AALA20150824011Detection Sys · faultyAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, THE RT WING BODY OVERHEAT LIGHT ILLUMINATED & REMAINED ILLUMINATED UNTIL AFTER LANDING. ACCOMPLISHED FIM TASK 26-18-00-810-801, BITE TEST SHOWS FAULT CODE 64. FOUND RT FWD STRSDR DIXA2015F00097Overheat Sensor · intermittentCREW REPORTED CLIMBING THROUGH FL 150, RED REAR BAY OVERHEAT LIGHT ILLUMINATED, CREW FOLLOWED CHECKLIST PROCEDURES. LIGHT EXTINGUISHED WHILE STILL CLIMBING THROUGH FL 180 RED REAR BAY OVER HEAT LIGHT ILLUMINATED FOLLOWED BY A BURNING ODOR AND LIGHT SMOKE IN CSDR COZA20150819060Overheat Sensor · false indicationRT WING BODY OVERHEAT LIGHT ILLUMINATED. BITE CHECK OF THE COMPARTMENT OVERHEAT DETECTION CONTROL UNIT DISPLAYED FAULT CODE 64. RESISTANCE CHECKS ON SENSING ELEMENTS ASSOCIATED WITH THIS CODE WERE PERFORMED. THE RT INBD L/E ELEMENT M1269 WAS FOUND OUT OF LISDR UIEA2015081700433Overheat Loop · faultySTATUS MSG, INTERMITTENT INFLIGHT, LT ENG OVERHEAT LP2. R & R LT ENG OVERHEAT LOOP IAW AMM 26-11-02. OPERATIONS CHECKED NORMAL.SDR ASAA2015081112837Warning Light · false activationLEFT SIDE "OVERHEAT" LIGHT WILL NOT EXTINGUISH. ACFT GROUNDED. PERFORMED FIM TASK 30-41, TASK 801, BITE PROCESSED. OPS CHECKED NORMAL. OK FOR SERVICE.SDR 29GA2015081200002Overheat Sensor · failedRT BLEED AIR LEAK ILLUMINATED. RAN THE QRH, THE LIGHT WENT OUT THEN CAME BACK ON. WE RAN THE QRH AGAIN AND SHUT THE NR 2 ENGINE DOWN. HEAVY SOOT DEPOSITS IN DUCT AREA. LOOP INSULATOR GROMMETS ON AFT ELEMENT DRY-ROTTED. R & R RT NACELLE DUCT ASSY ELEMENT SDR SIMA20150810001Warning System · false activationMAIN LANDING GEAR OVERHEAT EICAS MSG PRESENTED IN FLIGHT. COMPLETED PROCEDURE, DIVERTED & EMER DECLARED. DEFERRED MLG BAY OVERHEAT DETECTION SYS. M PROCEDURES COMPLIED WITH MEL 26-20. OPERATIONS CHECKED THE MLG OVERHEAT DETECTION SYS IAW AMM 26-14-00. MELSDR 29GA2015081200001Overheat Sensor · bentRIGHT BLEED AIR LEAK ILLUMINATED. IT EXTINGUISHED AND RE-ILLUMINATED. WE RAN QRH WITH 2 RESET ATTEMPTS, THEN SHUTDOWN THE NR 2 ENGINE. ALL PARAMETERS OTHER. R & R ELEMENT SENSING OVER HEAT TUBE IAW AMM 36-23-10-02. OPS CHECK GOOD ON GROUND.SDR 29GA2015071200001Overheat Sensor · bentRT BLEED AIR LEAK ILLUMINATED. IT EXTINGUISHED AND RE-ILLUMINATED. WE RAN QRH WITH 2 RESET ATTEMPTS, THEN SHUTDOWN THE NR 2 ENGINE. ALL PARAMETERS OTHER. R & R ELEMENT SENSING OVER HEAT TUBE IAW AMM 36-23-10-02. OPS CHECK GOOD ON GROUND.SDR SWIA201541389Loop · failedLEFT BLEED DUCT WARNING TURNS INTO A CAUTION AT FL310. REPLACED THE LT BLEED LOOP MT141. ALL CHECKS GOOD.
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