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 DLM90960523De Ice · failedANTI-ICE FAULT ILLUMINATES ON O.A.P. WITH ACFT IN AIR MODE AND ENG A/I ON...LEFT STRAKE LOWER SURFACE NOT HEATING AND ARCING. REPLACED STRAKE ASSEMBLY OPERATION NORMAL.SDR RAIA960231De-Ice Boot · wornSTL - FLT NR 7176 - AIRFRAME DE-ICE FAULTED IN FLIGHT, RETURNED TO STL WITHOUT INCIDENT. MAINTENANCE PATCHED HOLES IN RIGHT WING DE-ICE BOOT, OPERATIONAL CHECK GOOD DURING GROUND RUNS. (M)SDR 96ZZZX2097Heater Tip · burnedTHE WIRE INSIDE THE HEATED ELEVATOR HORN TIP SHORT CIRCUITED AND BURNED. SUBMITTER SUGGESTS THE SHORT MAY HAVE BEEN CAUSED FROM THE HEATED HORN ASSY CHAFING ON THE ELEVATOR.SDR COMA9660022Duct · crackedANTI-ICE DUCT WARNING MESSAGE ON EICAS. REPLACED CRACKED PICOLLO TUBE AT RT OUTBD WING.SDR 96ZZZX843Deice Pipe · chafe throughREMOVED ELEVATOR FOR C/W SOCATA SB 70-053. UPON REMOVAL, FOUND LT DEICE PIPE FOR ELEVATOR HORN WORN THROUGH AT ENTRANCE TO HORN. THIS INSTALLATION WAS DONE AT FACTORY. WEAR CAUSED BY LACK OF CLEARANCE AT PASS-THROUGH. SUBMITTER STATED TBM NEEDS TO ISSUE A SDR 9601089608Valve · failedDURING CLIMB, THE RIGHT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE PNEUMATIC AUGMENTATION VALVE AND OPERASDR 96ZZZX573Horn Tip · element failedLEFT HEATED HORN ON ELEVATOR FAILED. INSTALLED NEW HEATED TIP. KIT NR 128-4015-5 PREVIOUSLY INSTALLED. (HORIZONTAL STABILIZER LEADING EDGE KIT).SDR 9601119921Valve · failedDURING CLIMB, THE LEFT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE PNEUMATIC AUGMENTATION VALVE AND OPERATIONAL CHSDR 9601019945Press Reg Vlv · malfunctionedDURING FLIGHT, THE AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED DURING WING ANTI-ICE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. REPLACED ICE PROTECTION PRESDR CA960202002Valve · corroded(CAN)DURING PREFLIGHT THE DEICE SYSTEM TESTED AND RH DEICE BOOT WOULD NOT INFLATE. RH DISTRIBUTOR VALVE REPLACED. VALVE CORRODED INTERNALLY.SDR 9600859756Press Switch · malfunctionedEN ROUTE DTW-YHZ, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT REMAINED ON DURING WING ANTI-ICE OPERATION. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE TAIL ANTI-ICE VALVE, NO HELP. REPLACED THE PRESSURE SWITCH AND OPERATIONAL CHECK NOSDR USAAF96008Shutoff Valve · inoperativeCLT - FL 1295 - EN ROUTE PIT - LGA, CREW RECEIVED TAIL ANTI-ICING FAULT SHORTLY AFTER SELECTING TAIL ANTI-ICE. FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE TAIL ANTI-ICE SHUTOFF VALVE. (M)SDR COMA9660006Anti-Ice Duct · warningANTI-ICE DUCT MESSAGE ON EICAS TAKEOFF ABORTED. COULD NOT DUPLICATE DISCREPANCY. SYSTEM CHECKED NORMAL AND ACFT RETURNED TO SERVICE.SDR MWEA95531Temp Switch · inoperativeDURING FLIGHT, RIGHT ICE PROTECTION TEMP HI LIGHT ILLUMINATED. FLIGHT RETURNED TO MKE. REPLACED RT ICE TEMP HIGH SWITCH AND THERMOSTAT.SDR PLG121195E1De-Ice Boots · malfunctionedFLT NR 4948 - BOS-YQB - AFTER REACHING CRUISE ALTITUDE, THE CAPTAIN REPORTED THAT THE OUTER WING DE-ICE BOOTS WERE NOT INFLATING. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE DE-ICE BOOTS AND OPERATIONASDR DLM88954667Thermostat · malfunctionedBURNING ODOR, NO VISIBLE SMOKE ON SHORT FINAL. SMOKE ALARMS IN AFT LAVS ACTIVATED. ANTI-ICE IN USE, ODOR DISSIPATED WHEN ANTI-ICE SHUT OFF. REPLACED ANTICIPATORS AND THERMOSTATS L/R SIDE. NO SMOKE OR ODOR NOTED DURING ENGINE RUN WITH ANTI-ICE ON.SDR 96ZZZX398Seal · defectiveDURING INSPECTION, FOUND TKS ANTI-ICE FLUID LEAKING FROM RIGHT SIDE OF NOSE WHEELWELL. TRACED LEAK TO AFT SIDE OF FORWARD PRESSURE BULKHEAD. FOUND O-RINGS ON FORWARD PRESSURE BULKHEAD FITTINGS DEFECTIVE AND PUDDLE OF TKS FLUID IN FLOOR BOARDS. REPLACED O-RISDR PLG120495E1Lower Duct · damagedFLT NR 4401 - PQI-BOS - DURING FLIGHT, THE LEFT INTAKE HEAT FAILED. DUE TO EXISTING WEATHER CONDITIONS, THE AIRCRAFT DIVERTED INTO PWM AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE LOWER DUCT DSDR CA951206008Diode · open circuit(CAN)PILOT REPORTED RIGHT WING "HOT" ON GROUND WITH WING ANTI-ICE SELECTED OFF. DIODE FOUND OPEN WHICH ALLOWS ENGINE BLEED AIR TO PASS THROUGH THE WING ANTI-ICE VALVE, HEATING THE LEADING EDGE.SDR CA951129201Valve · failed(CAN)DE-ICING CONTROL VALVE FAILED BECAUSE OF LACK OF DRAIN HOLE. IT HAD BEEN PLUGGED BY POTTING COMPOUND WHEN VALVE HEATERS WERE INSTALLED.SDR COMA9512002Separator · leakingRT DUCT LEAK WARNING ACTIVATED. REPLACED LEAKING AIR FOIL DE-ICE WATER SEPARATOR.SDR CA951116012De-Ice Valve · inoperative(CAN)MALFUNCTION OF THE HORIZ STAB SURFACE DE-ICERS WAS SUSPECTED DUE TO FAILURE TO RECOGNIZE A THIRD BUMP AS SHOULD BE INDICATED ON THE PNEUMATIC PRESS GAUGE. FURTHER INVEST REVEALED THAT THE SOLENOID FOR PORT B, WHICH SUPPLIES PRESSURE TO THE HORIZ STAB BOOSDR 96ZZZX42Deice Boot · manual errorDEICE BOOTS CYCLE OUTBOARD WING THEN INBOARD WING AND TAIL. THE MM AND POH SAY THE INBOARD WING AND TAIL SHOULD CYCLE FIRST, THEN OUTBOARD WING. AFTER TALKING TO TBM NORTH AMERICAN SERVICE REP, FOUND THE BOOKS WERE WRONG. REFERENCE: MM, CHAPTER 30, SUB-CHAPSDR SIMA953062Deice Controller · malfunctionedORD - FLT 4340 - AIRFRAME DE-ICE FAULTY IN-FLIGHT. AIRCRAFT RETURNED TO ORD. LANDING UNEVENTFUL IN ORD. REMOVED AND INSPECTED AIRFRAME DE-ICE CONTROLLER 'B'. GROUND RUN CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 10799.0. (X)SDR CA951123106Circuit Breaker · malfunction(CAN)CIRCUIT BREAKER #2 ENGINE AND WING ANTI-ICE POPPED AFTER USING ENGINE ANTI-ICE. ON ARRIVAL CIRCUIT BREAKER RESET AND VALVE OPERATION CHECKED NORMAL. CONNECTORS REMOVED FROM THREE VALVES AND INSPECTED.NO EVIDENCE OF ARCING. CIRCUIT BREAKER REPLACED ON SPECSDR 9516369882De-Ice Syst · malfunctionedDURING CRUISE, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED INTERMITTENTLY WITH TAIL DE-ICE ACTIVATED. AIRCRAFT DIVERTED TO FSD AND LANDED WITHOUT INCIDENT. REPLACED TAIL SHUTOFF VALVE, PRESSURE SWITCH, AND AIRFOIL PRESSURE DELAY RELAY AND OPERSDR 95ZZZX6018Hose · failedUPON INSTALLATION OF DE-ICE KIT ONTO PARTIALLY CONNECTED SYSTEM, FIRST TEST OF DE-ICE SYSTEM, TAIL FAILED TO INFLATE. FOUND NEW HOSE TO HAVE SPLIT. REPAIRED SPLIT. AIRCRAFT FLEW ONE HOUR, TAIL BOOTS FAILED TO INFLATE. FOUND 3 HOSES SPLIT FOR TAIL BOOTS. RSDR 95ZZZX6233Anti Ice Valve · inoperativeMLI - FLT 365 - TAIL ANTI-ICE VALVE INOP OPEN. REPLACED THE ANTI-ICE VALVE ACTUATOR. REFERENCE OPERATOR CONTROL NR 95ZZZX6231, AND 95ZZZX6232.SDR COM11957Separator · brokenNR 2 ENGINE DUCT LEAK WARNING CAME ON DURING CLIMB, AIRCRAFT RETURNED TO MCO. REPLACED BROKEN WING DE-ICE BLEED AIR WATER SEPARATOR.SDR 95ZZZX5129Line · deterioratedDE-ICE BOOTS ON WINGS INFLATE DURING FLIGHT. VACUUM SIDE DE-ICE LINE ON RIGHT SIDE BENEATH A DUCT APPARENTLY HAS MOISTURE IN IT. CENTER FLOOR FS 173 RT. THE MOISTURE AND LOCATION OF THIS LINE CAUSE CORROSION TO SET IN. EATS HOLES IN LINE. ABOUT SIZE OF NRSDR 95ZZZX6034Heat Mat · delaminatedDURING PILOT'S PRE-FLIGHT, DISCOVERED DELAMINATION ON LT ELEVATOR HORN HEAT MAT. NO DELAMINATION ALLOWED PER BEECH 400A MANUAL. REMOVED AND REPLACED LT ELEVATOR HORN HEAT MAT.SDR COM60537Controller · defectiveWING ANTI-ICE SENSOR CAUTION MESSAGE DURING TEST. REPLACED THE TEMP CONTROLLER.SDR COM60536Leak Sensor · defectiveANTI-ICE DUCT MESSAGE AFTER 20 MINUTES OF USE, EICAS INDICATED LT WING. STANDBY SYSTEM OPERATES NORMAL. REPLACED DUCT LEAK SENSORS 527WK, 519WK, 525WK, 515WK.SDR JZBR10767Logic Box · misrepairedDURING A POST-FLIGHT INSPECTION, A TEST OF THE ANTI-ICING LOGIC BOX WAS ACCOMPLISHED. A DISCREPANCY WAS DISCOVERED (ENGINE 1 LO LCD INOP). ORDERED AND RECEIVED A SERVICEABLE LOGIC BOX FROM AN FAA APPROVED REPAIR FACILITY. DURING INSTALLATION ON THE AIRCRAFTSDR 95ZZZX4281Pipe · pin holeDURING MAIN CABIN BELOW FLOOR INSPECTION AT STR 345, WATER WAS FOUND DRIPPING FROM DE-ICE PIPE THAT SERVICES THE TAIL BOOTS. INVESTIGATION REVEALED PIN HOLE IN LOW POINT OF PIPE. REMOVED AND REPLACED PIPE. REMOVED PIPE WAS CUT OPEN, FOUND PIPE WAS SEVERELY SDR SWIA95597Reg Vlv Gasket · failedFIVE MINUTES AFTER TAKEOFF USING ONLY APU BLEED X FEED TO BOTH PACS, RT DUCT LEAK LIGHT, ILLUMINATED, TURNED OFF X FEED AND RT PAC, STARTED TIME AS PER CHECK LIST, AFTER 3 MINUTES BEGAN PRECAUTIONARY ENGINE SHUT DOWN CHECK LIST WITH ENGINE AT FLIGHT IDLE AS RTSDR 95ZZZM289Anti-Ice Vlv · inopFLT NR 10, MCO-EWR - AFTER TAKEOFF PASSING 10,000 FEET, LOWER AFT BDY OVERHEAT, NR 1 WING ANTI-ICE VALVE LIGHTS CAME ON, STANDBY LIGHTS ILLUMINATED. NR 1 WING BLEED VALVE, NR 1 PK VALVE AND LE VALVE CIRCUIT BREAKERS POPPED. NR 1 ENGINE SHUT DOWN PRECAUTIONARSDR DL72S952981Anti Ice Duct · crackedANTI-ICE DUCT CRACKED 22 INCHES FROM OUTBOARD END. REPAIRED PER SRM 57-50-03, FIG 12, AT HMV SHOP VISIT FOR WING L/E KRUGER FLAP.SDR 9510409978Anti Ice Duct · bindingON INITIAL SLAT EXTENSION AT 240 KNOTS, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH BLUE SLAT EXTEND LIGHT OFF. AIRCRAFT ROLLED TO THE LEFT. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. FOUND RIGHT WING ANTI-ICE 'T' DUCT BINDING. REPLACED 'T' DUCT. OPERATIOSDR S2YA950013Deice Supp Line · chafedFOUND THE TAIL DEICE SUPPLY LINE CHAFED AT THE POINT OF EXIT FROM THE CLEAR PLASTIC ROUTING 'PROTECTION' TUBE. THE LOCATION IS THE BASE OF THE VERTICAL STABILIZER, LOWER ZONE 331. THE LINE WAS REPAIRED AND REST OF THE FLEET IS BEING CHECKED. (X)SDR SWIA95593De-Ice Tube · failedLT ANTI-ICE DUCT WARNING WING ANTI-ICE SWITCH NORMAL OR STANDBY POSITION. REMOVED LT OUTBD WING LEADING EDGE, REMOVED PICCALO TUBE, INSTALLED LEADING EDGE, IAW MM 57-41-01, GROUND RAN A/C OPS CKS GOOD, SEE F/L 2536.SDR 95ZZZX6036Heat Mat · shortedPILOT REPORTED HORIZONTAL STABILIZER ANTI-ICE FAIL LIGHT IN THE AIR. INSPECTION OF SYSTEM REVEALED LT ELVATOR HORN HEAT MAT WAS BURNED. REPLACED LT ELEVATOR HEAT MAT. OPERATIONALLY CHECK GOOD.SDR 95ZZZX6037Heat Mat · crackedDURING 400-HOUR INSPECTION, MECHANIC FOUND RT ELEVATOR HORN HEAT MAT CRACKED AT TIP THROUGH BLACK CASTING AND ALUM. ANTI-ICE DE-ICE SYSTEM STILL FUNCTIONING OKAY, BUT NO CRACKS ALLOWED IN PART PER BEECH 400A MANUAL. REMOVED AND REPLACED RT ELEVATOR HORN HEATSDR COM11899De-Icer Boot · looseA 4 INCH AREA OF THE RT INBD DE-ICE BOOT HAS COME LOOSE. REPLACED DE-ICE BOOT.SDR USAA950532Anti-Ice Duct · crackedTPA - FLT 1569 - ON CLIMB-OUT OF TPA, NR 1 ENGINE OVERHEAT LIGHT CAME ON. FLIGHT RETURNED TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE COWL ANTI-ICE DUCT. (M)SDR 95ZZZX2902Anti-Ice System · contaminatedAEROSPACE SYSTEMS AND TECHNOLOGY, INC., TKS ANTI-ICE SYSTEM WAS INSTALLED IN THIS AIRCRAFT IAW STC SA2239C3 AND A 337 FORM. A BLADDER IN THE RIGHT WING HOLDS THE TKS FLUID WITH A FILLER CAP ON THE TOP WING SURFACE. THERE ARE WARNINGS ON EITHER SIDE OF THE FISDR 9508489940Seals · failedON APPROACH INTO MEM, PASSENGER AT ROW 16 REPORTED EXCESSIVE HEAT COMING FROM FLOOR AREA. BOTH FLOOR AND SIDEWALL WERE HOT TO TOUCH. ENGINE AND WING ANTI-ICE WERE ACTIVATED. CAPTAIN DECLARED AN EMERGENCY AND EQUIPMENT WAS CALLED AS A PRECAUTION. AIRCRAFT LSDR DHL95720002Clamp · looseON CLIMBOUT, NR 1 ENGINE STRUT OVERHEAT ILLUMINATED. ACCOMPLISHED ENGINE STRUT OVERHEAT AND FUEL DUMP CHECKLIST. AIR TURNBACK, LANDED WITHOUT INCIDENT. OPENED STRUT, FOUND WING ANTI-ICE VALVE UPPER FLANGE LOOSE, TIGHTENED SAME. RAN ENGINE AT TAKEOFF POWER,SDR 95ZZZX2643De-Ice Boot · defectiveLEFT FORWARD WING DE-ICE BOOT BALLOONING IN-FLIGHT. THIS UNIT WAS REMOVED AND REPLACED WITH A NEW UNIT. THIS UNIT WAS PREVIOUSLY INSTALLED 11-4-92. THIS IS A CONTINUING PROBLEM WITH THE MODEL 2000 AIRCRAFT.SDR 95ZZZX2642De-Ice Boot · defectiveRIGHT FOWARD WING DE-ICE BOOT BALLOONING IN-FLIGHT. THIS UNIT WAS REMOVED AND REPLACED WITH A NEW UNIT. THIS UNIT WAS PREVIOUSLY INSTALLED ONE YEAR PRIOR. THIS IS A CONTINUING PROBLEM WITH THE MODEL 2000 AIRCRAFT.
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