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 CA970618004Element · failed(CAN) #2 ENGINE OVERHEAT ON DESCENT. AIRCRAFT DIVERTED. LOWER OVERHEAT DETECTION LOOP FAILED, REPLACED.SDR USAABB97067Overheat Loop · bentPHL - FLT 14, ON CLIMB-OUT FROM PHL, PASSING THROUGH FL 200, CREW RECEIVED THE EICAS MESSAGES 'L ENG OVERHEAT'. LIGHT EXITNGUISHED WITH A REDUCTION IN POWER, BUT RETURNED WHEN POWER ADDED. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENASDR SWAA970460Overheat Light · illuminatedNUMBER 1 ENGINE OVERHEAT LIGHT ILLUMINATED, WITH OVERHEAT DETECTION SYSTEM ALREADY ON MEL. AIRCRAFT RETURNED TO OKC AND MADE AN UNEVENTFUL LANDING. INSPECTED, UNABLE TO DUPLICATE PROBLEM, CONTINUED SERVICE WITH SYSTEM PER MEL.SDR GAIA9726Sensing Element · shortedKHA - FLT 735 - ELP-TOL, AFTER TAKEOFF THE NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON. THE FLIGHT CREW PERFORMED A PRECAUTIONARY ENGINE SHUT DOWN AND RETURNED TO ELP. INVESTIGATION REVEALED A SHORTED OVERHEAT DETECTION LOOP ON THE NR 3 ENGINE STRUT. REMOVED ASDR COMA9760080Sensing Element · failedLEFT 14TH STAGE BLEED AIR WARNING ACTIVATED EN ROUTE TO CVG, RETARDED THRUST LEVER TO ELIMINATE WARNING. REPLACED THE LEFT ENGINE PYLON DUCT LEAK DETECTION LOOP.SDR COMA9710225Wire · chafedLEFTHAND BLEED AIR DUCT WARNING CAME ON DURING BOARDING. REPAIRED DAMAGED WIRE AT CENTER WING BLEED LEAK DETECTOR.SDR COMA9760072Overheat Element · defectiveRIGHT HAND ENGINE 14TH STAGE BLEED DUCT LEAK WARNING DURING DECENT. ENGINE SHUT DOWN DURING FLIGHT. REPLACED DEFECTIVE ENGINE PYLON BLEED LEAK DETECTION LOOP.SDR PLGA970418AOvertemp Warning · activatedBGR - DURING TAKEOFF ON A FERRY FLIGHT FROM BGR TO ALB, CREW RECEIVED AN OVERTEMP WARNING ON LEFT ENGINE. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO MAINTENANCE. MAINTENANCE GROUND RAN ENGINE AND REPORTED NO PROBLEMS FOUND. AIRCRAFT WAS RELEASED FOR FERRYSDR PLGA9704188Hot Light · illuminatedBDL - FLT 4446 - WHILE EN ROUTE TO BOS, CREW RECEIVED A RIGHT TAIL PIPE HOT LIGHT WARNING. AIRCRAFT DIVERTED TO BDL. THE WARNING LGIHT EXTINGUISHED WHEN THE POWER LEVERS WERE PULLED BACK. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED TAIL PIPE ARSDR 9707789884Temp Sensor · failedDURING CLIMB-OUT OF DFW PASSING 17,000, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE. LIGHT REMAINED ON. LIGHT EXTINGUISHED WHEN POWER RETARDED TO 1.5 EPR. FLIGHT RETURNED TO DFW AND LANDED WITHOUT INCIDESDR 97UAL900300Overheat Det · out of positionLOWER AFT BODY OVERHEAT LIGHT CAME ON IN FLIGHT FL370. DESCENDED DOWN TO FL 250 AND LIGHT WENT OUT APPROX 310 DURING THE DESCENT. *S/D* REPOSITIONED KEEL BEAM DETECTOR, REMOVED AND INSPECTED DUCT THAT RUNS THROUGH KEEL BEAM AND LEAK CHECKED. NO DEFECT NOTESDR SRAA970403Wire · brokenON PRE-FLIGHT INSPECTION FOUND NR 2 NACELLE OVERHEAT WOULD NOT TEST. FOUND LOWER RIGHT AFT SIDE OVERHEAT DETECTOR HAD BROKEN WIRE, REPAIRED BROKEN WIRE, SYSTEM OPS CHECKED GOOD PER M.M. CH 26-10-4.SDR REXA97078Hot Light · illuminatedTAIL PIPE HOT CAME ON DURING TAKEOFF, WENT OUT 30 SECONDS AFTER REDUCING TO FLIGHT IDLE. PERFORMED OPS TEST OF RT AND LT ENGINE FIRE AND TAIL PIPE HOT DETECTORS SYSTEM TESTS NORMAL. (M)SDR PLGA970322AOvertemp Light · illuminatedPVD - FLT 4787 - DURING TAKEOFF WITH ENGINE DE-ICE ON, THE RIGHT OVERTEMP LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. CREW REPORTED, TEMP LIMITS WERE NOT EXCEEDED PER GE MM. ENGINE WAS INSPECTED AND SYSTEM CHECKED WITH NO PROBLSDR VTZA97168Overheat Loop · failedFLT 6264 - BTV-IAD - DURING APPROACH, MADE AN SCHEDULED LANDING AT IAD WITH ONE DISCREPANCY WHICH WAS LEFT ENGINE OVERHEAT LIGHT CAME ON DURING APPROACH. AIRCRAFT WENT TO GAUGE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED OVERHEATSDR MALA975326Wire · chafedFLT 3333 - AFTER TAKEOFF FROM DTW, RIGHT TAIL PIPE HOT LIGHT ILLUMINATED, EXTINGUISHED WHEN POWER RETARDED BELOW 50 PERCENT TORQUE. FLIGHT RETURNED TO DTW. MAINTENANCE FOUND WIRE CHAFFED IN AFT NACELLE, REPAIRED WIRE. ALL CHECKS GOOD. (M)SDR UPS97222077Wire · chafedINSPECTION TYPE-N/A, CLIMB POWER 250 KTS ENG NR 2 OVERHEAT LT ON INFLIGHT 10,000 FT. ALL OTHER INDICATIONS NORMAL, ENGINE NR 2 SHUTDOWN PER CHECKLIST PROCEDURES. RETURNED AND LANDED MEM. UNEVENTFUL PREVIOUS FLIGHT BUT DIFFERENT CREW, SAME PROBLEM. PERFORMESDR REXA97028Connectors · dirtyRIGHT TAIL PIPE HOT LIGHT IS ACTIVATED. CLEANED ALL CONNECTORS AND CANNON PLUGS. GROUND RUNS OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE. (M)SDR COMA9760040Detector · malfunctioned14TH STAGE DUCT LEAK WARNING DURING FLIGHT. ENGINE WAS SHUT DOWN, BUT WARNING REMAINED. REPLACED DEFECTIVE 14TH STAGE BLEED LEAK DETECTOR.SDR P9IA97002Sensing Loop · shortedNR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE STRUT SENSING LOOP IAW BOEING MM 26-14-1. PERFORMED ENGINE RUN-UP WITH BLEED AIR ON. OPS CHECKS GOOD ON GROUND IAW BOEING MM 71-00. (M)SDR 96UAL901005Overheat Light · illuminatedRIGHT WING-BODY OVER HEAT LIGHT ILLUMINATED. ACCOMPLISHED DUCT LEAK CHECK IN RIGHT WING-BODY AREA. OPS CHECK NORMAL. NO SUBSEQUENT OCCURRENCES.SDR SWIA95795Wire · out of positionON CLIMBOUT, DUCT LEAK LIGHT FOR RIGHT ENGINE ILLUMINATED, IT STAYED ON FOR MORE THAN 3 MINUTES. SHUT DOWN RIGHT ENGINE PER QRH AND RETURNED TO RNO. INSPECTED A/C RIGHT ENGINE BLEED AIR SYSTEM, FOUND SUSPECT TEMP SENSOR WIRE TO BE IN CLOSE PROXIMITY TO BLEEDSDR USAASB96263Detection Loop · failedPIT - FLT 1212 - FLIGHT DIVERTED TO PIT DUE TO A RIGHT WING BODY OVERHEAT LIGHT. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE STRUT CAVITY OVERHEAT DETECTION LOOP. RAN ENGINE. ASDR TWAA9615501Element · failedSTL - FLT 475 - DURING CRUISE, SHUT DOWN NR 2 ENGINE, S/N 3953, DUE TO OVERHEAT WARNING. FOUND LOW RESISTANCE IN SENSING ELEMENT, MFG P/N 894120. REPLACED SENSING ELEMENT. ENGINE OVERHEAT WARNING SYSTEM OPERATION THEN CHECKED NORMAL. (M)SDR 97ZZZM65Sensing Element · failedSTL - DURING CRUISE SHUT DOWN NR 2 ENGINE, S/N 3953, DUE TO OVERHEAT WARNING. FOUND LOW RESISTANCE IN SENSING ELEMENT, MFG P/N 894120. REPLACED SENSING ELEMENT. ENGINE OVERHEAT WARNING SYSTEM OPERATION THEN CHECKED NORMAL. (M)SDR MALA965237Connector · looseDTW - FLT 3150 - IN CRUISE FLIGHT TO DTW WITH THE ENGINE ANTI-ICE ON, THE LEFT TAIL PIPE HOT LIGHT ILLUMINATED. THE CREW REDUCED POWER AND THE WARNING LIGHT EXTINGUISHED. MAINTENANCE SECURED A LOOSE CANNON PLUG TO THE HOT SENSOR. ALL CHECKS GOOD. (X)SDR SWIA95772Overheat Element · failedLT 14TH DUCT WARNING AND BLEED AIR DUCT AURAL AFTER TAKEOFF. WARNING DID NOT EXTINGUISH WITH LT 14TH BLEED CLOSED, WARNINGS EXTINGUISHED LT POWER REDUCTION BELOW 79 PERCENT N1. CONTINUED FLIGHT USING PARTIAL LT POWER. REMOVED AND REPLACED LT 14TH STAGE SENSSDR P5CA9600864Overheat Sensor · malfunctionedAIR TURNBACK DUE LEFT WING L/E OVERHEAT LIGHT ILLUMINATED DURING CLIMB. LIGHT EXTINGUISHED BY REDUCING THRUST NUMBER 1 ENGINE WITH PYLON VALVE CLOSED. NO PNEUMATIC LEAKS FOUND IN NR 1, NR 2 PYLON OR LEFT WING MANIFOLD. FOUND NR 1 PYLON OVERHEAT DETECTOR INTSDR USAASB96220Overheat Module · defectiveMCO - FLT 1176 - DURING CLIMB-OUT, THE LT WING BODY O/H LIGHT ILLUMINATED AT FL 020. CREW ACCOMPLISHED NORMAL AND ABNORMAL CHECKLIST. FLIGHT RETURNED TO FIELD AT MCO AS PRECAUTIONARY. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.SDR MALA965170Detectors · failedFLT 2973 - AFTER TAKEOFF FROM ESC, THE RIGHT TAIL PIPE HOT LIGHT ILLUMINATED. THE CREW RETARDED THE POWER LEVERS AND THE LIGHT REMAINED ON. THE CREW SHUT DOWN THE ENGINE, AND THE LIGHT WOULD INTERMITTENTLY ILLUMINATE. MAINTENANCE REPLACED THE OVERHEAT DETECSDR PLGA9610201Connector · dirtyPWM - FLT 4964 - EN ROUTE YOW, THE RIGHT TAIL PIPE HOT WARNING LIGHT ILLUMINATED. THE CREW SECURED THE ENGINE AND DIVERTED TO PWM, LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND MOISTURE IN THE CANNON PLUG. MAINTENANCE CLEANESDR 9622339755Temp Sensor · malfunctionedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING TAKEOFF. FOLLOWED COM AND LIGHT WENT OUT. FLIGHT RETURNED TO HOU AND LANDED WITHOUT INCIDENT. REPLACED TAIL COMPARTMENT SENSOR AND RIGHT COALESCER BAG. RAN AIRCRAFT TO FULL POWER, OPERATIONAL CHECKSDR 9621856608Overheat Switch · malfunctionedDURING CLIMB, THE RIGHT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE NR 3 ENGINE PYLON AFT OVERHEAT SWITCH TERMINAL AND REPAISDR AALA961447Sensor · defectiveDFW - FLT 2032 - AFTER TAKEOFF DFW DURING CLIMB-OUT AT FL 135, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. LIGHT EXTINGUISHED DURING DESCENT. REPLACED LEFT TAIL COMPARTMENT TEMPERATURE SENSOR DUSDR AALA961445Sensor · defectivePBI - FLT 1202 - AFTER TAKEOFF DFW DURING CLIMB-OUT, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED WHEN RIGHT PACK TURNED OFF. AIRCRAFT PROCEEDED TO PBI AND LANDED WITHOUT INCIDENT. PLACARDED RISDR USAASB96203Overheat Module · failedPIT - FL 133 - LEFT WING BODY OVERHEAT LIGHT ILLUMINATED ON TAKEOFF AND REMAINED ON IN CLIMB. CAPTAIN TURNED OFF LEFT BLEED SWITCH BUT LIGHT REMAINED ON. AT 10,000 FEET, CAPTAIN ELECTED TO RETURN TO FIELD AT PIT. ON DESCENT, LIGHT WENT OUT BUT ON FINAL APPRSDR MALA965151Connector · corrodedFLT 3157 - ON CLIMB-OUT FROM DTW, THE LEFT TAIL PIPE HOT LIGHT ILLUMINATED. THE CREW RETARDED THE POWER LEVER TO FLIGHT IDLE AND THE LIGHT REMAINED ILLUMINATED. THE CREW SHUT DOWN THE ENGINE AND RETURNED TO DTW. MAINTENANCE FOUND CANNON PLUG 161VP P10 PINSSDR 96ZZZX5146Overheat System · malfunctionDURING TROUBLESHOOTING FOR EXCESSIVE INSULATION MATERIAL LOOSE IN THE TAIL CONE, THE TAIL CONE BLEED AIR OVERHEAT WARNING WAS FOUND INOPERATIVE. THE SYSTEM TESTED NORMAL IN THE COCKPIT, BUT WOULD NOT TRIGGER WHEN HEATED IAW THE MM. INSTALLED GROUND STRAPS PESDR COMA9660147Element · malfunctionedANTI-ICE DUCT MESSAGE ON EICAS DURING TAXI. REPLACED LEFT FUSELAGE DUCT LEAK SENSOR LOOP.SDR 96UAL900696Overheat Sensor · inoperativeRIGHT WING OVERHEAT LIGHT CAME ON AFTER TAKEOFF. ACCOMPLISHED PROCEDURE AND LIGHT WENT OUT AFTER TWO MINUTES. APPEARS TO COINCIDE WITH HIGH POWER SETTINGS. REPLACED RIGHT WING LEADING EDGE CAVITY OVERHEAT DETECTOR SENSOR. CHECKS O.K.SDR SRAA960902Temp Ind · malfunctionedON CLIMBOUT, NR 1 NACELLE TEMPERATURE CLIMBED TO 4 UNITS ON BOTH A AND B LOOPS THEN DROPPED BACK TO NORMAL AT CRUISE ALTITUDE. INSPECTED ENGINE COWLING, PYLON AND ENGINE DUCTING, NO DISCREPANCY NOTED. PERFORMED ENGINE RUN TO TAKEOFF POWER, FOUND NACELLE TEMPSDR VTZA96351Overheat Light · illuminatedFLT NR 6484 - JFK-BOS - RETURNED TO GATE, DUE TO NR 2 PACK OVERTEMP LIGHT ILLUMINATED WHILE ON GROUND IN AUTO OR MANUAL. MAINTENANCE OPENED DMI 64100, MEL 21-18. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M)SDR SRAA960905Overheat Warning · activatedWHILE PULLING OFF OF RUNWAY, NR 2 ENGINE NACELLE OVERHEAT WARNING LIGHT CAME ON. SHUTDOWN NR 2 ENGINE WHILE TAXING.SDR SWAA960854Overheat Warning · illuminatedNR 2 ENGINE OVERHEAT WARNING ILLUMINATED IN FLIGHT, CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT LANDED AT MAF WITHOUT INCIDENT. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. DEFERRED DETECTION SYSTEM AND CONTINUED PER MEL 26-2.SDR 96FDEA01396Overheat Loop · out of positionLWR AFT BODY OVERHEAT LIGHT BLINKED ON MOMENTARILY ONCE WHILE IN FLIGHT. REMOVED GILLINER PANELS LOWER AFT CARGO COMPARTMENT. INSPECTED SENSOR, FOUND NUMEROUS SPOTS SENSOR RUBBING METAL BRACKETS. REPOSITIONED SAME, REMOVED KEEL BEAM PANEL, INSPECTED SENSOR SDR 96FDEA01393Overheat Loop · out of positionLOWER AFT BODY OVERHEAT LIGHT FLASHED ON AND OFF INTERMITTENTLY IN FLIGHT, BOTH PACKS ON BLEEDS 1 ENGINE 2 APU BLEED AND ENGINE 3 BLEED OPEN. LIGHT DOES NOT STAY ILLUMINATED LONG ENOUGH TO ISOLATE PROBLEM USING ABNORMAL CHECK LIST. ALSO, AFT CARGO SELECTED OSDR COMA9660132Overheat Det · malfunctioned14TH STAGE BLEED AIR DUCT FAIL MESSAGE. ENGINE SHUT DOWN AND RETURN TO FIELD. REPLACED DEFECTIVE BLEED LEAK DETECTOR LOOP AT RT ENGINE PYLON.SDR 9618132716Overheat Loop · out of positionNR 3 STRUT OVERHEAT LIGHT ILLUMINATED, SHUT DOWN NR 3 ENGINE, LIGHT REMAINED ILLUMINATED. AIRCRAFT DIVERTED TO ABQ, DUMPED FUEL AND LANDED WITHOUT INCIDENT. REPOSITIONED NR STRUT OVERHEAT LOOP. INSPECTED STRUT AND RAN NR 3 ENGINE AT 1.65 EPR FOR 5 MINUTES, SDR CA960827008Wire · shorted(CAN) LH WING BODY OVERHEAT LIGHT STARTED TO FLICKER, AIRCRAFT DIVERTED. WIRE HAD CHAFED THROUGH AND WAS SHORTING OUT INTERMITTENTLY. WIRE CONNECTED TO D866 OF SENSING ELEMENT M276 "OVHT DET SECTION 58" AT THE APU SHROUD AREA. REPLACED.SDR P9IA96025Sensing Element · looseDURING DESCENT, LOWER AFT BODY OVERHEAT LIGHT WAS INTERMITTENTLY FLICKERING ON AND OFF. SECURED LOOP IN SEVERAL SPOTS ALONG LT SIDE WALL AFT CARGO IAW MM 26-14-1. GROUND CHECKS NORMAL PER MM 26-14-0. (X)
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