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 RAIA201301120001Pressure Switch · malfunctionedDURING CLIMB THE FLIGHT CREW GAT A WING ANTI-ICE FAIL MESSAGE. AIRCRAFT RETURNED TO ORD. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE NR 2 LOW PRESSURE SWITCH. SYSTEM OPS CHECKED GOOD.SDR ASAA2013010893637Solenoid Valve · failedBOTH WING ANTI-ICE LIGHTS FAILED TO TEST. NR 1 ENGINE COWL VALVE OPEN LIGHT OUT FAILS TO TEST. ENGINE NR 1 AND WING CONTROL ANTI-ICE & RAIN CIRCUIT BREAKER TRIPPED. ACCOMPLISHED FIM TASK 30-11, TASK 810 C/B C148 OPENS INTERMITTENTLY ON GND. NR1 ENG GROUND SDR CA130109009Hose · collapsed(CAN) DURING CRUISE FLIGHT, THE CREW NOTICED THAT THE LT INBD SLAT WAS NOT SHEDDING ICE. THE ANTI-ICE FLEX HOSE FOR THE LT INBD SLAT WAS REMOVED AND FOUND TO BE DELAMINATED IN SEVERAL AREAS OF THE INNER LINING.SDR CVGA201301003Warning System · activatedANTI-ICE DUCT WARNING MESSAGE CAME ON INFLIGHT.SDR VNAA2012123100018Controller · malfunctionedCREW RECEIVED LEFT BLEED DUCT WARNING MESSAGE DURING CLIMBOUT. CREW PERFORMED QRH, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. WARNING MESSAGE EXTINGUISHED SEVERAL MINUTES AFTER QRH WAS RUN. MAINTENANCE TROUBLESHOT LEFT BLEED WARNING AND REMOVED AND REPLSDR UALA2012122707424Anti-Ice Valve · faultyWING ANTI-ICE EICAS MSG DISPLAYED. WING ANTI-ICE VALVE LIGHT REMAINED ILLUM WITH SWITCH OFF. POSITION 2. (1=L, 2=R). FRM CODE: 30-11-04--. SAMC TEXT: DUE TO RELIABILITY ISSUE. REPLACE THE RT VLV PER APPROVED MM. PERFORMED OPS CHECK AS PER AMM 30-11-00 ALLSDR RAIA201212240001Tube · leakingDURING CRUISE FLIGHT THE WING ANTI-ICING FAIL IN ICING CONDITIONS. AIRCRAFT MADE AN UNSCHEDULED LANDING AT DAY. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 LOW PRESSURE SWITCH AND NR 2 WING ANTI-ICING DISTRIBUTION TUBE BETWEEN THE NR 2 WING ANTI-ICINSDR SWIA201232428Shutoff Valve · inoperativeRIGHT WING ANTI-ICE MODULATING SOV INOPERATIVE. REPLACED RIGHT WING ANTI-ICE MODULATING VALVE,SDR ASAA2012121993501Circuit Breaker · trippedNR 1 ENGINE & WING CONTROL CIRCUIT BREAKER TRIPPED. CHECKED W2112-6049, NO SHORT OR GROUND, RESET CIRCUIT BREAKER C148 IAW SWPM 20-60-01. OPS CHECKED WING AND NR 1 ENGINE ANTI-ICE, OPS NORMAL REF MM 30-11-11/501.SDR ASAA2012112093347Anti-Ice Valve · failedPOSITIONING WING ANTI ICE ON BROUGHT A BRIGHT BLUE DISAGREEMENT LIGHT ON THE RT SIDE. UNABLE TO CHANGE WITH SWITCH. REPLACED THE RT ANTI ICE VALVE IAW AMM 30-11-11. LEAK AND OPS CHECKED GOOD IAW AMM 30-11-11.SDR QXEA2012111901406Tmu · malfunctionedCLIMB OUT, BOTH POWER LEVERS IN RATING DETENT, MCL SELECTED, AIRFRAME MODE SELECT WAS SELECTED TO SLOW. AFTER ALL BOOT SETS CYCLED DEICE PRESS CAUTION ILLUMINATED. AFTER RUNNING CHECKLIST, NO BOOT SETS WOULD INFLATE IN SLOW OR FAST. BOOT SETS WOULD INFLATE SDR QXEA2012111601408Tmu · malfunctionedDE-ICE PRESSURE CAUTION ILLUMINATED. DE-ICE PRESSURE NORMAL. DE-ICE PRESSURE CAUTION ILLUMINATION ERRATIC THROUGH ALL CYCLES. DIVERTED, LANDING UNEVENTFUL. ATTEMPTED TO RETRIEVE CDS DATA. UNABLE TO ACCESS ICE PROTECTION SYS. (REF FIM 30-10-00-801). GROUNDSDR ASOA20121015092Sleeve · leakingCREW REPORTED ICE COND- ANTI ICE SYS INOPERATIVE WITH WING ANTI/ICE FAIL. AN ODOR THAT SMELLED LIKE BURNED CRAYONS ENTERED THE CABIN. ANTI-ICE WAS OBSERVED TO WORK INTERMITTENTLY. MX R & R DUAL TEMP CONTROL VALVE SLEEVES THAT WERE FOUND LEAKING. OPS CHECKSSDR QXEA2012101201262Valve · failed"DE-ICE PRESS" CAUTION MESSAGE. RAN AS MUCH OF EMERGENCY CHECKLIST AS TIME ALLOWED BEFORE LANDING. LIGHT DID COME BACK ON AFTER GOING TO MANUAL THEN BACK TO "SLOW" NEVER DID GET PRESS-IND LESS THAN 18PSI IT DID HOWEVER JUMP TO 22 ABOUT THE TIME THE CAUTION MESDR CA121009017Hose · leaking(CAN) DURING A FUNCTIONAL TEST OF THE DE-ICE BOOT, WE HAVE CONNECTED AN AIR PRESSURE REGULATOR TO THE HOSE BLEED AIR FLEXIBLE LINE AND WE HAVE NOTICED THAT THE FLEXIBLE HOSE IS LEAKING. THIS HOSE IS DIRECTLY CONNECTED TO THE ENGINE P3 PICK UP, SO IF THE FLEXISDR UALA2012100805671Circuit Breaker · faultyL WING LEAK EICAS, FLIGHT DIVERTED. RESET CB D11, D12.Z22, Z23, F1, Q 7. NO FAULTS NOTED. PERFORMED BITE TEST OF BMC 1 & 2. NO FAULTS NOTED. PERFORMED IDLE RUN ON ENGINE 1 AND 2 FOR 5 MINS, RUNNING BOTH BLEED SYS. NO FAULTS NOTED.SDR SIMA20121005002Anti-Ice Valve · malfunctionedON FLIGHT 3945 THE CREW RECEIVED A WING ANTI ICE FAIL MESSAGE ON EICAS IN ICING CONDITIONS. THE CREW FOLLOWED AOM 1 PROCEDURE AND THE MESSAGE REMAINED. THE CREW DECLARED AN EMERGENCY AND CONTINUED THE FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRSDR CA121005007Vane · damaged(CAN) ICE VANE ASSY FOUND HANGING IN INTAKE OF COWLING ON LT ENGINE DURING A PREFLIGHT INSPECTION. UPON REMOVAL, VANE WAS FOUND TO BE CRACKED ALONG WITH BOTH MOUNTING BRACKETS.SDR CIEA201209050003Insulation · meltedSMOKE IN CABIN COMING FROM LT BENCH DUCT REAR SEAT. DURING CRUISE FLIGHT AND EVENTUALLY SUBSIDED BEFORE RETURNING TO DEPARTURE AIRPORT. MX INVESTIGATED AND FOUND HOOK AND LOOP ATTACHING THE INSULATION THAT WRAPS AROUND THE WING ANTI-ICE LINE MELTED AGAINST THESDR CA120828006Boot · burned(CAN) LT ELEVATOR HORN FAILED IN FLIGHT, "AMBER FAIL" ON PUSHBUTTON ANNONCIATOR PBA. LT ELEVATOR HORN WAS REPLACED. UPON REMOVAL OF THE FAULTY ASSY, NOTICED THAT THE BOOT ITSELF WAS DEFORMED DUE TO EXCESSIVE HEAT. ALSO NOTICED AN ELONGATED HOLE AND SUSPECT SDR SWAA2012092507972Guide · brokenLEFT WING NR 4 SLAT ANTI ICE SPRAY TUBE GUIDE BROKEN. REMOVED AND REPLACED NR 4 SLAT PER MM.SDR DALA1246530914Cover · corrodedRT WING HEATER BLANKET COVER NR 1410 HAS CORROSION ON LANDING AREA AND UPPER SURFACE AROUND SCREW HOLES (HARDWARE RUSTED). RT WING HEATER BLANKET COVER NR 1410 REPLACED.SDR DALA1246520914Cover · corrodedLT WING HEATER BLANKET COVER NR 1307C CORRODED AND HARDWARE HAS HEAVY RUST OFF A/C. LT WING BLANKET REPLACED.SDR DALA1246510914Cover · corrodedRT WING HEATER BLANKET COVER 1409 HAS CORROSION ON LANDING AREA OF A/C. RT WING HEATER BLANKET COVER 1409 REPLACED.SDR UALA2012071103723Anti-Ice Valve · faultyRT ANTI-ICE WING VALVE FAILURE. REPLACED RT WING ANTI-ICE VALVE PER MM. OPS AND INDICATIONS NORMAL.SDR DU4R2012010Diffuser · crackedS/O 127043 N/R 24783 DURING SCHEDULED INSPECTION, FOUND LEFT HORIZONTAL STABILIZER L/E ANTI-ICE DIFFUSER HAS SEVERAL CRACKS AT HSS 200, HSS 252, HSS 265.SDR QXEA2012062500536Warning Message · false activationDEICE PRESSURE CAUTION ILLUMINATED. BOOT PAIRS APPEARED TO OPERATE NORMALLY. SYS PRESSURE 20 PSI BOTH SIDES. RAN THE EMERGENCY ABNORMAL CHECKLIST, CAUTION EXTINGUISHED AND DID NOT REAPPEAR. COMPLIED WITH GENERAL VISUAL INSPECTION OF AIRFRAME DE-ICE BOOTS IAWSDR CA120613004Regulator Valve · failed(CAN) ON MAY 31ST 2012 FOUND AN AWI LEAK ON RT CTR SECTION. ON FURTHER INVESTIGATION IT WAS FOUND THAT THE AWI REGULATOR VLV O RING THAT SEALS THE VLV HALVES, POPPED OUT OF THE VLV BODY. THE VLV WAS REPLACED WITH AN OVERHAULED UNIT FROM STOCK & ALL FUNCTIONASDR CA120614007De-Ice Valve · faulted(CAN) UPON ARRIVAL, NOTICED RT NR 3 BOOT SEQUENCE NOT INDICATING EITHER PRESSURE OR LIGHT AND NOT INFLATING. FOUND TO BE FAULTY DUAL DEICE DISTRIBUTOR VALVE. REPLACED DISTRIBUTOR VALVE AND ACFT RETURNED TO SERVICE.SDR UALA2012061103214Relay · failedRT WING ANTI-ICE EICAS MESSAGE RAN CHECKLIST UNABLE TO MATCH COMMANDED POSITION. REPLACED RELAY K1155 AND RT WING ANTI-ICE VALVE PER MM 30-11-02. PERFORMED THREE SUCCESSFUL OP TESTS PER MM 30-11-02.SDR UALA2012051002675Monitor · faultySTATUS MESSAGE WAI CARD REPEAT GRIPE. TRIED TO RESET WAI CARD, NO HELP. UNABLE TO RUN WAI SYSTEM TEST VIA MAT. CAN NOT COMMUNICATE WITH CARD. SUSPECT BAD ACIPS OR LINEAR MONITOR (A3) AT P84. NO TIME TO FURTHER TROUBLESHOT, BOTH WAI VALVES DEACTIVATED. SDR REXA2012042000541Piccolo Tube · out of adjustANTI-ICE DUCT WARNING MSG- CONFIGURATION COWL A/I - ON, WING A/I - OFF. ON A/I SYNOPTIC PAGE - ONLY LEADING EDGE OF LEFT WING ILLUMINATED RED. MSG INTERMITTENTLY RETURNED EVEN WHEN 14TH STAGE BLEEDS REMOVED. FOUND MOUNT HARDWARE FOR SENSORS 1RT1HA & 1RT2HA SDR CVGA2012040500001Warning Message · illuminatedRED CAS MESSAGE "ANTI-ICE DUCT" ILLUMINATED ON CLIMBOUT WITH ICE ON.SDR A6WA201240405Shutoff Valve · inoperativeDURING FLIGHT IN ICING CONDITIONS, RECEIVED WING OVERHEAT RED WARNING. EICAS INDICATED RT WING L/E RED. C/W QRH, RECEIVED RT-WING OVERHEAT IN STANDBY MODE. R & R RT MODULATING SHUTOFF VALVE IAW AMM 30-12-14 LEAK AND OPS CK GOOD.SDR A6WA201240403Warning Light · false activationWING OVERHEAT WARNING ON TAKE OFF. HIGH SPEED ABORT. ACARS REPORTING 139 KIAS. WING ANTI-ICE WAS SELECTED NORMAL. WITH ASSISTANCE FROM CREW, RAN ENG AND OPS CHECKED IAW AMM 30-11-01. OPS CHECKED GOOD.SDR UALA2012031901789Valve · faultyABORTED TAKEOFF ABOVE 80 KTS BELOW 110. MAX BRAKE TEMP 290 RT OUTBOARD. INSPECT WHEELS & BRAKES FOR DEFECTS RELATED TO MAX BRAKING, OVERHEAT. USE CAUTION APPROACHING LANDING GEAR AREA. ACCMP'D INSPECTION OF LANDING GEAR WHEELS, ALL FUSE PLUGS INTACT.SDR QXEA2012031700237Deice System · malfunctionedDE-ICE PRESSURE CAUTION AFTER TAKEOFF. BOOT SET SECOND FROM RT WING TIP REMAINED INFLATED, ADVISORY LIGHT STAYED ON. BOOTS DEFLATED AFTER APPROX 20 MINUTES. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. PERFORMED OP'S CHECK OF DDV SYS IAW AMM SDR A6WA201240354Control Unit · malfunctionedSELECTED WING HEAT TO STANDBY IM ICING CONDITIONS AND RECEIVED WING O/H WARNING, LT ICING CONDITIONS AND C/W QRH (RT WING). R & R TEMP CONTROL UNIT IAW AMM 31-12-19. OPS CHECKED GOOD. REMOVED PLACARD AND MEL.SDR HNAA2012030700674Check Valve · failedWITH BOTH ENGINES SHUTDOWN AND APU BLEEDS OFF. DEICE PRESSURE SHOWS 24 PSI AND BOOTS STILL INFLATED. R & R APU LINK UP PRESSURIZATION CHECK VALVE. RAN APU DEICE PRESSURE WAS NORMAL, BOOTS PARTIALLY INFLATED WITH OUT LIGHTS ILLUMINATING. NORMAL 8 OPERATIONSDR HNAA2012030700673Timer · failedLEFT WING OTBD DEICE BOOT WILL NOT INFLATE IN SLOW OR FAST. INFLATES NORMALLY IN MANUAL. R & R AIRFRAME DEICE TIMER. OPS CHECKED GOOD IAW MM 30-10-00.SDR CA120312014Duct · ruptured(CAN) AFTER ARRIVING AT THE GATE AND DURING WALK-AROUND, FOUND NR 4 SLAT, LT WING, INBD BLOW OUT PANEL BLOWN WITH NO ANTI-ICING DUCT VISIBLE FROM THE OPENING. FURTHER INSPECTION REVEALED THE DUCTS TO BE DISINTEGRATED AND FRAYED WITH STRANDS OF TUBE MATERIAL BSDR REXA2012030200299Thermal Switch · defectiveABORTED T/O AFTER DEPARTURE ON CLIMBOUT WING OVERHEAT MASTER WARNING IN STBY MODE (RIGHT WING). RETURNED TO DTW. REMOVED AND REPLACED RT WING BACKUP OVHT THERMAL SW, SYSTEM OPC GOOD IAW CRJ 200 AMM 30-12-16. A/C OK FOR SVC.SDR FDEA201203020739Anti-Ice Valve · failedON CLIMB OUT, RECEIVED LT WING ANTI-ICE DISAGREE. WING ANTI-ICE WAS CYCLED OFF-ON BUT SAME RESULT. TRIED A SECOND ON-OFF CYCLE AND SAME RESULT. ALSO RECEIVED NR 1 AIR SYSTEM MANIFOLD FAILURE ALERT. DUMPED 9000 POUNDS FUEL AND RETURNED TO SEA. R & R LSDR FDEA201203020738Anti-Ice Valve · failedON CLIMB OUT, RECEIVED LEFT WING ANTI-ICE DISAGREE. WING ANTI-ICE WAS CYCLED OFF-ON BUT SAME RESULT. TRIED A SECOND ON-OFF CYCLE AND SAME RESULT. ALSO RECEIVED NR 1 AIR SYSTEM MANIFOLD FAILURE ALERT. DUMPED 9000 POUNDS FUEL AND RETURNED. R & R LEFT WING SDR REXA2012030100320Thermal Switch · defectiveAIR RETURN FOR WING OVERHEAT MASTER WARNING IN STBY MODE (RIGHT WING). RETURNED TO DTW. REMOVED AND REPLACED RT WING BACKUP OVHT THERMAL SWITCH. SYSTEM OPS CHECK GOOD IAW AMM 30-12-16. A/C OK FOR SERVICE.SDR SIMA20120301006De-Ice Valve · unserviceableDURING TAKEOFF ON FLIGHT 2704 CREW RECEIVED WING ANTI-ICE FAIL CAUTION MESSAGE. ON DESCENT CREW FOLLOWED AOM PROCEDURE WING ANTI-ICE FAIL CAUTION RETURNED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT WING ANTI-ICE LOW PRESSURE SWITCH ISDR REXA2012022900294Warning System · activatedABORTED T/O FOR WING ANTI ICE CAUTION. PLACED ON MEL.SDR CA120301011Duct · chafed(CAN) DURING CLIMB, CREW REPORTED A RED CAS MESSAGE, WING, STAB LEAK, THEY IMMEDIATELY PROCEED WITH THE EMERGENCY CHECKLIST AND THE CAS MESSAGE WENT AWAY. UPON LANDING THEY CONTACTED OUR MAINTENANCE DEPT AND REPORTED THE MALFUNCTION. THE ENTIRE WING, STABILIZESDR CA120219001Boot · failed(CAN) A LIGHT PULSING SENSATION WAS FELT IN THE LT CONTROL WHEEL SHORTLY AFTER ROTATION. FLAP RETRACTION AT 400. NO CHANGE FELT. ACCELERATED TO NORMAL CLIMB SPEED OF 150 KTS. PULSING SENSATION IN LT CONTROL WHEEL REDUCED SLIGHTLY. DURING THE CLIMB THE AIRSDR REXA2012021400226Cover · missingDIVERTED TO PIT FOR WING ANTI-ICE WARNING MESSAGE. INSTALLED HEAT COVER FOR STBY HEAT SENOR IAW AMM 30-12-12, OPS CHECK GOOD.
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