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 UIEA2021042601004Stud · brokenSTATUS MESSAGE R ENG FIRE LOOP 1(<P>TRANSFERRED TO MDDR 145950 IAW MEL 26-11-01-01, CAT C.</P><P>LOG PAGE 1465432: REMOVED AND REPLACED UPPER AFT FIRE LOOP DETECTOR PER B767 AMM 26-11-02 DURING REMOVAL OF UPPER AFT FIRE LOOP FOUND BROKEN STUD ALSO TERNIBAL WIRSDR ASAA2021042334647Wire Harness · damagedNUMBER 1 ENGINE B FIRE DETECTION LOOP DOES NOT TEST PROPERLY. GROUNDED - YES. PERFORMED B737-800 FIM 26-10 TASK 801 BITE SHOWS NO FAULTS. TEST PERFORMS NORMALLY WITH NO FAULTS. DUE TO HISTORY PERFORMED VISUAL CHECK OF ENG 1 FIRE DETECTION WIRE HARNESS. FOUND HSDR UIEA2021042200962Connector · dirtyR ENGINE FIRE LP 1 MESSAGE(<P>FORWARD TO MDDR 145720 IAW MEL 26-11-01-01, CAT C, DUE 2 MAY 21.</P><P>MIA MX, 23APR, LP 1355451, ITEM M10: ENSURED SECURITY OF TERMNALS ON RT ENG. LOOP 1 RESPONDERS, LOOP RESISTANCE WITHIN LIMITS, NO SHOTS TO GROUND OR INTERMITTESDR FDEA202104090862Wire Harness · failedPDIS 584 26-10 1474 09APR21 MEM OPEN U LOGPAGES:385225 DURING CLIMBOUT FROM PANC 12 MINUTES INTO FLIGHT RECEIVED LEVEL 3 AUDIBLE ENGINE 3 FIRE WARNING. THREE WARNINGS TWO CONSECUTIVE TIMES. NO VISUAL INDICATIONS. ALL ENGINE 3 INDICATIONS NORMSDR ASAA2021032534401Wire Harness · inoperative#2 ENGINE OVHT DET B INOP. GROUNDED - YES. REMOVED AND REPLACED FIRE DET HARNESS IAW B737-800 AMM 26-11-02-000-802 AND AMM 26-11-02-400-802. PERFORMED OPERATIONAL CHECK IAW AMM 26-11-02-040-003 ALSO PERFORMED OPERATIONAL CHECK IAW AMM 26-11-00-710-801.SDR FDEA202103220740Circuit Breaker · trippedAPU FIRE EXT 1 CIRCUIT BREAKER POPPED DURING FLIGHT. REVIEWED AIRCRAFT HISTORY BACK 90 DAYS NO ISSUES WITH APU FIRE EXT 1 CB INSPECTED WITH NO SIGN OF DAMAGE TO CB RESET BREAKER REF GMM 06-1-250, CB REMAINED CLOSED PERFORMED B767 FIM 26-15 FAULT TREE 803 ASDR DXTA022520213861Connector · unsecureFIRE DETECT FAIL L AMBER CAS: FIRE DETECT FAIL AMBER CAS ILLUMINATED FOR ABOUT 10 SECONDS UPON DESCENT INTO COLUMBUS.// SIGN OFF // UPON INITIAL INSPECTION OF LH ENGINE FIRE LOOP CANNON PLUG TO NOT BE FULLY TIGHTENED DOWN. SUSPECT THE LOOSE CANNON PLUG COUPLEDSDR UIEA2021021500314Wire · damagedSTATUS MESSAGE R ENG FIRE LP 2(<P>ITEM PLACED ON DMI 142461 IAW MEL 26-11-01-01. AIRCRAFT RELEASED TO ETOPS 120.</P><P>15 FEB 21 LP 1339197 ITEM 7 - MIA - T/S AS PER FIM 26-11 FT 804, FOUND THE LOWER FWD FIRE LOOP WIRE WITH DAMAGED INSULATION. REPAIRED WIRE ASSDR AALA202102159012Connector · out of positionSMOKE LAVATORY WITH ALARM BUT NO SMOKE DETECTED, LAVATORY 3F2R. REMOVED AND REPLACED SMOKE DETECTOR AT LAVATORY 3F. SMOKE DETECTOR ISSUE STILL EXISTED. **SUPPLEMENTAL REPORT: FOUND CANNON PLUG DISCONNECTED RESEATED AS REQUIRED ON LAV 3F-2R.SDR FDEA202102070298Connector · damagedDURING COCKPIT SET UP/PREFLIGHT & AFTER APU STARTED RECIEVED FIRE WARNING TONE, LWR CARGO FIRE, FLASHING DISCHARGE LIGHTS, PUSHED DISCHARGE, AFTER 2 MIN, STILL FLASHING, PUSH 2ND BOTTLE, CALLED FIRE& MX. EXITED AIRCRAFT. AFTER REPLACEMENT OF BOTTLES FOUNSDR ASAA2021020634060Wire Harness · inoperative#A FIRE LOOP SHOWS FAULT UPON TESTING, #1 FIRE SWITCH DOES NOT ILLUMINATE ON TEST ALSO, OPS NORMAL IN B LOOP. GROUNDED - YES. REMOVED AND REPLACED ENG #1 MW0315 HARNESS REF B737-900 AMM 26-11-02-400-801, OPS NML REF AMM 26-11-00-710-801. MOVED SWITCH TO NORMALSDR ASAA2021020634049Wire Harness · broken#1 FIRE TEST HANDLE DOES NOT ILLUMINATE DURING TEST. GROUNDED - YES. T/S FOUND ENG #1 B LOOP HARNESS MW0326 BROKEN OFF AT 12 OCLOCK POSITION. REMOVED & REPLACED MW0326 HARNESS, INSTALLATION TEST GOOD REF B737-900 AMM 26-11-02/401.SDR UIEA2021020100166Terminal · damaged"L ENG FIRE LP 1" EICAS MESSAGE. TRANSFERRED TO DMI 141760, PER DDG 26-11-01-01 CAT "C" DUE ON 11 FEB 21. REMOVED AND REPLACED LOWER AFT FIRE LOOP AND REPLACED TERMINAL END ON WIRE W5334-001R-16 WDM 26-11-11, IAW SWPM 20-10-13 AND AMM 26-11-02.SDR P5CA2021012800029Connector · looseRT ENGINE FIRE LOOP 1 STATUS MESSAGE DISPLAYED ENGINE FIRE DETECTION SYSTEMS, DETECTION LOOPS (ER RESTRICTED 120). TRANSFERED TO MDDR 141557, IAW DDG 26-11-01-01, CAT C, DD 07FEB21. FOUND LOOSE CONNECTOR AT LOWER LOOP RT SIDE, SECURED CONNECTOR. OPERATIONS SDR ASAA2021011933899Connector · dirtyDURING LL1 FOUND ENGINE 1 FIRE LOOP B SHOWS FAULT. GROUNDED-YES. CLEANED CONNECTORS OF FIRE DETECTION HARNESSES MW0325, MW0326 CHECKED ALL CONNECTIONS. ACCOMPLISHED GVI OF FIRE LOOPS OPERATIONS CHECK NORMAL, REF B737-900 AMM 26-11-00.SDR DALA2021011900334Connector · looseSMOKE ALARMS IN BOTH MID LAVS ACTIVATED AT CRUISE NO SMOKE PRESENT. CORRECTIVE ACTION: INDUCED SMOKE ON AFT, FWD MID LAVS RED LIGHTS ALARM CAME ON. RESET BOTH LAV SMOKE DETECTORS SUCCESSFUL. FOUND CALL LIGHT NOT WORKING WHEN SMOKE WAS INDUCED TO SMOKE ALARMSDR SWAA2021011841522Connector · looseAFT LAV SMOKE ALARM CAME ON DURING ARRIVAL TO APPROACH NO SMOKE/FIRE INDICATIONS. FOUND POWER CONNECTOR LOOSE ON SMOKE DET UNIT. TIGHTENED CONNECTOR PER SIP.SDR ASAA2021010233795Wire Harness · brokenDURING PRE FLIGHT ENGINE FIRE TEST REVEALED FAULT LIGHT. GROUNDED-YES. CW B737-800 FIM 26-10 TASK 805 STEPS F(4)(D). MANIPULATED MW0325 HARNESS. RESISTANCE AT LT CORE LOOP (RIGHT SIDE OF ENGINE) RING TERMINAL ERRATIC WIRE EASILY BROKE OFF WHILE CHECKING. SDR ASAA2021010133796Wire Harness · brokenTECH SERVICE REQUEST. FOLLOW UP TO RECENT REPORT OF NR 1 ENGINE A FIRE LOOP INOPERABLE, REF LOG PG 60007994. GROUNDED-YES. PER B737-800 FIM 26-10 TASK 805. INITIAL EVALUATION. ENGINE FIRE DET OPERATIONS TEST PASS. FIRE DET MODULE BITE TEST PASS. ACCOMPLSDR SWIA202054876Connector · unsecureSMOKE AFT LAV WARNING MESSAGE ON APPROACH AT 7000 FT MSL. RAN QRH HALF OF QRH FOR SMOKE AFT LAV, MESSAGE PERSISTED. NO SIGN OF SMOKE OR FUMES. TROUBLESHOT AFT LAV WARNING MESSAGE, PER SERVICE LETTER, NO DEFECTS NOTED. CONTINUED TROUBLESHOOTING AFT LAV WARNSDR ASAA2020121533695Wire Harness · chafedNR 2 ENGINE FIRE DETECTION WILL NOT TEST IN NORMAL POSITION. WHEN SELECTED TO B LOOP LIGHT REMAINS ON AND WARNING HORN REMAINS ON. A LOOP OPERATIONS NORMAL. GROUNDED-YES. ACCOMPLISHED T/S, PER B737-900 FIM 26-10 TASK 811 - REFERENCE B737-900 IPC 26-11-02-0SDR ASAA2020121433694Terminal · corrodedAPU DET INOPERABLE LIGHT ILLUMINATED AT CRUISE. GROUNDED-YES. REF B737-900 FIM 26-10 TASK 802, PERFORMED INITIAL EVALUATION, ENGINE/APU FIRE DETECTION CONTROL MODULE BITE PROCEDURE, FIM 26-10 TASK 801, NO FAULTS NOTED. REF B737-900 AMM TASK 26-15-01-210-801SDR MASA2020121110647Connector · unsecureBRAKE OVERHEAT WARNING IN FLIGHT, RESECURED BRAKE TEMP CONNECTOR.SDR UIEA2020111702410Connector · damagedNR 1 ENGINE FIRE LOOP 2 STATUS MESSAGE. FOUND PUSHED PIN ON CONNECTOR D4154B. RESEATED PIN 2. OPERATIONS CHECK GOOD, IAW AMM 26-11-01.SDR UIEA2020111202383Wire · shortedLT ENGINE FIRE LOOP 1 STATUS MESSAGE. FOUND SHORT TO SHIELD ON WIRES W 5324-451R-16 AND W5324-452R-16. REPLACED WIRES W5324-451R-16, W5324-452-16, W5324-453R-16, W5324-454R-66, W5324-456R-16. OPERATIONS CHECK GOOD AT THIS TIME, IAW SWPM 20-10-13, SWPM 20-30SDR P5CA2020110500372Wire · damagedSTATUS MESSAGE LT ENGINE FIRE LOOP 1. ITEM DEFERRED, PER MEL 26-11-01-01, CAT C, DUE 15NOV20, MDDR 137250. MTC NOTIFIED. TI 0842 DT. REPLACED TS683 (FWD LOWER DET) TERMINAL DUE TO BROKEN Z. REPLACED WIRE BETWEEN TS 681 AND TS 682 DUE TO RESISTANCE FLUX, ISDR ASAA2020102633439Terminal · looseAS REQUESTED FOLLOW-UP TO REPORT OF NR 1 ENGINE FAULT LIGHT ON FIRE/OH TEST. GROUNDED-YES. ACCOMPLISHED INSPECTION OF NR 1 ENGINE FIRE/OH DETECTORS LOOPS A AND B CONNECTIONS, PER TSR710220. FOUND TWO TERMINALS LOOSE ON HARNESS FOR THE CORE UPPER RIGHT AND CSDR P5CA2020102700364Wire · damagedSTATUS MESSAGE LT ENGINE FIRE LP 1. INSPECTED FIRE DETECTION SYSTEM LOOP. REPAIRED ONE WIRE AND OPERATIONS CHECKS NORMAL. GROUND TEST PASSED, AS PER FIM 26-11 FAULT TREE 804. NOTIFIED MCC.SDR UIEA2020101102215Terminal · damagedLT ENGINE FIRE LOOP 1 STATUS MESSAGE IN FLIGHT FL 320. PERF FIM 26-11 FT 804 SUSPECT AFOLT NR 1 (M10224) CARD AT FAULT. P/N 285N0021-36 ON ORDER. TRANSFERED TO MDDR NR 135892, IAW MEL NR 26-11-01-01, CAT C, DUE DATE 21OCT20. PLACARD INSTALLED. TROUBLESHOTSDR ASAA2020100933340Wire Harness · faultedON PREFLIGHT, NR 1 ENGINE A LOOP FAULT. NO FAULT NOTED ON B LOOP. GROUNDED-YES. ACCOMPLISHED TSR710174, REPLACED ENGINE NR 1 MW0315 AND MW0325 HARNESS, REF B737-900 AMM 26-11-02-400-801 AND REF AMM 26-11-02-400-802. OPERATIONS NORMAL, REF AMM 26-11-00-710-SDR UIEA2020091872015Wire · shortedLT ENG FIRE LP1 STATUS MESSAGE ENROUTE. FOUND WIRES BETWEEN D4230P TS681, TS 682 AND TS683 FIRE LOOPS SHORTED TO SHIELD. REMOVED AND REPLACED WIRES W5324-452R-16, -451R-16, -454R-16, -453R-16, -456R-16, -455R-16 IAW WDM 26-11-11 SWPM 20-10-06. PERFORMED OPSSDR AALA202009119007Connector · unsecureAIRCRAFT WAS NOT GROUNDED. LAVATORY 3F-1R FIRE DETECTOR INTERMITTENT ALARM AND WARNING LIGHT. WILL RESET BUT EVENTUALLY GOES OFF AGAIN. LAVATORY SMOKE DETECTOR UNUSABLE. SUPPLEMENTAL REPORT: FOUND CONNECTOR LOOSE AT DM003 LAV 3F-1R SMOKE DETECTOR. SECUREDSDR ASAA2020090733153Wire Harness · chafedOVERHEAT/FIRE TEST, ENG 1 OVERHEAT DOES NOT LIGHT UP. WHEN SWITCH PUT ON A OR B IT WORKS FOR BOTH. ON NORMAL, THE LIGHT DOES NOT COME ON. FIRE HANDLE ALSO DOES NOT LIGHT UP. WHEN OVHT DETECT SWITCH IS IN POSITION B, ENG 1 FIRE TEST WORKS IMMEDIATELY WITHOUSDR ASAA2020083193110Wire Harness · damagedNR 1 ENGINE MW0326 FOUND DAMAGED DURING ENGINE HARNESS INSPECTION. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENGINE CORE FIRE DETECTION HARNESS MW0326, IAW B737-900 AMM 26-11-02-000/400-802. C/W ENGINE FIRE DETECTION OPS TEST, IAW AMM 26-11-00-710-801. NO SDR UIEA2020081231686Wire · damagedLH ENGINE FIRE LOOP 1 EICAS MSG INTERMITTENT (ENGINE FIRE DETECTION SYSTEMS , DETECTION LOOPS. REPLACED WIRES W5324-452R-16 AND W5324-454R-16 IAW SPM 20-10-11 AND WDM 26-11-11. OPS CKS GOOD IAW AMM 26-11-00.SDR ASAA2020072832943Terminal · looseACCOMPLISHED TROUBLESHOOTING RECOMMENDATIONS PER TSR705030 FOR HISTORY OF #1 ENGINE B LOOP NOT TESTING PROPERLY AND CAUSING DELAYS. RESISTANCE CHECK OF ENG 1 LOOP B FROM CONNECTOR D1002. CHECKS WITHIN LIMITS. REF B737-800 FIM 26-10 TASK 805. RIGHT CORE DETECTOSDR DALA2020072762645Flex Coupling · kinkedON TAKEOFF AROUND 300 AGL RECEIVED EQIP BAY SMOKE FAIL CAUTION MESSAGES. COMPLETED CHECKLIST, RETURNED TO DEPARTURE. FOUND FAULT CODE 2613F0002, EE BAY LOW AIR FLOW SMOKE DET 1&2 ( A238 & A239) DETECT LOW AIR FLOW CH A & CH B. PERFORMED EFIM SOLUTION 2-41919,SDR ASAA2020072722941Connector · corrodedNR 2 ENGINE B SIDE FIRE LOOP WILL NOT TEST. GROUNDED - YES. PERFORMED FIM 26-10, TASK 810. BITE CHECK SHOWS FAULTED ENGINE 2 LOOP B LOW DETECTOR RESISTANCE. CLEANED CONNECTIONS. PERFORMED RESISTANCE CHECK ON ALL FIRE LOOPS ALL RESISTANCE WITHIN LIMITS. FSDR DXTA2020071503866Cable · damagedON SHORT FINAL, THE LT ENGINE FIRE DETECTION LIGHT ILLUMINATED. ABOUT 5 SECONDS LATER THE LT ENGINE FIRE WARNING LIGHT ILLUMINATED FOR ABOUT 2 SECONDS & EXTINGUISHED ON ITS OWN. NO CBS WERE TRIPPED. REMOVED THE UPPER,LOWER & SIDE SKIRT COWLINGS FROM LT ENGISDR MGTY2020062900003Wire · chafedWHILST CARRYING OUT CMP APU FIRE EXTINGUISHING FIRING CIRCUITRY INTEGRITY OPERATIONAL CHECK, SYSTEM FAILED EXTINGUISHING FIRING INTEGRITY CHECK DUE TO BROKEN WIRE ON LT FIRE BOTTLE CONNECTOR 053E1P1. WIRE 2W105H20-4 WAS FOUND TO BE SEVERELY CHAFED THROUGH OUTSDR MGTY2020062900002Wire · chafedCARRYING OUT FIRE BOTTLE CIRCUIT INTEGRITY OPERATIONAL CHECKS, RT FIRE EXTINGUISHER BOTTLE BLUE NR 1 SHOT. CONNECTOR 053E2P1 WIRE 2W106A20N-4 FOUND TO BE CHAFED, AND WIRE 2W102H20-4 FOUND TO BE SEVERELY CHAFED THROUGH OUTER INSULATION, BRAID AND INNER INSULATSDR MGTY2020062900001Wire · chafedWHILST CARRYING OUT FIRE BOTTLE CIRCUIT INTEGRITY OPERATIONAL CHECKS, RT FIRE EXTINGUISHER BOTTLE BLUE NR 1 SHOT. CONNECTOR 053E2P1 WIRE 2W106A20N-4 FOUND TO BE CHAFED, AND WIRE 2W102H20-4 FOUND TO BE SEVERELY CHAFED THROUGH OUTER INSULATION, BRAID AND INNER SDR ASAA2020062942836Ground Wire · brokenNR 1 ENGINE, B FIRE LOOP WAS INOPERATIVE. GROUNDED - YES. PERFORMED FIM 26-10 TASK 801. FOUND NO FAULTS ON BITE OR FROM FIRE LOOP TEST IN FLIGHT DECK. PERFORMED GVI OF THE FIRE LOOPS FOR THE NR 1 ENGINE. FOUND A BROKEN GROUND TERMINAL ON CORE LOOP B. REPSDR P5CA2020062960205Terminal · loose"R ENG FIRE LP 2" STATUS MESSAGE DISPLAYED. CHECKED & FOUND #2 ENG LOWER AFT LOOP 2 TERMINAL LOOSE. TIGHTENED TERMINAL IAW AMM 26-11-00, OPERATIONAL CHECKS OK.SDR ASAA2020061523797Wire Harness · inoperative#2 ENGINE B FIRE LOOP INOP. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE FAN FIRE DETECTION HARNESS MW0316 REFERENCE B737-900 AMM 26-11-02-400-801 AND 26-11-02-000-801. NO HELP. FOUND TERMINAL ON MW0326 BROKEN AT RIGHT HAND CORE FIRE DETECTION ELEMENT. REMOVSDR GZXA2020061200001Connector · chafed14TH STAGE DUCT CAS MESSAGE.SDR FDEA202006111184Wire Harness · faultedDURING CLIMB OUT, NUMEROUS BRIEF ECAM WARNINGS OF NR 2 ENG B LOOP FAULT. ONCE LEVEL AT CRUISE AND POWER REDUCED, WARNINGS STOPPED. CLOSED AND SECURED NR 2 ENGINE FAN, REVERSER AND CORE COWLS IAW MM 71-10-00, RAN NR 2 ENGINE IAW JRH FOR OVER 20 MINUTE'S AND SDR UIEA2020060981241Wire · shortedL ENG FIRE LOOP 1 MESSAGE. PERFORMED FIM 26-11 F/T 805, NO MESSAGES, FAULTS NOTED ON EICAS. CHECKED W/ INBOUND CREW, NO MESSAGES DURING FLT. PERFORMED A BITE OF ENGINE FIRE DETECTION IAW FIM 26-11 F/T 804, NO FAULTS OR MESSAGES NOTED. RE-OPENED DUE TO REPESDR FDEA2020060111092Wire Harness · defectiveDURING CLIMB OUT AT APPROXIMATELY 16,000 FT, NR 1 FIRE LIGHT AND ALERT ILLUMINATED, WENT OUT AFTER 30-40 SECONDS, SEEMS TO HAVE GONE OUT AFTER THROTTLES CAME BACK DURING LEVEL OFF. REMOVED AND REPLACED HARNESS FROM TB2 TO DH5 LUG A IAW AMM 26-11-03-4-1. DUE SDR ASAA2020060132767Wire Harness · damagedFOUND FIRE DETECT HARNESS CA244-02 AND CA243-02 DAMAGED DURING PERFORMANCE OF TASK CARD N8420000. MW0325 AND MW0326 ON NR 1 ENGINE. REMOVED AND REPLACED HARNESS CA243-02 IAW AMM 26-11-02. OPS CHECK GOOD. MNW0325 ROUTED HARNESS MW0326 IAW AMM 26-11-02-400-80
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