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 N6WA2014111700001Duct · unsecureAFTER TAKEOFF, WING ANTI-ICE WARNING. TIGHTENED DUCTS ON WING ANTI-ICE SYS & FLOW CONTROL VALVE. PERFORMED OPS CHECK ON WING ICE CONTROL & INDICATING SYS IAW AMM 30-12-00. OPS CHECKED GOOD.SDR FDEA201411173720Pressure Switch · failedWING ANTI-ICE DISAGREE AFTER TAKEOFF, FOLLOWED BY AIR SYS 1 OFF. AFTER CONSULTING MOC & GOC RETURNED. TROUBLESHOOTING IAW FIM 30-11 TASK 801. AIR SYS 1 OFF ALERT SUGGESTS USING FIM 36-23 TASK 803. FOUND FAULT BALL ON PNEUMATIC MANIFOLD FAULT INDICATOR PRESDR CA141110013Line · corroded(CAN) DURING A ROUTINE MAINTENANCE CHECK, TASK 7610/05 (UNRELATED TO THE ISSUE) A DE-ICE LINE WAS FOUND TO BE CORRODED UNDER THE CUSHIONED CLAMPS. THE CUSHION CLAMPS WERE WEATHERED AND HARDENED. THE DE-ICE LINE (PN 83010019-21) RUNS BETWEEN THE FUSELAGE AND THSDR AWKA20141121001Tube · bentWITH THE WING ANTI-ICE SYS ACTIVATED IN FLIGHT, THE INBD TEMPERATURE SENSORS WOULD TRIGGER THE LT & RT WING ANTI-ICE HOT CAS MSG. RAN THE ANTI-ICE SYS MONITORED THE TEMP SENSORS THROUGH THE IMT WITH NO ABNORMALITIES NOTED. BLEED LEAK MSGS WILL MOST LIKELY NOTSDR HNAA2014110700308Warning Light · illuminatedELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED IN FLIGHT. SELECTED ELEVATOR LT HORN HEAT TO ALTERNATE POSITION. GROUND RAN ACFT WITH CREW, SYSTEM OPS CHECKED GOOD IAW MM 30-16-00. OK FOR SERVICE.SDR SWIA201439814Loop · failedRETURNED TO THE FIELD WITH AN ANTI-ICE DUCT WARNING MESSAGE. CHANGED THE RT WHEEL BIN LOOP. OPS CHECKED GOOD.SDR UIEA2014103100537Hinge · crackedRIGHT WING SLAT NR 8 ANTI-ICE DUCT FWD HINGE ASSEMBLY IS CRACKED AT ATTACH TO DUCT. R & R FWD HINGE ASSEMBLY ON NR 8 SLAT RT WING ANTI-ICE DUCT COVER IAW AMM 30-11-05.SDR UIEA2014103100545Hinge · wornRIGHT WING SLAT 8 PNEUMATIC DUCT FOR WING ANTI-ICE HAS WORN HINGES ON COVER. R & R RT WING SLAT 8 PNEUMATIC DUCT FOR WING ANTI-ICE IAW AMM 30-11-05.SDR CA141031005Valve · failed(CAN) WHILE TAXING WITH ANTI-ICE FOR ICE CONDITIONS BOTH THE LT AND RT WING ANTI-ICE FAIL MESSAGE APPEARED. SUBSEQUENTLY THE LT WING ANTI-ICE FAIL MESSAGE CLEARED BUT THE RT WING ICE REMAINED FAILED. CONTINUOUS LT AND 5 WING AMBER INDICATION. THE FLIGHT CRESDR CA141021008Anti-Ice Valve · failed(CAN) DURING DESCENT IN ICING CONDITIONS, THE CREW RECEIVED A WING OVERHEAT WARNING. THE CREW COMPLETED THE REQUIRED CHECKLISTS AND PROCEDURES, AND DECLARED AN EMERGENCY WITH THE ATC. THE WARNING EXTINGUISHED UPON COMPLETION OF THE PROCEDURES, AND THE AIRCRAFTSDR 9JLA201410208307Vane · shortedTHE FLIGHT CREW REPORTED THAT THE RT AOA HT FAIL CAS MSG WITH THE ASSOCIATED RT PROBES HT AOA CB TRIPPED. THE CB WAS RESET IAW THE CHECKLIST WHERE IT TRIPPED AGAIN. TROUBLESHOOTING FOUND THE RT AOA VANE SHORTED TO GND. IT WAS ALSO FOUND THAT THE DEFECT IN TSDR RAIA201410090001Anti-Ice Valve · inoperativeWING ANTI-ICE FAIL MESSAGE ON EICAS DURING CRUISE, RETURNED TO DEPARTURE. MAINTENANCE REPLACED LT WING ANTI ICE VALVE, OPS CHECK GOOD.SDR SIMA20141008003Anti-Ice Valve · failedDURING DESCENT IN ICING CONDITIONS PASSING THRU APPROX 8000 FT, RECEIVED A RT WING OVERHEAT WARNING. COMPLIED WITH AOM VOL 1 EMERGENCY PROCEDURES & WING OVERHEAT EXTINGUISHED AFTER APPROXIMATELY ONE OR TWO MINUTES. RT WING ANTI-ICE VALVE FAILED. COMPLIED WISDR BKER2014093001Shutoff Valve · leakingAFTER DEPARTURE BOTH RED BLEED ANNUNCIATORS ILLUMINATED. THE CREW DIVERTED BACK TO BASE. PERFORMED ENG RUNS & DISCOVERED THE WING ANTI-ICE SHUTOFF & PRESS REGULATING VLV LEAKING THROUGH THE CTR PIVOT SHAFT & MATING GASKETS. THE WING ANTI-ICE SHUTOFF & PRESSSDR CA140929005Tube · distorted(CAN) HOSE LOCATED AT LEFT HAND STALL VANE LEADING EDGE (3RD INBOARD FROM WING TIP) TO BE LEAKING AND WAS REPLACED. HOWEVER, A 2ND LEAK WAS IDENTIFIED AT SLEEVE COUPLING ON INBOARD CONNECTION OF THE L/H, INBOARD DISTRIBUTOR VALVE. THE SLEEVE WAS REMOVED AND THSDR SWIA201439346Warning Light · false indicationBLEED AIR DUCT MASTER WARNING INFLIGHT. RT ENGINE BLEED AUTO SHUTOFF. PERFORMED BITE OF THE AILC AND PERFORMED A CHECK OF WING ANTI-ICE DUCT IAW AMM. NO DEFECTS NOTED.SDR 9JLA201409108117Boot · leakingFOR SEVERAL MONTHS THE CREW DESCRIBED AN INTERMITTENT IN FLIGHT VIBRATION, STARTING TYPICALLY WHILE CLIMBING THROUGH 12K'-13K'. THE VIBRATION WOULD CONTINUE WHILE AT ALTITUDE & STOP ONCE BELOW 10K'. ENG SPEED THRUST LEVER POSITION DID NOT INFLUENCE THE VIBRASDR 2014FA0000485Anti-Ice System · restrictedIT WAS REPORTED THAT THE ANTI-ICE PANELS ON THE ELEVATOR TIPS WERE NOT FLOWING ON THIS ACFT. THE SYSTEM WAS DISABLED AND THE ACFT CAME TO OUR SERVICE CENTER FOR AN ANNUAL INSPECTION. THE ELEVATOR TIP FLUID FEED LINES WERE FOUND TO HAVE A CREAMY WHITE SUBSTANSDR ASAA2014081108804Seal · crushedACCOMPLISHED NR 1 ENGINE HEALTH CHECK IAW T/C NG-36WC-00001. FOUND AIR LEAK AT GROUND WING ANTI-ICING SOLENOID VALVE CONNECTION. REPLACED CRUSHED SEAL IAW MM 30-11-12-000-801 AND MM 30-11-12-400-801. OPS/LEAK CHECK GOOD.SDR SIMA20140801002Light · inoperativePNEUMATIC ICE TEST INFLIGHT DID NOT SHOW OPEN INSCRIPTION ON WING. ALL OTHER INDICATES NORMAL. R & R LIGHT BULBS IAW AMM 20-13-04. OPERATIONS CHECKED IAW AMM 30-00-00. OPERATIONS CHECKED GOOD.SDR SIMA20140730001Manifold · faultyCLIMBING OUT IN ICING CONDITION STAB ANTI-ICE FAIL ON EICAS. FOLLOWED AOM CHECKLIST & WAS NOT ABLE TO RESTORE SYS. R & R HORIZONTAL STAB SWITCH MANIFOLD IAW AMM 30-12-14. PERFORMED OPERATIONAL CHECK OF ANTI-ICING SYS IAW AMM 30-00-00-700-802A. OPERATIONS CSDR SIMA20140709006Plate · crackedLEFT WING TELESCOPIC DUCT CLOSING PLATE IS CRACKED. INSTALLED NEW CLOSING PLATE & VERIFIED EDGE DISTANCE IAW AMM 27-81-00.SDR DALA2014071004023Heater Blanket · damagedDURING INSPECTION, VOIDS WERE FOUND OF A TOTAL AREA OF 23.6% ON RT WING HEATER BLANKET AREA REPAIRED IAW ER/A N./ 527365-14 REV ORIG.SDR DALA2014071004022Heater Blanket · debondedNINE DEBONDED AREAS ON RT WING HEATER BLANKET WERE FOUND AT INBD AREA . DAMAGE WAS REPAIRED IAW ERA 527365-14 REV ORIG..SDR DALA2014071004021Heater Blanket · debondedDBONDED AREAS ON LT WING HEATER BLANKET WERE FOUND AT INBD EDGE. REPAIRED IAW ERA 52736514 REV ORIG.SDR DALA2014071004020Heater Blanket · debondedDURING INSPECTION, VOIDS WERE FOUND OF A TOTAL AREA OF 37 PERCENT ON LT WING HEATER BLANKET. AREA WAS REPAIRED IAW ERA 527365-14 REV ORIG.SDR DALA2014070303927Heater Blanket · debondedDEBONDS OF, 12.000" X 0.500", IN OTBD EDGE AFFECTED FOR VOID OF 115 SQUARE", 14.000" X 0.500" IN OTBD EDGE AFFECTED FOR VOID OF 185 SQUARE", 55.000" X 0.500" IN INBD EDGE AFFECTED FOR VOID OF 1104 SQUARE", 12.000" X 0.500" IN INBD EDGE AFFECTED FOR VOID OF 45 SDR DALA2014070303926Structure · debondedDEBONDS OF 9.00" X 0.500" IN OTBD EDGE AFFECTED FOR VOID OF 16 SQUARE IN AND 58.00 X .0500" IN INBD EDGE AFFECTED FOR VOID OF 877 SQUARE IN ON LT WING HEATER, SM CARD 9, ZONE 00 SUMMARY. THIS NRC WAS ACCOMPLISHED IAW ETI-88-14-071, REV 7, ER/A 526807-14, REVSDR DALA2014070303925Heater Blanket · out of limitsDURING INSPECTION, VOID WERE FOUND OF 25 PERCENT THEREFORE THIS RT HEATER BLANKET IS OUT OF LIMITS IAW FIA. 1 VOIDA ACCEPTANCE CRITERIA 1, A CARD 4, ZONE 00. REPAIR WAS ACCOMPLISHED IAW ETI 88-14-071, REV 7 & ER/A 526807-14, REV ORIGINAL.SDR DALA2014070303924Heater Blanket · out of limitsDURING INSPECTION, VOIDS WERE FOUND OF 24.6 PERCENT THEREFORE THIS LT HEATER BLANKET IS OUT OF LIMITS IAW FIG 1 VOIDS ACCEPTANCE CRITERIA, 1, A. CARD 3, ZONE 00. THIS NRC WAS ACCOMPLISHED IAW ETI -88-14-071, REV 7, ER/A 526807-14, REV ORG.SDR SWIA2014061838213Sensor · failedWING ANTI-ICE SENSOR CAUTION MESSAGE. R & R RT WING CONTROL SENSOR IAW AMM. PERFORMED TEST OF NEW RT WING CONTROL SENSOR IAW AMM. R & R RT WING SUFFICIENT HEAT SENSOR IAW AMM. OPS CHECKED GOOD.SDR SWIA2014061738202Warning Message · false activationRT WING ANTI-ICE CAUTION MESSAGE WITH WINGS ON STANDBY. PERFORMED OPS CHECK OF WING ANTI-ICE CONTROL AND INDICATION IAW AMM. DID NOT RECEIVE RT WING ANTI-ICE CAUTION WHILE IN STBY MODE. OPS CHECKED GOOD AT THIS TIME.SDR SWIA201437931Overheat Sensor · failedDURING CLIMB OUT, RECEIVED A RT WING OVERHEAT MESSAGE. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. R & R RT WING OVERHEAT SENSOR AND CONTROL SENSOR WITH SERVICEABLE UNITS IAW AMM.SDR IPXA2014060483167Duct · chafed4C INSPECTION, REPAIR DOUBLER IS CHAFED AND EDGE IS BENT AROUND LT TELESCOPIC DUCT CUTOUT. REPAIRED IAW SR M57-40-01 REPAIR 10, FIG 201, REV 55.SDR AWKA201405140510D-Ring · leakingDURING CLIMB OUT & EN ROUTE, FLIGHT CREW RECEIVED AN AMBER SLAT ANTI-ICE COLD RT ALONG WITH WING ANTI-ICE HOT RT CASS MESSAGES. ACFT RETURNED FOR MAINTENANCE. THE RT WING ANTI-ICE BLEED AIR TUBE D-RING ROLLED. D RING WAS R & R, LEAK & OPS CHECKED NORMAL.SDR HNAA2014043000142Boot · damagedEVIDENCE OF BIRDSTRIKE UNDER RT HORIZONTAL STABILIZER. PERFORMED BIRDSTRIKE
INSPECTION, FUSELAGE TO NACELLE DE-ICE BOOT HAS 2 SMALL HOLES AND SMALL CUT TO REMOVE REMAINS. NO OTHER DEFECTS FOUND.SDR CA140430002Duct · ruptured(CAN) A RUPTURED COWL ANTI-ICE DUCT WAS DISCOVERED DURING MAINTENANCE. THE DAMAGED DUCT CAUSED SIGNIFICANT HEAT DAMAGE TO THE ENGINE WIRING HARNESS. ENGINE FAULTS, VSV POSITION DISAGREE AND VSV POSITION OUT OF RANGE WERE FOUND. THE NR 1 ENGINE WAS REPLACED SDR CA140417008Valve · failed(CAN) AFTER OPERATING A SINGLE SURFACE DE-ICE CYCLE THE OTBD WING DE-ICE BOOTS WOULD NOT DEFLATE. TROUBLESHOT SYS AND FOUND DISTRIBUTOR VALVE UNSERVICEABLE. DISTRIBUTOR VALVE REPLACED WITH O/H UNIT. OPS CHECK COMPLETED, SYS FUNCTION NORMAL.SDR SBAA201400001Panel · deformedDURING VISUAL INSPECTION NOTICED THAT LT & RT WING INBD TKS PANELS WERE SLIGHTLY DEFORMED ALONG LE FROM APPROX WS 37.00 TO WS 51.00. TKS PANELS DID NOT APPEAR LOOSE & SEEMED TO OPERATE NORMALLY.SDR CA140407008Sensor · shorted(CAN) ON DEPARTURE, CREW RECEIVED A WING ANTI-ICE CAUTION INDICATION. FLIGHT RETURNED TO DEPARTURE POINT AND LANDED WITHOUT FURTHER INCIDENT. THIS CAUTION LIGHT HAD A REPEAT ILLUMINATION OVER THE LAST FEW DAYS. MAINTENANCE ACTION COMPLETED. A DEFINITIVE PRSDR N6WA201404040030Sensor · faultyLT & RT WING ANTI-ICE CAUTION MESSAGE, LT INBD TEMP SENSOR. TROUBLESHOOT TO LT INBD TEMP SENSOR FAULTY. DEFERRED LT INBD WING TEMP SENSOR IAW MEL 30-12-04C CAT C ON DMI.SDR JIKA2014040101Switch · failedAPPROXIMATELY 10 MINUTES AFTER DEPARTURE, DURING CLIMB, LT WING OVERHEAT ANNUNCIATOR ILLUMINATED. PILOT & CO-PILOT FOLLOWED EMERGENCY PROCEDURES & RETURNED TO DEPARTURE. AFTER ONE MINUTE WHILE ON APPROACH, THE LIGHT EXTINGUISHED. REPLACED THE 350 & 450 DEGSDR 9JLA2014042204533Pressure Switch · failedTHE FLIGHT CREW REPORTED THAT THE LT TAIL DEICE LIGHT STAYED ON DURING ALL PHASES OF FLIGHT. TROUBLESHOOTING IDENTIFIED THE LT TAIL DEICE PRESS SWITCH WAS DEFECTIVE, PN 1106P55-1. THE PRESS SWITCH WAS R & R WITH NEW.SDR N6WA20140312004Warning System · malfunctionedLEFT BLEED DUCT MSG. PERFORMED EVENT HISTORY, NO MSG NOTED IAW CRJ700 FIM 30-11-00, ACFT OK SERVICE.SDR REXA2014030700280Warning System · false activationANTI-ICE DUCT WARNING, THEN ANTI-ICE DUCT CAUTION IN ICING CONDITIONS. RAN NON-NORMAL CHECKLIST. FLIGHT ATTENDANT REPORTED LIGHT ICE FORMING ON FRONT OF WING. WE INCREASED SPEED TO DISPERSE ICE. WHEN DISPERSAL WAS NOT SUCCESSFUL TURNED ANTI-ICE WING SWITCHSDR SIMA20140307009Warning System · false activationRT WING ANTI-ICE FAIL CAUTION MSG. PERFORMED OPERATIONS CHECK OF THE WING ANTI-ICE IAW AMM 30-12-00, OPERATIONS CHECKED GOOD.SDR CA140306012Anti-Ice Valve · failed(CAN) FLIGHT CREW REPORTED THAT WHEN HE SELECTED RT ENGINE ANTI-ICE HEAT ON HE DID NOT SEE A TORGUE DROP OR EGT DROP. THE PRESS TO TEST DID FUNTION. ACFT RETURNED TO BASE AND THE ANTI-ICE VALVE WAS REPLACED. ACFT RETURNED TO SERVICE.SDR J7SA0306201401Coupling · looseSTAB OVERHEAD CAS ILLUMINATED DURING CLIMB. LANDING & TAXI WERE UNEVENTFUL. TORQUED LOOSE COUPLINGS AT HORIZONTAL STABILIZER HEAT HOSE JOINTS. OPS & LEAK CHECKED SATISFACTORY.SDR HNAA2014030300065Boot · failedNR 2 BOOT ON RT WING WOULD NOT INFLATE OR INDICATE. R & R L/E 613BR IAW AMM 57-00-00. OPS CHECKED GOOD.SDR QXEA2014030200194Valve · failedDURING DEPARTURE, THE DE-ICE PRESSURE CAUTION ILLUMINATED. COMPLIED WITH EC. DE-ICE PRESSURE =19 PSI PHASE FLIGHT =CLIMB, THE INBD SECTION ON THE LT HORIZONTAL STAB WOULD NOT ILLUMINATE. IT TESTS OK. LIGHT MODE SWITCH=SLOW. RETURNED TO FIELD, LANDING UNEVEN
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