JASC 2613
Service difficulty reports · 1,797
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 USAASB96001Element · shortedFLT NR 1244 - CLT - LEFT WING BODY OVERHEAT ILLUMINATED IN FLT. ISOLATED LEFT BLEED AIR DUCT BUT OVERHEAT LIGHT REMAINED ON. MAINTENANCE FOUND OVERHEAT ELEMENT SHORTED. REPLACED ELEMENT. OPS CHECKS SAT. (M)SDR COMA9630004Overheat Warning · activatedRIGHT ENGINE TAIL PIPE HOT WARNING SHORTLY AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. GROUND RUNS WERE NORMAL AND ACFT RETURNED TO SERVICE.SDR UPS405162Sensor · shortedCREW REPORTED, RT WING LE OVERHEAT LIGHT ILLUMINATED. RAN ALL ABNORMAL CHECKLISTS AND OVERHEAT LIGHT FAILED TO EXTINGUISH. LIGHT REMAINED ILLUMINATED FOR OVER TWO HRS AFTER ENG SHUTDOWN. FOUND SENSOR S1048 IN PYLON NR 4 SHORTED TO GND.SDR P5CA9500876Overheat Warning · activatedRT WING LEADING EDGE OVERHEAT FAULT, ON TAXI OUT FOR TAKEOFF. RETURNED TO GATE, UNABLE TO DUPLICATE OVERHEAT CONDITION WITH EITHER APU OR ENGINE PNEUMATICS. DETERMINED TO BE FALSE WARNING.SDR COMA9531211Overheat Ind · activatedLEFT TAIL PIPE HOT WARNING AFTER TAKEOFF. ENGINE SECURED AND ACFT RETURNED TO FIELD. COULD NOT DUPLICATE DISCREPANCY. GROUND RUN AT 100 PERCENT POWER FOR 10 MINUTES. NO FURTHER TAIL PIPE HOT WARNING.SDR PLG121895E2Temp Sensor · contaminatedPVD/LGA - FLT 4783 - AFTER TAKEOFF, THE RT TAIL PIPE HOT LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO PVD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RT LOWER AFT SENSOR AND SYSTEM OPERATIONS CHECKED GOOD. AIRCRAFT WAS RELEASED BACK TO SERVSDR USAASB95021Detector · failedCLT - FLT NR 0127 - DURING CLIMB-OUT, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED HANDBOOK PROCEDURES INCLUDING ENGINE SHUTDOWN. FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE CORE OVERHEAT/FIRE DETECTOR ELEMESDR 95UAL900267Overheat Control · inoperativeCREW REPORTS RIGHT WING BODY OVERHEAT LIGHT FLICKERED DURING FLIGHT. TURNED OFF BLEED AND CLOSED ISOLATION VALVE, NO HELP. DIVERTED TO IAD. REPLACED THE OVERHEAT CONTROL UNIT. CHECKS O.K.SDR 95FDEA01794Overheat Wire · bareDIA - NR 2 FIRE WARNING IND ON MOMENTARILY ON APPROACH INTO DEN, LESS THAN 2 SECOND BELL AND LIGHT. SYS CHECKS OK. OPENED COWL AND INSPECTED ALL DUCTS AND ENGINE. FOR LOOSE CONNECTIONS OR BREAKS, CHECKED OK. FOUND EXPOSED WIRE ON OVER HEAT WIRE ADJACENT TOSDR UPS204931Overheat Module · malfunctionCREW REPORTED NR 1 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. APPROPRIATE CHECKLIST WAS PERFORMED AND ENGINE WAS SHUTDOWN. ACT NOTIFIED, EMERGENCY DECLARED AND FLIGHT PROCEEDED WITHOUT FURTHER EVENT TO DFW. REMOVED AND REPLACED OVERHEAT DETECTION MODULE PSDR CAL950944Overheat Light · illuminatedFLT NR 1444 - EWR - AIRCRAFT INBOUND, NR 1 ENGINE OVERHEAT LIGHT ILLUMINATES WITH THROTTLE ADVANCE. RETURNED TO BASE. MAINTENANCE REPLACED CONNECTOR AND ELEMENTS. (M)SDR 95UAL900167Overheat Loop · failedLOWER AFT BODY HEAT LIGHT ILLUMINATED ON CLIMBOUT. LIGHT OUT WITH NR 1 THROTTLE AT IDLE AND LEFT PACK OFF. LEFT DUCT PRESSURE SHOWS 10 PSI. FOUND KEEL BEAM LOOP RESISTANCE OUT OF LIMITS. REPLACED KEEL BEAM LOOP AND TESTED PER MM, TESTED NORMAL.SDR 95UAL900164Wire · chafedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT. LIGHT WENT OUT WITH ALL 3 ENGINES AT IDLE DURING DESCENT. FOUND CHAFED WIRES AT FWD DISCONNECT FOR DETECTOR M365, SEC 48 OVERHEAT DETECTOR. REPAIRED PER MM, PRESSURIZED DUCTS AND MOTORED ENGINE FOR SDR 95ZZZX5917Overheat Loop · out of positionLOG REPORT: F-GL534 AT CHS, ON TAKEOFF ROLL, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OUT ON POWER REDUCTION. INSPECTION OF NR 3 ENGINE STRUT FOUND OVERHEAT LOOP TOUCHING DUCT ASSY. REPOSITIONED OVERHEAT LOOP. PEFORMED LESDR 95UAL900138Overheat Warning · activatedSHORTLY AFTER TAKEOFF, RECEIVED EICAS MESSAGE OF NACELLE ENGINE OVERHEAT AND FIRE DETECTOR OVERHEAT.SDR UPS204398Overheat Wire · chafedPILOT REPORTED ENGINE NR 1 STRUT LIGHT ILLUMINATED IN FLIGHT. ENGINE NR 1 WAS SHUT DOWN, WHEN LIGHT WOULD NOT EXTINGUISH LIGHT OFF AFTER SHUT DOWN. FOUND WIRE NR W902-20 AT CONNECTOR DM9526B CHAFED THROUGH AT CONNECTOR BARREL. REPAIRED WIRE AS REQUIRED. RASDR CAL950788Harness · chafedFLT NR 1588 - EWR - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED ON APPROACH TO EWR. THE NR 2 ENGINE WAS SHUT DOWN AND BOTH LEFT AND RIGHT FIRE BOTTLES WERE DISCHARGED. THE LIGHT REMAINED ILLUMINATED FOR APPROXIMATELY ANOTHER EIGHT MINUTES AND THEN EXTINGUISHESDR AALA951485Over Temp Unit · defectiveSJU - FLT 1879 - EN ROUTE MIA/CUR DURING CRUISE, LOWER AFT BODY HEAT LIGHT ILLUMINATED. ACCOMPLISHED EMERGENCY CHECK LIST AND DIVERTED INTO SJU AND LANDED WITHOUT INCIDENT. REPLACED OVER TEMP ALARM CONTROL UNIT. INSPECTED DUCTS, RAN ENGINES, AND ACCOMPLISHESDR DL72W953406Element · shortedON TAKEOFF OUT OF ORF, HAD THE LOWER/AFT BODY OVERHEAT ILLUM. FOLLOWED PROCEDURES, LIGHT STAYED ILLUM. ISOLATED THE NR 1, NR 2, NR 3 ENG PNEUMATICS, LIGHT REMAINED ILLUM. OFF-LANDED IN CAE. FOUND RT OVERHEAT DET M365 SEC 48 SHORTED. REPLACED SAME, RAN ENGSDR AWXA9500531Loop Connector · shortedPHX - FLT 15 - ON CLIMB-OUT OF PHX, THE LT WING TO BODY OVERHEAT LIGHT ILLUMINATED. CREW CLOSED THE LT ENGINE BLEED WITH NO CHANGE. AIRCRAFT RETURNED TO PHX WITHOUT FURTHER INCIDENT. NO OVER WEIGHT LANDING WAS REQUIRED. MX REPAIRED SHORT AT LOOP CONNECTOR SDR 95FDEA01095Detection Unit · failedFSD - ON CLIMBOUT PASSING 15,000 MSL, THE LOWER AFT BODY OVERHEAT LIGHT STARTED FLASHING. BLEEDS WERE NR 1 ON, LT PACKON, NR 2 RT ON, RT PACK ON, NR 3 OFF, OVERHEAT LIGHT EXTINGUISHED WITHIN 5 SECONDS OF TURNING NR 3 BLEED ON AND SYSTEM TESTED GOOD. NO FURTHSDR 95FDEA01094Connector · looseLWR AFT BODY OVERHEAT ILLUMINATED IN FLT, COMPLIED WITH ABNORMAL PROCEDURES. LIGHT WENT OUT AND STAYED OUT AFTER TURNING OFF RIGHT PACK AND CLOSING NR 3 BLEED VALVE. RAN ENGINESAND APU LEAKED CHECK RIGHT PACK AND AIR CONDITION BAY. FOUND SEVERAL CLAMPS LEAKSDR 95FDEA01081Overheat Warning · malfunctionedDURING CLIMB, AFTER SETTING CLIMB POWER, LOWER AFT BODY OVERHEAT LIGHT CAME ON. RAN CHECKLIST 'C'. LIGHT EXTINGUISHEDWITH RETARD OF NR 1 THROTTLE, RETURNED TO MEM. REMOVED ANDREPLACED APU KEEL BEAM FIRE LOOP. MEG BOTH LOOPS, CHECK OK. INSTALL APU, OPS CHECSDR SRAA80295Temp Sensor · failedAFTER TAKEOFF FROM LUTTON, RIGHT WING OVERHEAT LIGHT ILLUMINATED, AIRCRAFT COMPLETED AIR TURN BACK TO LUTTON. PERFORMED DUCT PRESSURE CHECK ON THE ANTI-ICE SYSTEM. NO LEAKS NOTED, INSPECT TEMP SENSOR FOUND FAULTY REPLACED SENSOR, SYSTEM OPS CHECKED GOOD. (M)SDR DL72W953005Overheat Loop · cutAT FL 270, 25 MIN INTO FL, LOWER AFT BODY O/H LIGHT ILLUM INTERMITTENTLY FOR APPROX 1 MIN, THEN STEADY. C/W POM PROC AND LIGHT REMAINED ILLUM FOR 15 TO 20 MIN WITH NR 2 THROTTLE AT IDLE. AFTER 20 MIN WITH NR 2 THROTTLE AT IDLE LIGHT EXT WITH A COUPLE OF FLICSDR USAA950645Sensor · failedMCO - FLT 1018 - ON CLIMBOUT, LT WING BODY OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO MCO WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED LT ENGINE PYLON OVERHEAT SENSOR. (W)SDR 95ZZZM617Overheat · defectiveNR 2 ENGINE OVERHEAT LIGHT ILLUMINATED EN ROUTE TO PIE FROM MIA. FOUND DEFECTIVE OVERHEAT LOOP NR 2 ENGINE. REMOVED AND REPLACED OVERHEAT LOOP NR 2 ENGINE, OPS CHECKED GOOD. (M)SDR USAA950604Sensor · misalignedSAN - FLT 1152 - ON CLIMBOUT, NR 2 ENGINE OVERHEAT LIGHT CAME ON. THROTTLE REDUCED TO IDLE AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO SAN WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPOSITIONED CORE ENGINE DETECTOR. RAN ENGINE AT TAKEOFF ASDR USAA950598Overheat Unit · failedCLT - FLT 955 - FLIGHT EN ROUTE BWI TO BHM WHEN LEFT WING BODY OVERHEAT LIGHT CAME ON. FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OVERHEAT ACCESSORY UNIT. OPS CHECK NORMAL. (M)SDR COM31088Hot Warning · illuminatedRT TAIL PIPE HOT WARNING LIGHT CAME ON AFTER TAKEOFF. COULD NOT DUPLICATE PROBLEM. INSPECTED SYSTEM AND FOUND NO DEFECTS.SDR C2XA95CL086Detector · shortedFLT NR 3637 - SYR-SYR - NACELLE OVERHEAT ILLUMINATED ON TAKEOFF. RETURNED TO GATE. AIRCRAFT RELEASED IAW MEL 26-12-3. BDL MAINTENANCE CLEARED MEL BY REMOVING AND REPLACING THE NR 2 OVERHEAT DETECTOR. OPS CHECKED GOOD. (W)SDR MEJA9504002Overtemp Wire · defectiveDURING TAXI WHEN THE SPEED LEVER WAS ADVANCED TO HIGH, THE LEFT WING OVERTEMP LIGHT FLICKERED. AIRCRAFT WAS FERRIED TO SAT. REPAIRED WIRE FROM FUSELAGE CONNECTOR TO BLEED AIR FAIL SENSOR IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT INCORPORATED WIRING MANUAL 26SDR COM31060Heat Detector · dirtyRT TAILPIPE HOT WARNING ACTIVATED. REPLACED LOOSE SEALANT AT RT TAILPIPE HEAT DETECTOR.SDR 95ZZZW424Overheat Sensor · malfunctionedFLT 4943 - DCA - RIGHT ENGINE TAIL PIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF AT 300 FEET. CREW FOLLOWED EMERGENCY CHECKLIST AND SHUT DOWN RIGHT ENGINE. WARNING PERSISTED. WARNINGS STOPPED AFTER BOTH FIRE BOTTLES WERE DISCHARGED. SYSTEM INSPECTIONS SATISFACTSDR 9503519940Wire · chafedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CRUISE FLIGHT AT 33,000 FEET. FLIGHT DIVERTED TO BIS AND LANDED WITHOUT INCIDENT. FOUND WIRING TO RIGHT TEMPERATURE SENSOR CHAFED AND GROUNDING ON TUBING. REPLACED THE RIGHT TEMPERATURE SENSOR AND ISDR USAA950111Temp Sensor · inoperativePIT - FLT 1560 - AFTER CLIMB AND ENTERING CRUISE, THE TAIL COMPARTMENT TEMPERATURE LIGHT ILLUMINATED. THE CREW DECIDED TO RETURN TO PIT. MAINTENANCE REPLACED BOTH LEFT AND RIGHT TAIL TEMPERATURE SENSORS. OPERATIONS CHECKED GOOD. (Z)SDR DL72W950577Detector Unit · failedON CLIMB-OUT, NR 1 ENGINE STRUT OVERHEAT ILLUMINATED, UNABLE TO EXTINGUISH, SHUT DOWN NR 1 ENGINE. REPLACED DETECTOR UNIT, SECURED DUCT CLAMP AT 13TH STAGE VALVE, RETURNED TO SERVICE.SDR 95ZZZZ88Connector · looseDURING TAXI OUT FOR FLIGHT NR ADT 3 FROM MHZ, NR 2 NACELLE OVERHEAT LIGHT CAME ON. FOUND NR 2 NACELLE OVERHEAT PROBE CONNECTION LOOSE AND NR 2 MISG PLUG WET DUE TO DE-ICING, DRIED CANNON PLUG AND TIGHTEN CONNECTIONS, OPS CHECKED GOOD.SDR COM31009Detector · defectiveRT ENGINE TAIL PIPE HOT WARNING ACTIVATED. REPLACED DEFECTIVE HEAT SENSOR ON RT EXHAUST DUCT.SDR COM31008Connector · dirtyRT TAIL PIPE HOT WARNING ACTIVATED DURING CLIMB. CLEANED WIRING CONNECTION FOR TAIL PIPE HEAT SENSORS AND AIRCRAFT RETURNED TO SERVICE.SDR MRKA958Detector · looseTHE RT WING BODY OVERHEAT LIGHT FLICKERED SEVERAL TIMES, THEN STAYED ON STEADY IN FLIGHT. CHECKED RESISTANCE AT D742, AND REPOSITIONED OVERHEAT DETECTOR DUE TO PULLED FROM SUPPORT. OPERATIONAL CHECKED OK FOR CONTINUED SERVICE. (W)SDR COM31002Detector · dirtyRT 'TAILPIPE HOT' WARNING ILLUMINATED DURING FLIGHT. CLEANED WIRE CONNECTIONS AT TAILPIPE HEAT DETECTORS.SDR 9500652767Sense Loop · malfunctionedWHILE IN CRUISE FLIGHT, THE NR 3 STRUT OVERHEAT WARNING ILLUMINATED. PERFORMED PRECAUTIONARY SHUT DOWN OF THE NR 3 ENGINE. FOUND THE SENSE LOOP HAD FAILED. REPLACED THE LOOP AND TESTED THE SYSTEM. CHECKED OK. AIRCRAFT RETURNED TO SERVICE.SDR MRKA957Connector · looseTHE RT WING BODY OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. FOUND LOOSE CANNON PLUG ON THERMAL ANTI-ICE SENSOR, AND RT WING LOOP RUBBING ON FLUID LINE UNDER WING LEADING EDGE. SECURED CANNON PLUG AND REPOSITIONED OVERHEAT WARNING DETECTOR. RAN ENGINE AND WINSDR MRKA955Overheat Light · illuminatedTHE RT WING BODY OVERHEAT LIGHT INTERMITTENT IN FLIGHT. OPERATED RT PACK WITH NO FAULTS NOTED. SYSTEM CHECKED NORMAL. OK FOR CONTINUED SERVICE. (W)SDR MEJA9501002Connector · wetON FLIGHT 1851 IN CRUISE THE RIGHT WING OVERHEAT LIGHT CAME ON. AIRCRAFT TURNED BACK AND RETURNED TO MFE WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND MOISTURE IN THE WING ROOT CONNECTOR FOR THE WING OVERHEAT LIGHT SYSTEM. CLEANED AND DSDR 95ZZZX780Overheat Wire · chafedLEFT WING OVERHEAT ANNUNCIATOR LIGHT FLICKERED AFTER TAKEOFF. LEFT ENGINE BLEED, GENERATOR WAS SHUT OFF, AND AIRCRAFT RETURNED TO AIRPORT IAW AFM. SYSTEM WAS INSPECTED AND FOUND WIRE NR 6801DD-22 CHAFED. REPLACED WIRE AND PERFORMED OPERATIONAL CHECK OKAY.
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