JASC 2497
Service difficulty reports · 2,202
Reports filed under 2497 · Electrical Power 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 = '2497' 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 = '2497' 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 2012FA0000161Wire · misinstalledWHILE CONDUCTING THE ESSENTIAL AND CROSSFEED BUSS DIODES INSPECTION AS CALLED OUT IN MM 5-10-01 AND 24-61-01, 2 WIRES SLIPPED OUT OF BUSS 1 AND BUSS 2 CONNECTOR ON MALE END. WIRES APPEARED TO HAVE INCORRECT CRIMP CAUSING WIRES TO PULL OUT CREATING POWER LOSS.SDR QMLA2012031312027Wire · shortedON FINAL APPROACH, PILOT NOTICED THE NR 2 INVERTER LIGHT AS WELL AS THE P/R SAS AND GYRO LIGHTS WERE ALL ILLUMINATED ON THE CDS. A SHORTED WIRE WAS FOUND IN THE OVERHEAD CIRCUIT BREAKER PANEL. THE WIRE WAS REPAIRED, AND THE INVERTER WAS R & R. THE ACFT A SDR UALA2012031201573Wire · damagedTHREE WIRES DAMAGED IN FORWARD E AND E COMPARTMENT, RIGHT SIDE AFT OF CHILLER DURING CHILLER REMOVAL. REPAIRED WIRE W254-033-14 PER SWPM.SDR TRBA20120307001Plug · burnedTHE CREW REPORTED THE GPU CABLE ASSY PRODUCED STRONG SMOKE ODOR THAT CAME INTO THE COCKPIT. THE ACFT WAS REMOVED FROM SERVICE. REPLACED GPU PLUG IAW JIC 24-46-11. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.SDR CA120312020Switch · burned(CAN) PILOT REPORT ON APPROACH WHEN THE EXTERIOR LIGHTS WERE TURNED ON THERE WAS AN ODOR LIKE NAIL POLISH OR SOME KIND OF CHEMICAL ODOR. ACFT LANDED WITHOUT INCIDENT AND MAINTENANCE WAS CONTACTED AND DISPATCHED. THEY FOUND THE LT ESSENTIAL BUS TIE SWITCH HADSDR SWIA201229859Wire · chafedARCING IN AFT EQUIPMENT BAY. CHAFING WIRE AND CABLE ON FRAME AT FUSE STATION FS 672/00R. FRAME HAS ELECTRICAL ARCING DAMAGE AND SHIELD DAMAGE. (FLT 5535) REPLACED THE WIRES CD7C20WHT, CD8C20BLU, CD9C20DRN AND SHIELD. REPAIRED FRAME SECTION IAW REO.SDR SIMA20120228006Wire · chafedDURING MAINTENANCE INSPECTION FOUND CHAFE WIRE 681-110403 COMPLIED WITH SPECIAL REQUEST FOR INSPECTION OR REPLACEMENT OF WIRING. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND WIRE W166-8611-22 CHAFED REMOVED AND REPLACED WIRE. THE AIRCRAFT RETURN TO SERVICE.SDR DXTA2012022304884Diode · brokenBROKEN DIODE ON THE BACK SIDE OF THE PASSENGER SAFETY/FASTEN SEAT BELT SWITCH ON THE COCKPIT. THE CIRCUIT BREAKER TRIPPED IN THE BAGGAGE COMPARTMENT AND ELECTRICAL BURNING ODOR INSIDE COCKPIT. FOUND DIODE D1006 BURNED AND CRACKED IN HALF. INSTALLED NEW DIOSDR ABXR2012022000027Wire · arcedDURING INSPECTION FOUND WIRE W9021-015-16 SHOWING SIGNS OF ARCING. R & R AFFECTED WIRE IAW SWPM.SDR HALA2012021800064Wire · damagedRIGHT IDG TEMPERATURE SENSOR DISPLAYED IDG OUT: 80-180 IDG RISE 8-180 AT TOP OF CLIMB. ACCOMPLISHED FIM 24-20-00, REPAIRED DAMAGED WIRE, JACKED ON D10966 PLUG, IAW SWAPM 20-10-13, REPLACED RT GCU IAW 24-22-02. GROUND OPS CHECKED OK.SDR IPXA12671783Buss · inoperativeINSPECTION TYPE: E TOP, DURING APPROACH WITH FLAPS & GEAR UP, AUOPILOT AUTO THROTTLE ENGAGED, PASSING THRU HEAVY RAIN, MULTIPLE SIMULTANEOUS EICAS MESSAGES OCCURED INCLUDING STBY PWR, L/E FLAP DISAGREE, EQUIP COOLING, APU BOTTLE, AIR GRND SYS, AUTO BRAKE, AUTOSDR CA120216001Wire · chafed(CAN) WHILE CONDUCT EWIS TASK E-430 ON THE NR 3 NACELLE, NUMEROUS WIRES WERE FOUND TO HAVE BEEN CHAFED BY THE PHENOLIC BLOCK THAT SECURES THESE WIRES AS THEY PASS FROM THE RT MLG WHEEL WELL THROUGH THE FIRE WALL. THE WIRING AFFECTED IS AS FOLLOWS: 7160-30006DSDR 2012FA0000222Contactor · shortedPILOT REPORTED THAT ON LANDING, ACFT LOST ALL ELECTRICAL POWER. PERFORMED INSP AND TROUBLESHOOTING. FOUND BATTERY, STARTER AND STARTER RELAY AT FAULT. ACFT HAD A BURNED WIRE, ELECTRICAL ODOR. FOUND THAT THE STARTER STAYED ENGAGED AND IT ACTED LIKE AN ELECTSDR ASOA20120214020Terminal · looseTHE CREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM BEHIND THE CAPTAINS SEAT. MX R & R BURNED LOOSE TERMINAL LUGS AT DC BUSS NR 1 BUSS BAR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2012FA0000111Connector · burnedDURING INSPECTION FOR COMPLIANCE WITH SB1004 THE E303 CONNECTOR WAS FOUND TO BE BADLY BURNED. THE CONNECTION WAS REPAIRED IAW THE SB. INSPECTOR NOTES THAT THE INITIAL INSP OF EVERY ACFT HAS SHOWN NO COMPLIANCE WITH THIS SB AND ALL SHOW THE SAME BURNING OF THSDR REXA2012021200232Connector · damagedUNSCHEDULED LANDING FOR IDG NR 2 CAUTION IN-FLIGHT. REPINNED RT IDG OIL TEMP BULB CONNECTOR AND RECONNECTED IDG. OPS CHECKED IAW AMM 24-13-05. NO DEFECTS NOTED. REPINNED TEMP BULB CONNECTOR IAW ESPM 20. READY FOR SERVICE.SDR HNAA2012013000515Connector · contaminatedRT AC BUSS FAILED INFLIGHT. INSPECTED NR 2 AC GENERATOR. FOUND CONTROL ELECTRICAL CONNECTOR TO BE FULL OF OIL. CLEANED CONNECTOR PLUG. INSPECTED NR 2 AC CONTACTOR BOX. NO DEFECTS NOTED. CREW GROUND RAN ACFT. AC SYS OPERATES NORMAL. OK FOR SERVICE IAW MM SDR UALA2012013000607Wire · damagedREF WDM 24-21-21 PG 1 SHT 2, FOUND DAMAGED WIRE W8201-0002-02, AT TS33001. NEED NEW LUG INSTALLED AND WIRE SPLICED IN. SAMC TEXT: REF BSPWM 20-30-13 & 20-10-13, OK TO ACP SPLICE RPR IN PYLON AREA ON DAMAGED FEEDER WIRE. STARTED RMV'G WIRE FROM TERM BLOCK THRSDR AALA20120129JFK01Connector · defectiveJFK - CREW REPORTED LEFT GENERATOR TRIPPED AND CAUSED MULTIPLE STATUS MESSAGES. LEFT INTEGRATED DRIVE GENERATOR UNABLE TO BE RESET BY FLIGHT CREW. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CONNESDR ASOA20120119011Terminal · overheatedAFTER POWERUP, THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE COCKPIT. MX R & R TERMINAL LUG ON WIRE W179-0001-001N IN THE LT POWER DISTRIBUTION BOX, PERFORMED OPS CHECKS WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR UALA2012011300284Wire · unsecureCREW REPORT: LOOSE WIRING UNDER 5B. SECURED LOOSE WIRE AT 5B.SDR ASOA20120111006Circuit Board · defectiveTHE CREW REPORTED A BURNING SMELL IN THE CABIN BY SEAT 1A. THE ACFT RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, R & R THE CONTROL MODULE, PC BOARD, AND LIGHT BALLAST AT SEAT 1A, OPS TESTED WITH NO DEFECTS, AND THE ACFT WASSDR CA120111006Circuit Card · burned(CAN) ELECTRICAL SYSTEM FAIL AND ELECTRICAL SYSTEM FAULT CAS POSTED ON THE GROUND WITH APU GEN ON-LINE. AC SYNOPTIC PAGE MISSES ALL FLOW LINES AND DC SYNOPTIC PAGE MISSES APU BATTERY INFO. FOLLOWING VISUAL INSPECTION OF SECONDARY SECTION OF THE ACPC, THERE WSDR UALA2012010900213Wire · overheatedWIRING IN E&E COMPARTMENT JUST AFT OF RT OF TUNNEL HAS SIGNS OF OVERHEAT. SEE SMC10 WD24-53-51 DUE TO CHAFING AGAINST METAL CLAMP ON AC DUCT BELOW FLOORBOARD. SLEEVING DAMAGED ON WIRE RPR'D PER BOEING STD PRACTICES 20-10-13, PG 47.SDR MTNA0101051200001Connector · corrodedEN ROUTE FROM BWI TO EWR ON FLIGHT 8311. THE STANDBY ELECTRICAL POWER ON, CAUTION LIGHT CAME ON. THE PILOT TRIPPED AND RESET THE GENERATOR. THE GENERATOR DID NOT COME BACK ON LINE. THE FOLLOWING C/BS TRIPPED BUS POWER NR 2, STANDBY POWER, BLEED AIR HEAT, BSDR UALA2012010300007Wire · burnedTHERE WAS SMOKE, SPARKS AND SMALL FLAMES COMING OUT OF AFT GALLEY CART CONTROLLERS PANELS. ALL AFT GALLEY CART CONTROLLER POWER CIRCUIT BREAKERS ON AFT GALLEY POWER DISTRIBUTION WERE PULLED, POWER TO CART CONTROLLERS WERE REMOVED. CREW NOTICED DAMAGE ON PIGTSDR UALA2011122907143Wire · damagedN53 PIGTAIL LOUD POP AND SPARKS. C-B PULLED. SPARKS STOPPED. BARE WIRES. REPLACED PIGTAIL & TESTS NORMAL.SDR UALA2011122707114Feeder Cable · burnedNR 1 ENGINE IDG PHASE C, FEEDER CABLE AND THRU LEAD FOUND BURNED DURING PRELIMINARY INSPECTION. REMOVED & REPLACED IDG. REPLACED NR 1 IDG POWER FEEDER CABLE PHASE C TERMINAL LUG & HEAT SLEEVE. OPS CHECKED IAW AMM.SDR HALA2011122200605Connector · dirtyETOPS SIGNIFICANT SYS - ON 5 MILE FINAL, RT GEN DRIVE EICAS MESSAGE CAME ON. SECURED RT ENG ON LANDING. FOUND MESSAGE "RT IDG TEMP SENS". PFMD FIM 24-20-00. CLEANED CONNECTOR AND ENG RUN. OPS CHECKED OK. ACFT OK FOR SVC.SDR F3LA2011122100696Electrical Box · odorPAX & F/A'S REPORTED THE STRONG BURNING ELECTRICAL ODOR IN ROW 20-22 A/C LEFT. FOUND SEB ROW 21ABC EMITTING ELECTRICAL ODOR, PERFORMED INSPECTIONS OF AFT GALLEYS & LAVS. INSPECTED LIVE TV SYS RACK IN AFT CARGO PIT, NO PROBLEMS NOTED REF AMM TSM 24-00-00-810SDR CA111220003Wire · damaged(CAN) ON APPLICATION OF ACFT EXTERNAL POWER IN THE HANGAR, SMOKE WAS REPORTEDLY FOUND IN LOWER CONTACTOR BOX AREA, RT AC CONTACTOR BOX. RESOLVED ON W/O: 316378 TASKCARD: NR-00004, ON INSPECTION OF LIMITER BOX, ATTATCHED TO BOTTOM OF CONTACTOR BOX, HEAVY ARCINSDR CA120104003Terminal · loose(CAN) STARTER TERMINAL WAS FOUND LOOSE DURING 50 HOUR INSPECTION. STARTER REPLACED.SDR CA111216006Connector · burned(CAN) THE RIGHT APPROACH LIGHT WAS FOUND NOT WORKING DURING A SERVICE CHECK. TROUBLESHOOTING WAS CARRIED OUT OVER THE NEXT 10 DAYS. A LOOSE CONNECTOR WAS FINALLY LOCATED AT LOCATION 9812-P924. ON INSPECTION IT WAS FOUND THAT THE PINS WERE BURNED DUE TO THESDR AALA20111213JFK01Wire Harness · inoperativeJFK - INFLIGHT BOS-MIA. CREW REPORTED LEFT AC BUSS FAILED. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT INTEGRATED DRIVE GENERATOR HARNESS CABLE. SYSTEM GROUND CHECK NORMAL OPERATION.SDR UALA2011120706729Feeder Cable · damagedNR 1 ENG IDG FEEDER CABLES AT IDG BLUE AND YELLOW COLOR IDENTIFICATION SLEEVES DAMAGED. REPLACED IDENTIFICATION SLEEVES.SDR MALA110273Wire · failedON DEPARTURE, AFTER COMPLETION OF THE TAKEOFF CHECKLIST. RECEIVED SOLID LT SIDE MASTER WARNING. SOLID BRIGHT TAKE OFF INHIBIT LIGHT. SOLID LT OIL PRESSURE CWP LIGHT. F/O SIDE NR 2 PFD FLICKERED DIM, BRIGHT, AND THEN COMPLETELY OUT. ALSO OBSERVED VERY ACRIDSDR CA111209001Connector · shorted(CAN) DURING CLIMB THE LT ELEVATOR HORN HEAT CAUTION LIGHT CAME ON. THE ACFT WAS ALREADY OPERATING ON THE SECONDARY HEAT ELEMENT AND THUS RETURNED TO THE MTC BASE IT DEPARTED FROM. DURING MTC T/S IT WAS NOTICED THAT ALL OF THE NAVIGATION LIGHTS WERE U/S ALSO ASDR QXEA2011120101266Connector · corrodedCORROSION ON SEVERAL CONNECTOR PLUGS STA 15.0 BL0. ACFT DOWN FOR C-CHECK.SDR REXA201100884Wire · damagedIDG 2 CAUTION MSG. EMERGENCY DECLARED. IDG 2 INTERMITTENT BUT MOSTLY ON AFTER FL170. REPAIRED WIRE TO RT IDG OVERTEMP SWITCH IAW ESPM 20-17-10. RECONNECTED RT IDG IAW AMM 24-11-01. OPC GOOD.SDR A8JA201111260010Connector · corrodedDURING CLIMB, AT 5000 FT IN IMC CONDITIONS, CREW NOTICED RED 'AC FAIL' LIGHT & A FLASHING "MASTER CAUTION" LIGHT. CREW NOTICED AUTOPILOT DISENGAGE, ALTITUDE PRE-SELECT WENT BLANK, FLIGHT DIRECTOR "DISAPPEARED", & NR 1 ADI "TUMBLED". "NR 1 INVERTER FAIL" AMBSDR UALA2011112706498Wire · chafedELECRICAL WIRE CHAFING ON STRINGER RT WING DRY BAY WS 1217 STR L13 JUST FWD OF TANK ACCESS. FIBER SHEATH AND BRAIDED WIRE CONDUIT WORN THROUGH, INNER CONDUIT IS INTACT AND NO VISIBLE DAMAGE TO ELECTRICAL INSULATION OR WIRE. WEAR ON UPPER AFT EDGE OF STRINGERSDR CA111122005Clamp · out of position(CAN) THE UPPER AFT SCREW RETAINING PANEL 120A-2812 WAS FOUND TOUCHING A WIRING BUNDLE LOCATED BEHIND THE CENTER CONSOLE PANEL, 120A-2880. WE REPLACED AND REPOSITIONED THE CLAMP, RSGU 1.13/12-W5-SILICON, WITH CLAMP, RSGU-15/15-W6. THIS ALLOWED THE SCREW TO BSDR AALA20111122JFK01Cable Assy · faultyJFK - CREW REPORTED ELECTRICAL ISSUES FOLLOWED BY RIGHT GENERATOR FAILURE. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CABLE ASSEMBLY TO RIGHT INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECK NORMASDR FDEA201111194978Feeder Cable · burnedDURING C-CHECK, NR 3 ENGINE PYLON, POWER FEEDER CABLE ONE PHASE IS ARCING AND BURNING THRU STRUCTURAL MEMBER BELOW PRECOOLER PLENUM ASSY BETWEEN APPROX YN 259 AND YN 268. R & R NR 3 ENG PYLON POWER FEEDER CABLE IAW EO 8-2450-7-5009 PT2.SDR HCMA2012F00018Wire · shortedACFT DEPARTED. APPROX 10 MINUTE INTO FLIGHT, PILOT NOTICED SMALL ELECTRICAL PROBLEMS SUCH AS A SCRATCHY INTERCOM AND VOLUME CHANGING. NOTICED RADIO, GPS, VIDEO SCREEN AND AIR CONDITIONING SYS GO OFF LINE. DID NOT NOTICE A GENERATOR LIGHT AT THIS TIME. RETURSDR DXTA2011111404787Wire · chafedIN CRUISE AT FL230 A STRONG ELECTRICAL ODOR WAS DETECTED IN THE FWD CABIN AND COCKPIT. SECURED INTERIOR ELECTRICAL SWITCH AND ODOR DISSIPATED. FOUND THROTTLE QUADRANT PANEL WIRE CHAFED. REPAIRED PER WM 20-10-07. OPS CHECK GOOD.SDR UALA2011111106162Wire · damagedCREW ABORTED TAKEOFF AT APPROXIMATELY 80 KNOT DUE TO NR 1 GEN DRIVE LIGHT AND ASSOCIATED EICAS MSG. ACCOMPLISH HIGH ENERGY STOP CHECK PER MM 05-51-14 201. ITEM ROLLED FORWARD. ACP'D INSP PER AMM. NO DEFECTS NOTED. DUE TO RECENT REPORTS OF THE NR 1 ENG IDGSDR CA111109008Clamp · out of position(CAN) THE UPPER AFT SCREW RETAINING PANEL 120A-2812 WAS FOUND TOUCHING A WIRING BUNDLE LOCATED BEHIND THE CENTER CONSOLE PANEL (120A-2880). REPLACED AND REPOSITIONED THE CLAMP (RSGU 1.13/12-W5-SILICON) WITH CLAMP (RSGU-15/15-W6). THIS ALLOWED THE SCREW TO BE SDR CA111107001Wire · burned(CAN) DURING TAXI, CREW HEARD A LOUD BANG IN FLT DECK ASSOCIATED WITH NUMEROUS AC CIRCUIT BREAKERS (CBS) POPPING. AC FUEL PUMP & RT WINDSHIELD HEAT CBS AMONG THOSE POPPED. INITIAL INSPECTION, IT LOOKS LIKE 5 CABLES ARE COMPLETELY BURNED THROUGH AND 6 OTHER CSDR CA111104005Feeder Cable · burned(CAN) DURING 100 HR - ROUTINE INSPECTION, RT FWD FUSELAGE SIDE PANEL OPENED UP TO ACCESS TUBING INSPECTION, BOTTOM CABLE FOUND DAMAGED BEHIND SIDE PANEL DOOR TO CABLE CHAFING ON TAIL END OF PANEL SCREW. HOLE BURNED THROUGH CABLE INSTALLATION AND INTO CORE.
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