JASC 3010
Service difficulty reports · 2,242
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 9709909877Temp Contl Box · failedLEFT ICE PROTECTION TEMPERATURE LOW LIGHT ILLUMINATED WITH MAX CLIMB THRUST SET. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES. WITH LEFT SYSTEM OFF AND RIGHT SYSTEM ON AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED. WHEN TAIL WAS SELECTED, ICE PSDR AU971092Actuator · faulty(AUS) LH AND RH WING OUTER ANTI-ICE VALVES BOTH HAD SLIPPING CLUTCHES.SDR 97ZZZM686De-Ice Boot · tornLEFT INBOARD DE-ICE BOOT BOTTOM SIDE LOOSE. INSTALLED NEW BOOT.SDR 97ZZZX2395Deice Boot · blownRIGHT INBOARD WING DEICE BOOT BLOWN.SDR 9708909991Deice Timer · malfunctionedWHENEVER THE TAIL DE-ICE IS SELECTED, THE AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATES. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO DTW. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE CHANGED TAIL DE-ICE TIMER, OPERATIONAL CHECK SDR CA970716004Timer · intermittent(CAN) AFTER LANDING PILOT NOTED THAT BOTH THE LEFT AND RIGHT WING DEICER BOOTS WERE INFLATED. UNABLE TO DEFLATE WITHOUT TURNING OFF BLEED AIR. SWITCHING FROM AUTO TO MANUAL HAD NO EFFECT. TIMER REMOVED FROM AIRCRAFT. CONTACTS CLEANED AND TIMER WORKED FINE. NEWSDR DL757970722Anti-Ice Valve · malfunctionedDIVERTED SLC/LT WING ANTI-ICE EICAS MSG AND OVHD DISCRETE VLV LIGHT WITH WING SWITCH ON. NORMAL WHEN SWITCH OFF. CYCLED WING ANTI-ICE C/B, RAN APU CYCLED BOTH VALVES CK NML. A/C DIVERTED 2ND TIME W/LT WING ANTI-ICE EICAS MSG AND OVERHEAD DISCRETE VLV LIGHTSDR M8XA970006Ejector Valve · defectiveCOS - FLT 1332 - EN ROUTE FROM COS TO CPR, FLIGHT CREW RECEIVED ACAS MESSAGE 'AIRFOIL DE-ICE FAIL' ICING CONDITIONS PREVAILED IN CPR. FLIGHT ELECTED TO RETURN TO COS. AIRCRAFT LANDED COS WITHOUT FURTHER INCIDENT. M8XA MAINTENANCE PERSONNEL INSPECTED AIRCRAFSDR 97ZZZM565De-Ice Boot · looseRIGHT STABILON DE-ICE BOOT LOOSE.SDR CA970409004Deice Valve · corroded(CAN) DEICE DISTRIBUTION VALVE FAILED BECAUSE OF CORROSION. CORROSION CAUSED BY ACCUMULATION OF MOISTURE-DRAIN HOLE PLUGGED BY POTTING COMPOUND USED FOR INSTALLATION OF ELECTRICAL HEATERS.SDR 97ZZZX1325Line · holedDURING A SCHEDULED INSPECTION, NOTED THE SECOND CYCLE OF THREE WAS NOT HOLDING ENOUGH PRESSURE IN THE SURFACE DEICE SYSTEM. INSPECTION REVEALED A HOLE IN AN ALUMINUM LINE CAUSED BY A SCREW IN AN INSPECTION COVER MAKING CONTACT. SUGGEST MAKING SURE ADEQUATE CSDR COMA9760063Duct · splitANTI-ICE DUCT WARNING MESSAGE ON EICAS. THE LEFT WING ANTI-ICE DUCT ASSY (PICCALO TUBE) WAS SPLIT OPEN APROXIMATELY 4 INCHES AT THE OUTBOARD END. REPLACED TUBE ASSY.SDR COMA9760062Control Unit · malfunctionedANTI-ICE DUCT WARNING MESSAGE ON EICAS. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE RT BLEED LEAK UNIT FOR TROUBLESHOOTING.SDR 9705579945Anti Ice Valve · malfunctionedAIRFOIL ICE PROTECTION PRESSURE ABNORMAL AND PRESSURE HIGH LIGHTS ILLUMINATED WITH TAIL DEICE SELECTED AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TAIL ANTI-ICE VALVE. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TSDR 9705569919Press Switch · malfunctionedEN ROUTE MSP-HPN, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED WITH TAIL DEICE SELECTED. RESET CIRCUIT BREAKER WITH NO HELP. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TAIL AIR PRESSURE SWITCH. OPERATIONAL CHECK SDR VTZA97179Deice Boot · failedIAD/EWR - FLT 6276 - DURING TAXI AT 2010 HRS ON 3-14-97, AIRCRAFT RETURNED TO GATE DUE TO AIRFRAME DEICE CCT3 FAILS IN BOTH AUTO AND MANUAL MODES. MAINTENANCE INSP AND FOUND BLOWN DEICE BOOT AND REMOVED AND REPLACED LEADING EDGE, OPS CHECK OK. AIRCRAFT WAS RSDR RAIA970308De-Ice Control · failedSTL - FLT 7404 - LEFT ELEVATOR HORN HEAT FAILED. MAINTENANCE REPLACED LEFT DE-ICE CONTROLLER. (M)SDR 9705369920Control Unit · malfunctionedRIGHT ICE PROTECTION TEMPERATURE LOW LIGHT REMAINED ON AFTER TAKEOFF WITH AIRFOIL ICE PROTECTION SYSTEM ACTIVATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ELECTRONIC THERMAL CONTROL UNIT, LOW TEMPERATURE SENSOR, AND LOWSDR COMA9710169Press Regulator · leakingRIGHT BLEED AIR DUCT LEAK WARNING CAME ON AFTER TAKEOFF. REPLACED THE RT DEICE SYSTEM PRESSURE REGULATOR.SDR 97ZZZX1406Supply Tube · crackedDURING AN INSPECTION REQUIRING WING LEADING EDGE PANEL REMOVAL, THE OUTBOARD CENTER LEADING EDGE SECTION ANTI-ICING SUPPLY TUBE WAS FOUND CRACKED AND NOT CONNECTED. THIS WAS DUE TO MISALIGNMENT WHEN INSTALLED NEW AT THE FACTORY.SDR MALA975334Connector · failedFLT 3098 - OUTBOUND OF DTW, CREW REPORTED RIGHT ELEVATOR HORN HEAT LIGHT ILLUMINATED. RETURNED TO DTW. MAINTENANCE REPAIRED WIRES AND REPLACED CANNON PLUG ON ELEVATOR HORN HEAT. OPS AND SECURITY CHECK GOOD. (M)SDR 9704089902Thermostat · malfunctionedLEFT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF WITH ICE PROTECTION OFF AND CROSSFEED VALVE CLOSED. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THERMOSTAT AND ANTICIPATOR, OPERATIONAL CHECK NORMAL ON GROUND.SDR MALA975327Distributor Vlv · failedFLT 2974 - AFTER DEPARTING DTW, STABILIZER WARNING DE-ICE WAS SELECTED. CREW RECEIVED MASTER CAUTION AND DE-ICE TIMER LIGHTS ILLUMINATED WITH STABILIZER LIGHT CONTINUOUSLY ILUMINATED. CREW FOLLOWED QUICK REFERENCE HANDBOOK AND RETURNED TO DTW. MAINTENANCE RSDR COMA9760044Duct Assy · leakingA 14TH STAGE ANTI-ICE DUCT WARNING DURING TAKEOFF. REPLACED A DEFECTIVE SECTION OF 14TH STAGE BLEED AIR DUCT IN THE LEFT HAND GEAR WELL.SDR DLM90970269Heater · malfunctionedOFF SKED LANDING, ANTI-ICE PROBLEMS, POSSIBLE STRAKE HEATER TROUBLE. REPLACED RT STRAKE.SDR GTIA9700163Connector · dirtyDTW - FLT 640 - RIGHT ICE PROTECT TEMP LOW LIGHT DID NOT ILLUMINATE WHEN AIRFOIL ANTI-ICE SELECTED ON. LIGHT DID TEST, BUT DID NOT ILLUMINATE WITH THE RIGHT ICE PROTECT TEMP LOW LIGHT, WAS ABLE TO DUPLICATE DISCREPANCY. CLEANED ELEC CONNECTOR AT RIGHT AIRFOISDR 97ZZZM253Switch · failedDTW - FLT 626 - ON DESCENT WITH AIRFOIL ANTI-ICE ON, THE SUPPLY PRESSURE HIGH LIGHT CAME ON SEVERAL TIMES AND DUCT PRESSURE WAS 60 PSI. EACH TIME IT CORRECTED ON ITS OWN. REMOVED AND REPLACED AIRFOIL ICE PROTECTION HIGH PRESSURE SWITCH. SYSTEM OPS CHECK GOODSDR 97ZZZM251Pressure Switch · failedDTW - FLT 6337 - CREW RETURNED TO DTW AFTER INDICATION OF A POSSIBLE ANTI-ICING DUCT LEAK IN THE WING ANTI-ICE SYSTEM. AIR FOIL ICE PROTECTION PRESSURE ABNORMAL. ANNUNCIATOR REMAINED ON WHEN AIR FOIL ICE PROTECTION WAS UTILIZED (NORMAL DUCT PSI OF PLUS OR MINSDR 9701419909De-Ice Timer · malfunctionedTAIL DE-ICING WOULD NOT ACTIVATE WHEN SELECTED EN ROUTE. ALSO, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE TAIL DE-ICE TIMER, OPERATIONAL CHECK NORMAL.SDR VTZA97093De-Ice Boot · looseFLT 6190 - RDU-IAD - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO YOKE VIBRATION AND LOUD BANGING NOISE COMING FROM TAIL SECTION. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE FOUND A LOOSE DE-ICE BOOT. THE BOOT WAS REPLACED. (M)SDR CA970206004Circuit Breaker · failed(CAN) PILOT NOTED THAT THE LEFT ELEVATOR HORN HEAT CAUTION LIGHT CAME ON. HORN CIRCUIT BREAKER WAS FOUND UNSERVICEABLE.SDR COMA9710038Press Regulator · inoperativeINBOARD LEFT STABILIZER, RT STABILIZER AND INBOARD LEFT WING DEICE INOPERATIVE, LIGHTS COME ON, ON BOTH TIMES 1 AND 2. REPLACED RIGHT SIDE DE-ICE PRESS REGULATOR.SDR CA970225002Controller · failed(CAN) DURING CRUISE FLIGHT, THE LEFT HAND STABILIZER ANTI-ICE FAIL LIGHT ILLUMINATED. FLIGHT LANDED AND CONTROLLER WAS CHANGED.SDR CA970121006Deice Valve · failed(CAN) ON APPROACH AIRCRAFT ENCOUNTERED HEAVY ICING CONDITIONS. AFTER LANDING THE INBOARD HALF OF WING FOUND COVERED WITH ICE. WING DEICE DISTRIBUTOR VALVE WAS CYCLED BUT DID NOT WORK. VALVE REPLACED. A MOD WILL BE INTRODUCED TO INSTALL HEATER AROUND THE VALVESSDR 9701082761Ejector Duct · failedDURING CLIMB, FLIGHT ATTENDANT REPORTED A LOUD BANG FROM AFT AIRSTAIR AREA FOLLOWED BY NR 2 EPR GAUGE DROPPING TO ZERO AND AN AFT BODY OVERHEAT INDICATION. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED NR 3 ANTI-ICE MANIFOLD EJECTOR DUCT ANDSDR 97ZZZX349Distributor · failedDURING A 150 HR INSPECTION, IT WAS DISCOVERED THAT THE VERTICAL AND HORIZONTAL BOOTS WERE NOT INFLATING. THIS AREA IS IMPOSSIBLE FOR THE PILOT TO SEE DURING A FUNCTION CHECK AND MUST BE INSPECTED REGULARLY.SDR CA970109017De-Icer Boot · delaminated(CAN) PILOT REPORTED RT DE-ICER BOOT WOULD NOT INFLATE WHEN REQUIRED TO REMOVE ICE BUILD-UP ON LEADING EDGE DURING FLIGHT. MAINTENANCE FOUND BOOT INTERNALLY DELAMINATED BETWEEN CELLS AT W.S. 91.0. THIS AREA IS WHERE THE WING FLEXES (SKINS JOINED AT THIS SPOTSDR COMA9710015Regulator · malfunctionOUTBD WING ANTI-ICE SYSTEM FAIL WARNING ON BOTH TIMERS AND 2. REPLACED THE WING DE-ICE PRESSURE REGULATOR.SDR MALA965265Boot · puncturedFLT 3183 - EN ROUTE TO TVC, THE NR 2 INBOARD BOOT SECTION FROM THE WING TIP ON THE RIGHT SIDE DIDN'T INFLATE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE PATCHED A SMALL HOLE IN THE NR 2 BOOT AND REMOVED MOISTURE. ALL CHECKS SATISFACTORY. (M)SDR GLBA96246Circuit Breaker · failedDIK - ON DESCENT, THE 'WING ICE' CIRCUIT BREAKER STARTED TO SMOKE. PULLED BREAKER AND SMOKE STOPPED. (M)SDR COMA9660233De-Ice Fluid · smokingPASSENGER REPORTED SMOKE COMING FROM WINGS. SMOKE FOUND TO BE DE-ICING FLUID EVAPORTING.SDR COMA9660230Heat Probes · defectiveANTI-ICE DUCT WARNING MESSAGE ON EICAS WHEN WING DEICE SELECTED ON. REPLACED 6 DEFECTIVE HEAT PROBES IN RT WING LEADING EDGE.SDR VTZA96449De-Ice Boot · blownFLT 6501 - IAD-JFK - DURING TAXI, RETURNED TO GATE DUE TO CCT-1 FAULT ON AUTO AND MANUAL MODES. MAINTENANCE INSPECTION AND FOUND LEFT INBOARD DE-ICE BOOT BLOWN. MAINTENANCE REMOVED AND REPLACED DE-ICE BOOT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FSDR 96FDEA01703Duct · looseENGINE NR 1 STRUT OVERHEAT. 1ST LIGHT WENT OUT BEFORE CHECKLIST WAS RUN. 2ND LIGHT WENT OUT WHEN ENGINE NR 1 WING ANTI-ICE SWITCH TURNED OFF. AIRCRAFT DE-ICED AT IND ON THE GROUND PRIOR TO FLIGHT. RAN NR 1 ENGINE FOUND LEAKS IN STRUT AREA. TIGHTENED FLANGSDR COMA9610403Separator · crackedWING AND STABILIZER INBD DE-ICE BOOTS ARE INOP. REPLACED A CRACKED BLEED AIR WATER SEPARATOR.SDR COMA610226Temp Sensor · defectiveLEFT WING ANTI-ICE DUCT WARNING MESSAGE ON EICAS. REPLACED DEFECTIVE TEMP SENSOR PROBE AT LT WING LEADING EDGE.SDR C2XA96CL045De-Ice Boot · tornCLE - FLT 3176 - CREW REPORTED THAT AFTER TAKEOFF ALL AIRCRAFT DE-ICE BOOTS FAILED. AIRCRAFT RETURN TO STATION. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LEFT INBOARD WING DE-ICE BOOT IAW EMB-120 MM 30-10-01. OPERATIONAL CHECKS WERE GOSDR 97ZZZX354Switch · failedFLIGHT CREW REPORTED NO 'SURFACE DE-ICE' LIGHT WHEN DE-ICE BOOTS INFLATED. DETERMINED WING AND TAIL DE-ICE BOOT PRESSURE SWITCHES DEFECTIVE, MOST LIKELY DUE TO WATER CONTAMINATION. SUBMITTER SUGGESTS SWITCHES NEED TO BE INSTALLED IN A POSITION THAT WILL LIMISDR 97ZZZX353Switch · failedFLIGHT CREW REPORTED NO 'SURFACE DE-ICE' LIGHT WHEN DE-ICE BOOTS INFLATED. DETERMINED WING AND TAIL DE-ICE BOOT PRESSURE SWITCHES DEFECTIVE, MOST LIKELY DUE TO WATER CONTAMINATION. SUBMITTER SUGGESTS SWITCHES NEED TO BE INSTALLED IN A POSITION THAT WILL LIMISDR CA961230008Sensor · damaged(CAN) LEFT HAND, INBOARD LEADING EDGE WING TEMP SENSOR, NOT INSTALLED AS PER MAINTENANCE TASK. THE BRACKET HAD NOT BEEN INSTALLED OVER THE SENSOR AS SPECIFIED IN THE AMM. THEREFORE, THE SENSOR WAS DAMAGED WHEN THE MOUNTING SCREWS WERE TORQUED DOWN.
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