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 JBXA000261Thermoswitch · failedFLT 930 RDU/DCA ON CLIMBOUT HAD WING OVERHEAT MESSAGE. AIRCRAFT RETURNED AND LANDED AT RDU. REMOVED PANEL 620ML, REMOVED AND REPLACED TEMP SWITCHES 2S4HA, 2S5HA, 2S6HA. TEMP SENSORS 2RT2HA, 2RTHA AND REINSTALLED PANEL. OPERATIONAL CHECK GOOD IAW CL-65 MM 3SDR DLM88010452Duct · contaminatedFUMES FROM WING ANTI-ICE SYSTEM SET OFF SMOKE DETECTORS IN BOTH AFT LAVS - COULD NOT DUPLICATE - PERFORMED DUCT BURNOUT AS PRECAUTIONSDR TWAA0104901Regulator Valve · malfunctionedWITH WING ANTI-ICE ON, HOT SMOKEY SMELL FILLED THE CABIN. REPLACED THE RIGHT ANTI-ICE PRESSURE REGULATING VALVE. CHECK-C 3-3-01 STL.SDR DHL2001806638Diffuser · crackedC-CHECK, LT WING L/E ANTI-ICE DIFFUSER 1 INCH CRACK AT LOWER PART STA AFS 766.500 - XFS 766.950.SDR DHL2001806581Diffuser · crackedC-CHECK - LT WING ANTI-ICE DIFFUSER UPPER PART HAS A 1 INCH CRACK AT STA XFS 728.720. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. SDR DHL2001806575Diffuser · crackedC-CHECK - LT WING L/E ANTI-ICE DIFFUSER HAS A 1/2 INCH CRACK AT LWR PART STA XFS 747.500. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806574Diffuser · crackedC-CHECK - LT WING L/E ANTI-ICE DIFFUSER 1 INCH CRACK AT LWR. PART STA XFS 728.750. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806565Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER LOWER PART 1-1/2 INCH CRACK AT STA XFS 728. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806564Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER LOWER PART 1/2 INCH CRACK AT STA XFS 760-250. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806562Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSERS 1-1/2 INCH CRACK AT UPPER PART STA XFS 745.950. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUSDR DHL2001806561Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER LWR PART 1/2 INCH CRACK AT STA XFS 766.250. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSDR DHL2001806557Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER, 1 INCH CRACK AT UPPER PART STA XFS 766.500 - XFS 766.950. PERFORMED STOP HOLE. AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-SDR SIMA0698Connector · damagedDFW - FLT 3951 - CREW REPORTED BLEED LEAK 1 AND WING 1 ANTI-ICE FAIL ON EICAS. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY FOR THE BLEED PROBLEM. GROUND RAN AIRCAFT WITH NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED CANNON PLUG FOR LEFT WING BURST SWITSDR COMA0110042Boot · damagedWING DE-ICE FAIL WARNING. REPAIRED HOLES IN WING LEADING EDGE DE-ICE BOOTS, USING PATCH KIT.SDR MWEA010274Anti-Ice System · inoperativeLEFT OVERWING HEATER INOPERATIVE. REMOVED AND REPLACED HEATER BLANKET.SDR JBXA000252Control Panel · defectiveWING OVERHEAT IN FLT RIGHT WING. REMOVED AND REPLACED ANTI ICE CONTROL PANEL IAW CL-65 AMM 30-12-21. TEST FLEW A/C, CHECKED GOOD IN FLT.SDR VNAA0103004Anti-Ice System · failedDURING CLIMBOUT THE FLIGHT CREW RECEIVED A RIGHT WING MIDDLE AIRFOIL DEICE FAIL MESSAGE. THE FLIGHT CREW RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MIDDLE LEADING EDGE ASSEMBLY IN ACCORDANCE WITH DORNIER SDR SWIA972403Ejector Valve · malfunctionedAFTER TAKEOFF INBOARD LEFT AND RIGHT STAB AND INBOARD LEFT AND RIGHT WING DEICE LIGHT CAME ON BOTH TIMERS IN HEAVY AND LIGHT CYCLE. RETURNED TO LAX. INSTALLED SERVICEABLE RIGHT FOWARD EJECTOR VALVE FOR BOOTS IAW 30-10-00. RAN ENGINE AND OPS CHECK GOOD. REISDR SWIA972413Ejector Valve · failedVERTICAL FIN LEADING EDGE DEICE INOP. FAILED AIRBORNE. REMOVED AND REPLACED DEICE EJECTOR VALVE IAW 30-20-04. OPS CHECK GOOD. P/N 3D2376-06, S/N ON PM878, OFF PM805.SDR VNAA0102017Duct · failedDURING FLIGHT THE LEFT ENGINE INLET DEICE AND LEFT OUTBOARD WING DEICE FAILED. THE FLIGHT DIVERTED TO PIT WHERE HIGH WINDS AND TURBULENCE CAUSED A MISSED APPROACH. THE FLIGHT CREW THEN DIVERTED FOR MORE FAVORABLE LANDING CONDITIONS AND THE AIRCRAFT LANDED WITHSDR 20010410AP003Boot · leakingNOTED FUEL LEAK FROM BEHIND RT WING DE-ICE BOOT. AFTER PEELING BOOT BACK TO RESEARCH LEAK, NOTED NUMEROUS AREAS OF HEAVY CORROSION. AIRCRAFT WAS FERRIED TO FACILITY FOR REPLACEMENT OF LEADING EDGE ASSEMBLY.SDR MWEA010167Regulator Valve · stuckDURING CLIMBOUT FROM MILWAUKEE, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT CAME ON. AIRCRAFT RETURNED TO MILWAUKEE. MAINTENANCE REMOVED AND REPLACED THE RIGHT PRESSURE REGULATOR VALVE FOR STICKING OPEN.SDR COMA0160251Warning System · activatedANTI ICE DUCT WARNING. INSTALLED RUBBER BOOTS ON THERMAL SWITCHES WIRE CONNECTION LT OUTBOARD WING LEADING EDGE.SDR COMA0160247Valve · malfunctionedRT WING ANTI ICE CAUTION MESSAGE. REPLACED THE LT MODULATING VALVE.SDR COMA0160246Coupling · leakingWING ANTI ICE DUCT WARNING. REPLACED BLEED AIR COUPLING IN RT WHEEL WELL.SDR SWIA972378Boot · tornENTIRE LEADING EDGE DEICE SYSTEM FAILED AT CRUISE. UPON INSPECTION FOUND A LARGE TEAR IN THE UPPER PORTION OF THE LEFT OUTBOARD BOOT. DIVERTED FROM RDM TO RDD. COMPLIED WITH REPLACEMENT OF LEFT OUTBOARD DEICE BOOT. OPS CHECK AND FUNCTIONAL CHECK GOOD OF LESDR CA010222017Pressure Switch · intermittent(CAN) DURING FLTS WHEN DE-ICE SYS IS DEPLOYED & OAT IS IN -30 & BELOW RANGE, & EITHER 1 OR 3 MIN CYCLE DURATION IS SELECTED, SYS INDICATES PROPER OP THROUGHOUT CYCLE. UPON COMPLETION OF CYCLE AMBER DE-ICE CAWS CAUTION WOULD ILLUMINATE IN CONJUNCTION WITH FLASHSDR COMA0160185Warning System · false activationWING OVERHEAT WARNING. COULD NOT DUPLICATE. FUNCTION CHECK OF SYSTEM WAS NORMAL.SDR SIMA0274Timer · inoperativeDFW - FLT 3841 - EN ROUTE TO AMA, CREW REPORTED THE DE-ICE TIMER LIGHT CAME ON DURING OPERATION. FOLLOWED CHECKLIST AND COULD NOT INFLATE RIGHT WING BOOT MANUALLY OR IN AUTO. AIRCRAFT WAS LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED DE-ICE TIMER ISDR GLBA2001017Tube · damagedRETURN TO BLOCK - LEFT BLEED AIR FAIL, REPAIRED EVA TUBING LEFT I/B WING OPS CHECKED SYSTEM GOOD.SDR C1HA200195001Anti-Ice Valve · failedON CLIMBOUT WITH WING A/I ON THE ENG NR 1 WING ANTI ICE VALVE FAILED CLOSED. DIVERTED TO DFW FOR REPAIR. REMOVED AND REPLACED LEFT WING ANTI ICE VALVE IN VENTRAL AREA.SDR MALA010146Warning Light · illuminatedRT AIR VALVE LIGHT ILLUMINATED IN FLIGHT. AIR TURNBACK TO DTW. MAINTENANCE REPLACED ANTI-ICEVALVE P/N 6068T56P01, S/N OFF GRTB7662, S/N ON GRTG1442, PER SF340AMM. PERFORMED OPS CHECK, ALL CHECKS GOOD AT THIS TIME.SDR SWIA972309Pressure Switch · failedMIDDLE LEFT DEICE INOP INFLIGHT. DIVERTED TO FAT FROM VIS. REPLACED LEFT MIDDLE DEICE BOOT PRESSURE SWITCH AND PATCHED SMALL HOLE IN BOOT. OPS CHECKS GOOD. P/N ON: 211C117-183, S/N ON: N735, S/N OFF: 088D10021A.SDR G1FR100YHose · failedAFTER COMPLETING A MFG 1200 HR B INSPECTION, A MAINTENANCE GROUND RUN OPERATIONAL CK OF THE WING ANTI-ICE SYSTEM WAS REQUIRED AND ACCOMPLISHED. NO HEAT WAS NOTICED AT RT OUTBOARD SLAT WITH ANTI-ICE WINGS SELECTED AND GREEN OPERATIONAL LIGHT ILLUMINATED. FURTSDR CA010301010Timer · failed(CAN) THE FLIGHT CREW REPORTED THAT THE AIRFRAME DEICE SYSTEM WAS OPERATING ERRATICALLY IN THE AUTO SLOW MODE. THE DEICE TIMER WAS REPLACED AND THE AIRCRAFT WAS ARETURNED TO SERVICE.SDR RAIA00101012Pitch Horn · failed7136-STL- DURING CLIMBOUT, RUDDER AND ELEVATOR HORN HEAT FAULTED. MAINTENANCE REMOVED AND REPLACED THE ELEVATOR HORN IAW ATR42 MAINTENANCE MANUAL.SDR COMA0160126Duct · leakingWING OVERHEAT AND ANTI-ICE DUCT LEAK WARNING. COULD NOT DUPLICATE. DEFERRED MAINT PER MEL. SYSTEM WORKS OK IN STANDBY MODE.SDR CA010212026Pressure Switch · failed(CAN) PILOT REPORTED WHEN AIR FRAME DE-ICE ACTIVATED YELLOW CAUTION LIGHT STAYED ON. THE HORIZONTAL STABILIZER BOOT PRESSURE SWITCH WAS REPLACED AND SYSTEM CHECKED SERVICEABLE.SDR MWEA010045Valve · inoperativeLEFT ICE PROTECTION LIGHT HI TEMP ILLUMINATED 2 MINUTES AFTER TAKEOFF. REPLACED AUGMENTATION VALVE AND ANTICIPATOR ASSY.SDR SWIA972289Boot · failedINBOARD STABILIZER AND INBOARD WING DEICE BOOTS FAILED AFTER TAKEOFF. RETURNED TO SEA. REMOVED AND REPLACED INBOARD STABILIZER AND WING EJECTOR VALVE WITH SERVICEABLE UNIT. OPS CHECK GOOD. PANEL CLOSED. S/N ON: N3503, S/N OFF: Q7401.SDR SWIA972268Switch · failedRIGHT INBOARD STABILIZER DEICE BOOT INOP BOTH TIMERS. RETURNED TO FIELD. INSTALLED SERVICEABLE RIGHT STABILIZER PRESSURE SWITCH, IAW MM 30-10-00. RAN ENGINES, OPS CHECKS GOOD. S/N ON: 00497912, S/N OFF: 548048.SDR ASOA01002Ejector Valve · inoperativeFLT 4331 - DURING FLIGHT FROM ATL-ROA AIRCRAFT ENTERED ICING CONDITIONS AND STARTED ACCUMULATING ICE. CREW HAD A FAILURE OF THE LEFT AND RIGHT O/B STABILIZER AND VERTICAL FIN DE-ICE BOOTS. CREW DECLARED AN EMERGENCY AND DESCENDED TO 7,000 FEET. CREW FOLLOWESDR COMA0160068Warning Light · illuminatedLEFT WING ANTI-ICE CAUTION DURING T/O. COULD NOT DUPLICATE. SYSTEM TEST SATISFACTORY.SDR CA010111016Boot · delaminated(CAN) ON ANNUAL INSPECTION DE-ICE BOOTS WERE INFLATED FOR FUNCTIONAL TEST. THE INFLATION RIBS ON THE INBOARD BOOTS AT TRAILING EDGE BOTTOM WERE, FOUND TO BE DELAMINATING TOWARD THE TRAILING EDGE. NEW BOOTS WERE ORDERED AND BOTH SIDES REPLACED.SDR MWEA010034Relay · failedWHILE USING AIRFOIL ANTI-ICE LEFT HAND ICE PROTECTION TEMPERATURE HI ANNUNCIATOR ILLUMINATED. AFTER SECURING SYSTEM, RH ICE PROTECTION TEMP. HI ILLUMINATED. SECURED THE SYSTEM. -- PERFORMED SYSTEM TESTS ON RIGHT HAND AND LEFT HAND SIDES. ALL TESTS WERE WISDR VNAA0012030Warning System · failedAFTER 10 MINUTES INTO THE FLIGHT, THE CREW RECEIVED AN AIRFOIL DEICE FAIL CAS MESSAGE. DISPATCH ADVISED THE CREW TO RETURN TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE VERTICAL LEADING EDGE ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-0SDR VNAA0012029Boot · failedAFTER 10 MINUTES INTO THE FLIGHT, THE CREW RECEIVED A AIRFOIL DEICE FAIL CAS MESSAGE. DISPATCH ADVISED THE CREW TO RETURN TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE VERTICAL LEADING EDGE ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00.SDR 0307251Warning Light · illuminated0307251:DURING CRUISE, USING ANTI ICE SYSTEM, AIR FOIL ICE PROTECTION LIGHT CAME ON. CHECK LIST WAS PERFORMED AND ICE PROTECTION HIGH TEMPERATURE CAME ON, UNSATISFACTORY CHECK LIST WAS PERFORMED TOO. DUE TO ICING CONDITIONS AT DESTINATION, AIRCRAFT DIVERTED TOSDR SWIA972212Warning Light · false activationRIGHT INBOARD WING DEICE LIGHT ILLUMINATES ERRONEOUSLY. ABORTED TAKEOFF. MEL 30-10-1, MC 2762 RAN RIGHT INBOARD WING DEICE BOOTS. COULD NOT DUPLICATE AT THIS TIME. OPS CHECK GOOD.SDR SWIA972207Flow Valve · failedLEFT AND RIGHT INBOARD WING AND STABILIZER LEADING EDGE BOOTS (4) INOP AT ALL CYCLE/TIMER COMBINATIONS. DIVERTED TO SMF. DEFERRED MEL 30-10-1. REPLACED LEFT AND RIGHT INBOARD WING LEADING EDGE BOOTS FLOW CONTROL, VALVE. RAN BOTH ENGINES. OPS CHECK GOOD.
Back to JASC 3010