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 SWIA971326Valve · failedSIX SECONDS AFTER TURNING ON THE DEICE BOOTS THE LEFT AND RIGHT MIDDLE LEADING EDGE BOOTS FAILED. THE RIGHT OUTBOARD LEADING EDGE AND VERTICAL FIN AND LEFT INTAKE BOOTS ALL FAILED IN FLIGHT. RETURNED TO SEA. REMOVED AND REPLACED RIGHT PRESSURE REGULATOR VALSDR SWIA971323Switch · failedWITH WING ANTI-ICE SELECTED ON ANTI-ICE DUCT MESSAGE CAME ON SHOWING LEFT WING RED, SAME IN BOTH NORMAL, STANDBY MODES. RETURNED TO SLC. REPLACED 3 THERMAL SWITCHES IN LEFT WING MID SECTION AND HEAT SHRINK INSTALLED ON LEFT WIRE ENDS. RAN AIRCRAFT AND TAXIESDR 99ZZZX320Angle · corrodedDURING A C-CHECK, CORROSION NOTED ON RT WING ANTI-ICE DUCT IN LEADING EDGE AREA FSS 545 (DUCT SUPPORT ANGLES).SDR CA981125082Outlet · plugged(CAN) ON FIRST FLIGHT AFTER INSPECTION, DEICE BOOTS SELECTED ON AND WING DE-ICE BOOTS REMAINED INFLATED. DUE TO ICING CONDITIONS AIRCRAFT RETURNED TO MAINTENANCE BASE. WING DE-ICE BOOTS OUTLET VENTS WERE FOUND PLUGGED WITH TAPE FROM MAINTENANCE TASK THE PREVSDR CA981130002Valve · damaged(CAN) DRAIN HOLE PLUGGED WITH POTTING COMPOUND ALLOWING MOISTURE TO ACCUMULATE CAUSING MALFUNCTION.SDR CA981130001Dist Valve · plugged(CAN) DE-ICE DISTRIBUTION VALVE DRAIN HOLE PLUGGED WITH POTTING COMPOUND LEADING TO MOISTURE ACCUMULATION AND CAUSING DAMAGE TO SEALING SURFACES LEADING TO MALFUNCTION.SDR 99ZZZX4Deicer · contaminatedPILOT REPORTED TO MAINTENANCE ICE REMAINING ON TAIL AFTER LANDING. (SPECIFICALLY, BOTH HORIZONTAL SURFACE DEICERS.) OPERATIONAL CHECK OF BOOTS BROKE ICE FORM SURFACE, HOWEVER, A CLOSER INSPECTION OF SURFACE DEICERS REVEALED MINOR HOLES IN LEADING EDGES. FURSDR SWIA971311Regulator · failedLEADING EDGE BOOTS FAIL IN ALL MODES OF OPERATION. RETURNED TO FAT. REPLACED LEFT AND RIGHT DEICE PRESS REGULATORS, OPS CHECKS GOOD.SDR SWIA971309De-Ice Boot · failedLEFT OUTBOARD AND RIGHT OUTBOARD WINGS DEICE BOOTS FAILED. RETURNED TO FAT. REPLACED OUTBOARD WING EJECTOR FLOW CONTROL VALVE, OPS CHECKS GOOD.SDR 98FDEA00687Duct · separatedON DEPARTURE, THE LWR AFT BODY OVERHEAT LIGHT ILLUM. WHEN WING ANTI-ICE WAS TURNED OFF THE LIGHT WENT OUT. FOUND SURFACE THERMAL ANTI-ICE CROSSOVER DUCT SEPARATED IN LT OVERHEAD STAIRWELL AREA. REASSEMBLED DUCT WORK, CK SATISFACTORY.SDR VTZA98326Warning System · illuminatedIND-IAD - DURING CRUISE, EXPERIENCED A RIGHT WING ANTI ICE FAIL MESSAGE ON THE MASTER CAUTION PANEL. AIRCRAFT CONTRACTED MAINTENANCE CONTROL AND DISPATCH, DECISION TO DIVERT TO PIT WAS MADE, AS A PRECAUTIONARY MEASURE. UPON ARRIVAL AT PIT THE AIRCRAFT LANDEDSDR COMA9810252Pressure Reg · leakingLEFT HAND BLEED AIR DUCT LEAK WARNING. REPLACED THE LEFT HAND DEICE PRESSURE REGULATOR.SDR SWIA971299Deice Boot · failedON CLIMB, OUTBOARD WING BOOTS FAILED BOTH TIMERS, BOTH CYCLES. RETURNED TO FIELD. REMOVED AND REPLACED OUTBOARD WING DEICE BOOT IAW MM.SDR RAIA981101Fuse · failedFLT 7723 - JFK - ELEVATOR HORN HEAT FAILED. MAINTENANCE REPLACED FUSE. (M)SDR CA981123017Ground Strap · shorted(CAN) DURING FLIGHT, THE 'WING ANTI-ICE DUCT RT' APPEARED ON SEVERAL OCCASIONS. INVESTIGATION FOUND THE GROUNDING STRAP OF THE PICCOLO TUBE WAS TOUCHING THE HEAT SENSOR. WIRE REPOSITIONED.SDR SWIA971300Deice Boot · failedON CLIMB, LEFT OUTBOARD STABLIZER DEICE BOOT FAILED, BOTH TIMERS. RETURNED TO FIELD. RAN BOTH ENGINES BUT COULD NOT DUPLICATE ON GROUND ON ALL SETTINGS. OPS CHECKS GOOD.SDR DHL98715004Duct · brokenNR 7 SLAT DID NOT RETRACT WITH FLAPS SELECTED TO UP. ABNORMAL ROLL INDICATION. FOUND WING ANTI-ICING TELESCOPING DUCT ON NR 7 SLAT BROKEN AND HANGING OUT. REMOVED DUCT AND INSTALLED BLANKING PLATES PER MEL. CLOSED ANTI-ICING SHUTOFF VALVES IN STUB WINGS.SDR SWIA971296Valve · failedLEADING EDGE DEICE OUTBOARD LEFT AND RIGHT FAILED BOTH TIMERS IN HEAVY AND LIGHT CYCLES AFTER APPROX 6-8 SECONDS. RETURNED TO FIELD. REPLACED OUTBOARD BOOT DEICE EJECTOR VALVE. GROUND RAN 15 MINUTES, CHECKS GOOD.SDR SWIA971307Regulator · failedVERTICAL STABALIZER, LEFT AND RIGHT HORIZONTAL STABALIZER FAILED IN FLIGHT. RETURNED TO FAT. REPLACED LEFT AND RIGHT PRESSURE REGULATORS. OPS CHECKS GOOD.SDR SWIA971306Regulator · failedWING DEICE BOOT OUTBOARD, INBOARD AND MIDDLE FAILED IN FLIGHT IN ICING CONDITIONS. RETURNED TO FAT. REMOVED AND REPLACED 18 PSI REGULATOR. OPS CHECKS GOOD.SDR EISA98218Valve · malfunctionedON DEPARTURE FROM EMA, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. PERFORMED CHECKLIST PER AFM VOLUME 1 LIGHT EXTINGUISHED. CONTINUED FLIGHT TO BRU. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED AIR SHUTOFF VALVE IAW MM 75. (M)SDR TWAA9814302Gasket · leakingNR 1 STRUT OVERHEAT ILLUMINATED IN FLIGHT. EXTINGUISHED WHEN NR 1 BLEED SELECTED CLOSED. FLIGHT RETURNED TO STL. REPLACED 2 EA 13TH STAGE WING ANTI-ICE VALVE GASKETS. CHECK-C 8-23-98 MCI.SDR 98ZZZX3703Valve · leakPHX/LAX - FLT 643 - ENGINE FIRE INDICATION ON CLIMB-OUT NR 2 ENGINE. SHUT DOWN NR 2 ENGINE, RETURNED TO PHX.SDR VNAA9808024Deice Boot · defectiveDURING TAXI FOR TAKEOFF, CREW RECEIVED AIRFRAME DEICE FAIL MESSAGE. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED AIRCRAFT AND DEFERRED RT MIDDLE WING DEICE BOOT. AIRCRAFT WAS RELEASED AND FLOWN TO PIT. PIT MAINTENANCE REPLACED RT MIDDLE AIRFRAME LEADINSDR CA980818027Tube · melted(CAN) CREW REPORTED AIRFOIL LIGHT ILLUMINATED DURING TAIL CYCLE. MAINTENANCE FOUND THAT THE DEICE TUBING FOR THE TAILETS HAD MELTED DUE TO THE ROUTING BY THE LOGO LIGHTS. TUBING REPLACED AND RE-ROUTED.SDR 98ZZZX3237Anti Ice · inoperativeWING ANTI-ICE VALVE SUTCK IN THE OPEN POSITION. THIS ALLOWED THE WING DUCT IN THE CABIN TO OVERHEAT. THE FLIGHT WAS INTERRUPTED, BUT THERE WERE NO INJURIES.SDR 98ZZZM962Gasket · looseWHILE AT ALTITUDE, THE PILOTS TURNED ON THE WING AND HORIZONTAL STABILIZER ANTI-ICE SYSTEM, ONCE ENGAGED THE CREW IMMEDIATELY SMELLED 'BURNING RUBBER' AND HEARD A SOUND OF RUSHING AIR IN THE CABIN. THE WING STAB HEAT SWITCH WAS IMMEDIATELY TURNED OFF. INVESTSDR VNAA9807005Deice Boot · wornTHE RIGHT HAND WING SURFACE DE-ICE SYSTEM FAILED, DURING THE TAXI PRIOR TO TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE DEFERRED THE SURFACE DE-ICE SYSTEM PER THE MINUMUM EQUIPMENT LIST, AND THE AIRCRAFT WAS RETURNED TO SERVICE. ON 15 JULY 98, MASDR K3HA980090Anti-Ice Valve · looseNR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON AFTER TAKEOFF LIGHT WOULD EXTINGUISH AT 1.4 EPR. SECURED LOOSE BOLTS ON WING ANTI-ICE VALVE MM 30-13-0.SDR COMA9810157Current Sensor · failedCREW REPORTED F/O 'S AOA HEAT INOP. AVIONICS REPLACED THE RIGHT CURRENT SENSOR ASSEMBLY. UPON INSPECTION/TEARDOWN IN THE AVIONICS SHOP, THE CURRENT SENSOR FOR THE RIGHT AOA VANE HEAT WAS FOUND TO BE DAMGED BY SEVERE OVERHEATING. THE CURRENT SENSOR WAS REPLASDR ORJA98123Duct · crackedAIR TURN BACK DUE TO TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON DURING CLIMB. COMPLIED WITH EMERGENCY PROCEDURES. COULD EXTINGUISH LIGHT WITH POWER REDUCTION ONLY AND SO RETURNED FOR PRECAUTIONARY LANDING. FOUND CRACKED DUCT ABOVE A/C MACHINE AFT SIDE RT, ASSSDR COMA9860159Switch · malfunctionedANTI-ICE DUCT LEAK WARNING. COULD NOT DUPLICATE DISCREPANCY. TROUBLE SHOOTING FOUND NO DEFECTS. REPLACED MID WING LEAK SENSORS FOR TROUBLE SHOOTING.SDR 98ZZZX2630Motor · shortedPILOT/OWNER REPORTED SMOKE AND CIRCUIT BREAKERS TRIPPED IN-FLIGHT, LANDED WITHOUT INCIDENT. INVESTIGATION FOUND LT ENGINE DE-ICE DEFLATOR MOTOR SHORTED AND BURNT WIRING FROM MOTOR THROUGH FUSELAGE TO THE OVERHEAD PANEL IN COCKPIT.SDR 98ZZZX4098Line · chafedDURING AREA INSPECTION BEHIND PANEL F169, NOTED THE TKS MAIN SUPPLY LINE TO THE HORIZONTAL STABILIZER LEADING EDGE WAS ROUTED BEHIND THE AIR SUPPLY LINE TO THE LEFT ENGINE AIR JET PUMP. THE TKS LINE WAS UNDER TENSION, WAS MELTED, AND DEFORMED TO THE EXTENT THSDR SCNA98055Gasket · leakingENGINE NUMBER THREE STRUT OVERHEAT LIGHT ILLUMINATED ON CLIMBOUT. RAN COM CHECKLIST. LIGHT EXTINGUISHED WHEN THE NUMBER THREE ENGINE THRUST LEVER WAS RETARDED. RETURNED TO IAH. FOUND A GASKET ON THE WING ANTI-ICE HIGH PRESSURE SHUTOFF VALVE LEAKING. REMOVSDR P5CA9800778Control Card · overheatedAPPROXIMATELY 6 HOURS INTO FLIGHT HAD STRONG ODOR OF ELECTRICAL COMPONENTS OVER HEATING/BURNING. ALSO, HAD VISIBLE SMOKE HAZE. RAN SMOKE SOURCE AND ELECTRICAL FIRE CHECKLIST. CREW USED OXYGEN ODOR DISSIPATED AFTER 20 TO 30 MINUTES. FOUND WING ANTI-ICE CONTSDR TC8A98025Anti-Ice Duct · brokenFIRE WARNING NR 2 ON CLIMBOUT. REMOVED AND REPLACED BROKEN ANTI-ICE DUCT IAW MM 75-10-3 AND REPAIRED CRACK ON DIFFUSER IAW MM 72-00.SDR 98FDEA00331Shutoff Valve · malfunctionAFTER TAKEOFF, DUCT OVERHEAT LIGHT ILLUM FOLLOW BY ZONE 4 MAIN CARGO SMOKE WARN LIGHT AND BELL. SMELL SMOKE IN COCKPIT LIGHTS AND BELL EXTINGUISH THEN CAME ON ANOTHER. THE NR 3 ENG DUCT TEMP WAS 220 DEG NR 1 ENG WAS APPROX 180. OPER CKD WING ANTI-ICE SYS, ALSDR COMA9810109Control Valve · malfunctionLEFT AND RIGHT OUTBOARD WING DE-ICE CAUTION WARNINGS AFTER TAKEOFF. REPLACED THE DE-ICE EJECTOR CONTROL VALVE.SDR 98ZZZX1918Tubing · collapsedAT ANNUAL INSPECTION, THE BLUE PNEUMATIC LINE FOR RT WING DE-ICE BOOTS WAS FOUND COLLAPSED IN THE AREA JUST BELOW THE RT CABIN HEAT VENT LOCATED AFT OF THE CO-PILOT'S SEAT. THE VENT DUCTING APPEARED TO HAVE BECOME DISCONNECTED AND HAD HEATED THE TUBING ENOUGHSDR 9806929931T-Duct · crackedDURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH ROLL TO THE RIGHT. CREW RECYCLED SLATS WITH SAME RESULTS. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT USING FLAPS ONLY. MAINTENANCE FOUND THE RIGHT SLAT BINDING DUE TO RIGHT ANTI-ICE T-DUCSDR CA980603007Boot · cracked(CAN) CREW UNABLE TO ENGAGE RUDDER GUSTLOCK. INVESTIGATION FOUND THAT IT WAS SEIZED. THIS WAS ATTRIBUTED TO THE ANTI-ICE BOOT BEING CRACKED. PART TC: 9,914.SDR 9805749751Press Switch · erraticDURING CLIMB-OUT FROM DTW, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED UPON SELECTION OF WING ANTI-ICE. FLIGHT WAS DIVERTED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED WING ICE PROTECTION AIR PRESSURE SWITCH. OPERATIONAL CHECK NORMSDR COMA9810071De-Ice Boots · failedSTABILIZER AND WING LEADING EDGE DE-ICE FAILED. REPAIRED LEAKS IN WING AND STABILIZER DE-ICE BOOTS.SDR 98FDEA00208Gasket · leaking98-0074, DURING CLIMB-OUT, THE NR 3 ENG STRUT OVERHEAT LIGHT ILLUM. ENG NR 3 BLEED AIR SWITCH WAS CLOSED AT THE TIME THE LIGHT ILLUM. APPROPRIATE RED TABS WERE ACCOMPLISHED AND THE LIGHT WENT OUT PRIOR TO THE STEP REQUIRING POWER REDUCTION. WING ANTI-ICE WASDR COMA9860063Duct · crackedWING ANTI-ICE DUCT WARNING MESSAGE ON EICAS. REPLACED THE RIGHT WING BLEED AIR PICCOLO TUBE.SDR USAAF98025Switch · failedCLT - FLT 1210 - ON CLIMB-OUT OF CLT AIRCRAFT HAD A WING ANTI-ICE FAULT TWICE BETWEEN 9000 FEET - 11,000 FEET. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WING ANTI-ICE SWITCH IN OVERHEAD PANEL. PERFORMED OPERATIOSDR CALA9800269Sensor · inoperativeTHE RT AIR CONDITIONING SUPPLY TEMP HIGH LIGHT ILLUMINATED AFTER TAKEOFF WITH SMOKE IN THE CABIN. THE AIRFOIL ICE PROTECTION WAS ON. THE PACK WAS TURNED OFF AND THE SMOKE DISSIPATED. THE RT ICE PROTECTION HIGH TEMP SENSOR WAS REMOVED AND REPLACED IAW MM 30-SDR C2XA98CL012O-Ring · wornCLE - FLT 4043 - CREW REPORTED WHILE CLIMBING THROUGH 5,000 FEET WITH ANTI-ICE ON, THEY RECEIVED A LEFT HAND ENGINE BLEED LEAK ON EICAS AND A RED LEAK MESSAGE IN BLEED SWITCH ON OVERHEAD PANEL. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCESDR 98ZZZX1007Transition Duct · failedWING LEADING EDGE ANTI-ICE DUCT IS COLLAPSED BLOCKING AIRFLOW TO THE RIGHT WING ANTI-ICE. TT: 8,961.8 HOURS.
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