JASC 2697
Service difficulty reports · 1,401
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 ARWA20040905Wire · brokenNR 2 ENGINE FIRE DETECTION TEST FIRE SHUTOFF LEVER LIGHTS VERY DIM AND C/B POPPED OUT. REPAIRED WIRES OF FIREWALL DISC. BOX ENGINE NR 2 IAW MM 20-50-1. PERFORMED OPERATIONAL CHECK TEST DETECTION SYSTEM IAW M/M 26-10-0, FOUND NORMAL.SDR IXXA0400108OWire · chafedON APPROACH TO KRFD, THE NR 1 SHORT LIGHT AND NR 1 FIRE LIGHT ILLUMINATED INTERMITTENTLY THEN CAME ON STEADY, NR 1 ENGINE SHUTDOWN. DURING ENGINE SHUTDOWN, THE ENGINE DID NOT SHUTDOWN WITH THE FIRE HANDLE. ENGINE DID NOT SHUT DOWN UNTIL FUEL SHUTOFF LEVER WASDR 254041Wire · brokenLEFT ENGINE FIRE TEST WILL NOT TEST PROPERLY NO CHIME. REPAIRED BROKEN WIRE AT LT FIRE WARNING CIRCUIT BREAKER IAW MM 31-50-05, OP CHECKED GOOD.SDR AALA20040939Insulation · burnedPOP - MIN EQUIPMENT SMOKE MASTER WARNINGS STARTED AT TOP OF CRUISE 4-5X LASTING APPROX 30 SECS, WOULD CLEAR FOR APPROX 1-2 MINS, DIVERTED TO POP. INSPECTED EQUIPMENT BY AREA FOUND BURNED SPLICES ON LEFT RUNWAY TURN OFF LIGHT. PLACARD LEFT RUNWAY TURN OFF LIGSDR DELA20040003Connector · faultyDURING TAXI, THE LEFT FIRE T- HANDLE AND MASTER WARNING LIGHTS BEGAN FLASHING. T/S REVEALED FAULTY (OPENS) IN 2 CONNECTORS IN THE FIRE DETECTION ELEMENT HARNESS. TWO EA CONNECTORS WERE REPLACED WITH NEW UNITS AND F/T SATISFACTORY.SDR 63720Wire · brokenAIRCRAFT RETURN TO FIELD DUE TO FIRE EXT. DISCHARGE LIGHT ILLUMINATED. NO FURTHER INCIDENT. REPAIRED WIRE AT RT FIRE BOTTLE, OPS CK NORMAL.SDR AMTA200400918Wire · chafedRT TURBINE OVERHEAT DET 2 STATUS MESSAGE DISPLAYED. FOUND CHAFED WIRE JUST AFT OF DISCONNECT D40158P. REPAIRED PER WDM STANDARD PRACTICES CHAPTER 20. OPS CHECKS GOOD AT THIS TIME. (M)SDR QXEA200400538Wire · brokenCARGO BAY FORWARD SMOKE DETECTOR WIRES ARE BROKEN. REMOVED AND REPLACED WIRE 2612-1J3. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR USAASB04089Wire Harness · inoperativeBOS - FLT 1249 - FLIGHT DEPARTED PVD, EN ROUTE TO DCA, WITH THE NR 2 ENGINE 'A' FIRE LOOP ON MEL 26-2A. DURING CLIMB-OUT, THE NR 2 ENGINE 'B' FIRE LOOP FAULT LIGHT ILLUMINATED AND REMAINED ON. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. NO ESDR ASMF200406033Wire · failedAIRCRAFT RETURNED TO PLATFORM, "LEFT AIR COND SUPPLY TEMP HI" LIGHT TURNED ON. BREAKER B1-251 WAS RESEATED, TEMPERATURE SENSOR AND THERMAL SWITCH WERE DISCONNECTED AND FAIL CONTINUE. ENGINES WERE SHUTDOWN AND LIGHT WAS DEFERRED IAW MEL 21-2. DURING OVERNIGHT SSDR AMTA200400762Wire · chafedON TAKEOFF ROLL, STATUS MSG LEFT ENGINE OH LP2 ILLUMINATED DISAPPEARED ON THRUST REDUCTION AND REAPPEARED DURING INITIAL CLIMB. APPROXIMATELY 9,000 AGL WITH CLIMB THRUST SET DISAPPEARED FOR REMAINDER OF CLIMB. FOUND WIRE CHAFED IN NACELLE GOING TO OVERHEAT LSDR GUU2004F00018Wire Harness · out of positionDURING FLIGHT, RT ENGINE FIRE BOTTLE DISCHARGE LIGHT FLICKERS ON AND OFF. REPOSITIONED AND SECURED WIRE HARNESS AT SQUIB. OPERATIONAL CHECK NORMAL.SDR ATC0376Extinguisher · miswiredCARGO FIRE SUPRESSION/DETECTION, FORWARD CARGO BAY INCORRECT INSTALLATION. DURING A C1-CHECK, FOUND; FIRE DETECTION, AAE LTD SYSTEM TEST CARRIED OUT. DURING TEST, FOUND THAT BY TRIPPING A SYSTEM C/B ISOLATED THE B SENSORS. TRIPPING THE B SYSTEM ISOLATED THESDR RAIA00404019Wire · shorted5621 - STL - BRAKE 2 OVERHEAT INDICATION. MAINTENANCE DEFERRED NR 2 BRAKE HEAT INDICATION PER MEL 32-40-01. SUBSEQUENTLY CLEARED DMI BY REPAIRING SHORTED WIRE AT PIN A CANNON PLUG P 1090.SDR SWIA200413228Terminal · looseLEFT JET OVERHEAT FAIL MESSAGE INTERMITTENTLY ILLUMINATED AND THEN STAYED ON STEADY EN ROUTE. THE MESSAGE STAYED ILLUMINATED WITH SELECTION OF BOTH A AND B LOOPS. MESSAGE CONTINUED TO CYCLE ON AND OFF. INSPECTED WIRING AT LEFT ENGINE JET PIPE, FOUND 3 LOOSESDR DL73S040339Wire · damagedLEFT WING BODY OVERHEAT LIGHT STARTED BLINKING AFTER T/O. REPAIRED WIRING.SDR SWIA200413137Wire Harness · damagedMLG BAY OVERHEAT WILL NOT TEST. REMOVED AND REPLACED LT AND RT WHEEL BIN WIRING HARNESSES. OPS CHECKS GOOD.SDR MASA200400160Terminal · out of positionRETURNED TO GATE AFTER REJECTED TAKE-OFF. CREW RECIEVED A LT JETPIPE OVERHEAT WARNING LIGHT. MX REPOSITIONED TERMINALS FOR BOTH LOOPS A & B GROUNDING. MX REPOSITIONED THEM. OP CHECKS GOOD ON HIGH POWER RUN. NO PARTS USEDSDR BAQA094041Wire Harness · damagedWIRE HARNESS HAS DAMAGED SOLDER JOINTS ON UNIT. REPLACED WITH SERVICABLE UNIT. 04/02/2004SDR HEEA094027Connector · corrodedWHILE IN CRUISE FLIGHT NR 2 ENGINE FIRE LIGHT ILLUMINATED. FOLLOWED EMERGENCY CHECK LIST FOR ENGINE FIRE LIGHT. RETURNED TO BASE. INSPECTED FOR SIGNS OF FIRE AND OR SMOKE, NONE FOUND. FOUND DEFECTIVE (CORRODED) CONNECTOR. REPLACED CONNECTOR.SDR GUU2004F00002Wire · dirtyDURING FLIGHT, NR 2 ENGINE FIRE BOTTLE DISCHARGE LIGHT FLICKERS INTERMITTENTLY, CONTINUED. INSPECTED AND CLEANED WIRES ON NR 2 FIRE BOTTLE. COULD NOT DUPLICATE. OPERATIONAL CHECK NORMAL.SDR ESE2004F00000Connector · inoperativeA FIRE WARNING OCCURRED DURING CLIMBOUT. ON THE RT ENGINE. NO EMERGENCY DECLARED. AIRCRAFT MADE A PRECAUTIONARY LANDING. NO SECONDARY INDICATION OF MALFUNCTION WERE EVIDENT. CREW COULD NOT DUPLICATE PROBLEM. RT ENGINE FIRE DETECTOR CONNECTOR.SDR DHL2004755003Wire · brokenNR 2 ENGINE FIRE DETECTOR CIRCUIT GROUND ANNUNCIATOR ON P-6 IS ILLUMINATED. TRANSFERRED TO DMI 15476 PER MEL 26-9-1, PLACARD INSTALLED. FOUND WIRE BROKEN OFF AFT PLUG ON FIRE LOOP NR 2 ENGINE. REPLACED AFT PLUG ON NR 2 ENGINE FIRE LOOP PER BSW PM 20-62-17. OSDR GTIA031049Connector · inoperativeFLL - FLT 900 - FIRE WARNING LT ENGINE B-LOOP CONNECTOR P1-863 ON THE NR 1 ENGINE. OPS CHECK GOOD ON THE NR 1 ENGINE FIRE LOOP TEST. (M)SDR CA031224001Wire Harness · chafedF/A NOTICED SPARK FROM OXYGEN PNL. A/C REMAINED IN SERV SEVERAL DAYS. UPON INSPECT, WIRE BUNDLE DIRECTLY ABOVE LAV "E" SMOKE DETECT FOUND CHAFFED ON SMOKE DETECT. INSPECT FOUND ROUTING OF WIRE BUNDLE WITH LITTLE CLEARANCE BETWEEN BUNDLE AND DETECTOR AND REPSDR QXEA200301569Wire Harness · faultyCHECK FIRE DETECTION WARNING LIGHT ILLUMINATED EN ROUTE ALONG WITH RT SIDE A AND B ILLUMINATED. REMOVED AND REPLACED FIRE DETECTOR WIRE HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR XNOA1167Wire · chafedON TAXI OUT AFT LOWER BODY OVERHEAT ILLUMINATED. REPAIRED CHAFED WIRE AT LOWER BODY HEAT LOOP, STAIRWELL POS, IAW B727MM 26-14-0. OPS CHECK NORMAL.SDR QXEA200301441Wire Harness · inoperative2 BAGGAGE SMOKE DETECTOR INOPERATIVE. FOUND NR 2 BAGGAGE SMOKE DETECTOR WIRE HARNESS SEVERED BY CARGO DOOR AT PLUG 2612-P3. REMOVED AND REPLACED WIRE HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR UPS03641541Wire · faultyINSPECTION TYPE: N/A FIRE PROTECTION SYSTEM FAIL LIGHT ILLUMINATED. EICAS MSG: FIRE/OVHT SYS DISPLAYED. EICAS STATUS MSG: R ENG FIRE LP1 DISPLAYED. INDICATION APPEARED ON SHORT FINAL TO LANDING. TESTED SYSTEM, INDICATION EXTINGUISHED. REPLACED ALL WIRINSDR USAASB03193Wire Harness · meltedON APPROACH TO CLT, AT 1,500 FT, ENTIRE FIRE CONTROL PANEL ILLUMINATED & ALL FIRE BELLS SOUNDED EXCEPT FOR APU. CREW ALSO RECEIVED A LT WING BODY OVERHEAT INDICATION. CREW COULD NOT SILENCE BELLS OR EXTINGUISH LIGHTS. CABIN CREW VERIFIED NO SMOKE PRESENT, NSDR REXA03008Wire · looseLAVATORY SMOKE WARNING. FLIGHT ATTENDANT VERIFIED NO SMOKE, CREW ELECTED TO RETURN TO AIRPORT. UNEVENTFUL LANDING. MAINTENANCE FOUND LOOSE WIRE ON LAV SMOKE DETECTOR CANNON PLUG. SYSTEM DEFERRED PER MEL 26-16-01 CAT C. (M)SDR DHL2003805011Connector · damagedDURING CRUISE NR 1 FIRE LIGHT ILLUMINATED, WARNING BELL SOUNDED. PERFORMED PHASE ONE ITEMS LIGHT REMAINED ON (BLEW BOTH BOTTLES). DUMPED 19000 LBS. OF FUEL AND LANDED SAFE. R AND R NR 1 AND 2 ENG FIRE BOTTLES IAW MM 26-20-01. OPS CHECKED GOOD. NR 1 FIRE LOOP SDR DHL2003802014Connector · shortedNR 2 ENGINE SHORT CIRCUIT (FIRE LOOP "A") DETECTION CAME ON INTERMITTENTLY, ONCE SHORTLY AFTER TAKE-OFF, ONCE AT 3 HOURS. TRANSFERRED TO DMI LOG IAW MEL. PLACARD INSTALLED. NR 2 ENGINE SHORT CIRCUIT FIRE LOOP "A" DETECTION COME ON. INSPECTED NR 2 ENGINE FISDR EIA2003120Circuit Card · fireWHILE AT CRUISE, FL 400, THE RT WING OVHT LIGHT ILLUMINATED. THE CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST. THE NR 3 AND NR 4 FIRE LOOPS FAILED FIVE MINUTES LATER. DISPATCH AND TECH CENTER NOTIFIED. AN ACRID ODOR WAS DETECTED BY THE CREW, SHORTLY AFTER TSDR EVAS092017Wire · looseDURING TAIPEI TO BOM CARGO FLIGHT,SYSTEM REPORT (MAIN DECK CABIN SMOKE) WARNING MESSAGE, CHECK THIS AREA NO SMOKE CAN BE FOUND, BUT ACCORDING TO COMPANY PROCEDURE, CAPTAIN DECIDE TO DIVERT AIRPLANE. AFTER REPLACE 3L SMOKE DETECTOR AND PERFORM DETAIL CHECK WIRSDR CA030724004Wire · broken(CAN) DUCT OVERHEAT SENSOR WIRE PN W84C20 WAS FOUND BARE & BROKEN UNDER DUCT COUPLING CLAMP. THE ELECTRICAL CIRCUIT WAS COMPLETED THROUGH THE CLAMP AND DID NOT SHORT TO GROUND BECAUSE IT WAS ISOLATED BY THE SILICONE RUBBER COUPLING.SDR QXEA200300859Wire · damagedPDX- ON FLIGHT 2438 INTERMITTENT FIRE SYSTEM FAULT STATUS MESSAGE. MDC REPORTS LEFT ENGINE FIRE LOOP B FAILED/WIRING, OPEN CIRCUIT. REMOVED AND REPLACED FIRE DETECTION CONTROL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR C1HA200394014Wire · damagedLOWER AFTER BODY OVERHEAT LIGHT CAME ON DURING TAXI BACK TO GATE. REPAIRED DAMAGED WIRE ABOVE ROW 3DEF W298-122-16+ W298-012-16 IAW WIRING PRACTICES CH 20. REMOVED AND REPLACED FIRE AND OVERHEAT ACCY UNIT, OPS CHECK NORMAL IAW MM 26-14-11.SDR DHL2003362010Connector · dirtyIN FLIGHT ENGINE NR 1 LOOP -A- LIGHT ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. OPS NORMAL NR 1 LOOP MOVED TO -B- LOOP. REPOSITIONED -A- LOOP AND CLEANED CONNECTOR. SYSTEM OPS CHECKED NORMAL. OK FOR SERVICE.SDR 03165405Wire · looseDURING TAXI, THE CREW REPORTED THAT THE RT ENGINE FIRE INDICATION HAD ILLUMINATED AND DISCHARGED THE EXTINGUISHER BOTTLES. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPAIRED LOOSE WIRE SHIELDING ON THE RT ENGINE FIRE DETECTOR SDR DXTA200300041Ground Wire · damagedLEFT ENGINE FIRE WARNING LIGHT ILLUMINATED DURING CLIMB THRU FL260 WITH ENGINE/WING ANTI-ICE ON. REDUCED POWER TO 72 PERCENT ON EFFECTED ENGINE AND LIGHT EXTINGUISHED. REMOVED AND REPLACED LT ENGINE FIRE LOOP WITH A NEW PART IAW CESSNA 560XL MAINTENANCE MANUSDR 2003F00389Wire · unsecureDURING FLIGHT, LT FIRE BOTTLE DISCHARGE LIGHT CAME ON AND OFF. SECURED GROUND WIRE AT SQUIB. OPERATIONAL CHECK GOOD. (M0SDR DHL2003802007Connector · defectiveNR 3 FIRE DETECTOR LOOP-B SYSTEM FAILED TO TEST. TRANSFERRED TO DMI 12964 CAT-C IAW MEL 26-2-3, PLACARDS INSTALLED. REF DMI 12964 NR 3 FIRE DETECTOR LOOP-B SYSTEM FAILED TO TEST. REPLACED DEFECTIVE CONNECTOR AT FAN CASE RT PER DACO M/M 20-504. OPS CHECKED SDR DHL2003783010Wire · shortedENGINE NR 3 DETECTOR CIRCUIT GROUND FAULT LIGHTS ILLUMINATED AT P6 CIRCUIT BREAKER PANEL. DEFERRED PER DHL MEL 26-9-1 CAT-C. ASSIGNED CONTROL 12957. PLACARD INSTALLED. REF DMI 12957 ENGINE NR 3 DETECTOR GROUND CIRCUIT FAULT LIGHT ILLUMINATED. FOUND POOR ISDR CALA0300250Wire Harness · wornTHE FIRE FAULT LIGHT ILLUMINATED WHILE EN ROUTE FROM GCM TO IAH. THE AIRCRAFT WAS DIVERTED TO CUN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. TROUBLESHOOTING FOUND THE LEFT ENGINE CORE FIRE LOOP HARNESS WORN. THE CORE LOOP HARNSDR DHL2003751009Wire · brokenNR 1 ENGINE FIRE LOOP AT FORWARD END HAS 1 WIRE BROKEN OFF. REMOVED AND REPLACED FIRE LOOP CONNECTOR ASSEMBLY, P/N 878581-01, PER BSWP MAN 20-62-16. FIRE TEST NORMAL PER B727 M/M 26-11-00.SDR DHL2003801067Connector · looseRT WING NR 3 ENG FIRE EXT BOTTLE SQUIB CARTRIDGE (POS NR 5) ELECT CONNECTION HAS LOOSE PINS. REMOVED AND REPLACED ELECT CONNECTOR FROM NR 3 ENG FIRE EXT BOTTLE SQUIB CARTRIDGE (POS NR 5) IAW MM 20-50-1 PG 213. SEE J/C 8-26-20-003 FOR OPS CK.SDR AUS20030423Connector · contaminated(AUS) NR 1 ENGINE FIRE DETECT/OVERHEAT FAULT LIGHT ILLUMINATED DURING FLIGHT. LOOP (A) FAULT LIGHT WAS INTERMITTENT AND LOOP (B) FAULT LIGHT WAS ON CONTINUOUSLY. THE CORE DETECTOR WIRING WAS INSPECTED AND CONNECTOR D1208 WAS FOUND CONTAMINATED.SDR UPS03840424Wire Harness · chafedNUMEROUS INTERMITTENT FIRE WARNING ON NR 4 ENGINE INFLIGHT. PERFORMED ENG FIRE SEVERE DAMAGE CHECKLIST AND SECURED ENGINE. RECEIVED BOTH LIGHT AND FIRE BELL. INSPECTED FIRE WARNING HARNESS AND FOUND RT CORE CHAFED. REPAIRED WIRE PER EOM-2000-16032-A, GROUNDSDR 2003F00259Wire · meltedCLIMBING THROUGH16,500 FT MSL, LT BLEED AIR LIGHT FLASHED THEN STEADY. FOLLOWED EMERGENCY PROCEDURE AND LANDED. DURING DESCENT, BLEED AIR FAIL LIGHT EXTINGUISHED. INVESTIGATION REVEALED THAT THE BLEED AIR SENSING LINE HAD A MELTED PLACE, WHICH CAUSED THE BL
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