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 USAASB98251Duct · leakingBWI - FLT 2679 - ON CLIMB-OUT PASSING 13,000 FEET, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED CHECK LIST AND WHEN THRUST LEVER WAS PULLED BACK ON NR 1 ENGINE, LIGHT EXTINGUISHED. CREW DECIDED TO RETURN TO FIELD AT BWI. FLIGHT LANDED WITHOSDR SWAA982164Duct · failedAIR TURNBACK DUE TO NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF FROM BWI (NOTE ANY EPR SETTING ABOVE 1.75 CAUSED THE LIGHT TO RE-ILLUMINATE). AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED 13TH STAGE FUEL HEAT DUCTING PER BOEING MM. RAN SDR 98ZZZX3688Line · rupturedAS ICE DOORS WERE DEPLOYED, A LARGER THAN NORMAL TORQUE LOSS WAS NOTED. UPON LANDING, FOUND LEFT ENGINE BLEED AIR LINE FAILED. THIS LINE WAS MANUFACTURED IN MARCH '66. INNER NYLON OF LINE WAS HARD AND BRITTLE AND IS SUBJECT TO HOT BLEED AIR.SDR CALA9801698Duct · rupturedTHE RT FIRE DETECTOR LOOP LIGHT ILLUMINATED, FOLLOWED BY THE RT FIRE WARNING LIGHT AND BELL WHILE EN ROUTE FROM IAH TO CLE. THE RIGHT ENGINE POWER WAS REDUCED AND THE FIRE WARNINGS CEASED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MSDR 98UAL900447Duct · failedWHEN ENGINE ANTI-ICE WAS SELECTED ON THE NR 2 COWL ANTI-ICE DUCT TEMPERATURE CLIMBED TO 230 DEGREES. BEFORE IT WAS SELECTED AN ACRID SMELL WAS EVIDENT IN THE COCKPIT AND CABIN.SDR 98ZZZM780Anti-Ice Valve · leakingFLT 643 - PHX-LAX - ENGINE FIRE INDICATION ON CLIMB-OUT NR 2 ENGINE. SHUT DOWN NR 2 ENGINE, RETURNED TO PHX. REPAIRED LEAKS AT 8TH STAGE BLEED DUCT AT SECOND CONNECTION AFT OF FIRE WALL AND ENGINE ANTI-ICE VALVE AT 12 O'CLOCK POSITION. (M)SDR CALA9801417Anti-Ice Duct · blownTHE FIRE WARNING BELL SOUNDED FOLLOWED BY ILLUMINATION OF THE NR 3 ENGINE FIRE WARNING LIGHT ON CLIMB-OUT OF IAH AT ABOUT 900 FEET. THE NR 3 ENGINE POWER WAS REDUCED AND THE FIRE WARNINGS CEASED. A VALID FIRE TEST WAS RUN. THE LIGHT AND BELL CAME ON AGAIN WSDR AU981083Receiver · loose(AUS) RIGHT DE-ICE SYSTEM PRESSURE REGULATOR EXHAUST AIR RECEIVER LOOSE ALLOWING HOT AIR TO BLOW ONTO THE LEAK DETECTOR.SDR AU980980Receiver · loose(AUS) RIGHT DEICE SYSTEM PRESSURE REGULATOR EXHAUST AIR RECEIVER LOOSE ALLOWING HOT AIR LEAKAGE.SDR MZZA98184Valve · failedMNL - FLT CS879 - L/P 7910614 - DURING TAKEOFF ROLL IMMEDIATELY AFTER AN ESPECIALLY HARD JOLT, THE NR 3 FUEL HEAT VALVE LIGHT CAME ON AND OIL TEMPERATURE STARTED RISING. VALVE WAS SELECTED CLOSED AND CYCLING SWITCH WOULD NOT GO FULLY CLOSED. SUBMITTER SUSPECSDR SWIA971225Water Separator · malfunctionedON CLIMB-OUT, LEFT DUCT LEAK LIGHT CAME ON. FOLLOWED QRH AND SHUT THE LEFT ENGINE DOWN. REPLACED LEFT DE-ICE WATER SEPARATOR.SDR 98ZZZX2483Actuator · failedDURING AN ANNUAL INSPECTION OF THE ENGINE ANTI-ICE VALVE SYSTEM, FOUND THE ACTUATOR ERRATIC (THIS AIRCRAFT HAS BEEN MODIFIED, BY FIELD APPROVAL, FOR INSTALLATION OF THE BELL HELICOPTER 206B ENGINE ANTI-ICE ACTUATOR SYSTEM). REPLACED ACTUATOR.SDR 99ZZZX751Bleed Valve · malfunctionedENGINE NOT MAKING POWER. REMOVED AND REPLACED. AWAITING INSPECTION REPORT. REF: CONTROL NR 98-4-15.SDR DLM88980860Anti-Ice Duct · blownON TAKEOFF AT 8000FL, RT ENG FLAME OUT FOLLOWED POM. PLACED FUEL CONTROL TO OFF AND LANDED. REPLACED LEFT FRAME ANTI-ICE DUCT RAN ENGINE CKS OK.SDR 98FDEA00302Anti-Ice Duct · brokenNR 2 ENGINE LEFT HAND ENGINE INLET ANTI-ICE DUCT BROKEN IN HALF. LOCATED JUST AFT OF ANTI-ICE VALVE. REMOVED AND REPLACED ANTI-ICE DUCT IAW FED-EX M/M 75-10-00.SDR 98FDEA00278Anti-Ice Duct · damagedNR 2 ENG LEFT HAND ENGINE INLET A/I DUCT DAMAGED, LOCATED JUST FWD OF THE A/I VALVE. *S/D* REMOVED AND REPLACED ANTI-ICE DUCT PER FED-EX M/M 75-10-14.SDR 9806543231Anti-Ice Valve · malfunctionedEN ROUTE, POSSIBLE ICING CONDITIONS WERE REPORTED. THE NR 1 ENGINE ANTI-ICE VALVE WOULD NOT OPEN. FLIGHT CREW DIVERTED TO COS. MAINTENANCE REPLACED THE ANTI-ICE VALVE.SDR COMA9810100Valve · leakingLEFT HAND BLEED AIR DUCT LEAK WARNING DURING FLIGHT. REPLACED LEAKING DE-ICE PRESSURE REGULATOR VALVE.SDR DL73E980720Anti-Ice · odorAT 25,000, AN ELECTRICAL SMELL WAS NOTED IN ENTIRE AIRCRAFT WHEN ENGINE ANTI-ICE WAS TURNED ON. SMELL WENT AWAY WHEN ENGINE ANTI-ICE TURNED OFF. RAN ENGINES AND PACKS, INSPECTED FOR SOURCE, NO TROUBLE FOUND.SDR 98ZZZM927Poppet Valve · failedNR 4 ENGINE READS 7 PERCENT BELOW N1 REF AT 904 DEGREES TGT, ABORTED TAKEOFF AT LESS THAN 60 KTS, RETURNED TO GATE AT DEN. REPLACED FCU POPPET VALVE ASY. ENGINE STILL LOW ON POWER. (M)SDR AALA980556Anti-Ice Valve · failedYQX - FLT 141 - NR 1 ENGINE ANTI-ICE NACELLE VALVE FAILED TO OPEN. ICING CONDITIONS ANTICIPATED AT JFK. DIVERTED TO GANDER. NR 1 ENGINE NACELLE ANTI-ICE VALVE LOCKED OPEN AND DEFERRED PER MEL 30-1B AUTH NO 3-55DC-C. REMOVED AND REPLACED NR 1 ANTI-ICE VALVESDR MALA976026Anti-Ice Valve · internal faultDURING DESCENT, THE RIGHT AIR VALVE LIGHT ILLUMINATED, UNABLE TO RESET. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT ANTI-ICE START BLEED VALVE, OPS CHECK GOOD.SDR MALA976022Bleed Valve · failedDURING FLIGHT, THE LEFT ENGINE AIR VALVE CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE ANTI-ICE START BLEED VALVE, OPS CHECK GOOD.SDR REXA98058Valve · failedRIGHT ENGINE VIBRATES AND SOUNDS SIMILAR TO COMPRESSOR STALL. ALL OTHER INDICATIONS NORMAL. AFTER INSPECTION OF RIGHT ENGINE AND GROUND RUNS IN SEVERAL DIFFERENT POWER SETTINGS, NO DEFECTS NOTED. SWAPPED ANTI-ICING BLEED VALVE FOR TROUBLESHOOTING GROUND RUNSDR MALA976004Aisb Valve · failedDURING CRUISE FLIGHT, THE RIGHT AIR VALVE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT ANTI-ICE START BLEED VALVE, ALL CHECKS GOOD.SDR TWAA9801101Duct · damagedSLC - FLT 844 - DURING CLIMB, NR 3 ENGINE FIRE WARNING OCCURED. ENGINE SPEED REDUCED TO IDLE. RETURNED TO SLC. REPLACED NR 3 ENGINE ANTI-ICE DUCT, MFG PART NUMBER 65-26738-31 DUE TO HOLE IN DUCT. (M)SDR USAAF98008Shutoff Valve · inoperativeGSO - FLT 875 - FLT EN ROUTE RIC TO CLT, WHEN NR 2 ENGINE ANTI-ICE FAILURE OCCURRED. CREW RESET CIRCUIT BREAKER AND IT POPPED. DUE TO WEATHER CONDITIONS IN CLT, FLIGHT DIVERTED TO GSO. FLT LANDED GSO WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RIGHT ENGSDR SWAA980053Duct · rupturedNR 1 ENGINE FIRE WARNING INDICATION IN FLIGHT. ACTIVATED FIRE BOTTLES AND PERFORMED ENGINE SHUTDOWN CHECKLIST. MADE AN UNEVENTFUL LANDING AT STL. INSPECTED AND FOUND ANTI-ICE VALVE LINE RUPTURED. REPLACE LINE, ENGINE OIL STRAINER, HYD PUMP CASE DRAIN FILTESDR 98FDEA00009Anti-Ice Valve · leakingENGINE 1 STRUT OVERHEAT LIGHT CAME ON DURING CLIMBOUT. FOLLOWED THE RED TAB PROCEDURES AND LIGHT EXTINGUISHED. REMOVED AND REPLACED NR 1 ENGINE ANTI-ICE VALVE GASKET ON TOP SIDE OF VALVE. LEAK CHECK GOOD. REMOVED AND REPLACED NR 1 ENGINE STRUT OVERHEAT SENSDR PLGA971107ABleed Valve · failedBOS - FLT 4383 - ON CLIMB-OUT, THE RIGHT ENGINE ANTI-ICE BLEED VALVE FAIL LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BOS DUE TO WEATHER CONDITIONS. MAINTENANCE REPLACD THE RIGHT ANTI-ICE BLEED VALVE SYSTEM CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR 9720779998Anti-Ice Valve · inoperativeDURING CLIMB AS RIGHT ENGINE ANTI-ICE WAS SELECTED, THE ANTI-ICE LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE ANTI-ICE VALVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR SWAA970989Valve · failedDIVERTED TO OAK DUE TO NUMBER 2 ENGINE ANTI-ICE VALVE NOT OPENING. LANDED WITHOUT INCIDENT. REPLACED ANTI-ICE VALVE PER BOEING M/M.SDR USAASB98287Duct · failedMSY - FLT 2180 - AFTER TAKEOFF FROM MSY AT APPROX 2,500 FT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CHECKLIST WAS ACCOMPLISHED AND AS POWER WAS REDUCED ON THE NR 1 ENGINE, THE LIGHT EXTINGUISHED. CAPTAIN DECIDED TO RETURN TO FIELD AT MSY WHERE THE FLIGHTSDR AALA972023Sensing Line · crackedFLT 751 - AFTER TAKEOFF FLL DURING CLIMB-OUT, AFT COMPT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED WHEN POWER LEVERS RETARDED. AIRCRAFT RETURNED TO FLL AND LANDED OVERWEIGHT WITHOUT INCIDENT. PLACARDED RIGHT AUGMENTASDR C2XA97CL083Actuator · failedCLE - FLT 3058 - CREW REPORTED THAT THE LEFT ENGINE ANTI-ICE WOULD NOT WORK IN THE NORMAL OR STANDBY ACTUATOR MODE. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT ENGINE ANTI-ICE ACTSDR EISA97209Valve · leakingON TAKEOFF FROM BRU, THE NR 2 FIRE WARNING SOUNDED SHORTLY AFTER TAKEOFF, RETURNED TO BRU (ATB). FOUND UPPER LEFT ANTI-ICE VALVE LEAKING, RESECURED VALVE, AND RAN ENGINE. NO LEAKS NOTED. (X)SDR CA971010005Flange · cracked(CAN) BOTH ENGINE INLETS CRACKED IN THE RADIUS OF THE COWL ATTACH FLANGE ABOUT 5 INCHES LONG. REPAIRED. PART TC: 2,837.SDR CA971010011Fireshield · loose(CAN) SIX SPOTWELD RETAINING ANTI-ICING SOLENOID VALVE ASSEMBLY BRACKETS TO FIRESHIELD ASSY ARE UNDONE CAUSING BRACKET TO SEPARATE FROM FIRESHIELD. SUSPECT INCORRECT WELDING PROCESS. REPLACED.SDR 97FDEA00685Clamp · looseENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN CRUISE. CLOSED ENGINE NR 1, ANTI-ICE VALVE LIGHT WENT OUT. COMPLIED ENGINE STRUT OVERHEAT PROCEDURES IN CHECKLIST. TIGHTENED HIGH STAGE MODULATING VALVE CLAMP, OPERATIONAL CHECK. ON RUN GOOD, COWLING SECURED.SDR USAAD97159Anti-Ice Duct · failedPBI - FL 1681 - AFTER TAKEOFF, CREW RECEIVED THE LEFT ENGINE FIRE WARNING INDICATION. CREW WENT THROUGH EMERGENCY PROCEDURES AND WARNING EXTINGUISHED (ENGINE WAS NOT SHUT DOWN). FLIGHT RETURNED TO PBI AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND TSDR F3LA97146Fuel Heat Vlv · out of positionOMA - FLIGHT CREW REPORTED NR 2 ENGINE WAS SHUT DOWN DUE TO HIGH OIL TEMPERATURE. AIRCRAFT LANDED IN DEN WITHOUT INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE, REPOSITIONED FUEL HEAT VALVE AND CHECKED OK. (M)SDR 97FDEA00658Anti-Ice Duct · blownLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF AT TAKEOFF THRUST SETTING. RAN THROUGH RED TABS AND ISOLATED NR 2 ENGINE BLEED CAUSES LIGHT TO ILLUMINATE ABOVE 88 PERCENT AT 15,000 MSL. LIGHT REMAINED OUT AS LONG AS NR 2 WAS KEPT AT REDUCED THRUST. SDR DHL9780756CAnti-Ice Deflect · brokenENG NR 3, IN THE RT SIDE OF NOSE COWL L/E AT 3 O'CLOCK, ANTI-ICE DEFLECTOR BROKEN. ACCOMPLISHED ENG NR 3 NOSE COWL ANTI-ICE DEFLECTOR L/E AT 3 O'CLOCK REPAIR BY TRIMMING CRACKED SECTION IAW SB 71-105, PAGE 19. TREATED AREA OF TRIMMED DEFLECTOR PER SRM 51-1-8SDR TWAA9799004Valve · failedMCI - FLT 477 - DURING CLIMB, THE NR 2 ENGINE, FUEL HEAT VALVE STUCK IN THE OPEN POSITION CAUSING HIGH ENGINE OIL TEMPERATURE. SHUT DOWN ENGINE. REMOVED AND REPLACED THE FUEL HEAT VALVE, MFG P/N 3201115, MANUFACTURED BY WHITTAKER CONTROLS. OPERATIONAL CHECSDR CALA9701244Gaskets · wornTHE FIRE LOOP DETECTOR LIGHT BEGAN TO FLICKER WHILE EN ROUTE. ABNORMAL PROCEDURES WERE FOLLOWED AND TEST INDICATED NR 1 ENGINE FIRE. THE NR 1 ENGINE POWER WAS REDUCED TO IDLE AND THE FIRE LIGHT EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCSDR CA970806001Packing · failed(CAN) BLEED AIR ANNUNCIATOR LIGHT ILLUMINATED ON THE RIGHT HAND SIDE. CREW RETURNED TO HANGAR. INSPECTION FOUND THE PACKINGS ON THE BLEED AIR SYSTEM WERE BURNT AND HARD. SUBMITTER SUSPECTS THE USE OF THE WRONG PACKINGS.SDR 97FDEA00437Clamp · loose97-0132 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AT FLIGHT LEVEL 250, AFTER TURNING OFF NR 2 BLEED VALVE, LIGHT EXTINGUISHED WITHIN 2 MINUTES. NR 1 AND NR 3 BLEED VALVE WERE OPEN WITH BOTH PACKS ON. CHECKED LOWER AFT BODY LOOPS IN AFT STAIRS, NR 2 ENGINE ARSDR 97ZZZX4027Bleed Line · crackedDURING TAKEOFF, LEFT ENGINE ONLY MADE 72 PERCENT TORQUE. TAKEOFF ABORTED. RUN-UP WITH APR/SLR OFF, STILL ON 72 PERCENT TORQUE. FOUND ANTI-ICE BLEED LINE CRACKED. REMOVED AND REPLACED LINE. OPS CHECK OK.SDR 97FDEA00416Anti-Ice Duct · failedAPPROXIMATELY 1 MINUTE AFTER SETTING TAKEOFF POWER NR 1 FIRE WARNING SOUNDED. WARNING EXTINGUISHED WHEN THROTTLE WAS RETARDED. SUSPECT BLEED AIR LEAK. SEE PREVIOUS WRITE UP. INSPECTED ENGINE FOR BLEED AIR LEAK AND DISCREPANCIES ASSOCIATED. FOUND NR 1 ENGISDR HEEA0010343Servomotor · failedSERVO WILL NOT ACTUATE OPEN OR CLOSE.
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