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 SWIA2024020800004Connector · not seatedRECEIVED A WING OVERHEAT WARNING MSG AND THEN ANTI ICE DUCT WARNING MSG ON CLIMB OUT FROM DEN, RAN QRH AND IT CLEARED BOTH MSGS. TURNED IT BACK ON AND GOT BOTH MSG AGAIN. DID NOT LAND OVERWEIGHT AND DID NOT DECLARE EMERGENCY. (FLIGHT 4663 FILED CLOSED)THIS DISSDR 2024F00096Wire Harness · faultedENGINE 1 OVERHEAT LIGHT ILLUMINATED DURING CLIMB FRM 261 011 51, CORRECTIVE ACTION: HAS BEEN CHANGED HARNESS NW0325 IN TEST OK.SDR SWIA2024011800007Wire · looseL JET OVHT FAIL CAUTION MESSAGE INTERMITTENT. RAN QRH AND IT DID NOT RETURN UNTIL WE WERE PULLING INTO THE GATE. ONLY APPEARED FOR A COUPLE SECONDS EACH TIME. (FLIGHT 5253 FILED CLOSED)INSPECTED LH JET PIPE DETECTION SYSTEM IN REFERENCE TO AMM 26-11-04. WHILE SDR CALA2024011900156Wire Harness · chafedL ENG FIRE LP 2 EICAS. THE LEFT ENGINE FIRE LOOP 2 HAS A FIRE OR THERE IS A FAILURE OUT PUT. INTERMITTENT STATUS MESSAGE NO EICAS MESSAGE ON ARRIVAL. L ENG LP 2 INTERMITANT DURING CRUISE. TALKED TO CREW, WRITE UP IS IN REFERENCE TO LOGPAGE 6821086. MESSAGE WASSDR HALA20250107008Wire · damagedETOPS - ENG 2 FIRE LOOP A FAULT. WIRING CHECK AT FDU 2A CONNECTOR PIN J TO K 1.5K OHMS. J TO GND 1.5K OHMS. K TO GND 25.3 OHMS. AFTER DISCONNECTED 3015VCA READING CHANGED J TO GND 1.9K OHMS. K TO GND 29.3 OHMS. FOUND WIRE 3K001(B AND R)20 DAMAGED NEAR 3822VC2-SDR FDEA202312141937Unknown · unknownON CLIMB OUT WE GOT AN INTERMITTENT FIRE DET 2 FAULT AND AN INTERMITTENT FIRE INDICATION ON #2 ENGINE INCLUDING FIRE WARNING BELL AND RED LIGHTS IN #2 FIRE HANDLE AND #2 FUEL LEVER. FIRE INDICATIONS HAPPENED TWICE AND LASTED ABOUT 1 SECOND. ALL ENGINE INDSDR HYIA20231206002Unknown · unknownPILOT REPORTED COMBUSTION HEATER FIRE CAS MESSAGE ON IN FLIGHT. MAINTENANCE INSPECTED AND FOUND SHORTED WIRE FWD ON INSTRUMENT PANEL FROM PIN K AT AML CONNECTOR. REPAIRED WIRE WITH NO FURTHER DEFECTS NOTED.SDR U0GA20231122865Connector · dirtyAPU FIRE WARNING LIGHT AND AUDIO CAME ON TWICE DURING IN FLIGHT START OF APU BEFORE LANDING. EACH TIME IT CAME ON WAS ONLY FOR A BRIEF TIME, AND AFTER REDUCING SPEED TO 120 KNOTS IT STAYED OUT. EOP CHECKLIST CONSULTED AND IT APPEARED TO BE SPURIOUS INDICATIONSSDR ASAA2023103045916Wire Harness · damaged#1 ENGINE FIRE LOOP B INOP. GROUNDED - YES. (RESOLVED ON W/O: 1975101 TASKCARD: N/R-00002 ) PERFOMRED FIM 26-10 TASK 801 AND FOUND FAULT ENGINE 1 LOOP B LEFT CORE FAULT. PERFOMRED ELECTRICAL TESTS IAW FIM 26-10 TASK 805. FOUND HIGH RESISTANCE. PERFOMRED GVI OFSDR ASAA2023100645503Wire Harness · damaged#1 ENG MW0316 HARNESS HAS DAMAGE ON WIRE CONNECTING TO OUTBD FAN, TOP OVERHEAT ELEMENT AT FWD CONNECTION. GROUNDED - YES. PARTIALLY REMOVED #1 EMGINE MW0316 HARNESS REF MM 26-11-02-000-801.TWO CB'S PULLED AND TAGGED. R.CANNON 53815 10/06//2023. REMOVED #1 ENGISDR UIEA2023100700891Wire Harness · unknownENG 3 FIRE LOOP A & B FAILED(<P>R/R UPPER & LWR AFT DETECTOR ASSY IAW AMM 26-11-02. R/R HARNESS 61B45322 IAW AMM 26-11-02. R/R HARNESS WIRE AND ENG IDLE TEST RUN NORMAL IAW AMM 71-00-00. PERFORMED OPS CHECK, NO FAULTS FOUND FOR ENG 3 FIRE LOOP.</P>)SDR SWAA2023090897876Circuit Breaker · overheatedCREW REPORTS: FIRE WARN LIGHT ON GLARESHIELD ILLUMINATED NEXT TO MASTER CAUTION LIGHT WHEN MASTER CAUTION ILLUMINATED. NO OTHER OVERHEAT OR FIRE WARNING INDICATIONS<[01] RESET C/B?S RELATED TO MASTER CAUTION AND OVERHEAT/FIRE WARNING SYSTEM. ALL CHECKS NORMAL.SDR ASAA2023061743609Wire Harness · failed#1 ENG. OVERHEAT AS AUTOTHROTTLES MOVED TO MAXIMUM. WENT OUT IMMEDIATELY WITH POWER REDUCTION. EXISTING MEL HAD ONLY LOOP B ON OVRHT DETECTOR SELECTED. GROUNDED - YES. REF. B737-900 WDM 26-11-11 PG 1 SHT 1, WHILE OHMING OUT CORE DETECTORS AND SHAKE DOWN OF CORSDR 2023F00204Wire Harness · brokenON ARRIVAL INTO HOU AFTER LEVELING AND THE THRUST LEVERS ADVANCING THE EICAS, AURAL WARNINGS, RH ENGINE FIRE PUSH, AND FIRE BOOTLE SWITCH LIGHTS ALL ILLUMINATED AND GAVE THE INDICATION OF THERE BEING A FIRE ON THE #2 ENGINE. RETARDING THE THRUST LEVERS CAUSED SDR ASAA2023061543610Wire Harness · failedENGINE #1 A OR B FIRE LOOP WONT TEST. GROUNDED - YES. VERIFIED - REF. ASA L/P 60588323, WHILE T/S B LOOP, FOUND "A" LOOP OPEN AT CORE HARNESS MW0325. REF. B737-900 AMM 26-11-02, REMOVED/REPLACED #1 ENG. CORE DETECTOR HARNESS MW0325, INSULATORS AND CLAMPS. OPS SDR CALA2023060501756Circuit Card · unknownL ENG OH LP 1 STATUS MSG REPLACED LH OH CARD M10229 IAW AMM 26-10-01. CHECKED LOOP ROTABLE PARTS CHANGE WAS INDICATED - TT # 1461416 SN OFF 1161 RESISTANCE IAW FIM 26-11-802 (1500 OHMS), AND CHECKED CONTINUITY IPC REFERENCE # 26-11-00 OF WIRE HARNESS W3366 IASDR ASAA2023051043221Harness · chafedENG #1 FIRE LOOP "B" INOP. GROUNDED - YES. REMOVED AND REPLACED CORE FIRE DETECTOR HARNESS MW0326 REF B737-900 AMM 26-11-02.SDR AALA202304286543Circuit Breaker · trippedAIRCRAFT WAS NOT GROUNDED: CARGO FIRE DETECTION FAILED, DETECTOR FAULT. RESET CIRCUIT BREAKER. TESTS GOOD. IN ACCORDANCE WITH AMM 26-10-00.SDR ASAA2023013041752Harness · faultyENG #2FIRE DETECTOR WONT TEST CERT # TSAR174M. GROUNDED - YES. PERFORMED ENGINE DETECTION BITE TEST REF. FIM 26-10 TASK 801 FOUND #2 ENGINE UPPER FAN LOOP B FAULT. OPENED #2 ENGINE FAN COWLS FOUND BROKEN TERMINAL END ON UPPER FAN HARNESS. REPLACED FAN HARNESS SDR HALA2023013000017Wire Harness · faultedETOPS-DURING INTIAL TAXI ECAM ENG 1 FIRE LOOP A FAULT. INDICATED BTD. FOUND FWD AGB FIRE DETECTOR SHORT TO GROUND. REMOVED AND REPLACED FWD AGB FIRE DETECTOR PER AMM 26-12-17. NO FAULTS NOTED OK FOR SERVICE. REMOVED AND REPLACED FIRE HARNESS ASSY ( 4165KS) PERSDR HALA2023011900010Wire Harness · out of limitsETOPS-ENG B FIRE LOOP ON ECAM. CHECKED RESISTANCE BETWEEN PINS J-K AT FDU 2 LOOP B. FOUND RESISTANCE FLUCTUATING FRANTICALLY OUT OF LIMITS WHILE TAPPING HARNESS 4166KS. REMOVED & REPLACED HARNESS 4166KS PER AMM 26-12-62. RESISTANCE STAYED SOLID AT 1.5K OHMS. ESDR 2023F00031Connector · corrodedEMERGENCY BATTERY OVERHEAT INDICATION IN FLIGHT.SDR CALA2023011300105Terminal · corrodedFIRE APU INSPECTED APU COMPARTMENT FOR SIGNS OF FIRE DAMAGE AS PER AMM REMOVED APU FIRE BOTTLE IAW AMM 26-22-01 DUE TO APU FIRE 49-11-00-200 .FOUND NO EVIDENCE OF FIRE DAMAGE. REMOVED 2 WIRES 00-0609-3-7030, & 40-0366-3-0263, 00-0609-3-6950. BETWEEN DETECTOSDR DALA2023010900119Connector · damagedDIV TO LAX DUE TO LEFT DUCT LEAK CAUTION AND INDICATION. REMOVE AND REPLACED THE CONNECTOR D10648 IAW SWPM 20-62-14 HOUSING ASSY AND END CAP. INSTALLED CONNECTOR D10648 WITH ADHESIVE INSTALLED L/E PANEL. PERFORMED WING AND BODY DUCT LEAK TEST, OPERATES SATIS.SDR DXTA2023010377410Terminal · dirtyLEFT JETPIPE OVERHEAT. WARNING ACCOMPLISHED CHECKLIST ITEMS . RECIEVED THE WARNING LIGHT TO GO OUT TWICE THIRD TIME WOULD NOT GO OUT. PROCEEDED TO INFLIGHT ENGINE SHUT DOWN CHECKLIST. DIVERTED TO KAMA. GAINED ACCESS TO SENSING ELEMENT A2E2, CHECKED RESISTANCSDR 4DPA2022121500001Wire · damagedCREW REPORTED E2 FIREDET FAIL EICAS MESSAGE AFTER TAKEOFF. RETURN TO BASE AND EICAS MESSAGE EXTINGUISHED ON SHORT FINAL. MX TROUBLESHOT TO DAMAGED WIRE W102-1396-24 IN WIRE HARNESS 102. REPAIRED WIRE, OPS TESTED AIRCRAFT IN GROUND AND IN AIR CONFIG ALL OPS TSDR 4DPA2022121400001Wire Harness · damagedCREW REPORTED DURING TAKEOFF WE RECEIVED A E2 FIREDET FAIL MESSAGE THEN IT WENT AWAY. THE MESSAGE CAME BACK LATER AND WE RAN THE QRH AND THEN THE MESSAGE REMAINED UNTIL WE WERE SHORT FINAL AND TURNED THE APU FOR A RETURN TO BASE. MX TROUBLESHOT TO BAD ENGINE WSDR FDEA202212062879Fire Loop · shortedON DEPARTURE FROM MEM, PASSING 13,000, NR 2 ENGINE FIRE WARNING. ACCOMPLISHED RED ECAMS SHUTTING NR2 ENGINE DOWN. ABNORMAL GREEN & YELLOW HYD INDICATIONS. AFTER BOTH FIRE BOTTLES FIRED, CONTINUED TO HAVE NR 2 FIRE WARNING. DECLARED EMERGENCY AND RETURNED TO MSDR ASAA2022120141006Wire Harness · faultedOVERHEAT DETECTION LOOP A SHOWS A FAULT. GROUNDED - YES. PERFORMED B737-800 FIM 26-10 TASK 805. MW0325 HARNESS BAD. REMOVED AND REPLACED ENGINE 1 CORE FIRE DETECTION HARNESS MW0325 REF B737-800 AMM REF 26-11-02/401. ENGINE FIRE DETECTION OPS TEST OK. ETOPS GROSDR YENA2022120201190Cable · failedFLT#8640, JFK-JFK. (ETOPS) 'ENG 1 FIRE LOOP A FAULT THROUGH 2,000' MSL; REMOVED AND REPLACED #1 ENG HIGH TEMP CABLES 4181KS (GREEN/WHITE) AND 4182KS (BLUE/RED) IAW AMM 26-12-61. ALSO REMOVED AND REPLACED #1 ENG HARNESS 4165KS IAW AMM 26-12-61. OPS TEST GOOD.'SDR ASAA2022111940906Wire Harness · faultedENGINE 1 A LOOP INOP. GROUNDED - YES. REMOVED AND REPLACED MW0315 AND MW0325 HARNESSES IAW AMM 26-11-02. GROUND TEST GOOD.SDR ASAA2022111040742Wire Harness · failed#2 ENGINE FIRE TEST DID NOT ILLLUMINATE. GROUNDED - YES. REFERENCE TSR 713386 REMOVED & REPLACED MW0326 AND ETOPS GROUND VERIFICATION PASSED REF B737-800 AMM 26-11-02/401.SDR ASAA2022110640666Wire Harness · brokenFIRE TEST ENG 1 B SIDE FAULT DURING TEST. GROUNDED - YES. REMOVED AND REPLACED MW0316 FAN FIRE DETECTION HARNESS REF B737-800 AMM 26-11-02/401.SDR HNAA2022103100296Connector · dirtyLAV SMOKE MASTER WARNING DISPLAYED AND AUDIBLE ON TAKE OFF. UNABLE TO DUPLICATE ISSUE. INSPECTED #2 DAU AND FOUND THE CONNECTOR GUNKED. CLEANED CONNECTOR AND R+R DAU IN REF TO AMM 31 14 01. ALSO R+R LAV SMOKE PANEL AS PREVENTATIVE MX IN REF TO AMM 26 14 02.SDR ASAA2022092840123Wire Harness · damagedENG 2 FIRE DETECTION LOOP B IS INOP. GROUNDED - YES. REPLACED CORE FIRE DETECTION HARNESS MW0326 ENG #2 REF B737-900 AMM 26-11-02-400-802. OPERATIONAL TEST OK REF AMM 26-11-00-710-801.SDR 9JLA2022081132664Pcb · defectiveTHE MAINTENANCE TEAM DISCOVERED DURING PREFLIGHT CHECKS THAT THE APU FIRE LED LIGHT WAS INOP DURING APU FIRE TEST. THE SYSTEM FAULT WAS DEFERRED UNDER MEL 49-20-01 AND OPERATIONS WERE CONTINUED UNTIL MAINTENANCE COULD BE SCHEDULED. THE MAINTENANCE PROVIDER TRSDR ASAA2022041638038Wire Harness · damagedREF TASK CARD N8420001. DURING INSPECTION OF RIGHT ENGINE HARNESSES, FOUND HARNESS MW0325 SHIELDING TORN. GROUNDED - YES. REMOVED AND REPLACED MW0325 FIRE DETECTION HARNESS ON RIGHT ENGINE IAW B737-900 AMM 26-11-02. OPERATIONAL TEST GOOD IAW AMM 26-11-00-710-8SDR ASAA2022040737920Wire Harness · broken#1 ENGINE FIRE DETECTION HARNESS MW0315 HAS BROKEN TERMINAL LUG AT FAN UPPER FIRE DETECTOR ASSY. GROUNDED - YES. REPAIRED TERMINAL LUG AT FAN UPPER FIRE DETECTOR ASSY ON MW0315 HARNESS #1 ENGINE OPS CHECK GOOD REF B737 SWPM 20-31-11 AND B737-800 AMM 26-11-00-7SDR P5CA2022032800108Wire · brokenAPU FIRE DETECTOR LOOP A (W0906) WIRE FOUND BROKEN AT L/H AFT APU COMPT(<P>WIRE REPLACED BUT BEN-HAR SLEEVE TEMPOARY REPAIRED AS PER <SPAN>BOEING RDR NO.HKA-PAO-22-0028-07B</SPAN></P>)SDR ASAA2022032137733Harness · deterioratedREF T/C N8420001 RT ENGINE HARNESS INSP FOUND CORE FIRE DETECTION HARNESS MW0326 BRAID OVER DETECTOR MOSTLY MISSING AND RUBBER INSULATORS BADLY DETERIORATED. GROUNDED - YES. REF B737-900 AMM 26-11-02, REMOVED/REPLACED MW0326 CORE FIRE DETECTOR HARNESS. OPS NMLSDR ASAA2022020537361Wire Harness · faultedFIRE DETECTION SYSTEM #2 ENGINE FIRE LOOP B FAULT. GROUNDED - YES. REMOVED AND REPLACED CORE FIRE DETECTION HARNESS IAW B737-900 AMM 26-11-02 AND #2 ENG "B" LOOP OPS NML.SDR AC2A202202039201Connector · damagedPILOT REPORT IN FMR - #1 ENGINE FIRE LIGHT ILLUMINATED WITH NO SECONDARY INDICATIONS. PILOT REPORT IN OPERATOR AOCR - DURING CRUISE FLIGHT ENGINE 1 FIRE LIGHT INTERMITTENTLY ILLUMINATED THEN EXTINGUISHED. MAINTENANCE REPORT IN FMR - UPON RETURN TO BASE #1 ENSDR AWKA202201190031Connector · damagedON TAKEOFF, DURING GEAR RETRACTION, FLIGHT CREW RECEIVED A WING ANTI ICE LEAK WARNING MESSAGE. A FEW SECONDS LATER THE WARNING MESSAGE WENT AWAY AND THEN THEY RECEIVED L WING ANTI ICE FAIL, R WING ANTI ICE FAIL, & L WING A/I PRESS HI CAUTION MESSAGES AND L ENGSDR ASAA2022011437138Wire Harness · faultedNUMBER 2 ENGINE B FIRE LOOP INOPERATIVE. GROUNDED - YES. REMOVED AND REPLACED ENGINE FIRELOOP HARNESS MW0316 AND CORE HARNESS MW0326 REF B737-800 AMM 26-11-02 AND PERFORMED OPS CHECK EVERYTHING GOOD GROUND VERIFICATION SUCCESSFUL.SDR HALA2022011100009Wire · damagedETOPS - DURING INSPECTION OF ENG. 2 FIRE LOOP A FOUND WIRE # 3A001B (R) 20 DAMAGED (N1 SPEED PROBE 4087KS1). REMOVED AND REPLACED WIRE 3A001 R20 PER AMM 70-71-24 MK. (502110) 1/10/22. OPERATIONAL CHECK PENDING. OPS TEST OK PER AMM 26-12- 00-710-812-A. OK FSDR ASAA2022010237082Terminal · detachedDURING FIRE DETECTION TEST, ENG #2 FIRE HANDLE DOES NOT ILLUMINATE. ENG# 2 HANDLE ILLUMINATES DURING TEST OF "A" LOOP. GROUNDED - YES. VERIFIED FOUND TERMINAL LUG PULLED OFF WIRE AT CORE DETECTOR. REF. B737-800 AMM 26-11-02, RE TERMINATED A NEW LUG ONTO WIRE. SDR ASAA2021123037045Wire · pulledDURING FIRE TEST A FAULT OCCURRED ON B LOOP. #2 ENG. GROUNDED - YES. BITE TESTED FIRE DET MODULE WITH #2 FIRE DET SW IN NORMAL 2 ENG LOOP B AND ALL 3 FAULT DISPLAY LTS ON ALL THE TIME. SET ENG 2 FIRE DET SW BACK TO LOOP A ONLY LTS WENT OUT. FOUND WIRE PULLEDSDR ASAA2022031237047Contact · dirtyDURING FIRE TEST A FAULT OCCURRED ON THE B LOOP. GROUNDED - YES. PERFORMED ENGINE APU FIRE DETECTION CONTROL MODULE BITE TEST ENGINE 2 LOOP B FAN UPPER DETECTOR FAULT. PERFORMED TEST ENGINE 2 LOOP FIRE DETECTOR, CHECK WAS LUGS, CLEANED, CONTACTS AND REINSTALLESDR FDEA202112213115Control Panel · contaminatedAPU FIRE LEVEL 3 ALERT, MASTER WARNING ILLUMINATED, APU FIRE AURAL WARNING SOUNDED AND APU FIRE INDICATION IN APU FIRE HANDLE ILLUMINATED NEAR RZC AT FL350 CRUISING AT .85M. CONFIRMED INDICATIONS WITH F/O AND PERFORMED PHASE 1 BY PULLING AND ROTATING APU SDR ASAA2021121836966Wire Harness · failed#2 ENGINE FIRE LIGHT DOES NOT ILLUMINATE ON TEST. GROUNDED - YES. REPLACED ENGINE CORE DETECTION HARNESS MW0326 WITH SERVICABLE UNIT. ENG FIRE DETECTION OPS CHECKS OK. REF B737-800 AMM 26-11-02, 26-11-00, AND ASA MAINTENANCE PROGRAM 05-07-01, TABLE 3, ITEM 7.
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