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 01FDEA00028Warning Light · illuminatedNR 1 ENG STRUT OVERHEAT LIGHT CAME ON SHORTLY AFT ENG ANTI-ICE OPEN. COMPLIED WITH TROUBLESHOOTING PROC ON PAGE 2-7-10 OF CFM. LIGHT WENT OUT. FOUND HEAT EXCHANGER CRACKED. *S/D* REMOVED AND REPLACED NR 1 BLEED AIR HEAT EXCHANGER PER MM 36-11-051-4 FROM SSDR COMA0160102Element · malfunctionedRT 14TH STAGE BLEED AIR LEAK WARNING. REPLACED THE PYLON LEAK SENSE ELEMENT.SDR 01FDEA00015Detector · activated01-004 AT 5000 FT ON CLB OUT NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON. NO IRREGULARITIES NOTED. CLEANED OVERHEAT DETECTION ELEMENT. RAN NR 3 ENGINE IAW JET RUN HANDBOOK, NO LEAKS NOTED. OK FOR SERVICE.SDR MASA01007Sensing Element · intermittentFTL - 5822 - LGA-IAD - DIVERTED TO PHL DUE TO 14TH STAGE OVERHEAT MESSAGE ON EICAS. THE CAPTAIN RETARDED THE RIGHT POWER LEVER AND AFTER 3-5 MINUTES THE MESSAGE CLEARED AND FLICKERED ON AND OFF INTERMITTENTLY. AFTER LANDING IN PHL MAINTENANCE WAS CALLED. MASDR 20010212SG006Warning Light · illuminatedFLT 1325 - BWD - DURING CLIMB-OUT, THE RIGHT WING OVERHEAT LIGHT CAME ON. THE LIGHT WENT OUT WHEN LANDING GEAR WAS EXTENDED FOLLOWING THE EMERGENCY CHECKLIST. CREW RETURNED TO STATION. NO APPARENT MECHANICAL CAUSE. THIS TEMP SENSOR IS LOCATED IN THE WHEEL SDR COMA0160027Element · out of positionRIGHT HAND 14TH STAGE BLEED DUCT MESSAGE. REPOSITIONED LEAK SENSING ELEMENT.SDR COMA0160003Control Unit · malfunctionedLEFT HAND 10TH STAGE BLEED AIR DUCT LEAK MESSAGE.REPLACED THE BLEED LEAK CONTROL UNIT.SDR DL733002507Overheat Loop · wornAIR RETURN FOR LT WING BODY OVERHEAT HISTORY - REPLACED OVERHEAT DETECTION LOOPSDR DHL2000708027Sensor · damagedAFTER T/O NR 3 ENG STRUT OVERHEAT LIGHT ILLUMINATED,ABNORMAL PROCEDURES COMPLIED WITH. PLACED NR 3 ENGINE MODULATING VALVE ON DEFERRAL PER DHL MEL 36-11, DMI 3633.THIS SDR IS STILL OPEN. REMOVED AND REPLACED NR 3 ENGINE MOD VALVE SENSE LINE PER M/M 36-12-4SDR COMA061082Fire Loop · out of positionDURING CLIMB OUT OF CVG, RECEIVED LEFT JET PIPE OVERHEAT FAIL CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD. READJUSTED HARDWARE ON JET PIPE SENSING ELEMENTS LOOP "A" AND LOOP "B".SDR COMA0061064Element · malfunctionedRT 14TH STAGE DUCT MESSAGE. REPLACED THE PYLON LEAK SENSING ELEMENT.SDR SIMA3493Sensor · malfunctionedLGA - FLT 4555 - DURING CLIMB-OUT, CREW NOTED NR 2 BRAKE OVERHEAT INDICATION WAS FLUCTUATING AND AT ONE POINT POINTER ON INDICATOR DISAPPEARED. CREW RETURNED TO LGA. AN EMERGENCY LANDING WAS DECLARED. AIRCRAFT LANDED SAFELY. NO FURTHER INCIDENTS WERE REPORSDR 00FDEA00879Line · failed00-360 REPEAT WRITE-UP, AFT TO BOTH ENGINE AND WING A/I OFF THE NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON. SUSPECT AIR LEAK IN STUB WING. ** S/D ** R&R BUSTED BRAIDED LINE. LEAK CK GOOD USING APU AIR MM STANDARD PRACTICES. OK FOR SERVICE.SDR 00FDEA00877Control Unit · faulty00-358 AFT T/O, NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON. RED TAB ACCOMPLISHED. R&R CONTROL UNIT PER IAW MM 26-14-0. NO FAULTS NOTED.SDR 00FDEA00859Connector · faulty00-341 LWR AFT BODY OVERHEAT LIGHT, NR 2 & 1 ENGINE BLEED CLOSED. ** S/D ** R&R WIRE, CONNECTOR PER WIRING PRACTICE MANUAL 20-62-14. OPS CK OK.SDR 2000UALA00768Warning System · activatedAFT BODY OVERHEAT INDICATION FOLLOWED BY AN ABNORMAL ODOR IN THE COCKPIT. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED ENGINE RUN-UP ON BOTH ENGINES, AND PERFORMED PNEUMATIC SYSTEM TEST. NO BURNING SMELL AND NO AFT BODY OVERHEAT LIGHT ILLUMINATED.SDR 20010206SG004Warning Light · illuminatedHOB - FLT 1331 - LEFT WING OVERHEAT LIGHT CAME STEADY ON DURING CRUISE. CREW FOLLOWED CHECKLIST PROCEDURES, EXTENDED GEAR AND TURNED OFF LEFT BLEED. LIGHT WENT OUT AFTER ONE MINUTE. CREW RETURNED TO STATION WITH NO FURTHER PROBLEMS. NO APPARENT MECHANICAL SDR 00FDEA00788Detector · out of positionLOWER AFT BODY HEAT LIGHT CAME ON. REPOSITIONED AFT BODY OVERHEAT ELEMENT REF 26-14-001-2, 26-14-000-5, 30-13-000-5.SDR CA001129018Element · failed(CAN) A LEFT 14TH DUCT WARNING INDICATION WITH THE BLEED AIR DUCT AURAL WARNING WAS OBSERVED TRANSIENTLY AT FL210, THIS THEN CLEARED AND REAPPEARED AT FL290 AND STAYED ON. LEFT HAND ENGINE WAS SHUTDOWN AND AIRCRAFT LANDED UNEVENTFULLY. THE LEFT 14TH STAGE HEATSDR UPS00434469Warning System · illuminatedINSPECTION TYPE: ATB, RT WING OVERHEAT LIGHT ILLUM. REPAIRED WIRING.SDR UPS00434447Warning Light · illuminatedINSPECTION TYPE:C, RT WING OVERHEAT LIGHT ILLUMINATED.SDR SWAA002341Detector · looseAIR TURNBACK, IN FLIGHT ENGINE SHUT DOWN. DURING FLIGHT, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. PULLED FIRE HANDLE. DID NOT FIRE BOTTLES. FOUND NR 2 ENG FIRE DETECTION UPPER LOOP LOOSE AT BRACKET. SECURED LOOP PER MM.SDR CA001129014Element · failed(CAN) DURING CLIMB AT FL160 RT 14 STAGE DUCT MESSAGE WITH AURAL WARNING WITH ANTI ICE ON. CREW CARRIED OUT QRH PROCEDURE AND TRIED UNSUCCESSFULLY TO RESET THE SYSTEM, MESSAGE CLEARED WHEN RT THRUST LEVER RETARDED. MAINTENANCE ACTION: FOUND 14 STAGE DUCT ELEMENSDR 2000UALA00648Detector · damagedRIGHT WING-BODY OVERHEAT DETECTION SYSTEM INOPERATIVE. *S/D* REPLACED RIGHT HAND PYLON OVERHEAT LOOP M1204. SYSTEM OPERATION CHECKED NORMAL.SDR EISA20000193Clamp · looseNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED AFTER TAKE OFF ACCOMPLISHED CHECKLIST LIGHT WENT OUT AFTER NR 3 BLEED VALVE CLOSED. BEFORE CLOSING NR 3 BLEED VALVE RT. MAN PRESSURE 100PSI. CORRECTIVE ACTION: TIGHTENED CLAMPS ON 13TH STAGE MOD VALVE, OPS CHECK NSDR AU001034Connector · shorted(AUS) TAILPIPE OVERHEAT DETECTOR SHORT CIRCUITING AT CONNECTOR DUE TO CONTAMINATION.SDR SIMA2922Connector · contaminatedBOS - FLT 4914 - RIGHT TAIL PIPE HOT LIGHT ILLUMINATED. CLEANED AND DRIED CANNON PLUGS. OPS CHECK GOOD IAW SAAB AMM. (M)SDR AALA20001725Warning Light · illuminatedDFW - FLT 320 - EN ROUTE DFW-BDL - DURING TAKEOFF ROLL, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ABORTED TAKEOFF AT 140 KNOTS. RAN BOTH ENGINES 80 PERCENT WITH BOTH PACKS. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR 20010202SG007Overheat · illuminatedFLT 2563 - GDV - IN CRUISE BETWEEN STATIONS ON SHORT FLT THE RT WING OVERHEAT LIGHT CAME ON STEADY. THE RT BLEED WAS SHUTOFF AND GEAR WAS EXTENDED PER EMERGENCY PROCEDURES AND THE LIGHT WENT OUT. CREW SELECTED FULL HOT ON THE TEMP CONTROLLER ON ITITIAL CLIMBSDR 00FDEA00719Warning Light · illuminatedLWR AFT BODY OVERHEAT LIGHT CAME ON DURING CR. SWITCHING BLEEDS TO 1 AND 3 EXTINGUISHED. INSP ALL LOOPS DETECTOR, OK. NO FAULT FOUND.SDR 00FDEA00697Detector · failedLWR AFT BODY OVERHEAT LIGHT ILLUM. RED TABS FOLLOWED, LIGHT WENT OUT AFT 1 & 2 BLD TURN OFF WITH LEFT PACK OPERATED ON RT NR 1 PACK MONITORED. *S/D* REPLACED OVERHEAT LOOPS M322 & M365 (AFT AIRSTAIRS SECTION 48) PER BOEING 727 MM 26-14-11. AC GOOD FOR SERVSDR GAIA00625Loop · out of positionDISCREPANCY: DURING CRUISE, THE #3 ENGINE STRUT OVERHEAD LIGHT ILLUMINATED. EXECUTED PROCEDURES IAW KHA AOM VOLUME 1. THE AIRCRAFT CONTINUED TO TOL AND MADE AN UNEVENTFUL LANDING.CORRECTIVE ACTION: MAINTENANCE OPENED THE #3 ENGINE LOWER STRUT PANELS AND INSPECSDR 00FDEA00673Warning Light · illuminatedAT CR LWR AFT BODY HEAT LIGHT ON. *S/D* TIGHTENED CLAMPS VISUALLY INSP ALL DUCTS FOR LEAKS. NONE FOUND. OK FOR SERVICE.SDR 2000UALA00556Loop · damagedRIGHT WING BODY OVERHEAT INDICATION. *S/D* REPLACED RIGHT HAND PYLON OVERHEAT LOOP M1204. SYSTEM OPERATION CHECKED NORMAL.SDR EISA20000148Bolt · looseAFTER TAKEOFF NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL CHECKLIST, RESTABLISHED RIGHT PACK WITH NR 2 BLEED, FLIGHT NORMAL. FOUND WING ANTI-ICE HIGH PRESSURE VALVE COUPLING LOOSE AND LEAKING. TIGHTENED GLAND NUT AND BOLTS. RAN ENGISDR 00FDEA00671Warning System · overheatedLWR AFT BODY OVERHEAT LIGHT ILLUM DURING FLT. RAN CKLIST AND ISOLATED IT TO THE NR 1 ENG BLEED SYS. INSP PNEUMATIC SYS AND CARGO COMPT FOR LEAKS, AFT BODY OVHT SENSING ELEMENT, NO LEAK NOTED. NO FAULT FOUND.SDR COMA0060732Sensor · malfunctionedRIGHT HAND WING OVERHEATER WARNING. REPLACED WING TEMP SENSOR.SDR AALA20001449Sensor · malfunctionedDFW - FLT 1890 - DURING CLIMB-OUT, PASSING THROUGH 2,000 FEET, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY PROCEDURE CHECKLIST COMPLIED WITH AND LIGHT EXTINGUISHED. RETURNED DFW AND LANDED WITHOUT INCIDENT. RAN AIRCRAFT FOR EXTENDED PERIOSDR AALA20001447Clamp · looseDFW - FLT 1890 - DURING CLIMB-OUT, BETWEEN 8000-10,000 FT, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY PROCEDURE CHECKLIST COMPLIED WITH AND LIGHT EXTINGUISHED. RETURNED DFW AND LANDED WITHOUT INCIDENT. RE-TORQUED AUGMENTATION VALVE CLAMPSDR 00FDEA00621Sensing Element · chafedLWR AFT BODY OVERHEAT LIGHT CAME ON, BOTH PACKS ON WITH ENG 2 L + 3 BLEEDS, OPEN, LIGHT WENT OUT WHEN BLEEDS SWITCHED FROM ENG 2 TO ENG 1. INSTALLED SENSING ELEMENT CORRECTLY. CLEANED CONNECTORS. NO DUCT LEAKS. SYSTEM OK FOR SERVICE.SDR AU000720Detector · malfunctioned(AUS) LT AND RT PYLON BLEED LEAK DETECTOR LOOPS FAILED RESISTANCE CHECK. FOUND DURING INSPECTION IAW SB A601R-36-014.SDR 2000UALA00506Control Box · failedRIGHT WING-BODY OVERHEAT DETECTION SYSTEM INOPERATIVE. *S/D* REPLACED COMPARTMENT OVERHEAT CONTROL UNIT, WING-BODY OVERHEAT DETECTION SYSTEM TEST NORMAL.SDR 00FDEA00586Bushing · missingNR 3 ENGINE STRUT LIGHT DIMLY ILLUM. REPLACED BUSHING AND SECURED FIRE LOOP CLAMP. RAN ENG PER JET RUN HDBK. NO FAULTS FOUND. OK FOR SERVICE.SDR 00FDEA00585Detector · malfunctionedNR 3 ENGINE STRUT OVERHEAT FAINTLY ILLUM DURING DESCENT. RAN NR 3 ENG PER JET RUN HANDBOOK CHAP 5, NO DISCREPANCY NOTED. INSP NR 3 ENG STRUT, NO DISCREPANCY NOTED.SDR 00FDEA00582Detector · groundedLWR AFT BODY OVERHEAT LIGHT ILLUM. NR 1 ENG BLEED AND NR 2 ENG BLEED VALVE BOTH OPEN AND ILLUM. RAN NR 1 ENG WITH NR 1 BLEED OPEN, NO AIR LEAKS DETECTED. FOUND AFT BODY DETECTOR LOOP TOUCHING GROUND IN CLOSE PROXIMITY TO NR 1 BLEED DUCT. REPOSITIONED ELEMESDR LR7A00168Wire · chafedFLIGHT CREW REPORTED, DURING CRUISE THE NR 3 TURBINE OVERHEAT LIGHT CAME ON. MASTER FIRE WARNING LIGHT FLICKERING. STARTED RETARDING POWER AND WARNING LIGHTS WENT OFF AT 870°C TIT. CONTINUED ENGINE OPERATION AT THAT POWER SETTING OR LESS. INSPECTED WIRE HASDR 00FDEA00556Detector · faultyON CLIMBOUT, LOWER AFT BODY OVERHEAT LIGHT CAME ON. FOLLOW CKLIST WHEN ENG NR 2 BLD SHUT OFF LIGHT WENT OUT. FOUND CLAMP COMING ADRIFT ON LEFT OVERHEAT LOOP IN AIRSTAIR AREA. ENG RUN CARRIED OUT PER JET RUN HDBK & CK FOR AIR LEAKS. OVERHEAT LIGHTS TEST PERSDR NACA200000018Brake · overheatedON DOWN WIND AT AKN, WHEEL WELL WARNING LIGHT AND BELL SOUNDED. AS SOON AS THE GEAR WENT OUT AS PER PROCEDURES THE BELL AND LIGHT WENT OUT, VISUAL VERIFICATION WITH CONTROL TOWER EVERYTHING LOOKED NORMAL WITH THEM. INSPECTED MAIN GEAR BRAKES FOR LEAKAGE AND SDR GAIA00502Duct · rupturedFLT 838 - MHR-SAN - ON CLIMB-OUT, THE LOWER AFT BODY OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED AND LANDED AT MHR WITHOUT ANY FURTHER DIFFICULTIES. REMOVED AND REPLACED RUPTURED DUCT RUNNING THROUGH THE RIHT GEAR WELL BULKHEAD FORWARD OF APU. OPERATIONALSDR F3LA00189Detector · illuminatedDEN - FLT 522 - AIR RETURN. FLIGHT CREW REPORTED LT WING/BODY OVERHEAT LIGHT ILLUMINATED. AIRCRAFT LANDED OVERWEIGHT. MAINTENANCE PERFORMED WING/BODY OVERHEAT TEST AND FOUND SYSTEM SLOW TO RESPOND. REPLACED COMPARTMENT OVERHEAT MODULE. INSPECTED LT AIR CO
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