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 REXA2013080701570Warning Message · false activationAT 600 FT AGL ANTI-ICE DUCT MASTER WARNING. PERFORMED QRH MESSAGE WENT AWAY. AT ABOUT 2000 FT AGL MESSAGE RETURNED. PERFORMED QRH AND THE MASTER WARNING FOR RT 14TH DUCT DISPLAYED WITH 14TH STAGE BLEEDS CLOSED. QRH R 14TH DUCT PERFORMED. LANDED A REPLACESDR YENA20130803170Loop · out of positionACFT DIVERTED DUE TO BLEED 2 LEAK EICAS MESSAGE DURING CLIMB OUT. RUN QRH PROCEDURES AND MESSAGE EXTINGUISHED. PERFORMED FIM TASK 36-21-00-810-803-A, FOLLOW CH 1 SHORT CONDITION AT 1630 FOUND ODS LOOP INSULATION POSITIONED IMPROPERLY. REPOSITIONED INSULATIONSDR N6WA2013080201Warning Message · false activationLEFT BLEED DUCT MASTER WARNING MESSAGE IN FLIGHT. INSPECTED BLEED AIR LOOP, NO DEFECTS NOTED. INSPECTED LT SIDE BLEED AIR DUCT IN SAME AREA, NO DEFECTS NOTED IAW AMM 63-21-00.SDR AALA20130801002Sensor · faultyDFW CREW REPORTED TAIL COMPARTMENT HIGH LIGHT ILLUMINATED ON CLIMB OUT. FLIGHT RETURNED DFW, LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT & RT HIGH TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.SDR ASAA2013072395664Overheat Sys · no testNR 2 ENGINE OVERHEAT LIGHT DOES NOT ILLUMINATE DURING TEST. ACFT GROUNDED.SDR ASAA2013072095639Overheat Sensor · failedAFTER TAKE OFF WITH APU OFF. RECEIVED AN OVERHEAT DETECTOR AND WITH APU DETECTOR INOPERATIVE LIGHT. RETURNED TO DEPARTURE. ACFT GROUNDED. VERIFIED FAULT. REPLACED APU TAIL PIPE OVERHEAT DETECTOR ASSY WITH SERVICEABLE ONE. ACCOMP APU FIRE DETECTION OPS TESDR UALA2013071504952Switch · malfunctionedFWD EQUIPMENT OVERHEAT LIGHT, RETURNED TO FIELD. R & R OVERHEAT SWITCH S0041 & RELAY K626 IAW AMM 21-58-26, OPS CHECKED GOOD.SDR AALA20130713006Sensor · faultyTAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED ON CLIMB OUT. REPLACED RT & LT TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL.SDR ASAA2013071295578Detector · looseNR 2 ENGINE OVERHEAT ILLUMINATED ON GROUND. ASSOCIATED CONDITIONS WHEN OVHT DET SWITCH PLACED TO A LIGHT EXTINGUISHED AND FAULT ILLUMINATED. WHEN OVHT DET SWITCH PLACED TO B ENG 2 OVERHEAT REMAINS ILLUMINATED. WHILE ON DEFERRAL, ON THE FOLLOWING FLIGHT SITTISDR AALA20130710008Sensor · faultyLT STRUT DUCT LEAK MESSAGE & LIGHT DURING CLIMB OUT. REPLACED LT PYLON STRUT OVERHEAT SENSOR TS236. SYSTEM GROUND CHECKED NORMAL.SDR UALA2013071104842Warning Message · illuminatedCREW REPORTED NR 2 BLEED OVERHEAT PRV EICAS DISPLAYED.SDR AALA20130705011Duct · damagedTAIL COMPARTMENT TEMPERATURE HIGH, LIGHT ILLUMINATED. REPLACED DUCT & BOTH OVERHEAT SENSORS. SYSTEM GROUND CHECKED NORMAL.SDR ASAA2013070295447Overheat Sensor · inoperativeAPU DETECTOR INOPERATIVE INDICATOR STAYS ILLUMINATED. ACFT GROUNDED. RESET APU DETECTION CIRCUIT BREAKER. R & R TAILPIPE OVERHEAT DETECTOR ASSY OPS NORMAL. GROUND VERIFICATION GOOD.SDR UALA2013070204636Detector · faultyRT ENGINE OVERHEAD LP 2 STATUS MESSAGE, TROUBLESHOT IAW FIM 26-11-00, FOUND OVERHEAT DETECTOR DAMAGED. REPLACED DETECTOR IAW AMM, OPS TESTED OK, NO FAULTS SHOWING.SDR J7SA2013070302Warning Message · illuminatedRIGHT PYLON OVERHEAT CAS MESSAGE ILLUMINATED ON TAKEOFF. LANDING AND TAXI WERE UNEVENTFUL. OPENSDR CA130705004Warning Light · false activation(CAN) ON CLIMB OUT, THE ACFT EXPERIENCED A NR 2 ENGINE OVERHEAT INDICATION. FOLLOWING THE FOM CREW REDUCED POWER SETTING AND THE OVERHEAT INDICATION REMAINED ILLUMINATED. THE CREW THEN ELECTED TO SHUTDOWN THE ENGINE AT WHICH TIME THE OVERHEAT INDICATION STILSDR N6WA2013062702Overheat Loop · out of positionINTERIGATED MDC AND FOUND BLEED AIR DETECTION LOOP, MT 143 AND MT 205 FAULTY. INSPECTED LOOPS AND FOUND MT205 TOUCHING DUCT INSULATION. REPOSITIONED LOOP MT205 IAW AMM 36-21-03. OP'S AND LEAK CHECKED GOOD AT THIS TIME.SDR AALA20130626022Overheat Loop · inoperativeLT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT. ACCOMPLISHED QRH PROCEDURES & LIGHT EXTINGUISHED. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. REPLACED LT HAND WING OUTBOARD OVERHEAT LOOP. SYSTEM GROUND CHECKED NORMAL.SDR UALA2013062404356Connector · dirtyBLEED LOOP 2 BODY STATUS MESSAGE. NO STATUS MSG DISPLAYED, MESSAGE NOT ACTIVE. HAD PREVIOUS HIT ON LEG 8 16TH JUNE. CLEANED AND RESECURED LOOP INTERFACE CONNECTORS FOR LOOP 2 ZONES 13, 14 AND 15. TESTED REF AMM 26-18-04-401, NO CMC OR STATUS MESSAGES PRESENTSDR UIEA2013061700330Overheat Sensor · failedRIGHT DUCT LEAK LIGHT ON. REPLACED RT PACK BAY OVERHEAT SENSOR IAW AMM 26-18-01-024-005-001 AND TESTED IAW AMM 26-18-00-715-001-002. ALL NOW GOOD, OK FOR SERVICE.SDR ASAA2013061295090Overheat Sensor · false activationNR 1 ENGINE OVERHEAT LIGHT ILLUMINATED AFTER ENGINE START THEN WENT OUT CALLED MC CONTINUED TAXI WITH LIGHT OUT TWO MINUTES LATER NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED AGAIN. ACFT GROUNDED. ACCOMPLISHED TASK 26-11-00-710-801 AFTER COOL AND OPENED BOTH ENG CSDR UALA2013052803675Overheat Loop · shortedBLEED LOOP 2 BODY STATUS MESSAGE DISPLAYED ON EICAS. M LOOP 2, ZONE 18 IS SHORTED. TROUBLESHOT PER FIM 26-18 TASK 804. R & R NR 2 BODY LOOP DETECTOR IAW AMM 26-18-04. OPS CHECKED NORMAL, STATUS MESSAGE CLEARED.SDR ASAA2013052394896Wire Harness · failedDURING PRE-FLT INSPECTION, OVERHEAT/FIRE, ENG 1 OVERHEAT & ENG NR 1 T-HANDLE FAILED TO ILLUMINATE DURING TEST. ACFT GROUNDED. PERFORMED NR 1 ENG FIRE DET LOOP RESISTANCE TEST, RESISTANCE CHECKS OF A AND B LOOPS WITH IN LIMITS, SHOOK DOWN B LOOP OF FAN AND COSDR UALA2013052303590Overheat Loop · shortedTROUBLESHOT LEFT WING LEAK DETECTOR LOOP "B". FOUND SEGMENT 61HF CENTER CONDUCTOR SHORTING TO GROUND. R & R LOOP 61HF IAW, OPS CK GOOD IAW AMM.SDR ASAA2013052294877Warning Light · false activationAFTER STARTING NR 1 ENGINE HAD AND ENGINE OVERHEAT LIGHT ON THE FIRE WARINING PANEL. ALL OTHER INDICATIONS NORMAL, LIGHT EXTINGUISHED AFTER ABOUT 30-40 SECONDS. ACFT GROUNDED. PERFORMED ENGINE AND APU FIRE DETECTION BITE REF AMM 26-10-TASK 801 BITE CHECKED SDR UALA2013052103521Overheat Loop · faultedBLEED LOOP 1 BODY STATUS MESSAGE. REPLACED NR 1 LOOP M26144. ACCOMPLISHED FIRE TEST, NO MESSAGE.SDR UALA2013052103514Circuit Card · failedBLEED LOOP 1 BODY FAILURE OF BODY DUCT LEAK DETECTION LOOP OR LT DUCT LEAK OVERHEAT DETECTION SYS. DISCONNECTED M26143 & M26142 ZONE 13 LOOP SEGMENTS, CLEANED AND RECONNECTED, ALSO REPLACED LEFT DLODS CARD. OPS NORMAL, NO STATUS OR CMC MESSAGES.SDR ASAA2013052094854Overheat Sys · no testNR 1 ENGINE OVERHEAT LIGHT NOT ILLUMINATED DURING TEST. ACFT GROUNDED. PERFORMED OPS TEST OF THE FIRE & OVERHEAT DETECTION SYS IAW MM TASK 26-10-00-710-801. TESTED NORMAL. GROUND VERIFICATION CHECK PERFORMED. OK FOR SERVICE.SDR CA130507002Probe · unknown(CAN) OVERHEAT AND FIRE WARNING LIGHTS WOULD NOT COME ON WITH HEAT TEST OF JANITROL HEATER SYS. FOUND THERE ARE 2 TYPES OF THERMOSTATS THAT CAN BE USED. 1 HAS A CASE GROUND AND ONE HAS NOT.SDR UALA2013050703190Detector Loop · shortedBLEED LEAK, RIGHT WING LOOP 1 ZONE 10 SHORTED, RIGHT WING LOOP 2 ZONE 10 IS SHORTED. FOUND RT PACK HEAT EXCHANGE FLEXIBLE CONNECTOR AND CHECK VALVE DAMAGED. REPLACED BOOT AND CHECK VALVE PER MM, CHECKED OKAY.SDR PCSA2013050601Bushing · missingAT FL 250 LOWER CARGO AFT COMPARTMENT FIRE WARNING ILLUMINATED AND REMAINED ON UNTIL SHORT FINAL INTO NAS. MAINTENANCE REMOVED CARGO FROM AFT COMPARTMENT. INSPECTED CARGO AND COMPARTMENT NO EVIDENCE OF FIRE/SMOKE NOTED. ACCOMPLISHED SMOKE DETECTION TEST IAWSDR UALA2013042502878Controller · malfunctionedEICAS RT WING LOOP 2 MESSAGE FAULT HISTORY LEG 5, SHOWS MESSAGE 26-37043, MESSAGE IS NOT ACTIVE. ACCOMPLISHED RESISTANCE CHECK PER FIM 28-18 TASK 802. RT WING LOOP 2 RESISTANCE TO GROUND IS 1.495K OHMS, AND IS IN LIMITS. THERE ARE NO OTHER EICAS MESSAGES OSDR SWIA201333222Sensor · faultyWING OVERHEAT WARNING MESSAGE. (FLT 4724) APPLIED RTV/SEALANT TO LEFT OVERHEAT/CONTROL SENSOR IAW AMM.SDR AALA20130329020Sensor · shortedMIA - CREW REPORTED LEFT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CRUISE. FLIGHT CREW ACCOMPLISHED QRH CHECKLIST AND THE LIGHT STAYED ILUMINATED. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED SENSOR M1761 THAT HAD SDR SWAA2013032814199Overheat Sensor · faultyDIVERSION -- IN CRUISE LEFT WING-BODY OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED M 761 LEFT AND STRUT OVERHEAT DETECTOR IAW M/M.SDR CA130619003Loop · fractured(CAN) OPERATOR REPORTED AN EXHAUST PIPE OVERHEAT WARNING ON THE LT ENGINE DURING CRUISE FLIGHT. AFM PROCEDURES WERE FOLLOWED, HOWEVER THE OVERHEAT WARNING DID NOT GO OUT. PILOT ELECTED TO SHUTDOWN THE ENGINE. ACFT RETURNED TO THE AIRPORT AND LANDED WITHOUT SDR CA130226001Detector · failed(CAN) SHORTLY AFTER TAKEOFF THE CREW REPORTED A BLEED LEAK, RT ENG BLEED INOPERATIVE AND RETURNED TO LAND. NO EMERGENCY WAS DECLARED RT PYLON ODS DETECTORS CH 1 AND CH 2 REPLACED IAW AMM 36-21-02-04. CHECKS SERVICEABLE.SDR N6WA2013022505Overheat Loop · out of positionLEFT BLEED DUCT WARNING MESSAGE. INSTALLED STANDOFFS FOR BLEED LOOP SEGMENTS 139/140 FWD OF LT PRECOOLER IAW AMM 36-21-01. OP'S CHECK OF BLEED LEAK DETECTION SYSTEM IAW AMM 36-21-01. NO FAULTS AT THIS TIME.SDR YYFA20130223001Sensor · failedTAIL CONE OVERHEAT LIGHT ON AT 220 DEGREES WOULD NOT EXTINGUISH. R & R LT AND RT OVERHEAT SENSORS IAW AMM 36-20-02. OPS CHECKED GOOD.SDR 2013F00052Sensor · malfunctionedTAIL CONE OVERHEAT LIGHT ON AT 220 WOULD NOT EXTINQUISH, "FLICKERING". R & R LT & RT OVERHEAT SENSORS IAW MM 36-20-02. OPS CKD GOOD.SDR 2013F00050Sensor · inoperativeTAIL CONE OVERHEAT LIGHT ON AT 220, WOULD NOT EXTINQUISH FLICKERING. R & R LT & RT OVERHEAT SENSOR IAW MM 36-20-02. OPS CKD GOOD.SDR 2013F00040Sensor · intermittentTAIL CONE OVERHEAT LIGHT ON AT 220, WOULD NOT EXTINQUISH, FLICKERING". R & R LT & RT OVERHEAT SENSOR IAW MM 36-20-02. OPS CKD GOOD.SDR 2013F00049Sensor · intermittentTAILCONE OVERHEAT LIGHT ON AT 220, WOULD NOT EXTINQUISH FLICKERING. R & R LT & RT OVERHEAT SENSOR IAW MM 36-20-02, OPS CKD GOOD.SDR YYFA2013F00067Sensor · inoperativeTAILCONE OVERHEAT LIGHT ON AT 220, WOULD NOT EXTINQUISH "FLICKERING". R & R LT & RT OVERHEAT SENSOR IAW MM 36-20-02. OPS CKD GOOD.SDR N6WA2013022102Insulator · damagedLT BLEED DUCT MASTER CAUTION MESSAGE. FOUND DAMAGED CERAMIC INSULATOR AT JUNCTION BETWEEN MT 139 AND MT 202. R & R SAID ISOLATOR IAW CMM 26-14-14. OPS CHECK FOR LOOP "A" ONLY GOOD.SDR N6WA2013022101Overheat Loop · out of positionLEFT BLEED DUCT MASTER WARNING. FOUND LOOP MT 137 RESTING ON A HOT AIR DUCT, REPOSITIONED AWAY FROM DUCT. OP'S CHECKED GOOD IAW AMM 36-21-00. ALSO, CHECKED DUCTING FOR LEAKAGE, NONE FOUND. RAN AIR BLEED OF ENGINE 1 AND /OR APU WITH NO FAULTS NOTED.SDR UALA2013021901008Light · no testRIGHT ENGINE OVERHEAT DOES NOT TEST, NO LIGHT. REPLACED RIGHT ENGINE OVERHEAT LIGHT ASSY BASE.SDR ASAA2013020293796Overheat Sys · malfunctionedCAPTAIN SIDE ON 6 PACK MASTER CAUTION OVERHEAT DETECTOR WILL NOT ILLUMINATE ON FIRE FAULT INOPERATIVE OR OVERHEAT FIRE SELF TEST. ACFT GROUNDED. ACCOMPLISHED MASTER CAUTION DISPLAY TROUBLESHOOTING IAW FIM TASK 31-52-00-810-802. RECYCLED OVERHEAT DETECTION MSDR ASAA2013013193799Warning Light · illuminatedLEFT OVERHEAT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. FOUND LT SIDE WINDOW HEAT C/B P18-3 D3 OUT. RESET CIRCUIT BREAKER IAW AMM 20-60-01. OPS CHECKED LT SIDE WHCU IAW AMM 30-41-11. ALL OPS CHECKED NORMAL. RANG OUT SENSOR IAW AMM 30-41-21 RANG OUT GOOD. ALSDR N6WA2013013001Warning Light · false activationANTI-ICE DUCT WARNING MESSAGE ON TAKEOFF, PERFORMED OPS CHECK OF BLEED LEAK, DETECTOR AND WARNING SYS, NO DEFECTS NOTED, IAW AMM 36-21-00. PERFORMED OP'S CHECK OF WING ANTI-ICE SYS, NO DEFECTS NOTED IAW AMM 30-12-00.
Back to JASC 2613