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.

SDR SIMA200211603Detector · faultyDFW - FLT 3580 - CREW REPORTED THE RIGHT ENGINE TAIL PIPE HOT LIGHT ILLUMINATED. EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED ALL THREE DETECTORS IN THE RIGHT TAIL PIPE IAW SAAB MM. MAINTENANCE ALApr 26, 2002 · N400BR · Saab 340BSDR RAIA00204130Sensor · chafed5639-STL - RIGHT OVERHEAT WARNING CAME ON DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVER HEAT SENSOR WIRE.Apr 19, 2002 · N567HK · Jetair JETSTM4101SDR 02FDEA00269Detector · malfunctionedLWR AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLT. REMOVED AND REPLACED FIRE DETECTION PER MM 20-10-017-2.Apr 18, 2002 · N208FE · Boeing 7272S2FSDR DHL2002363003Control Unit1. MANIFOLD FAULT DETECT LOOPS RH SELECT B TEST FAILS. 2. DEFERRED PER MEL 36-12-03. CONTROL #9034 ASSIGNED. 3. REPLACED #2 OVERHEAT DETECTION CONTROL UNIT IAW M/M 26-16-11. OPS CK GOOD. THIS CLEARS DMI 9034.Apr 16, 2002 · N363DH · Airbus A300B4203SDR CX7A194J4Warning System · false activationON TAKEOFF ROLL TAIL PIPE HOT LIGHT ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OUT WHEN A/C RETURNED TO THE GATE.Apr 8, 2002 · N305CE · Saab 340BSDR CX7A194J2Warning System · false activationON TAKEOFF ROLL TAIL PIPE HOT LIGHT ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OFF WHEN A/C RETURNED TO THE GATE.Apr 8, 2002 · N311CE · Saab 340BSDR RAIA00203111Overheat Loop · shorted5529-STL- LEFT OVERHEAT LOOP LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE FIRE WIRE UNDER THE TAIL PIPE, OPS CK OK.Mar 29, 2002 · N573HK · Jetair JETSTM4101SDR CX7A194JWarning Light · false indicationRT TAIL PIPE HOT LIGHT ON T/O. NO TAIL WIND, ABORTED, REDUCED POWER, LIGHT WENT OUT. RAIN AND MOISTURE PREVAILED IN THE AREA.Feb 19, 2002 · N303CE · Saab 340BSDR 02FDEA00099Shim · broken02-46 #1 ENG STRUT OVERHEAT LIGHT ILLUM ON CLBOUT. R&R SHIM ON STARTER DUCT. OPS CK GOOD.Feb 13, 2002 · N481FE · Boeing 727227SDR 2002F01110Warning System · activatedTAIL PIPE HOT CAME ON AFTER TAKEOFF. TAIL PIPE HOT SENSOR AIR RETURN. (M)Feb 2, 2002 · N308CE · Saab 340BSDR 2002F01111Warning System · activatedTAIL PIPE HOT CAME ON AFTER TAKEOFF, AIR RETURN. TAIL PIPE HOT SENSOR. (M)Jan 31, 2002 · N311CE · Saab 340BSDR 2002F01112Warning Light · illuminatedON TAKEOFF ROLL AS TORQUE WAS PASSING 60 DEGREES AND TAIL PIPE HOT LIGHT ILLUMINATED. ABORTED TAKEOFF LIGHT EXTINGUISHED ABOUT 1 MINUTE LATER. (M)Jan 30, 2002 · N303CE · Saab 340BSDR SWIA200210612Warning System · malfunctionedABORTED TAKEOFF DUE TO WING OVERHEAT MSG. ACCOMPLISHED HIGH POWER ENG RUN WITH CREW ASSISTANCE. COULD NOT DUPLICATE. SYSTEM OPS CHECKS GOOD.Jan 30, 2002 · N594SW · Cndair CL6002B19SDR QXEA0200081Thermocouple · faultyBOI-RECEIVED A GEAR BAY OVERHEAT WARNING WHILE AT 25,000 FEET. NR 3 BRAKE TEMP INDICATED HOT. FOLLOWED EMERGENCY PROCEDURES AND DESCENDED TO 21,000 FEET. WARNING WENT AWAY AND REOCCURRED 10 MINUTES LATER. REPEATED EMERGENCY PROCEDURES AND LEFT LANDING GEARJan 28, 2002 · N604QX · Cndair CL6002C10SDR CA020215006Element · failed(CAN) LEFT 14TH DUCT WARNING ON AT TAKEOFF ROLL ABOVE V, ON EICAS, RED BY ENGINE. AIRCRAFT RETURNED TO TORONTO. RIGHT BLEED LEAK DETECTION CONTROL UNIT AND LOOP SENSING ELEMENT (A58WK) REPLACED.OPERATIONAL TEST OF 14TH STAGE BLEED PERFORMED AND OPERATION TEST Jan 16, 2002 · Cndair CL6002B19SDR DL73K020047Warning System · malfunctionedLEFT WING BODY OVERHEAT LIGHT ON IN FLT. DIVERTED TO MCO. REPAIRING OVERHEAT SYSTEM. TRIED CONTROLLER AND OVERHEAD PANEL, NO HELP. RE-INSTALLED ORIGINAL. INSPECTED FOR LEAKS, NONE FOUND. INSPECTED LOOPS FROM NR 1 ENGINE TO AC PACK BAY CONNECTORS. CHECKEJan 13, 2002 · N311DL · Boeing 737232SDR ASOA02020Element · malfunctionedFLT 4579 - DURING CLIMB-OUT OF TOL, THE LEFT 14TH DUCT LIGHT ILLUMINATED ALONG WITH AN ASSOCIATED AURAL BLEED AIR DUCT MESSAGE. THESE WARNINGS LASTED 1-2 SECONDS AND THEN WENT AWAY BUT CONTINUED TO INTERMITTENTLY REAPPEAR. AFTER THE PILOT HAD TRIED TO RETARDJan 13, 2002 · N871AS · Cndair CL6002B19SDR COMA0260046Element · malfunctionedFLIGHT 5991 L/H 14TH STAGE BLEED DUCT WARNING.REPLACED THE L/H PYLON LEAK DETECTOR ELEMENT.Jan 13, 2002 · N918CA · Cndair CL6002B19SDR SWIA200210519Sensor · malfunctionedDUCT FAIL LIGHT AND MESSAGE RIGHT SIDE WITH WING ANTI-ICE ON. REMOVED ALL RIGHT LEADING EDGES AND INSPECTED PICCOLO TUBES FOR CRACKS, NONE NOTED. REMOVED AND REPLACED RIGHT WING DUCT LEAK SENSORS IAW 30-11-41. COMPLIED WITH OPS CHECK OF WING ANTI-ICE SYSTEMJan 5, 2002 · N590SW · Cndair CL6002B19SDR SWIA200110487Wire · groundedAFTER TAKEOFF OUT OF SLC, RECEIVED WING OVERHEAT MESSAGE. DID QRH PROCEDURE, MESSAGE WENT OUT. THEN A FEW MINUTES LATER RECEIVED ANTI-ICE DUCT MESSAGE. DID QRH PROCEDURE. ANTI-ICE DUCT MESSAGE CONTINUED THEN WENT OUT AFTER SEVERAL MINUTES. FOUND A GROUNDEDec 30, 2001 · N426SW · Cndair CL6002B19SDR 2002F00041Switch · damagedMIA - FLT 473 - BOTH WING BODY OVERHEAT LIGHTS ILLUMINATES DURING TAKEOFF AND REMAIN ILLUMINATED DURING FLIGHT. DURING TROUBLESHOOTING FOUND TEST SWITCH DAMAGE, ENTERED IN DEFERRED ITEM. PERFORMED OPERATIONAL TEST, SYSTEM WORKS NORMAL ON BOTH SENSORS. REPLADec 19, 2001 · N235TA · Boeing 737205SDR 2002F00033Switch · damagedMIA - FLT 473 - BOTH WING BODY OVERHEAT LIGHT ILLUMINATES DURING TAKEOFF AND REMAINS ILLUMINATED DURING FLIGHT. DURING TROUBLESHOOTING FOUND TEST SWITCH DAMAGED, ENTERED IN DEFERRED ITEM. PERFORMED OPERATIONAL TEST. SYSTEM WORKS NORMAL ON BOTH SENSORS. (M)Dec 19, 2001 · N235TA · Boeing 737205SDR CA020131010Switch · failed(CAN) DURING APPROACH TO BASE AT 2,500 THE NR 1 ENGINE INDICATED A FIRE CONDITION. ONCE ENGINE SECURED, (PER IAC) T-HANDLE INDICATION EXTINGUISHED. CONTINUED WITH CHECK LIST (DID NOT FIRE BOTTLES), FIRE INDICATION REAPPEARED (T-HANDLE LIGHT & BELL). FIRED BOTHDec 5, 2001 · Dhav DHC8*SDR 01FDEA01024Loop · faulty1-385 DUR CLB LWR AFT BODY OVERHEAT LIGHT CAME ON. REPOSITIONED LOOP IN LEFT SIDE OF CENTRAL STAIRS PER MM 26-14-001-2.Dec 4, 2001 · N270FE · Boeing 727233SDR 01FDEA01012Overheat Loop · out of positionDURING CLIMBOUT NR 1 ENG STRUT OVERHEAT LIGHT ILLUM. NO LEAKS FOUND WITH ENG. REPOSITIONED OVERHEAT LOOP.Nov 28, 2001 · N492FE · Boeing 727227SDR SWIA200110380Warning System · malfunctionedON TAKEOFF PRIOR TO V1 RECEIVED A WING OVERHEAT MESSAGE AND ABORTED THE TAKEOFF. MESSAGE DISAPPEARED WITH THE POWER REDUCTION. PERFORMED AN OPERATIONAL TEST OF THE WING ANTI-ICE SYSTEM. OPS CHECK GOOD AT HIGH AND LOWER POWER SETTINGS IAW CRJ MM 30-12-00.Nov 25, 2001 · N416SW · Cndair CL6002B19SDR 2002FA0000113Overheat Loop · failedDURING A 5 YEAR FUNCTIONAL TEST OF THE REAR EQUIPMENT BAY OVERHEAT DETECT SYSTEM, THE FUNCTIONAL TEST FAILED. FOUND FUSE F36(3AMP) ON THE ZK PANEL BLOWN. THE FLIGHT CREW HAS NO WAY OF KNOWING THEIR OVERHEAT DETECT SYSTEM IS INOP, BECAUSE THE COCKPIT TEST CIRCUNov 8, 2001 · N12F · Braero BAE125800ASDR 01FDEA00951Clamp · loose01-357 #1 ENG STRUT OVERHEAT ILLUM IN GLT. TIGHTENED CLAMP ON HIGH PRESS MODULATING VALVE (SHUTOFF).Nov 1, 2001 · N151FE · Boeing 72722SDR 01FDEA00910Warning Light · illuminatedON CLIMB NR 1 ENG STRUT OVERHEAT LIGHT ILLUM. REMOVED AND REPLACED HIGH PRESSURE SUPPLY LINE PER MAINT PRACTICE.Oct 24, 2001 · N213FE · Boeing 7272S2FSDR SCNA01712Overheat Loop · defectiveLOWER AFT BODY OVERHEAT LIGHT WILL NOT ILLUMINATE WHEN TEST BUTTON IS PUSHED, WILL ILLUMINATE IF LIGHT IS PUSHED DIRECTLY. CORRECTED BY REMOVING AND REPLACING OVERHEAT DETECTOR.Sep 22, 2001 · N281SC · Boeing 727282SDR LR7A01078Wire · corrodedDURING DESCENT INTO OKO NR. 4 ENGINE NACELLE OVERHEAT LIGHT ILLUMINATED. NR. 4 ENGINE SHUTDOWN IAW ENGINE SHUTDOWN PROCEDURES (QRH), FIRE EXTINGUISHER DISCHARGED. REPLACED 3 EA. OVERHEAT DETECTORS IAW SMP 581 26-10 PG 206 PARA. 3. (PRECAUTIONARY). FOUND OVESep 15, 2001 · N405LC · Lkheed 382GSDR 01FDEA00815Connector · dirtyON DEPARTURE NR 3 STRUT O/H LIGHT CAME ON. REMOVED, CLEANED NR 3 ENG LOOP CONNECTOR PER MM REF ATA 20. RESECURED STRUT PANELS.Sep 8, 2001 · N497FE · Boeing 727232SDR 01FDEA00802Warning Light · illuminated01-300 LWR AFT BODY HEAT LIGHT CAME ON. CK DUCTS IN AIR CONDITION COMP & AFT AIRSTAIR AREA. NO DEFECTS NOTED. OPS CK PER MM 26-14-00-1.Sep 6, 2001 · N287FE · Boeing 7272D4SDR 01FDEA00794Warning Light · illuminatedUSING NR 2 ENG RT BLEED TO PROVIDE AIR TO RT PACK, LWR AFT BODY OVERHEAD LIGHT ILLUM. RED TABS FOLLOWED.Aug 31, 2001 · N466FE · Boeing 727225SDR RAIA00108025Detector · failed5402-EWR-RIGHT OVERHEAT CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED RIGHT OVERHEAT DETECTION CONTROL UNIT.Aug 26, 2001 · N559HK · Jetair JETSTM4101SDR 01FDEA00763Warning Light · malfunctionedON CLIMBOUT LWR AFT BODY OVERHEAT LIGHT ILLUM'D BET 180 & 200 ACCOMP RED TAB PROCED & THE LIGHT CK'D GOOD ON TEST & CONTINUED FLT ON NR 1 BLEED & PACK. RED TABS SAID LEAK IS BET NR 3 BLEED VALVE & NR 2 PACK VALVE. RAN ENGS AND CND CK'D ALL LOOPS IN AFT AIRSTAug 22, 2001 · N270FE · Boeing 727233SDR 2001UALA01748Sensing Element · faultyUNSCHEDULED LANDING DUE TO WING BODY OVERHEAT INDICATION. MAINTENANCE REPLACED AFT LOOP (SECTION 58) DETECTOR. ALSO REPLACED BOTH LOAD CONTROL VALVE CLAMPS. PERFORMED LEAK TEST FROM APU TO AFT PRESSURE BULKHEAD. NO LEAK WAS DETECTED. WING BODY OVERHEAT DETAug 18, 2001 · N364UA · Boeing 737322SDR C1HA200193016Clamp · looseUpon initial power reduction #1 eng strut overheat illuminated all eng parameters normal during running pocedure the light went out was on for about 1 min. never reilluminated during decent approach &final.ACTION TAKEN:inspected #1 engine strut area found clamAug 17, 2001 · N293AS · Boeing 727212SDR COMA0160599ValveDURING CLIMB OUT OF CVG RECEIVED A LEFT JET PIPE OVERHEAT CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD, AIRCRAFT LANDED SAFELY.REPOSITIONED AND TIGHTENED CLAMPS FOR THE LEFT 14TH STAGE SHUT FOF VALVE AND CHECK VALVE.Aug 16, 2001 · N962CA · Cndair CL6002B19SDR GAIA01295OPWarning System · malfunctionedFLT 202 - SEA-GEG - DURING CRUISE, THE NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. THE CREW ACCOMPLISHED ABNORMAL PROCEDURES AND THE LIGHT EXTINGUISHED. AIRCRAFT MADE AN UNEVENTFUL LANDING IN GEG. INSPECTED AIR DUCTS FOR LEAKS IN PYLON AREA. NO LEAKS WERAug 10, 2001 · N6809 · Boeing 727223SDR MALA010644Warning System · malfunctionedON FLIGHT 3219 OUT OF SUX, LEFT TAILPIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF. MEMORY ITEMS COMPLETED. QRH'D AND LIGHT WENT OUT ON RETURN TO SUX. AIR TURNBACK TO SUX. MAINTENANCE INSPECTED LT AFT TAILPIPE ASSEMBLY. NO DEFECT NOTED. CLEANED AND REST CANNONAug 9, 2001 · N451XJ · Saab 340BSDR BLI2001F00000Sensor · failedAIR DUCT OVERHEAT ANNUNCIATOR ON IN FLIGHT. AIRCRAFT LANDED, DUCT SENSOR REPLACED BY REPAIR STATION. SYSTEM OPS CHECKED GOOD. RETURNED TO SERVICE.Aug 8, 2001 · N58TC · Cessna 500CESSNASDR BLIA512C8801Sensor · inoperativeIN FLIGHT: DUCT OVER-TEMP ANNUNCIATOR ON. FOLLOWED FLT MANUAL PROCEDURES. CALLED MAINTENANCE. ARRANGED FOR SENSOR TO BE REPLACED. CABIN TEMPERATURE SYSTEM OPS CHECKED GOOD.Aug 8, 2001 · N58TC · Cessna 500CESSNASDR 01FDEA00669Control Unit · faulty01-268 DUR FLT WITH ENG ANTI-ICE OPEN LWR AFT BODY O/H LIGHT ILLUM. R&R FIRE DET O/H DETECTOR PER MM 20-10-017-2. TEST GOOD.Aug 8, 2001 · N461FE · Boeing 727225SDR DHL2001362027Harness · faultyMANIFOLD FAULT DETECT LOOPS ON LT SELECT WONT TEST ON BOTH. DEFERRED LT LOOP "A" IAW MEL 36-12-03."B" TESTS OK. REPLACED WIRE HARNESS 81HF IN AIRCONDITIONING COMPARTMENT FOR 'A' LOOP MAINFOLD FAULT DETECTION OPS CKS GOOD PER MM 26-16-00.Aug 7, 2001 · N362DH · Airbus A300B4203SDR C1HA200193014Overheat Loop · out of positionNR 1 STRUT OVERHEAT AT FL330, REDUCED PWR TO 80 PERCENT LIGHT WENT OUT. REPOSTIONED LOOP FOR STRUT OVERHEAT PER MM 36-22-1, OPS CHECKED GOOD.Aug 5, 2001 · N293AS · Boeing 727212SDR C1HA200193013Clamp · looseAT FL330 eng #1 strut overheat lite on followed COM pulled pwr back to 85% N1 on descent and lite went out at FL 290.ACTION TAKEN:Removed lwr pylon panels found pre-cooler clamps loose tightened leak checked and no leaks noted reinstalled panels OK for serviceAug 5, 2001 · N293AS · Boeing 727212SDR DHL2001726003Overheat Loop · faultyLOWER AFT BODY LIGHT ILLUMINATED DURING CLIMB AT 15000 FT. PERFORMED ABNORMAL PROCEDURE. UPON REDUCING THRUST ON NR 1 ENGINE, LIGHT EXTINGUISHED. RETURNED TO CVG. R&R OVERHEAT DETECTION SENSING ELEMENT WITH SERVICEABLE UNIT IAW B MM 26-14-1.Aug 5, 2001 · N726DH · Boeing 727228SDR 01FDEA00635Connector01-258 DUR CRUISE LWR AFT BODY O/H LIGHT ILLUM. R&R CONNECTOR D1304 OF R/H STAIRWELL ELEMENT M365 PER IAW 727-2 MM CH 20 SYS.Aug 2, 2001 · N461FE · Boeing 727225SDR 01FDEA00596Overheat Loop · malfunctionedLWR AFT BODY O/H LIGHT ISOLATED LEAK BETWEEN BLD VLV AND PACK VLV. REMOVED AND REPLACED FIRE DETECTOR PER MM 26-14-000-5. OPS CHECK GOOD ON GROUND.Jul 24, 2001 · N257FE · Boeing 727233
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