JASC 7260
Service difficulty reports · 1,098
Reports filed under 7260 · Turbine Engine Accessory Drive, 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 = '7260' 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 = '7260' 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 AU980886Driveshaft · failed(AUS) RIGHT ENGINE GEARBOX DRIVESHAFT FAILED AT THE FORWARD UNIVERSAL JOINT DAMAGING THE ENGINE `W' STRUT AND NR 1 AND NR 2 COMBUSTION CHAMBERS.SDR AU980994Seal · deteriorated(AUS) ENGINE ACCESSORY GEARBOX STARTER/GENERATOR SEAL LEAKING. PART TC: 54.SDR DLL10981430Chip Detector · not installedNR 1 ENG OIL LOSS IN EXCESS OF 4 QTS HR. DIVERTED SLC. ENG WAS NOT SHUTDOWN AND NO LOSS OF OIL PRESS. FOUND NR 1 ENG FINE SCAVAGE CHIP DET NOT IN HOUSING AND LAYING ON TOP OF OIL TANK. DET VISUALLY CKD OK BUT ONE O-RING FELL OFF WHEN HANDLED. REPLACED BOTSDR AALA981372Adapter · failedSJU - FLT 574 - DURING CRUISE NR 1 ENGINE WAS SHUT DOWN BY CREW DUE TO ENGINE FIRE. RETURNED AND LANDED SJU. REPLACED NR 1 ENGINE. SHOP FOUND THE AGB IDLER ADAPTER THREADED INSERTS WERE PULLED OUT CAUSING FUEL TO LEAK, FIRE AND ENGINE SHUTDOWN. GENERAL ELESDR 9809796637Seal · failedWHILE IN CRUISE FLIGHT, THE NR 1 ENGINE OIL QUANTITY AND PRESSURE DROPPED. THE ENGINE WAS SHUT DOWN AND THE FLIGHT CONTINUED TO NRT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE ACCESSORY GEARBOX CARBON SEALS FOR THE HYDRAULIC PUMP AND STARTER. SUBSEQUSDR HEEA0015043Gear · pittedRECEIVING INSPECTION REVEALED: PITS BEYOND SERVICEABLE LIMITS ON A/O SEP. GEAR TEETH. INSTALLED A NEW A/O SEP. GEAR.SDR MALA976152Chip Light · illuminatedLEFT ENGINE CHIP DETECTION LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT RETURNED TO DTW. MAINTENANCE REMOVED CHIP DETECTOR AND FOUND CHIP TO BE ALLOWABLE PLATING MATERIAL. RAN AIRCRAFT, ALL CHECKS GOOD.SDR VJ9800198Gearbox · leakingENGINE WAS SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL PRESSURE AND OIL QTY WENT TO ZERO. OIL PRESSURE LIGHT ILLUMINATED. FOUND THAT THE NR 2 ENGINE HAD A BANJO FITTING BROKEN FROM THE GEARBOX LOSING OIL. REMOVED THE GEARBOX. THE HELICOIL WAS PULLED OUT OF THE GSDR CA980623019Shaft · worn(CAN) ENGINE WAS CONSUMING OIL WHICH WAS EXITING FROM THE BREATHER. ACCESSORY GEARBOX WAS REMOVED AND SPLIT TO REPLACE THE CARBON SEAL. FURTHER INSPECTION OF THE GEARSHAFT ASSEMBLY SHOWED WEAR ON THE SPLINE SHAFT AND CRACKS ON THE CARBON SEAL FACE. THE STARSDR CA980623018Impeller · worn(CAN) ENGINE WAS CONSUMING OIL, IT APPEARED TO BE COMING FROM THE BREATHER. THE ACCESSORY GEARBOX WAS SPLIT TO REPLACE THE CARBON SEAL. EROSION PITTING WAS FOUND ON THE LEADING EDGE OF THE IMPELLER VANES. THE IMPELLER AND GEARSHAFT ASSEMBLY WERE CHANGED AS SDR VTZA98214Detector · malfunctionedBOS/IAD - FLT 6218 - DURING TAKEOFF AT 1800 HRS ON 6-7-98, ABORTED TAKEOFF DUE TO RT ENGINE OIL CONTAMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE AT BOS WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND NO METAL ON CHIP DETECTOR THENSDR VNAA9806001Seal · failedDURING CRUISE, THE RIGHT HAND ENGINE OIL PRESSURE DROPPED INTO THE WARNING (AMBER) RANGE. THE CREW EXECUTED LOW OIL PRESSURE PROCEDURES, CALLED OUT FOR IN THE CHECKLIST. THE RIGHT HAND PROPELLER WAS FEATHERED, AND THE POWER WAS SET TO FLIGHT IDLE. THE CREWSDR HEEA0014443Bearing · mismanufacturedRECEIVING INSPECTION REVEALED: RUST BEYOND SERVICEABLE LIMITS ON 3 AND 4 CAGE. INSTALLED A NEW 3 AND 4 CAGE.SDR MALA976140Chip Light · illuminatedIN FLIGHT THE LEFT ENGINE OIL CHIP DETECT LIGHT ILLUMINATED. ALL ENGINE PARAMETERS NORMAL. AIRCRAFT RETURNED TO MSP. MAINTENANCE INSPECTED LEFT ENGINE CHIP DETECTOR IAW GE MM 72-00-00 AND FOUND ACCEPTABLE MATERIAL DETERMINED TO BE OPERATING DEBRIS. AIRCRAFTSDR P5CA9800797Seal · leakingNR 4 ENGINE LOST OIL QTY AND PRESSURE. OIL PRESSURE LIGHT CAME ON AND TEMP BEGAN TO RISE. ENGINE SHUT DOWN. FOUND OIL LEAK TO BE FROM CSD PAD. REPLACED CSD SEAL PER BOEING M/M 24-11-01, LEAK CHECK OK.SDR 98UAL900209Gear · failedNR 2 ENGINE FLAMED OUT AND WAS SHUT DOWN. FLIGHT CONTINUED TO SFO UNDER AMBER ALERT. ENGINE WAS CHANGED FROM AIRCRAFT. UPON TEAR DOWN OF THE INLET GEARBOX, A MAIN BEVEL GEAR WAS FOUND FAILED.SDR REXA98096Seal · failedLEFT ENGINE LOST OIL PRESSURE. REMOVED AND REPLACED LEFT BB AXIS SEAL AND RUNNER. REF: OPERATOR CONTROL NR 98ZZZX2425. (X)SDR 98ZZZX2425Runner · failedLEFT ENGINE LOST OIL PRESSURE. REMOVED AND REPLACED LEFT BB AXIS SEAL AND RUNNER. REF: OPERATOR CONTROL NR REXA98096.SDR 98FDEA00373Washer · out of position98-0133, NR 1 OIL QTY WAS 16 QTS ON GRND AT LEVEL OFF FL 310 12 QTY. STARTED TIMING THE DROP AT 7 QTS, LOST 1 QT PER 7 MIN. PRECAUTIONARY LANDING IN DEN. WHEN WE LANDED ANALOG AND ECAM SHOWED 4 QTS. REMOVED WASHER LODGED BETWEEN SEAL AND AFT CASE OF TOWER SDR VTZA98192Diaphragm · separatedFLT 6377 - IAD-CRW - DURING APPROACH, MADE A SCHEDULED LANDING AT CRW WITH ONE DISCREPANCY WHICH WAS RT ENGINE FLAMED OUT. CREW SHUT DOWN ENGINE. AIRCRAFT WENT TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND IDLER SPUR GEAR DIAPHRAGM SSDR HEEA0014215Pump Assy · defectiveRECEIVING INSPECTION REVEALED: DEEP CASTING FLAWS BEYOND SERVICEABLE LIMITS ON PUMP ASSY. SCAVENGE PORT. INSTALLED A SERVICEABLE PUMP ASSY.SDR CA980529006Shaft · damaged(CAN) GENERATOR WOULD NOT COME ON LINE. INSPECTION FOUND THE GENERATOR DRIVE (FEMALE) IN THE ACCESSORY GEARBOX NOT TURNING. GEARBOX REMOVED FOR REPAIR.SDR EISA98105Fitting Boss · strippedIN-FLIGHT, NR 1 LOW OIL PRESSURE LIGHT ILLUMINATED, NR 1 OIL PRESSURE GAUGE READ JUST ABOVE LOWER RED RADIAL. OIL QUANTITY READ ZERO. PRECAUTIONARY SHUT DOWN OF NR 1 ENGINE. RETURNED TO BRUSSELS (BRU). GENERATED FROM PILOT REPORT. FOUND LEAKING FITTING ATSDR SCNA98043Gearbox · crackedDURING CRUISE FLIGHT, NUMBER TWO ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE DROPPED TO 25 PSI WITH THE QUANTITY DOWN TO .8 GALLONS. SHUT DOWN NUMBER TWO ENGINE AND DIVERTED TO DEN. REMOVED AND REPLACED NUMBER TWO ENGINE MAIN ACCESSORY GEARBOXSDR SWAA980806Gear Box · failedNR 2 ENGINE FAILED CLIIMBING THROUGH 31,000, AIRCRAFT RETURN TO DAL MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND ACCY GEARBOX FAILURE WITH DAMAGE TO RT T/B COWLING AND R/T INBD LANDING LIGHT LENS COVER. REMOVED AND REPLACED NR 2 ENGINE AND R/T I/B LANDINGSDR CALA9800803Gearbox · crackedNUMBER 2 ENGINE GEARBOX DATA PLATE MOUNT BOLT HOLE (UPPER AFT) BROKEN OUT. REPAIRED GEARBOX DATD PLATE MOUNT BOLT HOLE PER EC/RA 7261-01251.SDR USAASB98107N2 Gearbox · failedBWI - FLT 2400 - CREW DECLARED AN EMERGENCY AND SHUT DOWN THE NR 1 ENGINE IN FLT DUE TO LOSS OF OIL QTY AND PRESSURE AND TEMPERATURE INDICATIONS. FLT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT TAXIED TO THE GATE NORMALLY. TOTAL SSDR TC8A98020Cover Plate · loosePRECAUTIONARY SHUTDOWN NR 3 ENGINE ON SHORT FINAL. OIL PRESSURE STARTED FLUCTUATING BETWEEN 45 PSI AND YELLOW ARC. SHUT IT DOWN WHEN ITWENT BELOW THE RED LINE. REMOVED, INSPECTED AND REPLACED OIL FILTER PER MM 79-20-7, NO METAL FOUND IN FILTER, LEAK CHECKS SDR 9807241227Packing · failedWHILD CLIMBING THROUGH FL200 (TPE), THE NR 2 ENGINE OIL QUANTITY INDICATION DROPPED TO ZERO WITH THE INDICATED OIL PRESSURE DOWN TO 10 PSI. THE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED ONE MINUTE LATER. THE CREW THEN FOLLOWED COM PROCEDURES AND SHUT DOWN TSDR LR7A9806Gearbox · failedNR 2 ENGINE SHUTDOWN AT 1545Z DUE TO LOW ENGINE AND REDUCTION GEARBOX OIL PRESSURE. FOUND TACH DRIVE GEARS AND OIL PUMP DRIVE GEARS WOULD NOT TURN WHEN PROP WAS TURNED.SDR HEEA0014011Tube Assy · wornENGINE REMOVED DUE TO METAL. INSPECTION OF GEARBOX PARTS REVEALED: TUBE ASSY. FAILED DIMENSIONAL CHECK PER CEB1307. INSTALLED A NEW TUBE.SDR HEEA0014010Tube Assy · wornENGINE REMOVED DUE TO METAL. INSPECTION OF GEARBOX PARTS REVEALED: TUBE ASSY. FAILED DIMENSIONAL CHECK PER CEB1307. INSTALLED A NEW TUBE.SDR VTZA98155Chip Detector · activatedIAD/ILM - FLT 6623 - DURING CLIMB AT 1900 HRS ON 4-14-98, AIRCRAFT MADE AN UNSCHEUDLED LANDING AT IAD DUE TO RT ENGINE OIL CONTAMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED SMALL FUSDR CA990310067Gearbox · leaking(CAN) DURING CLIMB THROUGH FL 170, NR 2 ENGINE GEARBOX LIGHT FLICKERED. OIL PRESSURE WAS STILL IN THE GREEN AND THE POWER SECTION OIL PRESSURE WAS NORMAL. OIL QUANTITY INDICATION DROPPED RAPIDLY AND THE OIL PRESSURE LIGHT STARTED TO FLICKER. THE ENGINE WAS SDR CA981125001Gearbox · leaking(CAN) DURING CLIMB THROUGH FL 170, NR 2 GEARBOX OIL PRESSURE LIGHT FLICKERING. OIL PRESSURE WAS STILL IN THE GREEN RANGE AND THE POWER SECTION OIL PRESSURE LIGHT WAS NORMAL. OIL QUANTITY INDICATION DROPPED RAPIDLY AND THE LOW OIL PRESSURE LIGHT STARTED TO FLSDR 99ZZZX559Gearshaft · crackedCHROME PLATE REMOVED FROM SEAL FACE (INDEX 27) AND BASE METAL FOUND TO BE CRACKED IN SEVERAL PLACES. FMPI FOUND THE PROBLEM. CAUSE UNKNOWN.SDR DLL10980740Gearbox · failedBEGINNING DESCENT, -A- SYSTEM PRESSURE 0, QUANTITY REMAINED. IDG LOW OIL PRESSURE LIGHT ON, GEN DISCONNECTED. DISCONNECTED IDG. ON APPROACH NR 1 OIL QTY DROPPED, QTY BELOW 10. NR 1 ENG SHUTDOWN. AT GATE NR 1 ENG OIL QTY 0. REPLACED NR 1 ENG MAIN GEARBOX SDR CALA9800643Starter Gear · failedTHE NR 1 ENGINE STOPPED WHILE EN ROUTE FROM SAL TO IAH. THE AIRCRAFT WAS DIVERTED TO MID WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. ACCESSORY GEARBOX DISASSEMBLY REVEALED STARTER GEAR FAILURE.SDR USAABB98026Gearbox · failedABQ - FLT 28 - EN ROUTE LAX-PIT, AT FL370 CREW NOTE LEFT ENGINE SPOOL DOWN, ACCOMPANIED BY EICAS MESSAGE 'L ENG LP PUMP'. FLIGHT DIVERTED TO ABQ AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE GEARBOX. (M)SDR HEEA0013667Gearbox Cover · leakingENGINE REMOVED DUE TO AFT T/M LEAK. INSPECTION REVEALED: LEAKING AT COVER AFT T/M BORE.SDR WRLA98077Seal · leakingDURING INITIAL CLIMB-OUT, FLIGHT CREW NOTE NR 2 ENGINE OIL QUANTITY DROPPING. FLIGHT CREW ELECTED TO RETURN TO POINT OF DEPARTURE FOR MAINTENANCE. AIRCRAFT RETURNED TO POINT OF DEPARTURE, LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND 'GARLOCSDR CA970625001Gearshaft · cracked(CAN) SEVERAL CRACKS ORIGINATING FROM THE INNER SHOULDER AREA WORN TO APPROXIMATELY HALF THE THICKNESS FROM CONTACT WITH TORQUEMETER PISTON THRUST BEARING. THESE CRACKS RUN RADIALLY, THEN INTO THE THIRTY TOOTH GEAR, THEN AXIALLY FULL LENGTH OF THE GEAR. THE SDR P5CA9800503Seal · leakingEXCESSIVE OIL CONSUMPTION ON NR 2 ENG. FOUND GEN GARLOCK SEAL LEAKING. REPLACED SAME, LEAK CHECK GOOD REF MM 72-61-08. RAN ENG AT PART POWER PER MM 71-00-00.SDR RRXA98064Seal · cutDURING CLIMBOUT LOST OIL QUANTITY ON NR 3 WITH OIL PRESSURE FLUCTUATING. PUT NR 3 THROTTLE TO IDLE, AFTER 2 MINUTES LOW OIL PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED INFLIGHT SHUTDOWN CHECKLIST. ON GROUND CHK FOUND STARTER CASE SEAL LEAKS. REMOVED STARTER ASDR CA980305002Nut · loose(CAN) DURING DISASSEMBLY OF THE ENGINE DUE TO ICE INGESTION, THE CARRIER ASSEMBLY WAS PULLED. CLOSER INSPECTION REVEALED THAT THE BEARING RETAINING NUT WAS SPINNING FREE (NO TORQUE) ON HE GEARSHAFT, HELD BY ONLY ONE TANG OF THE KEYWASHER. THE GEAR IN QUESTION SDR USAASB98048Cover · looseTPA - FLT 1080 - ON CLIMB-OUT FROM TPA GOING THROUGH 10,000 FEET, THE NR 2 ENGINE OIL QUANTITY DROPPED TO ZERO FOLLOWED BY THE OIL PRESSURE DROPPING TO ZERO. CAPTAIN SHUT DOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT TPA. FLIGHT LANDEDSDR CA980305005Garlock Seal · worn(CAN) AIRCRAFT ABORTED TAKEOFF DUE TO #2 ENGINE OIL PRESSURE FLUCTUATING 45-60 POUNDS. INSPECTION FOUND THE HYDRO MECHANICAL UNIT FUEL PUMP GARLOC SEAL LEAKING. THE GARLOC SEAL WAS REPLACED AND THE AIRCRAFTRETURNED TO SERVICE.SDR CA970421050Stud · loose(CAN) LOOSE STUD ON ENGINE ACCESSORY DRIVE GEARBOX. REPLACED.SDR CA980317090Coupling · loose(CAN) UPON INSTALLING THE COUPLING ASSEMBLY INTO THE GEAR CASE OF ENGINE P-54214, IT WAS NOTICED THAT THE NTS TRIP PRESSURE COULD NOT BE SET UP. FURTHER INVESTIGATION REVEALED THAT THE INTERNAL SPLINE THAT COUPLES THE QUILL SHAFT TO THE COUPLING ASSY WAS TURNISDR VTZA98053Chip Detector · dirtyFLT 6602 - IAD-BWI - AIRCRAFT RETURNED TO GATE DUE TO RT OIL CONTAMINATION WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND FOUND SMALL CHIP ON DETECTOR AND REMOVED AND REINSTALLED CHIP DETECTOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETU
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