Rolls-Royce DART-529-8X
Service difficulty reports · 30
Newest first. General aviation reporting is voluntary.
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 engine_model_key = 'DART5298X' 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 engine_model_key = 'DART5298X' 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 CA120727005Line · chafed(CAN) DURING CLIMB OUT, HYDRAULIC FLUID WAS LOST AND CREW RETURNED TO DEPARTURE AIRPORT SAFELY. MAINTENANCE INSPECTED AND FOUND LT MLG DOWNLOCK ACTUATOR RELEASE HYD PRESSURE LINE CHAFED THROUGH ALLOWING HYDRAULIC FLUID TO BE LOST. LINE WAS REPLACED, AREA CLESDR CA111003001Coupling · swollen(CAN) LT ENGINE WAS SHUTDOWN AFTER LT ENGINE OIL PRESSURE LOST IN FLIGHT DUE TO OIL STARVATION. ACFT LANDED SAFELY ON CLOSEST AIRPORT. GROUND INSPECTION REVEILED THAT OIL STARVATION WAS CAUSED BY ENGINE BREATHER LINE COUPLING SWOLLEN AND CAUSED BREATHER RESTSDR 2010F00077Engine · unknownIN FLIGHT ENGINE SHUTDOWN. AUTO FEATHERING OF PROPELLER. ERRATIC FUEL FLOW. OVERTEMP (POSSIBLE). TURBINE SECTION SEIZED (ON THE GROUND AFTER LANDING). ROOT CAUSE NOT CURRENTLY KNOWN. ACFT RETURNED TO DEPARTURE.SDR 2007ADP828001Selector Valve · bypassingAIRCRAFT WAS ENROUTE, FLYING THE APPROACH FOR RUNWAY 03. ONCE THE CREW PERFORMED THE APPROACH CHECKLIST, AND GEAR DOWN WAS SELECTED BEFORE LANDING CHECKLIST THEY GOT THE RT MAIN AND NOSE GEAR LIGHT ONLY. CREW TRY THE EMERGENCY PROCEDURES DESCRIBED ON CHECKLISTSDR 2004F00082Control Rod · looseAIRCRAFT RELEASED FROM MAINTENANCE. DEPARTED VPC. CLIMBING OUT FROM 9,000 FT, RIGHT THROTTLE WOULD NOT RESPOND. RETURNED TO VPC WITH UNEVENTFUL LANDING. MAINTENANCE FOUND THE THROTTLE PUSH PULL ROD CAME LOOSE AT THE FIREWALL (ROD END SEPARATED FROM THE BARSDR CA030311002Bearing · disintegrated(CAN) R/H ALTERNATOR WOULD NOT STAY ON LINE. SENT FOR PREMATURE OVERHAUL (1000.0 HR TBO). FOUND REAR BEARING DISINTEGRATED TO THE POINT OF ROTOR RUB. THE OVERHAUL COMPANY IS HOLDING BEARING FOR POSSIBLE T.C. INSPECTION.SDR CA021115010Bearing · shorted(CAN) LT GENERATOR TRIPPED, PILOTS REPORTED AN UNDER VOLTAGE CONDITION.ACTION: LT GENERATOR REMOVED, UPON INSPECTION OF COMPONENT, GEARING ASSEMBLY PARTS HAD MIGRATED TO, AND SHORTED OUT A BRUSH HOLDDOWN SPRING TO THE GENERATOR CASE.SDR CA020226004Fitting · fractured(CAN) GEARBOX LOW OIL PRESSURE LIGHT CAME ON, ENGINE SHUTDOWN AND AIRCRAFT LANDED. GEARBOX OIL LEVEL FOUND LOW BUT STILL ON DIP STICK. OIL LEAK TRACED TO FAILED FITTING ON SUPERCHARGER. UNIT HAS OVERHAUL LIFE OF 2,500 HOURS. LINE IS PRESSURE CHECKED (LOW PRESSSDR CA010504015Fairing · cracked(CAN) WHEN DOING THE POST FLIGHT INSPECTION A CRACK WAS FOUND IN THE NOSE GEAR DRAG BRACE FAIRING ASSEMBLY. THE CRACK WAS ON THE L/H SIDE FORMER WHICH WAS CRACKED COMPLETELY THROUGH. IF LEFT UNREPAIRED A FAILURE OF THE FAIRING ASSEMBLY WAS POSSIBLE. THE CRACK SDR CA001128015Coupling · intermittent(CAN) CREW REPORTED INTERMITTENT NR 1 ENGINE FIRE WARN. MAINTENANCE FOUND FIRE WIRE COUPLING AT FIREWALL (LT UPPER) INTERMITTENT POOR CONNECTION CLEANED RE-ASSEMBLIED CHECKED SERVICEABLE..SDR CA001128016Element · broken(CAN) CREW REPORTED NR 1 FIRE TEE HANDLE LIGHT FLICKED. MAINTENANCE FOUND ALSO WOULD NOT TEST. FIREWALL FIRE ELEMENT FOUND BROKEN. ELEMENT REPLACED CHECKED SERVICEABLE.SDR CA000926010Rotor · cracked(CAN) ON PREFLIGHT, FIBERGLASS DUCT MATERIAL AND METAL FRAGMENTS WERE DISCOVERED IN ENGINE NACELLE/WHEEL WELL AREA.SUPERCHARGER ROTOR FAILED SENDING METAL FRAGMENTS THROUGH FIBERGLASS INLET DUCT.SUPERCHARGER AND DUCT WERE REPLACED, DEBRIS REMOVED FROM INLET PASDR CA000926009Rotor · cracked(CAN) CABIN SUPERCHARGER ROTOR FAILED IN FLIGHT.FLIGHT CREW ACTIVATED APU AS ALTERNATE SOURCE OF PRESSURIZATION AND AIR CONDITIONING.SDR CA000516019Rod · corroded(CAN) X-RAY INSPECTION OF AILERON PUSH ROD REVEALED SEVERE INTERNAL CORROSION.SDR CA991004032Disc · broken(CAN) CREW TAXIED FROM RAMP THEN HEARD NOISE FROM RIGHT SIDE OF AIRCRAFT. INCREASED POWER TO MOVE AIRCRAFT - WOULD NOT MOVE. FOUND NR 4 BRAKE DISC BROKEN AND JAMMED IN WHEEL RIM. WHEEL, BRAKE, AND DISC REPLACED.SDR CA981230009Actuator · failed(CAN) FUEL TRIM ACTUATOR FAILED AFTER TAKEOFF, UNABLE TO CHANGE FUEL TRIM SETTING. AIRCRAFT RETURNED TO BASE. THE UNIT WAS REPLACED.SDR CA990202006Line · cracked(CAN) ON GEAR EXTENSION, THE CREW OBSERVED FLUCTUATING HYDRAULIC PRESSURE. GEAR EXTENDED SLOWLY. AFTER LANDING, COMPLETE LOSS OF HYDRAULIC PRESSURE AND FLUID. TWO LEFT MAIN TIRES BLEW. MAINTENANCE FOUND A CRACKED LINE FLARE ON THE AUX/MAIN HYDRAULIC SELECTSDR CA981209007Fitting · broken(CAN) UPLOCK FRAME ATTACH FITTING FOR MAIN LANDING GEAR FOUND BROKEN AT FRONT SPAR.SDR CA981116003Gyro · failed(CAN) RIGHT HAND ADI GYRO FLAGGING NUMEROUS TIMES.SDR CA981116002Gyro · failed(CAN) LEFT ADI TOPPLED.SDR CA980825009Bellcrank · cracked(CAN) DEFLECTION CRANK FOUND CRACKED USING NDT TECHNIQUE. PART TC: 19,718.SDR 98ZZZX535Driveshaft · looseTHE BOLT SECURING THE FORWARD U-JOINT ONTO THE DRIVESHAFT HAD BACKED ALL THE WAY OUT. THE BOLT SECURING THE AFT U-JOINT TO THE DRIVESHAFT WAS LOOSE EVEN WITH THE LOCKING TAB WASHER INSTALLED. UPON INVESTIGATION, IT APPEARED THE WRONG LOCKING TAB WAS USED DURSDR CA971219025Turbine Disk · failed(CAN) DURING INSPECTION, WITH THE TURBINE EXPOSED, IT WAS FOUND THE HP TURBINE DISK HAD FAILED CAUSING SEVERE INTERNAL DAMAGE AND RESULTED IN PENETRATION OF THE TURBINE CASE. ENGINE WILL BE SHIPPED TO ROLLS FOR ASSESSMENT OF DAMAGE AND REPAIR. PART TC: 16,3SDR CA971110008Turbine Blade · failed(CAN) DURING MAINTENANCE RUN-UP, THE NR 1 ENGINE VIBRATION BEGAN TO INCREASE. THE NR 1 ENGINE WAS SHUTDOWN. INSPECTION FOUND A HOLE IN THE LOWER TURBINE CASE, WHICH INDICATED A TURBINE BLADE, OR BLADES, HAD FAILED AND EXITED THROUGH THE CASE. THERE WAS NO ASDR CA970728006Flex Line · ruptured(CAN) THE AIRCRAFT WAS ENROUTE WHEN THE CREW NOTICED A LOSS OF HYDRAULIC PRESSURE. THEY RETURNED TO ORIGIN AND THE AIRCRAFT WAS JACKED AND HYDRAULIC PRESSURE APPLIED. THE FLEXIBLE LINE FROM THE L/H HYDRAULIC PUMP TO THE FILTER WAS FOUND RUPTURED. NEW LINE INSTSDR CA970916007Pump · failed(CAN) CREW REPORTED NR 1 HYDRAULIC PUMP PRESSURE FAIL LIGHT ON. PUMP REPLACED.SDR CA970916008Line · chafed(CAN) CREW REPORTED LOSS OF HYDRAULIC FLUID. CLAMP ON RT EXT HYD LINE CHAFED THROUGH AT CLAMP. LT AND RT DRIVEN PUMPS, FILTERS REPLACED AND LINE AND CLAMPS REPLACED.SDR CA970529001Line · leaking(CAN) LOSS OF HYDRAULIC PRESSURE AFTER TAKEOFF. LANDING GEAR LOWERED USING EMERGENCY PROCEDURE. LEFT MLG OUTER DRAG STRUT FLEX LINE LEAKING. BOTH FLEX LINES REPLACED.SDR CA960927002Gyro · faulty(CAN) IN LEVEL FLIGHT, THE R/H HSI INTERMITENTLY INDICATED 10 DEGREES NOSE DOWN WITH NO FLAGS SHOWING. SHORTLY AFTER THE UNIT WAS INSTALLED, IT TOOK 20 MINUTES TO SPOOL UP ON ONE LEG BUT THE FAULT COULD NOT BE DUPLICATED. THE VERTICAL GYRO WAS REPLACED AND AIRSDR CA960909011Generator · hot(CAN) WHILE IN CRUISE FLIGHT, THE RIGHT HAND GENERATOR LIGHT CAME ON, FOLLOWED BY RIGHT HAND GENERATOR HOT LIGHT. THE ENGINE WAS SECURED AND THE AIRCRAFT RETURNED TO THE AIRPORT FOR AN UNEVENTFUL LANDING. THE GENERATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO
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