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 MYWA100080Overheat Loop · no testETOPS SIGNIFICANT SYSTEM - NR 2 ENGINE B-LOOP OVERHEAT DETECTION WOULD NOT TEST.SDR J7SA5752100528Overheat Loop · out of position'R 14TH STGE DUCT' CAS MESSAGE POSTED. CREW PERFORMED IN-FLIGHT SHUTDOWN OF RT ENGINE AND DECLARED AN EMERGENCY. ACFT LANDING UNEVENTFUL. MX FOUND NO INDICATION OF ACTUAL OVERHEAT OR FIRE. FOUND A GROMMET THAT PLACE THE LOOP IN A BAD ROUTING CONDITION. MOVSDR UALA2010052401775Sensor · faultyRH ENG BLEED OVERHEAT MSG. RESET BLEED SWITCH. NO FURTHER INDICATION. REPEAT GRIPE. SECURED RT ENG HIGH PRESS SHUTOFF VALUE PER MEL ITEM 3611R. BITE CHECKED BLEED COMPUTER FOUND RIGHT ENG FAV AND FAS FAULTING ON PREVIOUS FLT. FAS SENSOR PCN 481-9007. ALSO SCRESDR HALA2010051900220Warning Message · illuminatedETOPS SIGNIFICANT SYS - IN CRUISE FLT GOT STATUS MSG "L ENG OH LP Z" NO OTHER ALERTS, ALL OPS NORM. PERFORMED T/S IAW FIM 26-11-00/100, FIG 104, ALL CKS NRM IAW CHART. COULD NO DUPLICATE MSG - NO HISTORY NOTED OPS CKS NRM.SDR UALA2010051101606Loop · damagedBODY BLEED LOOP 1 MSG. BODY BLEED LOOP 1 MSG TOTAL BODY LOOP 1 RESISTANCE WAS 150 OHMS. LOOP 2 WAS 128 OHMS. FOUND HIGH RESISTANCE AT M26146 LOOP CONNECTION. CLEANED CONNECTOR AND RESECURED. RESISTANCE NOW CK'S 128 OHMS. NO FAULTS.SDR UALA2010050401501Circuit Card · faultyBLEED LOOP 2 BODY FAILURE OF BODY DUCT LEAK DETECTION LOOP OR RT DUCT LEAK OVERHEAT DETECTION SYS (DLODS) CARD. STATUS MSG-2631142 ACTIVE ER HARD MSG-2631142 ACTIVE ER HARD MSG-2631132 INACTIVE ER INTER. AHM FAULTING BLD BODY LP-2 ZONE 13,14 IS OPEN-INTMTNT-CRSDR REXA201000065Sensing Element · malfunctionedMLG OVERHEAT FAIL FOLLOWED BY MLG OVERHEAT WARNING. T/S WIRING PER FIM 26-10-00. REMOVED AND REPLACED RT WHEEL BIN HEAT SENSING ELEMENT IAW AMM 26-14-04. OPS CHECK GOOD. OK FOR SERVICE.SDR SWAA102405Overheat Sensor · faultyDIVERSION - INTERMITTENT WHEEL WELL LIGHT AND FIREBELL AT CRUISE. REMOVED AND REPLACED WHEEL WELL OVERHEAT DETECTOR PER MM.SDR AALA20100425LAX01Detector · faultyLAX - INFLIGHT SNA-DFW - CREW REPORTED LEFT WING BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. DETECTOR M1764 WAS PLACARDED AND THEN WAS REPLACED ON 05/02/2010 IN MIA. SYSTEM GROUND CHECK NORMAL SDR MASA2010032400246Warning System · malfunctionedLEFT JET LOOP OVERHEAT CAUTION IN FLIGHT INT. RESET SYSTEM.SDR UALA2010031500851Overheat Loop · out of positionREPEAT GRIPE BODY DUCT OVERHEAT LIGHT ON MOMENTARILY AFTER SECOND ENG START. RAN ENGINES 1 AND 2 GOT DUCT OVERHEAT GOT LIGHT AGAIN. REPLACED CARD M691, NO HELP. RE-INSTALLED ORIGINAL CARD. FOUND DETECTION LOOP TS226 LAYING ON APU BLEED DUCT JUST FWD OF APUSDR UALA2010031500855Detection Sys · out of positionADP INOPERATIVE PERFORMANCE PENALTIES WILL BE APPLIED BECAUSE BODY LOOP DETECTION SYSTEM IS DEFERRED. FOUND DETECTION LOOP TS226 LAYING ON APU BLEED DUCT JUST FWD OF APU BLEED VALVE. REPOSITIONED LOOP. RAN ENG. DUCT LEAK LIGHT REMAINS EXTINGUISHED.SDR ASAA1057499Overheat Sensor · inoperativeAPU DET INOP LIGHT ILLUMINATED. INSPECTED AND FOUND M1975 TAIL PIPE APU OH DETECTOR INOP. REPLACED DETECTOR REF MM 26 15 01. PERFORMED OPS TEST REF MM 26 15 00. SYS OPS TEST NORMAL.SDR MASA2010021500138Warning System · activatedWING OVERHEAT WARNING IN FLIGHT. CLEANED / RE-SEATED AILC C/P PER AILC TEST AND RUNS OPS GOOD.SDR CALA2010021500030Detector · failedON DESCENT INTO EWR THE LEFT WING BODY OVERHEAT LIGHT STARTED FLICKERING AND THEN STAYED ON STEADY. THE CHECKLIST WAS RUN, RESULTING IN THE APU BEING SHUTDOWN. THE LIGHT REMAIN ON FOR THE REST OF THE FLIGHT. AN EMERGENCY WAS DECLARED AND LANDING ACCOMPLISHESDR MASA2010020700129Warning System · malfunctionedWING OVERHEAT WARNING IN FLT RT WING. OP CHECKED WITH CREW CND NFAR-014615.SDR 2010FA0000062Control Box · unknownREPLACED THE OVERHEAT CONTROL BOX AND THE EXHAUST PIPE FIRE ELEMENT. NO FURTHER PROBLEMS NOTED.SDR IPXA10658064Sensing Element · malfunctionedDIV - RT BLEED DUCT LEAK LIGHT, EICAS MESSAGE IN FLIGHT. R & R ELEMENT (TS216) IAW MM 26-18-01-4. ADJ/TEST IAW MM 26-18-01-5.SDR MALA090159Detector · malfunctionedLT TAIL PIPE HOT ILLUM DURING CRUISE, DID NOT ILLUM AGAIN DURING THE FLIGHT. REMOVED OLD SEALANT AND REPLACED WITH NEW.SDR PCSA2009111701Shim · damagedENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED CLIMBING THROUGH FL260. THE STRUT OVERHEAT PROCEDURE WAS ACCOMPLISHED IAW THE AOM AND THE LIGHT EXTINGUISHED. MAINTENANCE REPLACED THE DAMAGED 6TH STAGE DUCT SHIMS AND THE OVERHEAT DETECTION ELEMENT, RETORQUED THESDR AALA20091102TUL14Control Module · faultyLANDED ABQ ACCT CREW REPORTED LEFT WING/BODY OVERHEAT LIGHT ILLUMINATED. LOWERED ALTITUDE TO FLIGHT LEVEL 250 CAUSING INCREASED FUEL BURN. LANDED ABQ WITHOUT INCIDENT FOR FUEL. PLACARD LEFT WING/BODY OVERHEAT INDICATOR INOPERATIVE AND RE-DEPARTED. REPLACEDSDR AALA20090914TUL06Sensor · faultyTAIL HIGH TEMPERATURE WARNING INDICATION LIGHT ILLUMINATED. RETURNED BNA AND LANDED WITHOUT INCIDENT. REPLACED LEFT TAIL TEMPERATURE SENSOR.SDR AALA20090911SEA01Sensor · faultyCREW REPORTED TAIL COMPARTMENT OVER TEMP INDICATION AT 18,000 FEET AND DID NOT EXTINGUISH. RETURNED TO SEA AND LANDED WITHOUT INCIDENT. REPLACED TAIL COMPARTMENT TEMPERATURE SENSOR.SDR A6WA200940512Overheat Loop · damagedAT CRUISE ALTITUDE, RECEIVED MLG BAY OVERHEAT FAIL CAUTION MESSAGE INTERMITTENTLY. FOLLOWED BY MLG BAY OVERHEAT WARNING MESSAGE WITH TRIPLE CHIME. C/W QRH, BTMS 1-1-1-1. REMOVED AND REPLACED RT WHEEL WELL LOOP IAW AMM 26-14-00. OPS CHECK GOOD. (K)SDR NSVA2009037SSensor · malfunctionedLEFT BLEED AIR LEAK LIGHT ILLUMINATED, CREW RAN CHECKLIST. PRECAUTIONARY LEFT ENGINE SHUT DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. FERRIED TO ALB FOR MAINTENANCE. REMOVED AND REPLACED LT BLEED AIR SENSOR LOOP. OPS CHECK GOOD.SDR ASAA0956287Overheat Sensor · out of limitsAPU DET INOP LIGHT IS ILLUMINATED. FAULT VERIFIED. ACCOMP FIM:26 10/801 FIRE DET BITE. FOUND APU FAN UPPER FAULT PER FIM RANG OUT ALL 3 DET LOOPS AND FOUND LOOP M1925 TAILPIPE OUT OF LIMITS. REPLACED APU TAILPIPE OVERHEAT DET ASSY REF MM 26 15 01, OPS CHECSDR ASAA0956266Overheat Sensor · faultyAPU DET INOP ILLUMINATED ON FINAL. ACCOMPLISHED QRH APU WAS NOT RUNNING. VERIFIED FAULT STILL CURRENT. VERIFIED P/N WITH SEAMC. REPLACED TAILPIPE OVERHEAT DETECTOR ASSEMBLY WITH SERVICEABLE ONE. ACCOMP INST, TEST PASS REF M/M 26 15 01 400 802.SDR CA090723003Element · damaged(CAN) FLT CREW REPORTED AN ANTI ICE DUCT FAIL MSG ON EICAS ALONG WITH ANTI-ICE DUCT FAIL SWITCH LIGHT. THE SYNOPTIC PAGE ON EICAS SHOWS LT FUSELAGE DUCT IN RED. ACFT WAS NEVER IN ICING CONDITIONS AND RETURNED TO AND LANDED WITHOUT FURTHER INCIDENT. MX FOUND SDR CHQA200900156Element · intermittentFLIGHT 5516, IAH TO ATL. THE FLIGHT CREW REPORTED AN ANTI-ICE DUCT FAIL MESSAGE ON EICAS, WITH WING ANTI-ICE DUCT FAIL ILLUMINATED ON THE PUSH BUTTON. THE SYNOPTIC PAGE ON EICAS SHOWS THE LEFT-HAND FUSELAGE DUCT IN RED. THE AIRCRAFT WAS NEVER IN ICING CONDISDR DXTA2009071303728Overheat Sensor · intermittentREAR BAY OVERHEAT ANNUNCIATOR ILLUMINATED IN FLIGHT SHORTLY AFTER TAKEOFF AT ABOUT 15000 FT ALTITUDE. LIGHT CAME ON TWICE FOR .5 MINUTE TOTAL, THEN STAYED OFF. NO SECONDARY INDICATIONS. PREFORMED EMERGENCY LANDING. REMOVED AND REPLACED THE REAR BAY OVERHEASDR PCSA2009051801Sensor · out of positionNR1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN NR1 ENGINE AND RETURNED TO DEPARTURE. WINDMILLING 15 MINUTES, OIL PRESSURE WITHIN LIMITS. MX FOUND NR 1 STRUT SENSING ELEMENT OUT OF POSITION. THE ELEMENT WAS REPOSITIONED AND A PNEUMATIC LEAK CHECK WAS SDR SWIA200921569Sensor · failedFLT 6733 - "R BLEED DUCT" WARNING MESSAGE. REPLACED BOTH BLEED AIR TEMP SENSORS.SDR IPXA09M55740Overheat Loop · faultyATB - CREW CALLED DISPATCH WITH AN AVIONICS FAN FLOW INDICATION POSSIBLE OVERHEAT. RETURNED TO HNL. LANDED WITHOUT INCIDENT. DEFERRED MANIFOLD FAIL DET LOOP. FOUND D1-117 2.9 MEGA OHMS RO GND AND C5-13420 M OHMS TO GND. REPLACED D1-117 PER MM 36-23-07. RSDR AALA2009042200001Switch · faultedDFW TAIL COMPARTMENT OVERHEAT LIGHT ILLUMINATED. EMERGENCY DECLARED RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND SWITCH FAULTED. REPLACED LEFT AND RIGHT HAND SWITCH IN AFT TAIL CONE AREA. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSSDR AALA2009042100002Valve · leakingPSP - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED, RETURNED TO PSP WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TEMPERATURE SENSOR PNEUMATIC GROUND CONNECTION VALVE.SDR AALA2009040300001Detector · faultyWING TO BODY OVERHEAT LIGHT ILLUMINATED. EMERGENCY DECLARED RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FAULTY DETECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.SDR NSVA2009017Detector · malfunctionedLEFT TAIL PIPE HOT LIGHT CAME ON IN FLIGHT, WENT OFF AFTER 3-5 MINUTES. ENGINE WAS NOT SHUT DOWN. REMOVED AND REPLACED LT TAIL PIPE ASSY WITH ALL 3 SPOT DETECTORS ON/OFF P/N:7071125-507, ALL 3 SPOT DETECTORS TSO: 183FH, IAW AMM 54-30-05-02. OPS CHECKS GOOD.SDR DL777090644Pump · looseDURING NR 1 ENG RUN FOUND HYD PUMP BACKING OUT AT THE 2 O`CLOCK POSITION. REMOVED HYD PUMP FOR ACCESS TO DAMAGED STUD. REMOVED AND REPLACED NR 1 ENG PER TRANSMITTAL 11T003.SDR IPXA09655124Circuit Card · damagedINSPECTION TYPE:ETOP ATB - WHILE CLIMBING OUT, CREW RECEIVED RIGHT BLEED DUCT EICAS MESSAGE. NO EMERGENCY WAS DECLARED. ACFT OOS T/S IN PROGRESS. REMOVED AND REPLACED DETECTOR CARD PER AMM 26-10-01-4. T/S RT BLEED DUCT LEAK CAUTION EICAS MESSAGE. FOUND ELSDR A6WA200940139Overheat Loop · malfunctioned188294/3 - RT 14TH DUCT WARNING MESSAGE ON TAKEOFF. ABORTED AT 80 KNOTS, BRAKE TEMPS 4, 4, 1, 2. REMOVED AND REPLACED PYLON 14TH STAGE BLEED LOOP. OPS CHECK GOOD. (K)SDR A6WA200940123Element · malfunctioned14TH DUCT O/H, C/W QRH RED LENG TO IDLET MSG WENT AWAY AND REAPPEARED 5 MINUTES LATER. LANDING WEIGHT 49,000, BTMS 6-5-5-6. REMOVED AND REPLACED LT PYLON 14TH STAGE LENS ELEMENT A59WK IAW AMM 36-21-04. OPS AND LEAK CHECK NORMAL. (K)SDR IPXA09154957Detector · inoperativeINSPECTION TYPE:N/A ON CLIMBOUT JUST AFTER AUTO PILOT FAILED GREEN HYD OVHT LITE RAN CHECKLIST, RETURNED TO FSD, MANUALLY EXTENDED GEAR PER CHECKLIST REMOVED AND REPLACED HYD OVERHEAT DETECTOR UNIT IAW AMM 29-33-12-04 AN D TSM 29-33-00 OPS CHECK OK.SDR A6WA200940114Sensor · malfunctionedDLY RT 14TH STAGE DUCT OVERHEAT ILLUMINATED AFTER T/O, CW QRH WARNING PERSISTED WITH RT 14TH STAGE TURNED OFF. REMOVED AND REPLACED BLEED AIR SENSING LOOP A40WK IN RT WHEELWELL OPS CHECK GOOD AT THIS TIME IAW AMM 36-21-00. (K)
SDR MALA090027Seal · leakingON TAKEOFF TAILPIPE HOT ILLUMINATED ON CWP. RESEALED TAILPIPE HOT SENSOR PER JC NR 2610-301. OPS CHECK GOOD. ACFT GOOD TO RETURN TO SERVICE. RT TAILPIPE HOT SENSOR.SDR IPXA09654817Circuit Card · not seatedINSPECTION TYPE:ETOP ATB - RIGHT BLEED SYSTEM DUCT LEAK. A/C IS CURRENTLY OOS. CHECK CARRIED OUT PER TASK PER FIM 26-18-00 AND FOLLOWED WDM 26-18-21. NOTICED CARD M691 NOT SEATED PROPERLY. SAME RESEATED C/W TASK 26-18-00 TEST PASSED. PERFORMED ENGINE RUN SDR AALA2009021201021Overheat Loop · brokenMIA - RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED ON DEPARTURE. EMERGENCY DECLARED AND FLIGHT RETURNED TO MIA WITHOUT INCIDENT. REPLACED LOOPS M371 AND M269 ON RIGHT WING. SYSTEM GROUND CHECK NORMAL OPERATION.SDR UPS09M54651Overheat Sensor · shortedRECEIVED LEVEL 1 ALERT - NR 2 ANTI-ICE DUCT. UNABLE TO CONTINUE TO MSP DUE TO ICING CONDITIONS. FOUND THE DI90 NR 4 DUCT OVERHEAT SENSOR SHORTER TO GROUND. REPOSITIONED OVERHEAT SENSOR. NO DUCT LEAKS NOTED. SYSTEM CHECKS NORMAL PER FIM 30-22-00-1 AWR COMPLISDR CHQA200900028Element · false indicationFLIGHT 5584, IAH TO MOB - ON CLIMB OUT OF IAH THE FLIGHT CREW RECEIVED A LEFT 14TH STAGE DUCT LEAK WARNING. THE QRH WAS FOLLOWED AND THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE 14TH STAGE DUCTING AND FOUND THE HEAT SHISDR AALA2009010600150Detector · malfunctionedMIA INFLIGHT - CREW REPORTED RIGHT WING TO BODY OVERHEAT INDICATION. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED RIGHT WING BODY OVERHEAT DETECTOR CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR COMA2008122750048Overheat Loop · out of positionEN ROUTE PHL-BOS RECEIVED A RIGHT 14TH STAGE DUCT MESSAGE, FLIGHT RETURNED TO PHL. REPOSITIONED THE RIGHT PYLON HEAT DETECTION LOOP.
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