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 ASAA2017022019881Wire Harness · failedINTERMITTENT FAULT LIGHT ILLUMINATED DURING CLIMB, ON THE FIRE PANEL FOR ABOUT 2 MINUTES, THEN EXTINGUISHED. ACFT GROUNDED. REPLACED THE NR 2 ENGINE FAN FIRE DETECTION HARNESS, IAW AMM 26-11-02-000-801, AND REPLACED THE 2 ENGINE UPPER FAN FIRE DETECTOR IAWSDR UIEA2017020700150Circuit Card · not seatedINTERMITTENT RT ENGINE OH LP 1 STATUS MESSAGE DURING CRUISE. PERFORMED ENGINE FIRE DETECTION SYSTEM BITE IAW FIM 26-11 TASK 804, SEATED THE CIRCUIT CARD M689 IAW AMM 26-10-01/401 FAULT CLEARED.SDR ASAA2017012619564Wire Harness · damagedNR 1 ENGINE WIRE HARNESS MW0326 HAS BROKEN SHEILDING. ACFT GROUNDED. REMOVED AND REPLACED CORE FIRE DETECTION HARNESS. OPS NORMAL IAW AMM 26-11-02.SDR MUIA20170126001Insulator · wornCREW REPORTED FIRE WARNING DURING FLIGHT, NO EVIDENCE OF FIRE FOUND, PERFORMED GENERAL VISUAL INSPECTION OF FIRE DETECTION SYSTEM, REPLACED 6 WORN INSULATORS AND CLEANED CONNECTORS - PERFORMED SATISFACTORY SELF TEST OF SYSTEM.SDR ASAA2017011719428Terminal · defectiveTHE NR ENGINE B FIRE LOOP FAILED A TEST. ACFT GROUNDED. REMOVED AND REPLACED BOTH TOP LUG TERMINALS (FOUND ONE BAD AND THE OTHER ONE QUESTIONABLE) FOR THE RIGHT CORE FIRE DETECTOR IAW AMM 26-11-02. REMOVED AND REPLACED RIGHT CORE FIRE DETECTOR AS PRECAUTIONSDR ASAA2017010519255Wire · brokenNR 1 ENGINE FIRE LOOP TEST FAILED FOR LOOP A. FAULT LIGHT AND NR 1 ENGINE FIRE LIGHT WOULD NOT ILLUMINATE DURING TEST. ACFT GROUNDED. DURING TROUBLESHOOTING FOUND A BROKEN WIRE OFF TERMINAL LUG AT M1760. REPLACED THE TERMINAL LUG IAW SWPM. LEFT ENG FIRE DSDR ASAA2017010419242Wire Harness · damagedNR 1 ENG FIRE DETECTOR LOOP AT 3:00 POSITION BONDING JUMPER AT SENSOR JUNCTION BRACKET HAS BROKEN STRANDS. (90% LOSS). ACFT GROUNDEDS. IAW AMM 26-11-02, REMOVED & REPLACED MW0325 CORE FIRE DETECTION HARNESS, OPS NORMAL IAW AMM.SDR IPXA2017010612449Connector · dirtyENG 3 FIRE LB B INTERMITTENT STATUS MESSAGE APPEARED AT CRUISE PHASE OF FLIGHT REPLACED NR 3 ENG LOOP B FIRE DET CARD ASSY PER MM 26 10 01. NO HELP A1983212 1-1-17. CLEARED AND SECURED CONNECTOR D4154P AND OPS CK GOOD PER MM 26 11 00.SDR ASAA2016123019222Wire Harness · damagedDAMAGE FOUND ON HARNESS MW0326 ON ENGINE NR 2 WHILE PERFORMING T/C N7420001. GROUNDED - YES. ON DEFERRAL.SDR ASAA2016122919221Wire Harness · damagedWHILE ACCOMPLISHING T/C N8420000, LEFT ENGINE EXTERNAL ENGINE HARNESS GVI, FOUND CORE FIRE DETECTION HARNESS MW0326, FRAYED AT THE 6 O'CLOCK POSITION. ESN862272. GROUNDED - YES. ON DEFERRAL.SDR ASAA2016122919203Wire Harness · failedNR 1 ENGINE A LOOP OF FIRE DETECTION SYSTEM INOP. GROUNDED - YES. ENGINE/APU FIRE BITE SHOWS WIRING OPEN OR DETECTORS FAULT. FAULT LIGHT ILLUMINATED WHEN SWITCHED TO A LOOP. AFTER OPENING INBOARD TR FAULT LIGHT EXTINGUISHED. DISCONNECTED ALL A LOOP DETECTORS, SDR HDNA724312160001Wire · unsecureON STARTUP, THE NR 2 ENGINE FIRE LIGHT FLICKERED. TECHNICIAN FOUND WIRE 2WC2A20 AT PIN C ON WARNING LIGHT UNIT. REPOSITIONED AND SECURED WIRE AT WARNING LIGHT UNIT, PERFORMED FUNCTIONAL TEST IAW MM-92-116, 92-119. NO FURTHER DEFECTS NOTED.SDR JIKA2016122801Terminal · exposedDURING CLIMB AT 5000FT, THE RIGHT ENGINE FIRE ANNUNCIATOR ILLUMINATED. ABOUT 5 SECONDS LATER THE FIRE WARNING ANNUNCIATOR ILLUMINATED. REDUCED POWER AND LEVELED OFF. DECLARED AN EMERGENCY. THERE WERE NO VISUAL SIGNS OF A FIRE IN THE RIGHT ENGINE. SHORTLYSDR ASAA2016122419140Wire Harness · damagedNR 2 ENGINE, CORE FIRE DETECTION HARNESS DAMAGED. ACFT GROUNDED. THE WIRE HARNESS WAS REMOVED AND REPLACED IAW AMM 26-11-02. OPS CHECKED GOOD IAW AMM 26-11-00-710-801.SDR ASOA201612221378Control Unit · inoperativeFIRE SYS FAULT STATUS IN FLIGHT. R & R EXTINGUISHER CONTROL UNIT, OPS CHECKED GOOD, NO DEFECT NOTED AT TIME, OR SINCE THE CONTROL UNIT WAS REPLACED, ACFT OK FOR SERVICE.SDR COZA20161223103Wire Harness · shortedNR 2 ENGINE FIRE LOOP LIGHT DID NOT TEST. WHILE PERFORMING RESISTANCE CHECKS ON THE #2 ENGINE LOOP A DETECTORS NOTICED RESISTANCE CHANGES WHEN THE FIRE DETECTOR HARNESS WAS MOVED OR DISTURBED. REPLACED THE FIRE LOOP HARNESS AND #2 FIRE LOOP LIGHT TESTED OK.SDR ASAA2016121619058Terminal · looseMAINT ENTRY: DURING FIRE TEST OF FIRE DISCHARGE HANDLES, NR 1 FIRE DISCHARGE HANDLE LIGHTS INOPERATIVE. ACFT GROUNDED. TROUBLESHOT IAW FIM 26-10 TASK 801, FAULT 31 ENG WIRING OPEN FOR DETECTOR FAULT A LOOP. GVI DETECTOR LOOP A, FOUND LOOSE TERMINAL ON LT CORESDR HALA2016121600550Wire · brokenLEFT ENGINE FIRE LOOP 1 MESSAGE ON STATUS PAGE. FOUND A BROKEN WIRE. TERMINATED THE WIRE IAW WDM 26-11-11. BITE CHECK OK, NO FAULTS NOTED. OK FOR SERVICE.SDR ASAA2016121519057Terminal · looseRIGHT ENGINE UPPER RIGHT CORE DETECTOR TERMINALS LOOSE ON WIRE HARNESS. ACFT GROUNDED. REPLACED THE TERMINALS, OPS TEST PASSED IAW AMM 26-11-02/801 AND 26-11-00/501 AND TASK CARD N8420001. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2016121119008Connector · looseDURING TEST, THE CARGO FIRE DETECTOR AFT CARGO FIRE WARNING LIGHT DOES NOT LIGHT. DETECTOR FAULT LIGHT ILLUMINATED. ACFT GROUNDED. FOUND CONNECTOR ON A1 SMOKE DETECTOR LOOSE, SECURED CONNECTOR, OPS CHECKED GOOD IAW AMM 26-16-00.SDR ASOA201612093084Connector · looseTHE CREW REPORTED A SMOKE AFT LAV WARING MESSAGE DURING DESCENT. FA ADVISED THERE WAS NO SMOKE, FIRE OR FUMES. MAINTENANCE INSPECTED AND FOUND LOOSE CONNECTOR ON THE SMOKE DETECTOR. CONNECTED THE CONNECTOR AND OPS CHECKED GOOD.SDR UIEA2016120600989Wire · chafedWIRES RUBBING ON RT ENG INBD SIDE. REMOVED AND REPLACED THE WIRE IAW SWPM 20-10-11 AND SWPM 26-11-21. OPS CHECKED GOOD IAW AMM 26-11-00.SDR ASOA201612053085Connector · dirtyTHE CREW REPORTED LAV SMOKE WARNING MESSAGE . NO SMOKE FIRE OR ODOR WAS NOTED. MAINTENANCE INSPECTED AND REMOVED THE CONNECTOR P8100, CLEANED AND REINSTALLED. OPS CHECKED GOOD.SDR FDEA201612034319Wire · looseTHE TWO AGT LOW LIGHTS DOES NOT ILLUMINATE IN THE COCKPIT. PERFORMED ENGINE FIRE TEST IAW AMM 26-11-02-5.TEST OK.DISCONECTED THE CONNECTORS FOR THE CARTRIDGES IAW AMM 26-21-05-4. INSPECTED THE DISCHARGE CATRIDGES, STILL GOOD, INSPECTED THE DISCHAGE LINSDR N6WA2016112101Connector · looseSMOKE AFT LAV MASTER WARNING MESSAGE, EMERGENCY DECLARED. OPS CHECKED AFT SMOKE DETECTOR IN LAV OPS CHECKED GOOD IAW AMM 26-16-00. FOUND THE AFT LAV SMOKE DETECTOR CONNECTOR LOOSE. TIGHTEN CONNECTOR IAW AMM 26-16-01 STEP A (5) PULLED TOILET SHROUD NO DEFECTSSDR QXEA2016112100733Wire · chafedFIRE DETECTION WARNING WITHOUT BELL OR EVIDENCE OF FIRE ON THE T HANDLES. NR 2 ENGINE FIRE DETECT FAULT LIGHT A&B ILLUMINATED AND CIRCUIT BREAKER J7 POPPED. FOUND CHAFED WIRE IN THE NR 2 NACELLE. REPAIRED THE WIRE. OPERATIONAL TEST OF FIRE DETECTION SYSTEM GOOSDR ASAA2016110818601Wire Harness · damagedWHILE PERFORMING TC 72470004, NOTED LOOP WIRE HARNESS ON INBOARD SIDE, SHIELDING DAMAGED. GROUNDED - YES. REMOVED FIRE DETECTION HARNESS ON ENG #2 MW0326 PARTIAL INSTALL REF B737-900 AMM 26-11-02 ALL ELECTRICAL CONNECTIONS & AFT INBD CLAMP & ISOLATOR REQUIRE ISDR SWAA2016110109291Plug · dirtyDECLARED EMERGENCY, WHEEL WELL FIRE WARNING LIGHT AND BELL CAME ON AT 12,000 MSL 230KIAS. BOTH WENT OUT/OFF WHEN GEAR WAS EXTENDED. CLEANED WHEEL WELL SENSING ELEMENT CONNECTOR PLUGS PER AMM.SDR ASAA2016102918502Wire Harness · damagedNR 2 ENGINE CORE FIRE LOOP MW0326 SHIELDING BROKEN. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE CORE FIRE LOOP MW0326, OPS CHECK GOOD, IAW AMM 26-11-02.SDR ASOA20161022030Terminal · damagedRIGHT ENGINE FIRE WARNING ON LANDING. WARNING CONTINUED AFTER BOTH BOTTLES DISCHARGED. NO EXTERNAL SIGNS OF FIRE. REPAIRED AND INSTALLED TERMINAL TO RT ENG FIRE DETECTION HARNESS IAW ESPM 20-20-00. REMOVED AND REPLACED ENGINE FIRE BOTTLES AND CARTRIDGES IAW SDR ASAA2016102218443Wire Harness · damagedRIGHT ENGINE INSPECTION FOUND NR 2 ENGINE CORE DETECTION MW0326 HARNESS INSULATIONS ARE MISSING. ACFT GROUNDED. REMOVED AND REPLACED THE WIRE HARNESS IAW AMM 26-11-02. ENGINE FIRE DETECTOR OPS TESTED NORMAL IAW AMM 26-11-00.SDR ASAA2016101818395Connector · damagedAPU DETECTOR FAULT LIGHT ILLUMINATED. ACFT GROUNDED. LOCKS BROKEN FOR PINS 1 & 3 OF CONNECTOR D40062P. REPLACED THE CONNECTOR IAW WDM 26-11-31 PAGE 3. APU DETECTOR FAULT LIGHT OUT. APU FIRE DETECTION OPERATIONAL TEST PASSES, IAW AMM 26-15-00/501. GROUND VERSDR QXEA2016101900654Wire · chafed"CHECK FIRE DET" WARNING LIGHT AFTER ENGINE START WITH FAULT A AND FAULT B LIGHTS ILLUMINATED FOR ENGINE 1. ENG 1 FIRE DET IND CB (K7) HAS POPPED. CB K7 WILL NOT RESET WITH POWER APPLIED TO A/C. DISCONNECTED CONNECTORS. FOUND CHAFED WIRE W19A.20.4/BLU APP.SDR DUFA20161013002Ground Wire · chafedJUST AFTER BEGINNING HIS DESCENT, THE PILOT NOTICED HIS LEFT WING OVERHEAT LIGHT HAD ILLUMINATED STEADY. FOLLOWING PROCEDURES, THE PILOT CLOSED HIS LEFT BLEED AIR VALVE, TURNED OFF THE LEFT GENERATOR AND EXTENDED THE LANDING GEAR. AFTER A COUPLE OF MINUTES HADSDR CHIR20161009001Wire · nickedFIRE DETECTION WARNING LIGHT ILLUMINATED DURING FLIGHT. FAULTY PORTION OF THE NR 1 FIRE DETECTION SYSTEM WAS REPLACED FOR MULTIPLE NICKS IN THE WIRE SHIELDING AND SUSPECTED FAULTY SPLICES. NO FURTHER REOCCURRENCES HAVE BEEN REPORTED. FAULTY PORTIONS OF THE NSDR CHIR20161008001Wire · nickedNR 1 ENGINE FIRE LIGHT ILLUMINATED IN FLIGHT (FALSE ACTIVATION). INSPECTED SYSTEM. NO FAULTS FOUND. REPLACED FWD UPPER & LOWER DETECTORS FOR TROUBLESHOOTING. AIRCRAFT RETURNED TO SERVICE. FAULTY PORTION OF THE NR 1 FIRE DETECTION SYSTEM WAS REPLACED FOR MUSDR ASAA2016100718237Wire Harness · brokenWHILE ACCOMPLISHING T/C 78472000, FOUND A BROKEN GROUND STRAP ON THE NR 2 FIRE HARNESS AT THE TURBINE CASE 3 O`CLOCK POSITION. JUST FORWARD OF THE 16TH STAGE BLEED AIR STRUT DUCT. ACFT GROUNDED. R & R THE WIRE HARNESS IAW AMM 26-11-02. PERFORMED A NR 2 FIRESDR CHIR20161007001Wire · nickedNR 1 ENGING FIRE DETECTION LIGHT ILLUMINATED DURING FLIGHT. INSPECTED SYSTEM. NO FAULTS FOUND. REPLACED BOTH AFT UPPER & LOWER FIRE DETECTORS. SYSTEM TESTED. AIRCRAFT RETURNED TO SERVICE. FAULTY PORTION OF THE NR 1 FIRE DETECTION SYSTEM WAS REPLACED FOR SDR CHIR20161006001Wire · nickedDURING CRUISE FLIGHT, THE NR 1 ENGINE FIRE DETECTION LIGHT FALSE ACTIVATED. SYSTEM INSPECTED. NO FAULTS FOUND. CHANGED THE SYSTEM AMPLIFIER FOR TROUBLESHOOTING. ACFT RETURNED TO SERVICE. FAULTY PORTION OF THE NR 1 FIRE DETECTION SYSTEM WAS REPLACED FOR MULTIPSDR ASAA2016100518222Wire Harness · damagedWHILE PERFORMING TASK CARD N8420000, FOUND THE NR 1 ENGINE CORE FIRE DETECTION HARNESS MW0326 BRADED SHIELDING BROKEN. ACFT GROUNDED. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTION HARNESS IAW AMM 26-11-02. OPS CHECKED GOOD.SDR CHIR20161003001Wire · nickedNR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING FLIGHT. FALSE FIRE WARNING. FAULTY PORTION OF THE NR 1 FIRE DETECTION SYSTEM WAS REPLACED FOR MULTIPLE NICKS IN THE WIRE SHIELDING AND SUSPECTED FAULTY SPLICES. NO FURTHER REOCCURRENCES HAVE BEEN REPORTED. SUSDR QXEA2016100300630Connector · damagedDURING AIRCRAFT MOVEMENT, THE SMOKE CAUTION ILLUMINATED AND THE AFT CARGO CAUTION LIGHT CAME ON. INSPECTION FOUND THE AFT CARGO COMPARTMENT FORWARD SMOKE DETECTOR TO HAVE THE FAULT LIGHT ILLUMINATED. CLEANED AND SEATED PINS TO THE DETECTOR AND REINSTALLED THSDR ASMF201611017Wire Harness · damagedDURING TRANSIT CHECK, THE RIGHT ENGINE FIRE HANDLE LIGHT WAS NOT ILLUMINATED DURING FIRE DETECTION TEST AND LOOP B OF RIGHT ENGINE WITH FAULT. MAINTENANCE PERSONNEL PERFORMED RIGHT ENGINE FIRE DETECTION TEST IAW AMM 26-10-00, DETECTING LINE OPEN AT MW0326 WIRSDR JIKA2016081601Wire · shortedENROUTE TO CCS PILOT REPORTED RIGHT WING OVER HEAT STEADY ANNUNCIATOR LIGHT ILLUMINATED. THE PILOT EXECUTED THE WING OVERHEAT STEADY ANNUNCIATOR PROCEDURE FROM THE EMERGENCY CHECK LIST. THE RT WING OVER HEAT LIGHT EXTINGUISHED WITHIN THE ALLOTTED TIME FRAME.SDR P5CA2016081800227Wire · damagedFOUND APU FIRE DETECTOR WIRE W720-452-18R AND W720-451-18R DAMAGED. REMOVED AND REPLACED THE WIRE IAW AMM 26-15-02-004-001 REV 87, AMM 26-15-02-404-020 REV 87, WDM 26-15-11- REV 41 & SWPM 26-63-13 / 21-10-11 REV 62. OPS CHECKED GOOD.SDR A6WA201644207Connector · unsecureSMOKE TOILET CAUTION MSG WITH INTERMITTENT SMOKE DETECTOR BEEP. ON GROUND TAXI WITH RT EMERGENCY ONLY AND BOTH PACKS ON. DURING INSPECTION OF LAV SMOKE DETECTOR FOUND CONNECTOR NOT SECURED. R & R SLIDE LATCH IAW ESPM 20-17-10. OPS CK GOOD IAW AMM 26-16-00 SDR FDEA201608082842Wire · chafedNR 1 ENGINE FIRE AGENT LOW DURING CRUISE AND DECENT. CLEARED AFTER BLOCK IN TO GATE FOUND SHEILD ON WIRE TO P1-1261 WORN TO CENTER CONTACT IAW WDM 23-33-01. REPAIRED THE WIRE IAW SWP 20-10-01. OPS CHECKED IAW AMM 23-21-06-5. OK FOR SERVICE.SDR ASOA20160808019TGround Wire · damagedLAVATORY SMOKE EICAS MESSAGE AFTER TAKEOFF. FOUND 300M OHM OF CONTINUITY TO AIRFRAME GROUND WIRE W102-8013-22. SPLICE REPAIRED THE WIRE AT FRAME 20, STRINGER 19R. OPS CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR ASAA2016080417618Terminal · separatedNR 2 ENGINE "B" LOOP INOPERATIVE. ACFT GROUNDED. FOUND NR 2 ENGINE FAN UPPER FIRE DETECTOR ASSY LOOP B CONNECTOR CRIMP SEPARATED TERMINAL FROM WIRE. RECRIMPED NEW TERMINAL ON NR 2 ENGINE FAN UPPER FIRE LOOP B CONNECTOR IAW WDM 26-11-11. PERFORMED ENGINE APSDR UIEA2016080400667Connector · looseFWD EICAS MESSAGE FOR RT ENGINE FIRE LOOP 1 AND 2. PERFORMED TROUBLESHOOTING IAW FIM 26-11 FT 804, FOUND HI & RES C PIN. FOUND 1 & 2 LOWER LOOP CONNECTOR LOOSE. SECURED IAW AMM 26-11-02 TEST GOOD & IAW AMM 26-11-00.
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