JASC 7510
Service difficulty reports · 869
Reports filed under 7510 · Engine Anti-Icing 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 = '7510' 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 = '7510' 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 VNAA2014111700009Anti-Ice Valve · failedCREW REPORTED LT COWL ANTI-ICE MESSAGE IN FLIGHT WITH SWITCH OFF. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT COWL ANTI-ICE VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.SDR CA141018001Structure · cracked(CAN) DURING INSPECTION, A CRACK WAS DISCOVERED IN THE ENGINE AIR INLET ANTI-ICE LIP WHERE THE BLEED AIRHOSE ATTACHES TO THE LIP. THE COWLING WAS REMOVED AND DELIVERED TO AN APPROVED ACFT WELDING FACILITY WHERE THE LIP CRACK WAS REPAIRED WITH APPROVED METHODSSDR CA140919006Shutoff Valve · failed(CAN) DURING AIRCRAFT STARTUP IT WAS REPORTED THAT THE LEFT HAND DEICE WAS NOT INDICATING CORRECTLY, UPON INSPECTION BY MAINTENANCE THE P3 SHUTOFF VALVE LOCATED AT THE ENGINE FIREWALL WAS FOUND TO BE UNSERVICEABLE,THE SWAGGED CAP HAD CAME OFF THE VALVE,AS WELLSDR DALA2014070303862Duct · blownAIR RETURNED FOLLOWING A NR 2 ENGINE FIRE INDICATION. MAINTENANCE FOUND THAT THE NR 2 ENGINE ANTI-ICE DUCT WAS BLOWN OUT AND REPLACED THE DUCT. ALL CHECKED NORMAL AND THE ACFT HAS RETURNED TO SERVICE.SDR ASAA2014061308179Anti-Ice Valve · intermittentLEFT ENGINE ANTI-ICE VALVE STUCK CLOSED, RAN QRH EXERCISED SWITCH BECAME INTERMITTENT. ACFT GROUNDED. PERFORMED FIM TASK 30-21-00-810-805 AND FOUND VALVE TO BE INTERMITTENT. REMOVED LT ENGINE COWL TAI VALVE REF MM 30-21-11. INSTALLED LT ENG COWL TAI VALVE SDR ASAA2014061108159Anti-Ice Valve · malfunctionedNR 1 ENGINE ANTI-ICE COWL LIGHT AT FIRST INTERMITTENT THEN STEADY, BRIGHT BLUE WHEN ANTI-ICE SWITCH SELECTED ON. ACFT GROUNDED. PERFORMED 30-21, TASK 805. OPS CHECKED NR 1 ENGINE ANTI-ICE VALVE. OPEN, CLOSED, BRIGHT ANN LIGHT NUMEROUS TIMES, OPS NORMAL IAWSDR HALA2014052800071Anti-Ice Valve · failedLEFT ENGINE ANTI-ICE DISAGREE LIGHT ILLUMINATED ON EICAS WHEN VALVE SELECTED TO OPEN. REPLACED LT ENGINE ANTI-ICE VALVE AMM 30-21-03. OPS CHECKED OK. OK FOR SERVICE.SDR ASAA2014052407907Valve · failedRIGHT ENGINE ANTI-ICE INTERMITENT AMBER "TAI" INDICATION. ACFT GROUNDED. REPLACED NR 2 ENGINE WIRE HARNESS IAW AMM 71-51-03. TAI AMBER LIGHT EXTINGUISHED BUT FOUND TAI BLUE VALVE OPEN LIGHT WILL NOT EXTINGUISH. REPLACED NR 2 ENGINE TAI VALVE IAW AMM 30-21-1SDR CA140407003Heater · burned(CAN) DURING APPROACH ON SHORT FINAL MASTER CONTROL CAUTION "ENG ADP HTR 1" CAME ON. AT THE SAME TIME PILOTS NOTICED A LIGHT SMELL IN THE FLIGHT DECK. AFTER LANDING THIS SMELL WAS LESS. PILOT ASKED CABIN CREW ABOUT ANY SMELL OR SMOKE IN THE CABIN. THEY TOLD SDR CA140403006Actuator · inoperative(CAN) AT TOP OF CLIMB, THE MASTER CAUTION LIGHT FOR THE RT ICE VANE ILLUMINATED. IT WAS DECIDED TO RETRACT THE ICE VANES AND COMPLETE THE MANUAL EXTENSION PRIOR TO DESCENT. PRIOR TO DESCENT, A MANUAL EXTENSION WAS ATTEMPTED. THE HANDLE COULD NOT BE PULLED ASDR ASAA2014030707109Valve · failedNR 2 ENGINE ANTI-ICE VALVE COWL VALVE OPEN SHOWS DISAGREEMENT. POSITION IN OPEN OR COWL. TAI SHOWS ON PANEL. ACFT GROUNDED. DIVERSION TIME: 52 MINUTES. R & R NR 2 ENG COWL TAI VALVE IAW AMM 30-21-11-400-801. OPS CHECK NORMAL IAW SAME.SDR CHQA20131229469Anti-Ice Valve · failedCREW RECEIVED AN NR 1 ENGINE ANTI-ICE VALVE FAIL MESSAGE IN FLIGHT. RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. REPLACED ENGINE ANTI-ICE VALVE. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.SDR CA131216024Anti-Ice Valve · failed(CAN) CREW ABORTED TAKEOFF BELOW 60 KTS DUE TO MASTER CAUTION ANTI-ICE. TROUBLESHOOTING CARRIED OUT AND NR 2 COWL ANTI-VALVE WAS REPLACED ALONG WITH THE THE NR 1 COWL ANTI-ICE VALVE AND ENGINE/WING ANTI MODULE FOR PRECAUTION.SDR ASAA2013072495671Anti-Ice Valve · inoperativeRIGHT ENGINE ANTI-ICE VALVE NOT RESPONDING TO SWITCH POSITION. ACFT GROUNDED. RAN ENGINE CYCLED ANTI-ICE VALVE OPERATES NORMALLY GROUND VERIFICATION CHECK OK REF 30-21-00-710-801.SDR AALA20130725002Duct · rupturedDFW CREW REPORTED LT ENGINE FIRE WARNING JUST AFTER GEAR UP. LIGHT INDICATION WENT OUT WHEN THROTTLE MOVED TO IDLE. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND UPPER ANTI ICE DUCT RUPTURED.
REPLACED ANTI ICE DUSDR UALA2013052903742Controller · failedNR 2 ENGINE ANTI-ICE VALVE FAILED TO OPEN ON ENGINE RUN. ACCOMPLISHED CMC TEST ENGINE RUNNING STILL FAILED TEST. REPLACED NR 2 ENGINE ANTI-ICE VALVE CONTROLLER IAW MM. OPS CHECKED GOOD ON IDLE RUN IAW TASK 30-21-00-730-806-003.SDR CA130417009Anti-Ice Valve · malfunctioned(CAN) NR 1 ENGINE ANTI-ICE AMBER LIGHT ILLUMINATED ON CENTER DU PANEL WITH ALL OTHER INDICATIONS SHOWING NORMAL. DUE TO ICING CONDITIONS CREW DID AN AIR TURNBACK , AND LATER THE NR 1 ENGINE COWL ANTI-ICE VALVE WAS REPLACED.SDR UALA2013040902367Anti-Ice Valve · failedEICAS MESSAGE, ENGINE ANTI-ICE DISPLAYED AND ENGINE ANTI-ICE VALVE LIGHT REMAINED ILLUMINATED WITH SWITCH OFF. NR 1 REMOVED AND REPLACED LEFT ENGINE ANTI-ICE VALVE PER AMM. NO HELP. REPLACED NOSE COWL ANTI-ICE VALVE FROM KNOWN GOOD NR 2 ENGINE AS PER AMM.SDR UALA2013040502291Anti-Ice Valve · stuckLEFT ENGINE ANTI ICE VALVE STUCK IN CLOSED POSITION. REMOVED AND REPLACED NR 1 ENGINE ANTI-ICE VALVE IAW AMM.SDR UALA2013031301492Warning Light · false activationON POWER UP FOR TAKEOFF, ANTI ICE ON. LEFT ENGINE BLEED CYCLED OFF. LEFT ENG ANTI-ICE SELECTED ON BLEED TRIPS AT POWER SETTINGS ABOVE 50% N1.IF ANTI-ICE IS SELECTED TO OFF POSITION BLEED DOES NOT TRIP. RESET LEFT ENGINE ANTI-ICE AND BLEED SWITCHES-NO HELP.SDR CA130221006Adapter · failed(CAN) NR 1 ENGINE INTAKE ADAPTER CB TRIPPED IN FLIGHT. DIVERTED TO BASE. MAINTENANCE FOUND THE NR 1 INTAKE ADAPTER BURNED FROM ARCING. REPLACED NR 1 ENGINE AIR INTAKE ADAPTER HEATER IAW AMM 30-21-15-000-801 & 30-21-15-400-801, PARA 1-4, COMPLETED, PARA 5 OPSDR UALA2013011400245Controller · failedRT ENGINE ANTI- ICE VALVE WILL NOT CLOSE. CREW CYCLED SWITCH, BLEEDS AND SD RT ENGINE AND RESTARTED, NO HELP. REPACED RIGHT ENGINE ANTI-ICE CONTROLLER AND OPS CHECKED OK.SDR UALA2013011400243Anti-Ice Valve · failedLEFT ENGINE ANTI-ICE VALVE FAILED IN CLOSED POSITION. VALVE REPLACED. PERFORMED TEST PER TASK 30-21-00-730-806-003. TESTED GOOD.SDR UALA2013010700079Anti-Ice Valve · damagedHMG HAS BEEN DEF IN COMPLIANCE WITH MEL CARD. REPLACED NUMBER 1 ENGINE COWL TAI VALVE REF AMM, NO HELP. ENG ANTI- ICE VALVE REPAIRED AND HMG SYSTEM HAS BEEN RESTORED PER MEL CARD. RAN CHECK & HMG CHECKED NORMAL. PERFORMED LEFT ENGINE ANTI-ICE VALVE TEST ASDR CA121204007Anti-Ice System · failed(CAN) 1 & 2 ENGINE ANTI-ICE FAIL EICAS MESSAGE AFTER T/O 1500` AGL. ENGINE TAI SYSTEM TESTED IAW AMM 30-21-00-710-801A NIL FAULTS. ACFT RELEASED FOR SERVICE IAW TECH SUPPORT AND MOC CONCURANCE.SDR UALA2012092705457Louver · brokenLEFT ENGINE TAI EXHAUST LOUVER IS BROKEN AND LOOSE. REMOVED DAMAGED LOUVER. OK TO CONTINUE IN SERVICE UNTIL GRILL REPLACEMENT.SDR CALA2012051600354Anti-Ice Valve · malfunctionedLEFT ENG ANTI-ICE EICAS MESSAGE AND LT ENG DISAGREEMENT LIGHT ILLUMINATED IN FLIGHT. AIR RETURN WAS DONE. R & R LT ENGINE TAI VALVE IAW AMM30-21-03-404- 016, OPS AND LEAK CHECKS OK. ROTABLE PARTS CHANGE WAS INDICATED - TT 1537808, SN OFF 01011, VALVE, ANTI-ISDR CA120417010Heater · cracked(CAN) DURING INSPECTION IT WAS NOTICED THAT THE BACK OF THE HEATED LIP WAS CRACKED ARCOSS FROM TOP TO BOTTOM . THE OTHER SIDE WAS INSPECTED AND ALSO FOUND CRACKED 2 TIMES IN THE SAME LOCATION.SDR CA120222007Actuator · inoperative(CAN) LT MAIN ENGINE ANTI-ICE CIRCUIT BREAKER POPPED. AFTER RESET ON THE GROUND, IT POPPED WITHIN 2 SECONDS AGAIN". STANDBY MODE SERVICEABLE. ACTUATOR FUNCTION CHECKED AND FOUND INOPERABLE IN "MAIN ANTI ICE OFF" SELECTION, ALL OTHER 3 SELECTIONS SERVICEABLESDR CA120116001Deice System · malfunctioned(CAN) ACARS MESSAGE THAT THEY HAD SMOKE/FUMES IN THE FLIGHT DECK, FOLLOWED BY ENGINE ADPT HEAT 1 CAUTION LIGHT ILLUMINATED. CAPTAIN ADVISED SOCC OF SITUATION, AN EMERGENCY WAS DECLARED AND ACFT WAS TURNED BACK. ADVISED DUTY OFFICER AND MOC OF EVENTS. MOC ASDR CA120112007Duct · cracked(CAN) ON DECENT CREW OBSERVED NR 2 ENGINE FIRE WARNING INDICATION. COMPLETED FIRE DRILL, FIRE LIGHT STAYED ON, FIRE BOTTLE DISCHARGED. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE IGV ANTI-ICE DUCT CRACKED AT WELDED FLANGE. DUCT AND FISDR UALA2012010600145Anti-Ice Valve · faultyLEFT ENGINE ANTI ICE VALVE DOES NOT OPEN WHEN SELECTED, ON GROUND. REPLACED ENGINE ANTI-ICE VALVE PER MM. ACCOMPLISHED ENGINE RUN PER JRH AND ACCOMPLISHED MAT TEST OF ENGINE ANTI-ICE VALVE. TEST PASSED AND STATUS MESSAGE CLEARED, INDICATION ON EICAS NORMALSDR CHQA201100188Anti-Ice Valve · inoperativeCREW REPORTED THAT DURING FLIGHT RECEIVED AN ENGINE 2 ANTI-ICE VALVE FAIL MESSAGE AND A WING ANTI-ICE FAIL MESSAGE ON THE EICAS. THE CREW DIVERTED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH THE ENGINE 2 ANTI-ICE VALVE AND THE RIGHT WING ASDR AALA20110428PHX02Duct · crackedPHX - CREW REPORTED DURING CLIMBOUT LOOP-A LEFT ENGINE LIGHT ILLUMINATED, FOLLOWED BY NUMBER 1 ENGINE FIRE HANDLE LIGHT AND BELL. REDUCED NUMBER 1 ENGINE TO IDLE PER QRH PROCEDURE AND LIGHT WENT OUT AFTER APPROXIMATELY 3 SECONDS. EMERGENCY DECLARED FLIGHT RESDR 2011FA0000291Valve · damagedBOTH GROMMETS DAMAGED CARB HEAT VALVE SHAFT. TEFLON BUSHING WORE AND DAMAGED PIVOT SHAFT IN APPROX 2000 HRS OF OPERATION. ACFT WAS MFG IN 2008.SDR E81RJT229431Element · shortedINVESTIGATED REPORTED ENGINE ANTI-ICE SYS FAIL INDICATION. FOUND (1) HEATING ELEMENT OPEN IN RT INBD WING L/E ANTI-ICE PANEL. ALSO NOTED FAULT IN RT WING L/E ANTI-ICE JUNCTION BOX CURRENT SENSOR CS10. FURTHER TROUBLESHOOTING REVEALED THE WIRING TERMINALS, ATTSDR FDEA201012264753Pressure Switch · inoperativeON DESCENT TURNED ON ENG - WING ANTI-ICE RECEIVED "A WING A-ICE L DISAG ALERT SHORTLY AFTER RECEIVED AN AIR MANF 1 FAIL" COMPLIED WITH QRH AND DIVERTED, WITHOUT INCIDENT. R & R LT MANIFOLD FAILURE DETECTION PRESSURE SWITCH IAW MM 36-23-03-4. ALSO REPLACED NRSDR VNAA2010121000008Anti-Ice Valve · failedCREW REPORTED A LT COWL ANTI-ICE CAUTION MESSAGE. ACFT RETURNED AND LANDED WITHOUT INCIDENT. MX USING THE ACFT MM REMOVED, REPLACED, AND TESTED THE LT ANTI-ICE VALVE. ACFT WAS RELEASED FOR SERVICE.SDR UALA2010112204310Anti-Ice Valve · faultyRIGHT ENG ANTI-ICE INTERMITTENT. VALVE FOUND FAULTY. ENG ANTI-ICE VALVE REPLACED. VALVE OPERATIONAL CHECK NORMAL.SDR MYWA100117Anti-Ice Valve · inoperativeETOPS SIGNIFICANT SYSTEM: NR 1 ENGINE ANTI-ICE LIGHT ILLUMINATES AT HIGH THRUST SETTINGS.SDR IPXA10M63576Sensor · inoperativeON DESCENT THROUGH 14000, ENCOUNTERED MODERATE ICING. SELECTED A/I ON AND REC'D A LEVEL 1 ENG 2 A-ICE OFF ALERT. DIVERTED. REPLACED DUCT BURST SENSOR. REPLACED NR 2 ENG COWL A-ICE MAN FAIL SENSORS IAW 30-22-11-4. FOLLOWED FIM 30-22-07. RAN ENG AND TEST INSP FSDR CA101104005Boot · damaged(CAN) DURING THE WALK AROUND PRIOR TO FLIGHT, THE PILOT NOTICED EVIDENCE OF A BIRD STRIKE ON THE RT ENGINE INTAKE. MX INVESTIGATION REVEALED NO STRUCTURAL DAMAGE, HOWEVER, THE INTAKE DEICE BOOT HAD SEVERAL PIN HOLES IN THE AREA OF THE BIRD STRIKE. IT IS SUSPSDR 2010F00157Flex Duct · brokenBOTH ENGINE INLET ANTI/DE-ICE MANIFOLDS WERE BROKEN ON BOTH ENGINES.SDR CA100703002Anti-Ice System · malfunctionedDUAL ENGINE POWER ROLLBACK DURING FLIGHT AT FL330, THE PILOT NOTICED THAT THE AIRSPEED WAS DROPPING OFF QUICKLY AND THAT THE N1 HAD ROLLED FROM 91 PERCENT TO 85 PERCENT ON BOTH ENGINES. AS THE ACFT DESCENDED, ANTI-ICE WAS TURNED OFF AND THE POWER RETURNED TOSDR AALA20100605DFW01Duct · blownDFW - CREW REPORTED NUMBER 2 ENGINE FIRE LOOP HAD A FIRE INDICATION FOLLOWED BY WARNING BELL. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ANTI ICE DUCT THAT WAS BLOWN. SYSTEM GROUND CHECKED NORMAL OPERATSDR QXEA2010041900279Heater · odorSTRONG ODOR NOTED IN CABIN. FERRIED. FOUND NR1 ENGINE INTAKE HEATER HAS VERY "FOUL" ODOR NEAR THE CONNECTION. REPLACED HEATER AND PERFORMED "BURN OFF" RUNS IAW SL DH8-400-5L-21-012A. NO ABNORMAL ODOR. RETURNED TO SERVICE.SDR FDEA201003190936Anti-Ice Valve · malfunctionedNR 2 ENG ECAM ENG 2 N, AC VALVE NOT OPEN ENG NR 2 ANTI ICE INOP MEL 19MAR10 23:05 MEM U RELEASED FOR SERVICE IAW MEL: 30-21-01-B CATEGORY: C EXPIRATION: 29MAR10 "MEL 30-21-01-B: ENGINE (IDENTIFY 1 AND/OR 2) NR 2 ANTI-ICE VALVE- INOP. ENGINE NACELLE VALVSDR UALA2010030800805Anti-Ice Valve · faultyLEFT ENG ANTI ICE VALVE TAKES ABNORMALLY LONG TIME TO CLOSE. REPLACED VALVE. LEAK CHECKED OKAY. NORMAL GROUND CHECK OF BOTH ENGINE ANTI VALVES.SDR IXXA100018OAnti-Ice Valve · defectiveDURING CLIMB OUT WITH ANTI-ICE ON NR 4 ENG COMPRESSOR STALLED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED NR 4 INBD ANTI-ICE CONTROL VALVE REGULATOR. OPS CHECK GOOD IAW MM 75-10-1. ACFT WAS RETURNED TO SERVICE.SDR UALA2010021900633Anti-Ice Valve · faultyRT BLEED WOULD OPEN AFTER ENG START. RT ENGINE COWL ANTI-ICE VALVE LOCKED CLOSED INSTEAD OF RT PRSOV FOR BLEED PROBLEM. RT ENG NAI VALVE REACTD, BACK TO NML POSITION. REPLACED R-PRVC WITH BORRWED PART, NO HELP, BLD WOULD NOT OPEN. REPLACED RT ENGINE PRSOV
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