JASC 3010
Service difficulty reports · 2,241
Reports filed under 3010 · Airfoil Anti/De-ice 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 = '3010' 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 = '3010' 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 RRXA001099Valve · failedWHEN WING ANTI-ICE IS TURNED ON - RIGHT 1506 VALVE DISAGREE LIGHT COMES ON WITH NO DROP IN PNEU PRESS FEFI CODE 30-11-00. REMOVED AND REPLACED RIGHT WING ANTI-ICE VALVE IAW M/M 30-00-00. OPS OK ON CHECK.SDR SWIA972210Ejector Valve · malfunctionedCLIMBING THROUGH 17,000 FEET, LEFT AND RIGHT OUTBOARD LEADING EDGE DEICE INOP LIGHTS ILLUMINATED. TIMER 2 HAD THE SAME RESULT AFTER PROCEEDING PER QRH. AFTER LEAVING 6000 FEET AND ICING CONDITIONS THE BOOTS WORKED FINE. RETURNED TO SEA. REMOVED AND REPLACEDSDR COMA0061052Controller · malfunctionedRIGHT HAND WING ANTI-ICE CAUTION MESSAGE.COULD NOT DUPLICATE. REPLACED THE ANTI-ICE TEMP CONTROLLER FOR TROUBLESHOOTING.SDR CA010111018Timer · malfunctioned(CAN) DEICER BOOTS ARE RUNNING CONTINUALLY WHEN SELECTED, THE TIMER NORMALLLY ALLOW A 20 SEC DELAY AFTER A COMPLETE INFLATION SEQUENCE TO START OVER AGAIN. AT THE PRESENT TIME, THERE IS NO DELAY AT THE END OF A FULL SEQUENCE, IT JUST STARTS ALL OVER AGAIN RIGHSDR MWEA001246Sensor · inoperativeAFTER AIRFOIL ICE PROTECTION WAS SELECTED ON THE LH ICE PROTECTION TEMP HIGH ANNUNCIATOR ILLUMINATED. -- REMOVED AND REPLACED TEMP HIGH SENSOR.SDR SWIA972193Regulator · failedLEADING EDGE ICE PROTECTION TIMER 1 FAILED IN FLIGHT BOTH LIGHT AND HEAVY. RETURNED TO SBA. INSTALLED SERVICEABLE 18 PSI REGULATOR FOR NUMBER TWO SIDE IAW 30-1-00. RAN ENGINE ON GROUND FOR 20 MINUTES. OPS CHECK GOOD. SN ON B2423SDR 20001227SH009Contactor · failedTHIS CONTACTOR, PN 128-384054-5, WHEN INSTALLED IN THE K-251 POSITION OF THE HORIZONTAL STABILIZER DEICE SYSTEM CAUSES THE SYSTEM TO FAIL WHEN THE AIRCRAFT IS AT AN ALTITUDE THAT A MINUS 10 DEGREES OR COLDER RAM AIR TEMPERATURE IS ACHIEVED. (X)SDR SWIA972157Regulator · failedTHREE MINUTES AFTER TAKE OFF, LEFT DUCT LEAK LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURE 6:39 LIGHT REMAINED ILLUMINATED. AFTER 3 MINUTES, SHUT DOWN ENGINE (LEFT). LIGHT EXTINGUISHED AT THAT TIME. RESTARTED LEFT ENGINE WITH LEFT BLEED/PACK OFF. RETURNED TO LSDR CA010108011Regulator · failed(CAN) DURING SCHEDULED INSPECTION, BOTH FORWARD AND AFT DE-ICE PRESSURE REGULATORS IN THE NR 2 NACELLE FAILED THE FUNCTION TEST PRESCRIBED IN MAINTENANCE TASK 3010/04. BOTH REGULATORS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. S/N RF3346 6058 CYC SDR CA001228029Filter · plugged(CAN) PENUMATIC DE-ICE SYSTEM FAILED IN FLIGHT. DE-ICE PRESSURE WAS DOWN TO 12-15 PSI INFLIGHT AND 8-10 PSI ON GROUND. MANUAL PRESSURE 1518 +/-1 PSI. MAINTENANCE FOUND THE SYSTEM FROZEN, AND ALL THE WATER SEPARATOR FILTERS PLUGGED WITH SOOT. THE FILTERS WERE ASDR 20001227SH013Duct · damagedPILOT REPORTED THE WING DEICE SYSTEM WAS INOPERATIVE. AFTER VERIFYING ELEC PORTION OF SYS WAS FUNCTIONING, A GROUND OPER CHK PERFORMED. DISCOVERED VERY LITTLE FLOW GETTING TO RT SLATS, LT SLATS APPEARED TO BE GETTING SUFFICIENT HEAT, BUT BOTH SIDES ARE REQUISDR MWEA001199B-Nut · damagedWHEN TAIL SELECTED RIGHT ICE PROTECTION TEMP HIGH LIGHT ON. FOUND B-NUT AT RIGHT ICE PROTECTION THERMOSTAT STRIPPED. B-NUT WAS REPLACED.SDR MWEA001183Sensor · inoperativeCLIMBOUT OF MKE, RIGHT ICE PROTECTION TEMP HIGH LIGHT CAME ON. REMOVED AND REPLACED THE HIGH TEMP SENSOR.SDR RAIA0011006Tube · failed6317-BOS- STABILIZER ANTI ICE FAIL EICAS MESSAGE ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED ANTI ICE TUBE ASSEMBLY.SDR CALA0001811Panel · shortedTHE LEFT WING UPPER ANTI-ICE BLANKET CONNECTION PANEL WAS DISCOVERED TO BE BURNED DUE TO A SHORT CIRCUIT. THE LEFT WING UPPER INTERFACE PLATE WAS REMOVED AND REPLACED AND THE UPPER WING SURFACE HEATERS WERE PLACARD INOPERATIVE. APPROPRIATE CIRCUIT BREAKERS WSDR COMA0060903Sensor · misinstalledLEFT WING OVERHEAT WARNING. SEALED THE OVERHEAT SENSOR WITH HIGH TEMP SEALANT.SDR SWIA972087Ejector Valve · failedLEADING EDGE DEICE BOOT (MIDDLE/BOTH WINGS) INOP IN FLIGHT. RETURNED TO SLC. WORKS FINE ON GROUND. REMOVED AND REPLACED WING MIDDLE DEICE EJECTOR VALVE GROUND. RAN AIRCRAFT AT LOW AND HIGH PRESSURE AND ALL BOOTS OPS AND LEAK CHECKS OK.SDR 20001129SH015Blanket · shortedLEFT HORIZONTAL STABLILIZER HEAT BLANKET SHEARED, BURNING A .6250 INCH HOLE IN THE LEADING EDGE OF THE HORIZONTAL STABILIZER 5 INCHES OUTBOARD FROM THE INBOARD EDGE. (X)SDR SWIA972060Ejector Valve · failedLOSS OF OUTBOARD LEADING EDGE WING DEICE. RETURNED TO SLC. REMOVED AND REPLACED OUTBOARD WING EJECTOR VALVE WITH SERVICEABLE UNIT IAW MM 30-20-04. OPS CHECKS GOOD. P/N ON: 3D237606, S/N: PJ334, S/N OFF: N3517.SDR SWIA972062Boot · failedMIDDLE LEFT WING DEICE BOOT FAILED ON CLIMBOUT, BOTH TIMERS. RETURNED TO LAX. REMOVED AND REPLACED PRESSURE SWITCH FOR LEFT WING MIDDLE DEICE BOOT WITH SERVICEABLE UNIT. OPS CHECKS GOOD. P/N ON: 211C117-183, S/N: M414, S/N OFF: V08082A.SDR PLGA001018Warning Light · illuminatedBOS-PQI - FLT 4720 - DURING FLIGHT, CREW NOTED THAT THE STABILIZER DE-ICER BOOT STATUS LIGHT WAS ON. CREW RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM AFTER SEVERAL SYSTEM CHECKS. THE AIRCRAFT WAS RETURNED TO SDR DLM88002031Duct · brokenTAIL COMPARTMENT TEMP HI LIGHT ILLUMINATED ON CLIMBOUT AT FL190. REPLACED BROKEN AIR CONDITIONING DISTRIBUTION DUCT.SDR SWIA972038Regulator · failedRIGHT DUCT LEAK LIGHT ON INFLIGHT. FOLLOWED QRH AND LIGHT DID NOT GO OUT AFTER 3 MINUTES. SHUT DOWN RIGHT ENGINE AND RETURNED TO SLC. TROUBLESHOOT RIGHT BLEED AIR SYSTEM. REMOVED THE RIGHT DEICE AIR PRESSURE REGULATOR AND INSTALLED A SERVICEABLE REGULATOR.SDR SWIA972036Boot · failedTIMER ONE LIGHT VERTICAL STABILIZER BOOT FAILED. RESET TO TIMER TWO, VERTICAL BOOT FAILED FOR SECOND TIME. FOLLOWED QRH PROCEDURE AND ALL BOOTS FAILED. REPEATED THREE MORE TIMES, EACH TIME ALL BOOT SECTIONS FAILED. DIVERTED TO IDA. RAN AIRCRAFT AND PERFORSDR DL72S001990Isolation Valve · chafedWHILE TROUBLESHOOTING WING ANTI-ICE PROBLEM FOUND RIGHT BLEED AIR ISOLATION VALVE WIRING CHAFING ON PNUEMATIC DUCT BETWEEN THE VALVE AND THE AFT PACK VALVE. WHILE INSTALLING PNUEMATIC DUCT FOUND WIRE BUNDLE FOR LEFT BLEED ISOLATION VALVE CHAFED. REPAIRED WIRSDR SWIA972019Boot · inoperativeRIGHT OUTBOARD STABILIZER BOOT INDICATES INOP. RETURNED TO SEA. INSTALLED SERVICEABLE OUTBOARD STABILIZER EJECTOR VALVE AND RIGHT DEICE PRESS REGULATOR. FUNCTIONAL TEST GOOD. 30-10-00 S/N: N0190 S/N OFF: N218 EJECTOR VALVE, S/N: RF2220, S/N OFF: RF1SDR RAIA0010002Boot · failed7323-BMI- CCT 1 VERTICAL STABILIZER AIRFOIL DEICE FAILED DURING TAXI. MAINTENANCE DEFERRED SYSTEM PER MEL. MAINTENANCE REPLACED VERTCAL STABILIZER LEADING EDGE/BOOT ASSEMBLY.SDR CA000925016Valve · failed(CAN) WHILE ACCOMPLISHING MAINTENANCE TASK 3010/04, BOTH DEICE PRESSURE RELIEF VALVES IN NR2 NACELLE FAILED STEPS 8 THROUGH 15. THE VALVES WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. VALVE S/NS RF-3388 & RE-3394.SDR DL73K001850Valve · stuckNR 1 ENG ANTI-ICE COWL VALVE FAILED TO OPEN IN FLIGHT. REPLACED NR 1 ENG ANTI-ICE VALVE. GROUND OPS NML. LK CHECK GOOD.SDR VNAA0009020Control Valve · failedFLIGHT 4060 WAS EN ROUTE TO CAE AND HAD AN AIRFOIL DE-ICE FAIL. FLIGHT 4060 WAS IN ICING CONDITIONS AND WAS INSTRUCTED TO RETURN TO PIT FOR MAINTENANCE. MAINTENANCE INSPECTED AND REPLACED THE EJECTOR FLOW CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE SDR VNAA0009018Control Valve · failedFLIGHT 4170 LEVELED OFF IN CRUISE AND FOUND THEY WERE IN ICING CONDITIONS WHEN THE CREW RECEIVED A AIRFOIL DE-ICE FAIL CAS MESSAGE. THE CREW DECIDED TO RETURN TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE EJECTOR FLOW CONTROL VALVE IN ACCORDANCE WITH DOSDR MWEA00813Connector · failedWHEN TAIL BUTTON IS PUSHED, ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATES. REMOVED AND REPLACED CONNECTOR.SDR VNAA0009012Valve · failedFLIGHT 4191 WAS IN ICING CONDITIONS AND HAD THE RIGHT HAND INBOARD DE-ICE BOOT FAIL. FLIGHT 4191 RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND REPLACED THE EJECTOR FLOW CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-13-06. OPERATIONAL CHSDR 00FDEA00605Switch · closedAT 800 FEET CLIMBING OUT, ANTI-ICE DUCT OVERHEAT LIGHT ON, WHEN CORRESPONDING BLEED AIR SWITCHES CLOSED, NO HELP. WHEN NR 3 ENGINE POWER RETARDED LIGHT WENT OUT. RAN NR 3 ENGINE PER JET RUN, HANDBOOK CHAPTER 5 OPERATIONAL CHECK GOOD. FOUND RIGHT WING ANTI-ISDR RAIA0007025Boot · failed6153-JFK- AIRFRAME DEICE INOPERATIVE IN BOTH AUTO AND MANUAL MODES. MAINTENANCE INSPECTED AND DEFERRED AIRFRAME DEICE SYSTEM PER MEL. MAINTENANCE REPLACED LEFT HORIZONTAL STABILIZER LEADING EDGE/BOOT ASSY.SDR SIMA1991Anti-Ice Valve · inoperativeHOU - FLT 3622 - CREW ABORTED TAKEOFF DUE TO WARNING INDICATION ON EICAS HOWEVER, THE CREW COULD NOT IDENTIFY WARNING. HAD THE CREW TO PERFORM PREFLIGHT COCKPIT CHECKS AND TEST TO SEE IF ANY OF THE SYSTEMS FAILED. NO SYSTEM FAIL CREW THEN PROCEEDED TO TRY TASDR RAIA0007018Boot · failedBWI- WING ANTI-ICE FAULT LIGHT ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND DEFERRED WING DEICE SYS PER MEL. MAINTENANCE REPLACED LEFT HORIZONTAL STABILIZER LEADING EDGE/BOOT.SDR RAIA0007006Seal · failed7202-STL- DURING TAXI RIGHT DUCT FAIL CAPTION ILLUMINATED. MAINTENANCE REPLACED RIGHT DUCT BLEED SEALS.SDR 20001030SH001Gasket · defectivePASSENGER INFORMED FLIGHT CREW OF SMOKE IN AREA AT LT REAR CABIN BY DIVAN SEAT AND NOTED CARPET APPEARED TO BE MELTED. AIRCRAFT DIVERTED TO LAS VEGAS AS EMERGENCY LANDING. MAINTENANCE DISCOVERED DEFECTIVE GASKET AT EXIT DUCT THAT ROUTES BLEED AIR TO LT WING.SDR GAIA00363Duct · crackedFLT 202 - DFW-SEA - ON CLIMB-OUT OF DFW, ENGINE NR 3 STRUT OVERHEAT LIGHT CAME ON. ABNORMAL PROCEDURES WERE USED. OVERHEAT LIGHT WENT OUT. AIRCRAFT MADE AN UNEVENTFUL LANDING AT SEA. FOUND SEVERAL PNEUMATIC DUCT LEAKS IN STUB WING. REPLACED AND RESECURED SDR RAIA0006010Valve · failed6315-BOS- WING NUMBER 2 ANTI-ICE FAULTED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED RIGHT WING ANTI-ICE VALVE.SDR RAIA0006007Switch · failed6305-BOS- WING ANTI-ICE FAILED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED WING ANTI-ICE HIGH PRESSURE SWITCH.SDR 2000UALA00309Regulator · failedBLEED VALVE MALFUNCTION PREVENTING ANTI-ICING ON ONE WING AND ENGINE. *S/D* FOUND FAILED PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV). REPLACED PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV).SDR 0001939868Duct · looseSLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED ON APPROACH INTO IND. AIRCRAFT ROLLED SLIGHTLY TO THE LEFT. PERFORMED COM PROCEDURE FOR NO-SLAT LANDING AND LANDING WAS NORMAL. MAINTENANCE CORRECTED A LOOSE ANTI-ICE ''T'' DUCT ON THE RIGHT WING AND ADJUSTED SDR VNAA0005015Line · disconnectedWHILE CLIMBING THROUGH FL170 THE AIRCRAFT BEGAN TO ACCUMULATE ICE. THE CREW SELECTED THE FAST CYCLE FOR THE DE-ICE BOOTS AND RECEIVED A RIGHT HAND INBOARD BOOT FAIL CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK, CONTACTED MAINTENANCE, AND RETURSDR 00FDEA00362Valve · faultyBLEED AIR 2 FAULT ALERT WHEN ANTI-ICE ON. REPLACED PRESS REG PILOT VLV OF NR 2 ENG AND FUNCTION TEST WAS GOOD PER MM 36-12-20. REPLACED PSC-1 AND RTS PASSED PER MM 36-10-02.SDR VNAA0005013Ejector Valve · failedWHILE EN ROUTE, THE CREW EXPERIENCED AN AIRFOIL DE-ICE FAIL ON THE TAIL IN FAST AND SLOW MODES. MAINTENANCE ADVISED THE CREW TO RETURN TO PIT DUE TO ICING CONDITIONS REPORTED EN ROUTE TO EVANSVILLE. MAINTENANCE INSPECTED AND REPLACED THE EJECTOR FLOW CONTROLSDR 2000UALA00252Connector · failedRIGHT WING ANTI-ICE VALVE INOPERATIVE. *S/D* MAINTENANCE REPORTED FINDING BURNT WIRING IN STUBWING VALVE CONNECTOR D932. CONNECTOR WAS REPLACED. OPERATIONAL CHECK NORMAL. NO FURTHER PROBLEMS REPORTED.SDR RAIA0005016Boot · leaking6220-DCA- CREW REPORTS DEICE SYSTEM CCT NR 1 FAULT LIGHT ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND DEFERRED PER MEL. MAINTENANCE REPLACED LEFT INBOARD WING LEADING EDGE.SDR CA000516027Timer · failed(CAN) WHILE ON APPROACH, THE PILOT SELECTED DE-ICE ON. AFTER 8 SECONDS, A DE-ICE FAIL WARNING WAS OBSERVED. SELECTING THE DE-ICE OFF DID NOT CANCEL THE WARNING LIGHT SO THE PILOT SECURED THE CIRCUIT BREAKER. MAINTENANCE LATER DETERMINED THAT THE DE-ICE TIME
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