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 AALA20001324AWarning Light · illuminatedDFW - FLT 434 - DURING CLIMB THROUGH 17,000 FEET, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. ON TAXI TO GATE SMOKE OBSERVED FROM NR 2 ENGINE. ACCOMPLISHED ENGINE HIGH POWER RUN. NO SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR CA000918010Circuit Board · failed(CAN) REJECTED TAKEOFF AT 80 KNOTS FOR A FIRE/OVERHEAT SYSTEM FAULT. DISPLAYED ON THE (EICAS) ENGINE INDICATION AND CREW ALERT SYSTEM. (CARGO INDICATION) THE A FAULT CARDS WERE SWAPPED, NIL FIX PROBLEM REPEATED. SUSPECT TO BE THE AFT LOGIC TEST CARD. REPLACED SDR AALA20001289Sensor · defectiveDFW - FLT 519 - TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. LIGHT WENT OUT WHEN HP BLEED OFF SELECTED, BUT CAME BACK ON APPROXIMATELY ONE MINUTE LATER AND STAYED ONFOR APPROX 2 MINUTES BEORE EXTINGUISHING FOR REST OF FLIGHT. REPLACED SDR 00FDEA00509Warning Light · illuminatedLWR AFT OVERHEAT WARN LIGHT CAME ON DURING FLT. LIGHT WENT OUT AFT CLOSING LEFT ENGINE 2/APU BLEED SWITCH. RAN ALL 3 ENGINES AT HI POWER FOR 20 MIN, BUT COULD NOT DUPLICATE. REF PER 727 JET RUN HANDBOOK.SDR GAIA00441Detector · out of positionFLT 2731 - LRD-BRO - LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED ON DESCENT INTO BRO. FOLLOWED AOM LOER AFT BODY OVERHEAT PROCEDURES. THE AIRCRAFT MADE AN UNEVENTFUL LANDING IN BRO. REPOSITIONED AFT BODY HEAT WARNING STRIP. OPERATIONALLY CHECKS GOOD. AIRCRAFSDR GAIA00437Module · malfunctionedFLT 2708 - MEM-SLC - DURING CLIMB-OUT, THE LOWER BODY AFT OVER HEAT LIGHT WAS ILLUMINATED. THE AIRCRAFT CONTINUED TO SLC AND MADE A NORMAL ROUTINE LANDING. MAINTENANCE REPLACED THE FIRE AND OVERHEAT DETECTION UNIT. CARRIED OUT ENGINE RUN ON BOTH NR 1 AND NRSDR 00FDEA00460Detector · chafedLWR AFT BODY OVERHEAT CAUTION LIGHT ILLUM WITH NR 2 ENG AND 3 BLDS OPEN AND BOTH PACKS ON. RAN ALL 3 ENG PER JET RUN HDBK FOR 5 MIN, BLDS ON AND NO LEAK FOUND. FOUND LWR AFT LOOP CHAFING. REPOSITION LWR LOOP, OPS CHECK NORMAL PER B727-200 JET RUN HDBK.SDR 00392H.P. Bleed Valve · leakingDISCREPANCY: DURING CRUISE THE #3 STRUT OVERHEAD LIGHT ILLUMINATED. THE CREW COMPLIED WITH THE APPROPRIATE CHECKLISTS, AND LIGHT WENT OUT WHEN #3 ENGINE WAS RETURNED TO IDLE POSITION. A/C CONTINUED TO HSV AND LANDED WITHOUT FURTHER DIFFICULTIES. CORRECTIVE ACTSDR SIMA1972Connector · contaminatedPIT - FLT 5050 - DURING CLIMB, LEFT ENGINE TAIL PIPE HOT LIGHT CAME ON. FOLLOWED AOM PROCEDURES AND SHUTDOWN ENGINE. LIGHT WENT OUT AFTER 3-4 MINUTES. MAINTENANCE FOUND MOISTURE ON CANNON PLUGS, CLEANED AND RESEALED OVERHEAT DETECTOR TERMINAL IAW SAAB MM 26SDR 00FDEA00447Warning Light · false indicationLWR AFT BODY OVERHEAT LIGHT ILLUM. PERFORMED RED TAB PROC. INSP LEFT AFT SECTION DUCTS AND HEAT SENSING ELEMENT FOR SIGNS OF LEAK OR DAMAGE, NONE FOUND. CLEANED HEAT SENSING ELEMENT CONNECTORS. RAN APU AND ENG WITH BOTH PACKS ON LIGHT STAYS OFF. TEST PER SDR 00FDEA00443Warning Light · false indicationNR 1 ENGINE STRUT OVERHEAT LIGHT ILLUM AFT T/O. LIGHT WENT OUT AFT 2 MIN. SYS TEST GOOD. INSPECTED DUCTING AND OVERHEAT LOOP, NO DISCREPANCIES NOTED. TEST GOOD PER MM 26-14-000-5.SDR CA000714008Warning System · failed(CAN) THE FLIGHT CREW REPORTED DURING CRUISE L 14TH DUCT WARNING MESSAGE APPEARED ON EICAS WITH AURAL BLEED AIR DUCT MESSAGE. THE FLIGHT CREW INITIATED LT ENGINE SHUT-DOWN AND LANDED AT THE NEAREST AVAILABLE AIRPORT. TROUBLESHOOTING CARRIED OUT AND NOT ABLE TSDR GAIA00366Fire Loop · out of positionFLT 302 - DFW-TYS - ON CLIMB-OUT, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. ABNORMAL PROCEDURES WERE USED. OVER HEAT LIGHT EXTINGUISHED WHEN NR 3 ENGINE THRUST LEVER WAS RETARDED. RIGHT BLEED TRIP FOLLOWED. USED ABNORMAL PROCEDURES. USED NR 2 ENGINE BLEESDR CA000621017Sensor · failed(CAN) DURING CRUISE FLIGHT THE LT WING OVERHEAT LIGHT ILLUMINATED FOR APPROXIMATELY 1 MINUTE AND REMAINED OFF FOR THE DURATION OF THE FLIGHT.A SUBSEQUENT INSPECTION COULD NOT REVEAL ANY FAULT, ALL ASSOCIATED WIRING WAS THOROUGHLY INSPECTED ALL LT BLED AIR LINESDR 00FDEA00390Detector · chafedON CLIMB, LWR AFT BODY OVERHEAT LIGHT FLASH INTERMITTENT. FOUND AFT BODY DETECTOR LOOP IN AFT AIRSTAIRS CHAFED THROUGH. *S/D* REMOVED AND REPLACED ELEMENT PER B727 MM 26-14-1.SDR COMA0060508Fire Loop · false indicationLANDING GEAR BAY OVERHEAT WARNING. WHEEL BIN FIRE DETECTION LOOP DEFECTIVE. REPLACED WHEEL BIN ASSY.SDR AALA006095Duct · leakingLAS - AT APPROXIMATELY 1000 FT ON TAKEOFF, THE TAIL COMPT TEMP HIGH AND MASTER WARNING LIGHT CAME ON. DELAYED 30 SECONDS TO SEE IF LIGHT WOULD GO OUT AND PULLED POWER BACK TO 1.4 EPR. LIGHT STAYED ON. DECLARED AN EMERGENCY AND MADE IMMEDIATE RETURN TO LAS. SDR 00FDEA00355Warning Light · illuminatedLOWER AFT BODY HEAT LIGHT ILLUM IN FLT. UTILIZED RED TAB PROC. LIGHT REMAINED ILLUM. *S/D* REPLACED CONNECTOR PER 727-200 MM 20-62-14. REMOVED AND REPLACED PANELING PER 727-200 MM 26-14-1. NO FURTHER DEFECTS NOTED. OK FOR SERVICE.SDR CA000530064Sensor · overheated(CAN) ENGINE SHUT DOWN IN FLIGHT DUE TO 14TH STAGE DUCT OVERHEAT MESSAGE. MESSAGE APPEARED, BLEEDS CLOSED WITH NO SUCCESS.MESSAGE STILL APPEARED. EMERG LANDING DECLARED. 14 STAGE LOOP REPLACED.SDR USAABB00066Warning System · activatedPHX - FLT 152 - CLIMBING THROUGH FL230, CREW RECEIVED THE RIGHT ENGINE OVERHEAT LIGHT AND THE EICAS MESSAGE R ENG OVHT. CREW SECURED THE BLEED. AFTER APPROXIMATELY FIVE MINUTES, THE LIGHTS EXTINGUISHED. FLIGHT RETURNED TO PHX AND LANDED WITH NO FURTHER INCISDR USAASB00138Fire Loop · failedPIT - FLT 2004 - ON CLIMB-OUT FROM PIT, EN ROUTE TO LGA, THE CREW NOTED AN ENGINE OVERHEAT WARNING ON THE NR 2 ENGINE. THE A LOOP FOR THE NR 2 ENGINE WAS ON MEL AT THE TIME. THE WARNING WAS AT FIRST INTERMITTENT THEN BECAME STADY AS THE AIRCRAFT CROSSED THROSDR 00FDEA00324Detector · malfunctionedLWR AFT BODY AND ENGINE NR 3 STRUT OVERHEAT LIGHTS FLICKER INTERMITTENTLY. INSPECTION WHEEL WELL AND PERFORMED GROUND OPS CHECK. COULD NOT DUPLICATE PROBLEM AT THIS TIME, PER MM CHAPTER 26.SDR SWAA000812Detector · erraticABORTED TAKEOFF. NR 2 ENG OVERHEAT DETECT LIGHT ILLUMINATED WITH TAKEOFF THRUST SET. REMOVED AND REPLACED NR 2 ENG LOWER OVERHEAT LOOP DETECTOR PER MM.SDR JBXA0000172Warning Light · illuminatedMLG OVERHEAT FAIL CAUTION MSG ILLUMINATED IN FLT. MLG OVERHEAT WARNING ILLUMINATED IN FLT FOR 30 SECONDS AND WENT OUT. THEN CAME BACK ON AND REMAINED ON IN FLT. RETURN TO RDU. REMOVED AND REPLACED LT WHEEL BIN IAW CL-65 AMM 26-14-00 AND 53-83-01. OPS CHECSDR 00FDEA00306Warning Light · illuminatedNR 1 & 3 ENGINE STRUT OVERHEAT LIGHT BOTH FLICKERED 5 MIN AFT T/O. CHECKED NR 1 & 2 ENG OVERHEAT SENSORS FOR PROPER INSTALL PER MM 26-14-000-1. ALL IND SAT DURING RUN AS PER JET RUN HANDBOOK. AC OK TO CONTINUE.SDR COMA0060383Warning System · false indicationCARGO OVERHEAT MESSAGE. COULD NOT DUPLICATE. NO EVIDENCE OF OVERHEAT.SDR COMA0060379Detector · malfunctionedCARGO OVERHEAT MESSAGE. REPLACED SMOKE DETECTOR.SDR SIMA1104Smoke Detector · malfunctionedCLE - FLT 4337 - BAGGAGE SMOKE LIGHT CAME ON IN FLIGHT. DISCHARGED BOTH FIRE BOTTLES AND DECLARED AN EMERGENCY. AIRCRAFT HAD NORMAL LANDING. INSPECTED CARGO AREA. NO EVIDENCE OF SMOKE OR FIRE DAMAGE. FOUND FORWARD SMOKE DETECTOR FAULTED. REMOVED AND REPLSDR 00FDEA00254Warning Light · activatedENG 3 STRUT OVERHEAT LIGHT CAME ON. REMOVED ACCESS PNLS 5501 & 5502 INSP NR 3 PYLON OH DETECTOR ELEMENT LOOP AND ASSOCIATED DUCTING. NO DISCREPANCIES NOTED OR EVIDENCE OF AIR LEAKS. SYS CK NORM IAW MM 26-14-000-5. REINSTALLED ACCESS PNL. AC OK TO CONTINUESDR SROM200000005Wire · chafedLEFT HAND WING/BODY OVERHEAT INDICATION. FOUND CHAFED SHORTED WIRE AT D-866 IN APU COMPARTMENT. REPLACED SAME AND OPS CHECKED PER MAINTENANCE MANUAL 26-18-0.SDR GAIA00170Line · leakingFLT 1723 - BOS-TOL - THE AIRCRAFT ENCOUNTERED A NR 3 ENGINE STRUT OVERHEAT WHICH WENT OUT WHEN THE THROTTLE WAS RETARDED HALFWAY BACK. THE AIRCRAFT CONTINUED TO TOL AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. REMOVED AND REPLACED A FLEX LINE FOR THE NR 3 ENSDR CA000410038Element · failed(CAN) 14TH STAGE DUCT WARNING MESSAGE IN CRUISE. SENSING ELEMENT REPLACED.SDR DL73K000625Controller · malfunctionedON DESCENT INTO TPA PASSING THROUGH 15000 FT, RECEIVED A WHEEL WELL FIRE INDICATION. AFTER PERFORMING APPROPRIATE PROCEDURE WHEEL WELL FIRE LIGHT BECAME INTERMITTENT. T/S PER MM. UNABLE TO DUPLICATE DISCREPANCY. REPLACED COMP OVHT CONTROLLER MODUEL AS PSDR GAIA00162Line · leakingDURING SCHEDULED FLIGHT 509, MCO-TOL, ON CLIMB-OUT, ENGINE NR 1 STRUT OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED TO MCO AND MADE A ROUTINE LANDING. MAINTENANCE FOUND FLEX LINE IN PYLON LEAKING. REPLACED FLEX LINE. RAN ENGINE AT CRUISE POWER. NR 1 ENGINSDR GAIA00161Anti-Ice Valve · leakingDURING SCHEDULED FLIGHT 509, MCO-TOL, ON CLIMB-OUT, ENGINE NR 3 STRUT OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED TO MCO AND MADE A ROUTINE LANDING. FOUND AIR LEAK AT ANTI-ICE VALVE. FOUND MOUNTING BOLT LOOSE. RE-TORQUED BOLTS. LEAK CHECKED. RAN ENGINESDR USAASB00083Element · failedMCO - FLT 1640 - ON CLIMB-OUT FROM PBI, CAPTAIN RECEIVED A RIGHT WING BODY OVERHEAT INDICATION. AFTER CHECKING ALL THE SPECIAL PROCEDURES, CAPTAIN ELECTED TO DIVERT TO MCO. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOSDR GAIA00115Fire Loop · malfunctionedFLT 1850 - SEA-FWA - DURING CRUISE, THE NR 3 ENGINE FIRE DETECTION LOOP ILLUMINATED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT FWA. REPOSITIONED NR 3 ENGINE FIRE DETECTION LOOP. OPERATIONALLY CHECKED SYSTEM GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR GAIA00114Fire Loop · malfunctionedFLT 1849 - FSD-SEA - DURING CRUISE, THE NR 3 ENGINE FIRE DETECTION LOOP ILLUMINATED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT SEA. REMOVED AND REPLACED NR 3 ENGINE LOWER FIRE LOOP ASSEMBLY IAW B727 MM 26-70-00. OPERATIONALLY CHECKED SYSTEM GOOD. AIRCRAFT WASSDR GAIA00113Connector · dirtyFLT 1849 - FSD-SEA - DURING CRUISE, THE NR 3 ENGINE FIRE DETECTION LOOP ILLUMINATED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT SEA. CLEANED CONNECTOR ON NR 3 ENGINE FIRELOOP. OPERATIONALLY CHECKED SYSTEM GOOD. COWL CLOSED AND THE AIRCRAFT WAS RETURNED TO SERVSDR MALA000184Wire · brokenLT TAILPIPE HOT DETECT CIRCUIT BREAKER TRIPPED, WILL NOT RESET. MX COMPLETED 409 CAR NR 077093 AND REINSTALLED ZONE 3 COWL. REPAIRED BROKEN WIRE. OPS CHECK GOOD.SDR 00FDEA00094Warning Light · illuminatedNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUM. POWER REDUCED PER RED TABS AND LIGHT EXTINGUISHED. REPLACED ALL THE CLAMPS AND RETORQUED SWIVEL GLAND, RAN APU AND ENGINE. LEAK CHECK OK PER BAC MM 36-00-001. OK TO CONTINUE.SDR 00FDEA00092Warning Light · illuminatedDURING DESCENT, LWR AFT BODY OVERHEAT LIGHT ILLUM. RED TAB PROCEDURE. LIGHT OUT ON GROUND & SYS TEST GOOD. REPEAT.SDR 00FDEA00088Warning System · activatedLOWER AFT BODY OVERHEAT ILLUM DURING FLT, LIGHT FLICKERED CONTINUOUSLY WHILE CRUISING. COMPLIED WITH CK LIST PROC. REPEAT WRITE UP. REMOVED AND REPLACED FIRE DETECTOR, RAN ENGINES AT HI POWER FOR APPROX 10 MIN. OVERHEAT DETECTOR SYS OPER CK NORMAL PER 727 SDR 00FDEA00086Overheat Light · illuminatedLWR AFT BODY OVERHEAT LIGHT ILLUM DURING FLT. REPEAT WRITEUP. REPOSITIONED ENTIRE LOOP LEFT SIDE FROM 1183 AFT. RAN ALL 3 ENG WITH AIRSTAIRS UP AND CK LEAKS. NO LEAKS FOUND. RAN BOTH PACKS ONE AT A TIME DURING GROUND TIME WITH NO LWR AFT BODY OVERHEAT CONSDR 00FDEA00085Fire Loop · out of positionLWR AFT BODY OVERHEAT LIGHT ILLUM. COMPLIED WITH CKLIST AND LEFT THE NR 2 BLD & PACK CLOSED REMAINDER OF FLT. REPOSITIONED FIRE WIRE. SYSTEM FUNCTIONAL CK. OK PER MM 26-14-001.SDR DL73K000217Wire · chafedREPAIRED SHORTED WIRE W448-001-20 PER WD 26-12-01. REPLACED LOOP CONNECTOR D858. ALL OPERATIONAL CHECKS NORMAL. LEFT WING BODY OVERHEAT.SDR CA000110071Loop · faulty(CAN) IN CRUISE LT 14TH DUCT WARNING MESSAGE RESULTED IN LEFT ENGINE SHUT DOWN. EMERGENCY DECLARED, UNEVENTFUL LANDING COMPLETED. REMOVED AND REPLACED FAULTY FIRE LOOP.SDR COMA0060006Detector · malfunctionedLEFT 14TH STAGE BLEED AIR DUCT LEAK WARNING. REPLACED FAULTY BLEED AIR LEAK DETECTOR.SDR P2EA99343Connector · contaminatedMSP - FLT 705 - DURING FLIGHT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED, THE SAME LIGHT REMAINED EXTINGUISHED AT REDUCED THROTTLE SETTINGS. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH NO INCIDENT. CLEANED CANNON PLUG ON FIRE TEST UNIT AND FIRE PROTECTISDR 99FDEA00491Overheat Loop · inopNR 1 ENG STRUT FLICKERED ON T/O ROLL MOMENTARILY AND THEN EXTINGUISH AT 4,000' ALT, LIGHT ILLUM STEADY. *S/D* REMOVED AND REPLACED OVERHEAT LOOP PER MM 26-14-1, LEAK CK NORMAL. LIGHT OPER CK NORM. OK FOR SERVICE.
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