JASC 2697
Service difficulty reports · 1,399
Reports filed under 2697 · Fire Protection System Wiring, 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 = '2697' 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 = '2697' 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 ASAA2015100413320Wire Harness · damagedFOLLOW-UP TO RECENT HISTORY WITH NR 2 ENG FIRE WARNING LOOP A TEST FAIL. ACFT GROUNDED. R & R MWO325 IAW MM 26-11-02, OPS CK NORMAL. TSR CLOSED.SDR CA151005001Wire · chafed(CAN) AIRCRAFT DECLARED AN EMERGENCY AFTER SHUTTING DOWN NR 1 ENGINE IN FLIGHT AFTER ENGINE FIRE WARNING LIGHT. CREW BLEW THE 2 FIRE EXTINGUISHER BOTTLES, BUT LIGHT REMAIN ON. THE PLANE LAND SAFELY. MAINTENANCE FOUND FIRE WIRE P/N D1384N TO BE THE FAULT. THEYSDR ASAA2015092913280Wire Harness · failedNR 2 FIRE HANDLE NOT ILLUMINATING ON TEST. ACFT GROUNDED. REPLACED MW0325 HARNESS, OPS CK NORMAL REF MM 26-11-00.SDR FDEA201509122852Wire · damagedDURING PREFLIGHT, NR 2 ENGINE, AGENT 1 INDICATES DISCHARGED. REMOVED CONNECTOR FROM DISCHARGE HEAD & REMOVED BONDING WIRE IAW AMM 26-21-15-04. REPLACED WIRES DK20-50, DK16-61 & DK16-62 IAW WDM 26-21-03 & ESPM 20-53-31.SDR ASAA2015090912992Wire Harness · chafedDURING FIRE TEST, ENGINE NR 2 LOOP A INOPERATIVE. ACFT GROUNDED. FOUND ENGINE NR 2, LOOP B TESTING GOOD. FOUND ENGINE NR 2 LOOP A FAN UPPER DETECTOR FAULT CYCLED SHIP POWER FAULT DID NOT RETURN DETERMINED TO BE INTERMITTENT FAULT IAW FIM 26-10, TASK 805. TESDR ASAA2015090512935Terminal · brokenNR 2 ENGINE WIRE HARNESS HAS A BROKEN TERMINAL LUG. ACFT GROUNDED. REPLACED TERMINAL LUG AT NR 3 DETECTOR OF MW0325 ON NR 2 ENGINE, REF MM 26-11-02. ENGINE FIRE DETECTION, OPS TEST NORMAL, REF MM 26-11-00.SDR HEER20150904696Wire Harness · not reportedNR 2 ENGINE FIRE LIGHT ILLUMINATED WITH AUDIO, NUMEROUS TIMES DURING TAKEOFF, CRUISE AND LANDING. REPLACED OTBD FLAME DETECTOR HARNESS ASSEMBLY.SDR FDEA201508262700Connector · defectiveINTERMITTENT LEVEL 2, ENG 1 LOOP A, ALERT DURING FLIGHT. ALERT HAPPENED AT ALL FLIGHT LEVELS & WOULD LAST APPROX 15 SECONDS. IAW WMD 26-11-01 R & R MOD BLOCK S3-529 16BA BX. IAW WDM 26-11-01 02 03 & THE HOOKUP CHART R & R CONNECTOR P1-9952.SDR FDEA201508262699Connector · defectiveINTERMITTENT LEVEL 2, ENG 3 LOOP AN ALERT DURING FLIGHT. REPEAT WRITE UP. ALERT HAPPENED AT ALL FLIGHT LEVELS & WOULD LAST ABOUT 15 SECONDS, DID NOT ALERT AT THE SAME TIME AS THE NR 1. IAW WMD 26-11-01 R & R MOD BLOCK S3-529 16BA BX. IAW WDM 26-11-01 02 03SDR JJBA20150822003Connector · disconnectedLAVATORY SMOKE DETECTOR WILL NOT TEST. FOUND CONNECTOR LOOSE.SDR ASAA2015081912950Wire Harness · brokenFAULT INOPERATIVE, OVERHEAT FIRE EXT TEST INOPERATIVE NR 2 ENGINE. ACFT GROUNDED. FAULT INOPERATIVE WAS FOR B LOOP, FOUND BROKEN WIRE AT TERMINAL FOR UPPER DETECTOR REF WDM 26-11-11 & 26-11-21. RE-TERMINATED NEW LUG REF SWPM 20-30-11. ENGINE FIRE TEST NORMASDR WX0A2015081972821Connector · looseDURING CRUSE THE DSCH LIGHT ILLUMINATED FOR THE CARGO FIRE BOTTLE NR 2. FOUND CONNECTOR TO NR 2 CARGO FIRE BOTTLE PRESS SWITCH P1-53 LOOSE. REMOVED NR 2 CARGO FIRE BOTTLE & WEIGHED IT, FOUND BOTTLE TO HAVE FULL CHARGE. REINSTALLED NR 2 CARGO FIRE BOTTLE IAWSDR AALA20150729001Overheat Loop · chafedDURING CRUISE PILOT REPORTED NUMBER 2 ENGINE OVERHEAT LIGHT ILLUMINATED. DIVERTED AND LANDED UNEVENTFULLY. FOUND NUMBER 2 ENGINE LOOP `A` WIRE CHAFED. R & R RT ENGINE OVERHEAT LOOP. PERFORMED OPERATIONAL CHECK IAW AMM 26-11-02. SYS CHECKED NORMAL.SDR ASAA2015070912385Wire Harness · failedDURING FIRE WARNING TEST, NR 1 TEE HANDLE AND NR 1 ENGINE OVERHEAT LIGHT FAILED TO ILLUMINATE. ACFT GROUNDED. REPLACED CORE HARNESS IAW MM 26-11-02. GROUND VERIFICATION TEST PASSED.SDR ASAA2015053011904Wire Harness · brokenNR 1 OVERHEAT TEST SYSTEM, FAULT IN B LOOP. ACFT GROUNDED. DUPLICATED DEFECT. FOUND NR 1 ENGINE LT CORE UPPER TERMINAL END BROKEN. REPLACED NR 1 ENGINE LT CORE MW0326 B LOOP FIRE DETECTOR HARNESS, REF MM:26-11-02, OPS CK NORMAL.SDR VE7A2015051800001Connector · dirtyDURING CRUISE FLIGHT, NR 2 ENG FIRE LIGHT & TONE CAME ON, MUTED TONE & BOTH WENT OUT, ONLY TO COME ON LATER, RETURNED TO LOCATION. RELEASED TO MX, INSPECTED & CLEANED PLUGS ON ALL FIRE DETECTORS. PERFORMED FIRE DETECTION SYS CHECKS & COULD NOT DUPLICATE.SDR ASAA2015042711542Terminal · damagedFIRE TEST "B" LOOP ON NR 2 ENGINE DOES NOT TEST. ACFT GROUNDED. REPAIRED DAMAGED TERMINAL LUG FOR THE "B" LOOP ON THE UPPER RT CORE DETECTOR IAW AMM 26-11-02-960-802. ENGINE FIRE DETECTION, OPS TEST GOOD IAW AMM 26-11-00-710-801.SDR ANCF2015042201Connector · looseAFTER START ENG 2 FIRE LOOP A FAULT PRESENTED. PROCEDURE WITH MANTO DIDN´T WORK. FDU 2 SHOWS ON LAST LEG & GND REPORT 261215 ENG 2 FIRE LOOP A & FDU2 IWD2 FAULT NOT PRESENT ON ENG SHUTDOWN. DUE TO PREVIOUS HISTORY ENG 2 FIRE LOOP A DEFERRED INOPERATIVE UNDESDR ASAA2015041811383Terminal · corrodedNR 2 ENGINE, RT CORE FIRE DETECTOR HARNESS AFT TERMINALS CORRODED, MW0326. ACFT GROUNDED. R & R MW 0326 HARNESS ON NR 2 ENGINE IAW AMM 26-11-02. OPS CHECK NORMAL.SDR IPXA2015042588377Connector · no testINSPECTION TYPE:1-3C, NR 2 ENGINE, NR 2 FIRE BOTTLE CONNECTOR NR 25-WE, PIN "A", NO 28VDC PRESENT DURING FIRE BOTTLE DISCHARGE TEST. ON 1584VC CONNECTORS FOUND PIN "N" AND SOCKET "N" DAMAGED. REPLACED PIN AND SOCKET ON PLUG AND JACK CONNECTORS.SDR IPXA2015042588376Connector · no testINSPECTION TYPE:1-3C, NR 2 ENGINE, NR 2 FIRE BOTTLE CONNECTOR PIN "A", NO 28VDC PRESENT DURING THE FIRE BOTTLE DISCHARGE TEST. ON 1584VC CONNECTORS FOUND PIN "N" AND SOCKET "N" DAMAGED. REPLACED PIN AND SOCKET ON PLUCK AND JACK CONNECTORS.SDR UIEA2015041700237Connector · looseSTATUS MESSAGE IN FLIGHT, RT ENGINE FIRE LOOP 1. INSPECTED RT ENG LOOP & FOUND LOOSE CONNECTION AT UPPER LT COWLING. SECURED CONNECTOR, OPERATIONS CHECKED GOOD IAW AMM 26-11-00.SDR CA150410005Wire · damaged(CAN) DURING FLIGHT IT WAS REPORTED THAT THE LT ENG FIRE WARNING LIGHT CAME ON. THE PILOTS PERFORMED AN ENG SHUTDOWN AS WELL AS EMER CHECKLIST. BOTH FIRE BOTTLES WERE ACTIVATED BUT THE FIRE INDICATION REMAINED ON. AN UNEVENTFUL EMER LANDING WAS PERFORMED. SDR ASAA2015040311226Wire Harness · failedNR 2 ENGINE "B" LOOP INOPERATIVE. ACFT GROUNDED. FOUND NR 2 ENGINE "B" LOOP DETECTOR, RT SIDE CORE, OPEN. REPLACED RT SIDE CORE LOOP FIRE DETECTOR IAW AMM 26-11-01-401. ENGINE FIRE OPS TEST GOOD IAW AMM 26-11-00-710-801.SDR QXEA2015031600148Connector · shortedWHEN PEFORMING CAUTION/ADVISORY LIGHT TEST, THE ADVISORY LIGHTS TEST SETS OFF THE "FIRE BELL" AND THE "ENGINE FIRE PRESS TO RESET" RED WARNING LIGHTS. FOUND SHORT ON CONNECTOR PLUG, CONNECTOR 2600-J24 BETWEEN PINS C AND B, R & R CONNECTOR. ALL OPS CHECKS GOOSDR ASAA2015031410948Terminal · brokenTECH SERVICES REQUESTS FOLLOW-UP TO RECENT HISTORY OF APU FIRE/OH DETECT INOPERATIVE LIGHT ON INTERMITTENTLY. ACFT GROUNDED. WHILE CHECKING DETECTOR TERMINALS, FOUND TAIL PIPE DETECTOR TERMINAL POST BROKEN. R & R TAIL PIPE DETECTOR. OPS CK GOOD. REF AMM 26SDR JIKA2015031301Wire · chafedDURING CRUISE ON TRAINING FLIGHT, THE PILOT SIMULATED AN ENG FIRE BY TESTING AMP SIDE OF THE LT FIRE SYS TO ILLUMINATE THE FIRE WARNING T HANDLE. THE RED LIGHTS ILLUMINATED FOR APPROX ONE SECOND & THEN EXTINGUISHED, DESPITE THE SWITCH STILL BEING DEPRESSED. SDR ASAA2015022310752Shield · deterioratedNR 1 ENGINE WIRE HARNESS SHIELD DETERIORATED. ACFT GROUNDED. REPLACED CORE FIRE DETECTION WIRE HARNESS IAW MM 26-11-02. OPS NORMAL.SDR 39LA20150220107Connector · dirtyDURING FINAL APPROACH THE NR 2 ENG FIRE WARNING LIGHT IN THE T HANDLE WAS FLICKERING WITH NO VISUAL SIGNS OF FIRE. CLEANED FORE & AFT ENG DECK FIRE LOOP CONNECTORS IAW MM CHAPT 26-10-3.SDR SIMA20150219004Wire Harness · malfunctionedFIRE SYSTEM FAULT STATUS IN FLIGHT. FOUND BRAIDED HARNESS ON ELEMENT, ADJUSTED HARNESS & ACCOMPLISHED OPS CHECK GOOD IAW AMM 26-10-00.SDR N6WA2015021901Connector · not seatedSMOKE AFT MASTER WARNING. RESEATED AFT LAVATORY SMOKE DETECTOR CONNECTOR. PERFORMED OPERATIONS CHECK IAW AMM 25-16-00. OPERATIONS CHECKED GOOD.SDR LR7A2015020600511Wire · chafedDURING SCHEDULED FLIGHT, APU FIRE LIGHT ILLUMINATED IN FLIGHT. REPAIRED CHAFING WIRE IN APU FIRE DETECTION SYS IAW SMP 581 26-10, OPS CHECK GOOD.SDR IPXA2015020485563Wire · damagedDURING INITIAL DESCENT, RECEIVED AN INTERMITTENT LEVEL 1 FIRE DETECTOR FAILURE, THEN RECEIVED A LEVEL 3 ENGINE FIRE INDICATION. EMERGENCY DECLARED SHUTDOWN ENGINE NR 3. REPAIRED THE TERMINAL AT UPPER LT LOOP A, DH4A AND DH4C IAW SWPM 20-30-11. REPLACED HARSDR 2WAA20150128003Connector · looseFIRE LOOP A, INTERMITTENT LT ENGINE ON. TROUBLESHOT THE FIRE LOOP AND FOUND A B-NUT ON SENSING ELEMENT LOOSE, SECURED THE B-NUT IAW MM 26-10-04, OPS CHECK GOOD IAW MM 26-00-00.SDR HEER20150127725Wire · shortedWHILE OUTBOUND, THE APU FIRE LIGHT ILLUMINATED INTERMITTENTLY. FOUND WIRE FROM CONTROL PANEL GOING TO GROUND SHORTED. REPLACED WIRE W3033F24.SDR HEER20150121717Connector · corrodedAPU FIRE LIGHT AND ORAL WARNING ACTIVATED AND EXTINGUISHED. FOUND PINS CORRODED IN CONNECTOR P457 AT APU FIRE DETECTOR, REPLACED PINS AND CONNECTOR AND COMPLETED FOLLOW MAINTENANCE CHECKS.SDR CA150107007Connector · shorted(CAN) FIRE SYS FAULT CAUTION MESSAGE DISPLAYED AT THE GATE. RESET OK BUT CAME BACK ON WITHIN MINUTES. MAINTENANCE TROUBLESHOOTING AS FOLLOWS. CONTINUITY CHECK FOR LOOP B CARRIED OUT AT FIDEEX CANNON PLUG WITH NO FAULTS FOUND. FOUND 26VDC AT PIN 10, 11 CONNECTSDR HEER20150104676Connector · contaminatedDURING CRUISE FLIGHT NR 2 ENGINE FIRE LIGHT ILLUMINATED. FOUND MOISTURE ON CONNECTORS FOR NR 2 FWD AND AFT FLAME DETECTORS.SDR A6WA201442228Connector · disconnectedRECEIVED SMOKE CAUTION MSG IN FLIGHT WHILE PAX WAS IN LAVATORY. INSPECTED LAVATORY & FOUND NO EVIDENCE OF SMOKE IN LAVATORY. AFTER THOROUGH INSPECTION OF SINK & TOILET ELECTRICAL COMPONENTS. GAINED ACCESS TO LAVATORY SMOKE DETECTOR & FOUND CONNECTOR DISCONNSDR SWIA201440241Wire · chafedLEFT JET OVERHEAT FAIL. REPAIRED CHAFED WIRES TO LT ENGINE LOOP A & LOOP B IAW ESPM. OPS CHECKED FIRE DETECTION SYSTEM - GOOD IAW AMM.SDR ASAA2014112909772Insulation · missingFOUND WIRE HARNESS HAS APPROXIMATELY SIX INCHES OF SHIELDING MISSING ABOUT 3 FEET FROM TERMINAL LUG ON B2 FIRE LOOP, NR 2 ENGINE. ACFT
GROUNDED.SDR ASOA20141124137HConnector · corrodedTHE CREW REPORTED THAT THE LAVATORY SMOKE EICAS MESSAGE KEPT GOING OFF FOR MOST OF THE FLIGHT. MAINTENANCE INSPECTED THE ACFT AND CLEANED CORROSION FROM THE CONNECTOR, OPS TESTED THE SYS WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR R61A201411201198Wire Harness · damagedCREW RECEIVED NR 2 ENGINE FIRE WARNING MESSAGE. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. ACFT REMAINS OUT OF SERVICE.SDR CA141120026Wire · faulted(CAN) LT ENGINE FIRE BELL WENT OFF IN CRUISE. VISUALLY CONFIRMED FALSE INDICATION. LANDED, MAINTENANCE CONFIRMED FAULTY FIRE WIRE, SYS TESTED AND SERVICEABLE.SDR ASAA2014111509669Connector · brokenNR 2 ENGINE FIRE DETECTION SYS DOES NOT TEST PROPERLY. ACFT GROUNDED. T/S AND FOUND LUG BROKEN OFF OF RT SIDE FIRE DETECTOR ENGINE CORE. REPLACED LUG IAW SWPM REF 20-30-11. PERFORMED FIRE AND OVERHEAT DETECTION SYSTEM/OPS TEST IAW AMM REF 26-10-00-710-801, SDR ALGA1110201433982Connector · dirtyDURING ACFT RUN UP AFT BAGGAGE COMPARTMENT SMOKE LIGHT ILLUMINATED. CLEANED SMOKE DETECTOR CONNECTOR OPERATIONS CHECKED SYS, SYS CHECKED GOOD.SDR ASOA2014102811525Connector · damagedFIRE SYSTEM FAULT STATUS MESSAGE MDC REPORTS LT ENGINE FIRE LOOP B OPEN. FOUND PUSHED BACK CONTACT ON CONNECTOR J551 PIN EE R & R CONTACT IAW ESPM 20-16-43, FIRE SYS FAULT IS GONE, COMPLIED WITH OPS TEST OF THE FIRE EXINGUISHER SYSTEM IAW AMM 21-10-00-710-80SDR DALA2014101305504Terminal · brokenAIR TURNBACK DURING CLIMB, THE NR 1 ENGINE FIRE INDICATION LIGHT ILLUMINATED WITH ALARM BELL. ACFT RETURNED TO DEPARTURE. MAINTENANCE REPLACED COCKPIT FIRE PANEL AND FIRE DETECTION CONTROL MODULE. FOUND TERMINAL BROKEN ON HARNESS MW0316 REPLACED SAME. REPSDR JIKA2014093002Wire · brokenEN ROUTE PILOT NOTICED THE RT OVERHEAT CB POPPED & WOULD NOT RESET. PILOT PERFORMED PRECAUTIONARY PROCEDURES & PERFORM IN FLIGHT SHUTDOWN OF RT ENG & ENG SECURING CHECKLIST ITEMS. PILOT DECLARED AN EMER & LANDED AT WITHOUT FURTHER INCIDENT. TROUBLESHOOTING SDR REXA2014092801005Connector · looseLAVATORY SMOKE DETECTOR NOT TESTING. FOUND ELEC CONNECTOR LOOSE. RECONNECTED ELEC CONNECTOR IAW AMM 26-16-01. OPERATIONS CHECKED GOOD. OK TO CONTINUE.
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