JASC 2400
Service difficulty reports · 1,188
Reports filed under 2400 · Electrical Power System, 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 = '2400' 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 = '2400' 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 CALA2017091503160Power Supply · faultySEATS 5A 5B HAD SPARKS AND A LITTLE SMOKE AFTER USING SEAT OUTLETS. UNPLUGGED. REPLACED THE IN SEAT POWER SUPPLY AT SEATS 5A, 5B IAW 44-21-14, OPS CHECKED NORMAL.SDR 19MA2017102608379Buss · failedACFT DEPARTED, AFTER ABOUT 10 MIN INTO FLIGHT, PILOT EXPERIENCED A RIGHT GENERATOR TIE ANNUNCIATOR LIGHT. THE PILOT RESET THE BUSS TIE, BUT LIGHT CAME BACK ON. SHORTLY AFTER THE LIGHT ILLUMINATED A SECOND TIME THE LT GENERATOR FAIL LIGHT ILLUMINATED. AT THAT SDR DALA2017090606680Electrical Sys · unknownRETURNED TO DEPARTURE DUE TO A SUSPECTED ELECTRICAL PROBLEM, CAUSING FLICKERING LIGHTS AND PULSATING IN THE CONTROL COLUMN. PERFORMED A STDBY POWER SYS OPS TEST WITH NTF. REPLACED THE BATTERY AND CHARGER, LEFT TRU, RELAYS K105 AND K109. RAN LEFT ENGINE WITHSDR ASAA2017090321795Warning Light · false activationOVERHEAD ELECTRICAL LIGHT STAYS ILLUMINATED. ACFT GROUNDED. PERFORMED P5-13 ELECTRIC LIGHT MESSAGE BITE IAW FIM 24-31 TASK 801. FOUND MESSAGE FOR SPCU INOPERATIVE. MESSAGE CLEARED AND ELECTRIC LIGHT EXTINGUISHED. INTERMITTENT FAULT IAW FIM 24-34 TASK 802.SDR ASAA2017083121793Warning Light · false activationWHEN SWITCHING FROM GROUND POWER TO APU POWER, THE RIGHT SOURCE OFF LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED A POWER SWITCH FROM GROUND POWER TO APU POWER SEVERAL TIMES WITH NO DEFAULTS NOTED. GOOD FOR RETURN TO SERVICE AT THIS TIME.SDR FDEA201708292398Contactor · detectedWHILE WORKING INBD WRITE UP, DETECTED SMOKE IN COCKPIT. LOOKED TO CIRCUIT BREAKER PANEL 131VU SAW FLICKER OF FLAME FROM BEHIND PANEL. OPEN PANEL AND EXTINGUISHED FLAMES. INSTALLED NEW APU START CONTACTOR 5KA. DAMAGED CONTACTOR 5KA MANUFACTURER INTERTECHNIQSDR ASAA2017082321701Warning Light · false activationELEC LIGHT ILLUMINATED DURING POWER TRANSFER ON GROUND. ACFT GROUNDED. PERFORMED FIM 24-31-801. SPCU 1 INOPERATIVE FAULT APPEARED AND CLEARED DURING BITE TEST. INTERMITTENT FAULT.SDR 2017FA0000534Regulator · malfunctionedTHE PILOT REPORTED THE SMELL OF SOMETHING ELECTRICAL BURNING IN THE COCKPIT AND MADE AN EMERGENCY LANDING WITHOUT INCIDENT.SDR UIEA2017081411467Stator · damagedSTATUS MESSAGE RIGHT ENGINE EEC C1. REMOVED AND REPLACED THE RT ENG CONTROL ALTERNATOR STATOR AS PER AMM 73-21-08, RAN ENGINE OPS AND LEAK CHECKS OK. NO MESSAGES THIS CLEARS MEL 73-21-01 </SPAN><BR DATA-MCE-BOGUS="1" /></P>)SDR 2017FA0000551Belt · mismanufacturedHAD INFLIGHT FAILURE OF THE ALTERNATOR. POST FLIGHT INSPECTOR SHOWED THE ALTERNATOR PULLEY HAD BROKEN, CAUSING THE BELT TO COME OFF THE ALTERNATOR. NO DAMAGE TO THE BELT WAS NOTED. INSTALLED THE NEW ALTERNATOR ON THE ACFT. WITH IDLER PULLEY AT ITS CLOSESTSDR DALA2017070305168Switch · malfunctionedDURING TAKEOFF AT APPROXIMATELY 100 KNOTS, RECIEVED A TAKEOFF WARNING WITH A CONFIGURATION LIGHT. CREW ABORTED THE TAKEOFF. MAINTENANCE PERFORMED PSEU BITE. NO EXISTING FAULTS. PERFORMED PSEU TAKEOFF WARNING TEST IAW FIM 31-51-00-810-801. FOUND ONE FAULT 3SDR CALA2017061601825Module · odorVISUALLY DETECTED LIGHT SMOKE IN THE CABIN. ODOR THROUGHOUT THE ACFT. METALLIC OR PLASTIC IN NATURE. PERFORMED CONDITIONAL INSPECTION AMM 05-51-26-800-801C1. ONLY FINDINGS WERE FAINT ELECTRICLA ODOR NEAR ROWS 9, 10, AND 11 IN SEAT POWER. R & R THE SEAT POSDR CALA2017061101791Socket · looseFA REPORTED ELECTRICAL BURNING ODOR AT ROWS 8-10. ODOR DISIPATED MINUTES LATER. ISOLATED TO ROWS 8-10. F/O WENT TO THE AREA OF ODOR & DID NOT DETECT ANYTHING. ODOR SEEMED TO BE ELECTRICAL IN NATURE. INSPECTED THE AREA FOR OBVIOUS ELECTRICAL PROBLEMS, FOUNSDR UIEA2017060900991Motor · failedSTRONG ODOR OF SMOKE IN THE FLIGHT DECK. TROUBLESHOOTING SHOWED MAIN DECK CARGO PDU 9R MOTOR BURNED, TRIPPING THE CIRCUIT BREAKER. AND 10R OVERHEATED. BOTH PDU'S REMOVED AND COVER PLATE INSTALLED.SDR ASAA2017052420867Circuit Breaker · trippedSTANDBY BUSS SECTION 2 CIRCUIT BREAKER TRIPPED. ACFT GROUNDED. RESET THE CIRCUIT BREAKER IAW AMM 26-60-01. NO DISCREPANCIES NOTED. FUNCTIONAL CHECK OF SPCU OK IAW AMM 24-34-11.SDR P5CA2017052500143Warning Message · false activationAT FL 180 DURING DECENT, BOTH UTILITY BUSS EICAS MESSAGES CAME ON. BOTH GENERATORS NORMAL. RESET BOTH BUSSES IAW QRH, ALL RETURNED NORMAL IAW FIM 24-FAULT CODE 72, FIGURE 712. FUNCTION NORMAL IAW AMM 24-51-05, UTILITY BUSS TEST & FUNCTION NORMAL.SDR 2017FA0000201Solenoid · defectiveTHE SOLENOID WORKED WHEN FIRST INSTALLED. AFTER ONE OR TWO FLIGHTS IT BECAME INTERMITTENT, IT WOULD TAKE MORE THAN ONE FLIP OF THE MASTER SWITCH TO OBTAIN POWER TO THE PANEL AND STARTER. AFTER ANOTHER FLIGHT IT WOULD NOT CLOSE. TESTED THE DEVICE WHILE INSTALLSDR MASA2017051412300Circuit Card · odorSTRONG ELECTRICAL ODOR AFT LAVATORY, NO SMOKE. ISOLATED TO A PCU CARD AT 23CD.SDR IPXA2017041416115Buss · failedRIGHT EMERGENCY BUSS FAILED. PERFORMED FIM 24-25-01-00. REPLACED THE SENSE RELAY R2-5157 IAW WDM 24-61-51. REPLACED RT EMERGENCY AC FEED RCCB B1-138 IAW MM24-50-01. REPLACED EPCU IAW MM 24-08-01. PERFORMED EPCU RTS TEST IAW MM 24-08-01 TEST PASSED. PERFORMED SDR AALA201703179034Outlet · damagedHEAVY WHITE SMOKE FROM POWER PORT AT SEAT 7D/E. SMOKE STOPPED AFTER POWER TURNED OFF. FOUND LIQUID DAMAGE. REMOVED AND REPLACED SEAT POWER BOX AT 7DEF IAW AMM 44-22-44-000-801 (AALA201703179018) AND AC OUTLET UNIT AT 7D IAW AMM 44-22-43-000-801. OPERATIONASDR IPXA2017031415124Buss · no testNO EMERGENCY AC NOR DC BUSSES TEST DURING PREFLIGHT ANNUNCIATOR LIGHTS TEST. PERFORMED ANNUCIATOR CONTROL UNIT TEST WITH BAF SWITCH ON IAW MM 33-15-01. OPS CHECKED GOOD. ALL LIGHT ILLUMINATED.SDR HALA2017030600049Circuit Breaker · trippedMULTIPLE CIRCUIT BREAKERS TRIPPED.SDR DXTA2017030506378Unknown · multiple failLOW FUEL 1 AND LOW FUEL 2 ANNUNCIATION LIGHTS FLASHED ON AND THEN BACK OFF AT 90 KIAS, DURING TAKE-OFF ROLL. AT APPROXIMATELY 8000 FT. MSL DURING THE CLIMB, THE SAME LIGHTS FLASHED ON AND THEN WENT OFF AGAIN. NO OTHER SECONDARY INDICATIONS NOTED. UPON EXTSDR CALA2017021700374Electronic Unit · faultyEMERGENCY SLIDE/OVERWING LIGHT DOES NOT GO OFF RIGHT BOTH RIGHT FWD AND AFT OVER WING EXIT ANNUNCIATOR LIGHTS ILLUMI NATED IN FLIGHT REMOVED AND REPLACED PSEU PER AMM 32-09-10-400-801 AND PERF ORMED PSEU OPERATIONAL CHECK FOUND NO FAULTS OVERWING DOOR WARNI SDR AALA20170206001Module · no testCOCKPIT PANEL 5 EMERGENCY LIGHT SWITCH FAILED DURING TEST. REPLACED AND TESTED WINDOW HEAT AND EMERGENCY LIGHTS MODULE IAW AMM 30-41-02 AND AMM 30-41-00. ACCOMPLISHED SATISFACTORY OPERATIONAL TESTS ON EMERGENCY LIGHTS IAW AMM 33-51-00. PASSENGER OXYGEN DOORSDR FDEA201701310297Panel · malfunctionedELECTRICAL PANEL HAS TWO ON LIGHTS FOR EMERGENCY POWER, SHOULD HAVE ONE OFF AND ON. REMOVED AND REPLACED ESCP IAW AMM 24-08-02-4 AND PERFORMED ADJUSTMENT AND TEST IAW 24-08-02-5. OPS CHECKED GOOD.SDR HNAA2016123000351Inverter · odorMODERATE ELECTRICAL ODOR IN COCKPIT AND GALLEY. ISOLATED TO SECONDARY INVERTER.SDR DALA2016122710121Receptacle · failedAIRCRAFT SUSTAINED HEAT AND FIRE DAMAGE COCKPIT FLOOR STIFFENER DUE TO ELECTRICAL FIRE ORIGINATING AT THE EXTERNAL GROUND POWER RECEPTACLE. MAINTENANCE REPAIRED DAMAGED STIFFENER IAW ERA 552502-14.SDR DALA2016122110052Control Unit · failedDURING CLIMB OUT, LT & RT UTILITY BUSS OFF CAUTION MESSAGES ON EICAS. NO LUCK RESETTING OR RECYCLING CIRCUIT BREAKERS. RETURNED TO DEPARTURE. PASSENGERS REPORTED A BURNING ODOR IN THE MID CABIN. FOUND BPCU WILL NOT POWER UP AND TO HAVE A FAINT ODOR. R & R SDR UIEA2016111800845Warning Message · illuminatedSTATUS MESSAGE LT IDG VALVE.. ACCOMPLISHED FIM 24-20 FT 802 TABLE 102, LT ELECTRICAL GENERATOR SYS COOLER +28V WIRING, GCU MESSAGE, C837 L IDG VALVE C/B NOT OPEN. CLEARED STATUS, RAN ENGINE L GEN IAW T1074, NO FAULT.SDR DXTA2016111706330Outlet · burnedLEFT OUTLET BELOW THE OVEN TEMP CONTROL SPARKED AND BURNED A CHARGER WHEN INSERTED INTO IT. FOUND BOTH OUTLETS BELOW OVEN TEMP CONTROLLER DEFECTIVE, REPLACED 2 OUTLETS UNDER OVEN TEMP CONTROLLER WITH NEW OUTLETS IN REF WITH GL500 SPM 20-21-00, OPS CHECKED GOSDR BUEA20161104001Relay · hotDETECTED A BURNING ELECTRICAL ODOR AT 160000 FT ALL THE WAY TO THE GATE, NO SMOKE OBSERVED IN THE FLIGHT DECK ONLY ODOR IN THE FLIGHT DECK. NO EMERGENCY DESCENT, NO DECLARED EMERGENCY, UNEVENTFUL LANDING, NO CREW OXYGEN UTILIZED. AIRCRAFT MAINTENANCE WAS NOSDR 2016FA0000539Belt · shearedSQUEALING SOUND AT ENGINE START VOLTMETER SHOWING DISCHARGE. ALTERNATOR BELT WAS SHEARED.SDR HSYA2016092216AUnknown · multiple failBUSS 1 ALL 3 ROWS ALL CIRCUIT BREAKERS TRIPPED, ENGINE FIRE LIGHT ILLUMUNICATED, WENT OUT ON TAXI IN, ELECTRICAL BURNING ODOR.SDR HALA2016072100291Module · failedNR 2 ENGINE SHUTDOWN, AC BUSS 2 FAULT ON ECAM. REMOVED & REPLACED THE NR 2 ECMU IAW AMM 24-29-34. BITE TEST FAILED NR 1 ECMU ATA 242255 GLC-2(9XU2)/ECMU(1XM1). REMOVED & REPLACED CONTACTOR 9XU2, OPS CHECKED OK IAW AMM 24-22-55-400-803A. ACCOMPLISHED TSM 24-SDR ASAA2016071817420Circuit Breaker · trippedDURING THE CROSSFEED CHECK AT CRUISE, THE CROSSFEED SWITCH WAS PLACED IN THE OPEN POSITION WITH NORMAL INDICATIONS. WHEN PLACED BACK IN THE CLOSED POSITION DURING THE CYCLE, THE X-SWITCH WAS INADVERTENTLY PLACED BACK IN THE OPEN POSITON CAUSING THE CROSSFEED SDR JIKA2016071901Electrical Sys · power lossENROUTE, THE PILOT REPORTED A LIGHTNING STRIKE AND LOSS OF ELECTRICAL POWER. THE PILOT CONTACTED ATC, DECLARED AN EMERGENCY AND LANDED AT THE NEAREST AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT, ENGINES AND PROPELLERS NO EVIDENCE OF LIGHTNING STSDR UIEA2016060200392Relay · malfunctionedSTANDBY POWER SYS CHECK FAILED IF EITHER TB14FC3 IS JUMPERED TO GROUND. STBY BUSS OFF LIGHT DOES NOT COME ON OR IF P6J17 CB IS RESET. R & R STBY POWER RELAY K105 IAW AMM TASK 24-33-01-004-004 PAR 2 & TASK 24-33-01-404-005 PAR 3.SDR A6WA201643950Electrical Sys · abnormalCREW REPORTED THAT WHEN THEY APPROACHED THE ACFT IT WAS CONNECTED TO GROUND POWER. CREW REPORTED THAT POWER WAS CYCLING ON & OFF UN-COMMANDED & THAT THEY COULD SMELL A BURNED ELECTRICAL ODOR.SDR UIEA2016051600311Relay · failedLEFT ENG 350 27-NO 28VDC DETECTED. R & R RELAY XLD4N009 K1036. OPERATIONS CHECKED OK IAW 31-41-00.SDR YENA20160504366Module · failedRETURNED TO DEPARTURE. ELECTRONIC DC BATTERY BUSS FAULT MESSAGE DISPLAYED ON ECAM WHILE CLIMBING THROUGH 2000 FT. R & R NR 1 SDAC MODULE IAW AMM 31-55-34. PERFORMED OPS CHECK. NO FAULT ON DISPLAY.SDR QXEA2016042100274Unknown · unknownPRIOR TO GOING "DOORS UP", RAMPERS NOTICED A STATIC DISCHARGE FROM FWD FUSELAGE ON BOTH SIDES. DISCHARGE IS NOTICEABLE TO THE TOUCH AND IS CONTINUOUS. ACFT WAS NOT PLUGGED INTO GROUND POWER AT ALL, AND WAS RUNNING ON APU POWER ONLY. NO ABNORMAL INDICATIONS SDR QMLA2016041316040Unknown · malfunctionedWHILE EN-ROUTE, THE ACFT EXPERIENCED A MOMENTARY COMPLETE LOSS OF ELEC POWER THAT LASTED ABOUT 2 SECONDS, THEN RETURNED TO NORMAL WITH AN AMBER GOV LIGHT ILLUMINATED. WE RETURNED TO BASE FOLLOWING THE EMER PROCEDURE FOR AN AMBER GOV LIGHT & LANDED WITHOUT INCSDR OZCA20160310113Relay · failedENROUTE LOST LT MAIN BUS & ALL ASSOCIATED BUSES. R & R LT MAIN BUS RELAY. ALL OPERATIONAL CHECKED OK.SDR QMLA2016030116016Panel · burnedPILOT WAS PERFORMING GND RUN FOR ENG COMPRESSOR WASH, PILOT NOTICED SOME SMOKE FROM PEDESTAL SWITCH AREA & A BURNING SMELL, BLUE LIGHTS ON FUEL PUMP, TAXI & LANDING LIGHTS FLICKERED ACCORDING TO THE PILOT. ACFT WAS SHUT DOWN & DISCONNECTED THE BATTERY. REMOVSDR 2016FA0000083Motor · failedBRUSH BROKE LOOSE AND LODGED IN MOTOR. MOTOR SHORTED AND SMOKE ENTERED THE COCKPIT.SDR ASAA2015121014208Control Unit · malfunctionedELECTRONIC LIGHT ON OVERHEAD ELECTRICAL PANEL FOUND ON PREFLIGHT WITH APU AS ELECTRIC SOURCE. ACFT GROUNDED. P5-13 BITE SHOWS SPCU FAULT. ACCOMPLISHED FIM TASK 24-34, TASK 802, SYSTEM BITES NORMAL, NO FAULTS.SDR CA151204004Outlet · failed(CAN) GPU WAS TURNED ON TO PERFORM MAINTENANCE ON ACFT. ONCE POWER WAS ON THE GPU CABLE SURGED. IMMEDIATELY TURNED GPU OFF AND INSPECTED THE ACFT`S EXTERNAL POWER OUTLET. IN DOING SO FLAME WAS NOTICED COMING FROM THE BACK OF THE OUTLET, FROM THE VOLTAGE PROSDR BIER20151124466Fuse Link · arcedACFT ARRIVED FOR ANNUAL INSPECTION. DURING PRE-INSPECTION GROUND ENGINE RUN TO VERIFY SYSTEM OPERATION, NOTICED ERRATIC AMP INDICATIONS. WITH LT ALTERNATOR "OFF", CROSSTIE SWITCH "ON" AND RT ALTERNATOR "ON", NOTICED INDICATIONS OF 32 AMPS ON LT SYSTEM AND 28.SDR YENA20151121580Contactor · inoperativeEMERGENCY GENERATOR TEST FAILED. R & R RELAYS 12XE AND 16XE, NO HELP, REF SWPM 20-46-50. R & R 3XC 3 POLE CONTACTOR IAW AMM 24-25-55. NO HELP. CONTINUED ON DEFECT 1730594-2.
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