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 CA051116003Boot · tornIN CRUISE FLIGHT, A THUMPING NOISE WAS DETECTED ON THE RIGHT SIDE OF AIRCRAFT. AFTER LANDING IT WAS FOUND THAT A NEWLY INSTALLED RIGHT INBOARD WING BOOT LOWER HALF HAD TORE LOOSE FROM THE GLUE, AND WAS TRAILING BEHIND THE AIRCRAFT ABOUT 8 FEET HITTING THE LOWSDR CA051223016Boot · splitCREW REPORTED A FAIL INDICATION FOR THE RT HORIZONTAL STAB DEICE BOOT. UPON INSPECTION BY MAINTENANCE THE BOOT HAD A 12 INCH SPLIT AND WAS REPLACED. NO IN FLIGHT HANDLING PROBLEMS WHERE REPORTED.)SDR QXEA200501504Timer · malfunctionedSEA FLIGHT NR 2177, AIRFRAME AUTO DEICE DOES NOT OPERATE IN SLOW OR FAST MODE. AIRFRAME MANUAL WORKS NORMAL. MAINTENANCE REPLACED AIRFRAME DEICE TIMER. FUNCTIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.SDR QXEA200501496Valve · malfunctionedSEA FLIGHT NR 2327: WHILE DESCENDING ON APPROACH AND OAT-2 DEG C, THE DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED. AFTER SELECTING AIRFRAME MODE TO SLOW, THE NR 1 BOOT PAIR LIGHT ON FO'S SIDE WASN'T ILLUMINATED. RAN THE CHECKLIST AND THE DEICE LIGHT DIDN'T GO SDR 2006FA0000329Boot · damagedINADVERRTENT ACTIVATION OF ANTI-ICE SYSTEM ON GROUND, RESULTING IN DAMAGE TO ANTI-ICE BOOTS WAS CAUSED BY AN INTERMITTENT GROUND OF CIRCUIT THAT IS NORMALLY OPEN. THE WIRE NR H255A20 RUNS FROM THE CONTROLLER TO THE REMOTE CIRCUIT BREAKER. (K)SDR QXEA200501384Deice System · malfunctionedSEA FLIGHT 2434, DEICE PRESSURE CAUTION ILLUMINATED INFLIGHT. CHECKLIST WAS RUN. CAUTION LIGHT STAYED ILLUMINATED UNTIL DESCENDING THROUGH 10,000 FEET. MAINTENANCE INTEROGATED CDS WITH NO RELATED FAULT CODES FOUND. PERFORMED FUNCTIONAL TEST OF THE AIRFRAMESDR QXEA200501364Brush Block · damagedSEA FLIGHT NR 2345, PROP DE-ICE CAUTION LIGHT ILLUMINATED. RAN ONE (1) CYCLE IN FLIGHT PER CHECKLIST. RT PROP DEICE ADVISORY LIGHT ONLY CAME ON. NO ELEC LOADS NOTED ON ANY PHASE A/C. MAINTENANCE TROUBLE SHOT. FOUND NR 1 ENGINE BRUSE BLOCK GAP DISTANCE TO SDR AALA20050695Heater · overheatedAIRCRAFT AIR INTERRUPTED INTO BNA DUE TO HOT SPOT AND DISCOLORIZATION OF SIDEWALL PANEL AT SEAT 17A. FOUND OVERWING DE-ICING HEATER OVERHEATING. PULLED AND COLLARED CIRCUIT BREAKER AND PLACARDED SYSTEM. AIRCRAFT DEPARTED TO BWI. SYSTEM GROUND CHECKED NORMASDR MASA200500782Duct · damagedASH 2893 ALB - A-ICE DUCT WARNING. MX REMOVED AND REPLACED DUCT ASSY, OPS CHECKED GOOD.SDR MASA200500781Warning System · false activationASH 2893 ALB - LEFT WING ANTI-ICE WARNING MESSAGE. CONTRACT MAINTENANCE PERFORMED A TEST OF THE SYSTEM BUT WERE UNABLE TO DUPLICATE THE DISCREPANCY.SDR AU510001602Anti-Ice Valve · faultyRT WING ANTI-ICE MESSAGE. THERMAL ANTI-ICE VALVE FAULTY.SDR 4508909252005Relay · failedRED CAS STAB OVERHEAT, BURNING SMELL IN CABIN. CREW ADVISED THE RED (STAB OVHT) CAS MESSAGE ILLUMINATED WITH CWP AND TRIPLE CHIME DURING CLIMB THROUGH FL 30.0. THE THRUST LEVERS WERE JUST BELOW MCR, 82% N1 AND -29 TEMP. CREW SELECTED ANTIICE *OFF* AND PULLESDR CA060219002Regulator · malfunctionedNR 2 ENGINE FORWARD DE-ICE VALVE P/N 28E96-2D WAS FOUND DAMAGED DURING 3 MONTH LUMP INSPECTION WHILE PERFORMING ZONAL TASK CARD 422 (PANEL 422DT) THERE DC FEED CABLES WERE POSITIONED WRONG AND HAD CHAFED THROUGH RUBBER COATING OF TERMINAL AND HAD SHORTED AGAINSDR COMA0560487Element · malfunctionedFLIGHT 5414 - LEFT 14TH DUCT WARNING MESSAGE. REPLACED THE BLEED LEAK SENSE ELEMENT.SDR 05FDEA02543Pressure Switch · failedEN ROUTE AT FL 350, IN AND OUT OF POSSIBLE ICING CONDITIONS, WHEN INITIATING WING A/I ON, RECEIVED AIR SYS 3 OFF (LEVEL 1) ANNUNCIATED, WITH NR 3 BLEED (AMBER) AND NR 3 MANF (RED) LIGHTS ILLUMINATED. QRH PROCEDURES FOLLOWED. DIVERTED INTO TO KDEN. RED MANF SDR RAIA00508016Odor · detectedFLT 8002 - ALB - SMELL IN CABIN/FLIGHT DECK WHEN ANTI-ICE SYSTEM WAS ACTIVATED. MAINTENANCE DEFERRED THE ANTI-ICE SYSTEM.SDR CA050815004Isolation Valve · leaking(CAN) WHILE COMPLETING THE DE-ICE PRESSURE REGULATOR FUNCTION CHECK THE WING DE-ICE ISOLATION VALVE WAS FOUND TO BE LEAKING (NOT CLOSING COMPLETELY) ALLOWING AIR PRESSURE TO BOTH WINGS. TWO OTHER ISOLATION VALVES WERE FUNCTION CHECKED AND WERE ALSO FOUND NOT CSDR S2YA05043Boot · inoperativeDURING FLIGHT, THE CREW REPORTED ELEVATOR HEAT MESSAGE. SINCE WEATHER WAS ENROUTE, THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED THE RT ELEVATOR HORN ASSEMBLY IN ORDER TO REPAIR THE HEAT WITH OPERATIONAL CHECKS GOOD THE AC WAS RETURNED TO SERVICESDR QXEA200501125Switch · malfunctionedSEA - DE-ICE PRESSURE ON DURING DESCENT (9 PSI) DURING TAXI PRESSURE RETURNED TO NORMAL (SELECTED BOOT AIR TO ISO AS PER CHECKLIST). REPLACED NR 1 & 2 LOW PRESSURE SWITCHES (55) PERFORMED FUNCTIONAL CHECK OF BLEED AIR SYSTEM IAW AMM 21-11-00, PAGES 501-503. OPSDR ASMF200506026Thermoswitch · failedAIRCRAFT ARRIVED WITH CAPTAIN REPORT WHEN AIRFOIL ANTI-ICE IS IN USE, THE AIRFOIL PRESS ABNORMAL LIGHTS TURNED ON, THE TIME PRESS INDICATION SHOWS 60 PSI, THE LAND R ICE PROTECT TEMP LOW LIGHTS TURNED ON AND LT AND RT AIR COND TEMP HIGH LIGHTS TURNED ON. ANTISDR CA050625001Piccolo Tube · cracked(CAN) WHILE CARRYING OUT INSPECTION IAW S/B 601R-30-029, MAINTENANCE FOUND 2 CRACKS IN THE OB PICCOLO TUBE ASSY. BOTH CRACKS ARE APPROX 1INCH IN LENGTH, THE FIRST CRACK IS 77.5 INCH FROM THE OB END, THE SECOND CRACK IS 83 INCH FROM OB END.SDR MASA200500407Detector · failedASH 2972 HSV TO PHL, THE AIRCRAFT DIVERTED TO CLT AFTER THE ANTI-ICE SYSTEM CAME ON IN FLIGHT FOLLOWED BY A REDUCTION IN AIRSPEED, BOTH UNCOMMANDED. MAINTENANCE TROUBLESHOT THE SYSTEM AND REMOVED AND REPLACED THE ICE DETECTORS AND RELAYS.SDR RAIA00505007Control Valve · malfunctionedFLT 5773 - STL - STAB ANTI-ICE FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED STAB ANTI-ICE CONTROL VALVE.SDR QXEA200500973Deice System · malfunctionedOUTSIDE RT GREEN TAIL LIGHT ILLUMINATES MOMENTARILY, DEICE PRESSURE 20 PSI WITH ON LT LIGHT ILLUMINATING AND "ISO" SELECTED PER CHECKLIST. MX REPLACED RT OUTBOARD DDV. PERFORMED FUNCTIONAL TEST OF AIRFRAME DEICING SYSTEM. ALL CHECKED GOOD. ACFT RETURNED TOSDR COMA0560299Anti-Ice System · malfunctionedFLIGHT 5345 ANTI ICE DUCT WARNING. INSPECTION OF WING ANTI ICE SYSTEM, FOUND NO DEFECTS.SDR COMA0560279Element · malfunctionedFLIGHT 5673- ANTI ICE DUCT WARNING. REPLACED THE LT FUSELAGE SENSING ELEMENT A47WK.SDR COMA0560228Warning System · malfunctionedFLIGHT 5175 - DURING TAKEOFF ROLL, RECEIVED A RIGHT WING ANTI ICE CAUTION, ABORTED TAKEOFF AND RETURNED TO THE GATE. C/W RTO INSPECTION AND PERFORMED AN OPERATIONAL CHECK OF THE WING ANTI ICE SYSTEM. DISCREPANCY COULD NOT BE DUPLICATED.SDR COMA0560201Sensor · malfunctionedFLIGHT 5060 RECEIVED A WING OVERHEAT WARNING DURING CRUISE FLIGHT. CREW DECLARED AN EMERGENCY AND RETURNED TO CVG. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED WING OVERHEAT SENSOR.SDR 69761Annunciator · illuminatedTHE PILOTS TOOK OFF FROM DUJ ABOUT 60NM FROM PKB. ON LAST FLIGHT OF THE DAY CHECKS, NOTICED THAT WHEN THE SURFACE DEICE WAS CYCLED THAT THE TAIL DEICE AND INBOARD WING DEICE ANNUNCIATORS REMAINED ILLUMINATED, ALONG WITH ABNORMAL INDICATIONS ON THE VACUUM AND SDR RAIA00503009Warning Light · illuminatedBDL - AIRFRAME ANTI-ICE INOP WARNING INDICATION. MAINTENANCE INSPECTED ANTI-ICE DETECTION SYSTEM AND PERFORMED OPS CHECK. FOUND SYSTEM OPS NORMAL.SDR A6WA200540082Pressure Switch · failedON TAKEOFF IN ICING CONDITIONS, BOTH WING ANTI-ICE CAUTION MESSAGES. TRANSFERRED TO STANDBY GOT RT WING ANTI-ICE CAUTION MESSAGE. COMPLIED WITH QRH AND MANUALL OPENED 14TH STAGE VALVE MODULATED OPEN/CLOSED. LEFT WING ANTI-ICE SOV CLOSES. EXITED ICING CONDISDR MALA050221Deice System · inoperativeAIR RETURN DUE TO TAIL DEICE INOP. NO FURTHER INFORMATION AT THIS TIME.SDR DXTA200500604Sensor · failedABORTED T/O DUE TO WING A/I HOT L CAS MESSAGE. RAN ENG, TURNED ON SLAT ALI FELT LT & RT WING L/E'S DID GET WARN. I/B LT WING L/E REMOVED TO INSPECT WING L/E A/I DUCT O-RING. ACCESSED IMT I/B, MID & O/B WING, TEMP NORMAL. COULD NOT DUPLICATE CN SUBSEQUENT SDR 2005UALA00163Duct · chafedLEFT WING BLEED LEAK MESSAGE AFTER TAKEOFF. A SMALL HOLE WAS FOUND IN A WING-ANTI ICE DUCT FLANGE. THE HOLE WAS CAUSED BY A CLAMP CHAFING THE DUCT FLANGE. THE DEFECTIVE DUCT WAS REPLACED AND A NEW CLAMP INSTALLED.SDR COMA0560127Anti-Ice System · faultyFLIGHT 5574 RECEIVED A LEFT WING ANTI-ICE WARNING DURING CRUISE FLIGHT, RETURNED TO CVG. REPLACED THE LEFT WING LEADING EDGE INBOARD AND MIDDLE ANTI ICE SENSORS.SDR COMA0560121Warning Light · false indicationFLIGHT 5532 ANTI-ICE DUCT WARNING. COULD NOT DUPLICATE. OPERATIONAL CHECK OF ANTI ICE SYSTEM WAS NORMAL.SDR COMA0560104Anti-Ice System · crackedFLIGHT 5869 RIGHT WING ANTI ICE DUCT WARNING. REPLACED THE OUTBOARD PICOLO TUBE.SDR CWQR20050001Heat Shield · crackedDURING INSPECTION FOUND THE LEADING EDGE HEAT SHIELD FLANGE CRACKED ON BOTH LEFT AND RIGHT WINGS. SUBMITTED CESSNS/CITATION SERVICE CONDITION REPORT 181187 WITH PICTURES.SDR 2005FA0000487Anti-Ice System · malfunctionedDURING REPLACEMENT OF THE 17VE, ELEVATOR HORN DEICE INDICATION PROBLEM DISCOVERED THAT TEMP SENSOR FOR HORN ASSY HAD FAILED IN HIGH OHM AREA 288-300 OHM RANGE. PROBLEM WOULD NOT ALLOW FAIL LIGHT ON ASSOCIATED SWITCH ON 17VE PANEL TO ILLUMINATE DURING TEST DESCSDR COMA0560049Controller · malfunctionedFLIGHT 5147 WING OVERHEAT MESSAGE. REPLACED THE CONTROLLER.SDR QXEA200500062Deice System · malfunctionedSEA FLIGHT NR 2430 DURING DESCENT AND CRUISE, THE DE-ICE PRESS CAUTION LIGHT CAME ON. RUNNING THE APPROPRIATE CHECKLIST EXTINGUISHED THE LIGHT BUT IT CAME BACK ON WHEN BOOTS WERE SELECTED BACK ON. THE LEFT, MOST OUTBOARD BOOT SEGMENT LIGHT FLICKERED OFF AND SDR COMA0560036Anti-Ice System · false indicationFLIGHT 4959 ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. INSPECTED AND OPERATIONAL CHECKS WERE NORMAL.SDR S2YA05002Tube · damagedDURING FLIGHT, THE TAIL DEICE BECAME INOPERATIVE. DUE TO ENROUTE WEATHER, THE CREW PERFORMED AN AIR-TURN-BACK. THE SYSTEM WAS INSPECTED AND MECHANIC REPAIRED THE EVA TUBING IN THE LT STABILIZER ABOVE THE LOGO LIGHT. THE SYSTEM WAS INSPECTED AND WITH NO FURTSDR COMA0560025Warning System · activatedFLIGHT 5880, RT WING OVERHEAT CAUTION, DEFERRED MAINT PER MEL.SDR RAIA00412028Pressure Switch · failed3648- ABE- AIRFRAME DE-ICE BOOTS CCT2 AND CCT3 FAULTS. REMOVED AND REPLACED PRESSURE SWITCH.SDR RAIA00412033Warning Light · false indication5609- STL- WING ANTI-ICE FAIL MESSAGE IN FLIGHT. MAINTENANCE TEST ANTI-ICE SYSTEM. NO DEFECTS NOTED.SDR COMA0470083Shutoff Valve · malfunctionedFLIGHT 4975 RIGHT ENGINE BLEED CAUTION MESSAGE. REPLACED THE RIGHT WING ANTI-ICE SOV.SDR COMA0460681Sensor · malfunctionedFLIGHT 5097 LEFT WING ANTI-ICE CAUTION MESSAGE DURING T/O. REPLACED THE OVERHEAT SENSOR.SDR 2004UALA01208O-Ring · leakingFLIGHT DIVERTED WITH A WING LEAK, RESTRICTED TO NO ICING. FOUND FAN AIR VALVE THERMOSTAT LEAKING ONTO OVERHEAT LOOP - REPLACED SENSOR AND O-RING.SDR RAIA00412008Ejector Valve · lack of lubeCRW - AUTO AND MANUAL ICE PROTECTION SYSTEM FAULT, CCT2 LIGHT NOT GOING OUT. MAINTENANCE LUBED EJECTOR VALVE, RAN ENGINES AND PERFORMED DE-ICE TEST.
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