Rolls-Royce TAY-650-15

Service difficulty reports · 164

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 = 'TAY65015'
  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.

SDR 2010FA0000216Turbine Blades · fracturedTHE REPORT SUGGEST THAT THE LPT3 BLADE HAD FRACTURED IN HIGH CYCLE FATIGUE THAT HAD PROPAGATED FROM AN INTERGRANULAR CRACK ON THE AIRFOIL T/E.Sep 9, 2009 · Turbine SectionSDR CA070109005Valve · malfunctioned(CAN) DATE OF DELAY NOV 8, 2006 CADORS NR: 2006C2915. THE FLIGHT CREW WAS NOTIFIED THAT DURING TAXI FOR DEPARTURE FUEL WAS LEAKING FROM LT WING. AIRCRAFT TAXIED OFF RUNWAY BY WHICH TIME THE LEAK HAD STOPPED. FLIGHT CREW IN CONTACT WITH MAINTENANCE CONTROL Nov 8, 2006 · Fokker F28MK0100 · Fuel StorageSDR CA070110005Warning System · malfunctioned(CAN) THE REFERENCED AIRCRAFT AN EVENT INVOLVING THE AUTOMATIC SILENCING OF CABIN CHIMES. NORMALLY THE FLIGHT CREW WILL ADVISE THE FLIGHT ATTENDANTS TO TAKE THEIR POSITIONS FOR LANDING WITH 3 CHIMES SELECTED MANUALLY IN THE COCKPIT. IT APPEARS HOWEVER IN LAOct 9, 2006 · Fokker F28MK0100 · Interphone/Passenger Announcement (PA) SystemSDR CA060919005Actuator · malfunctioned(CAN) FLIGHT CREW REPORTED THAT THE SPEED BRAKE WOULD NOT RETRACT UPON SELECTION TO DO SO. FOLLOWING LANDING. BOTH PADDLES CONFIRMED OPEN. AIRCRAFT WAS FERRIED TO BASE, WHERE THE SPEED BRAKE ACTUATOR WAS REPLACED. SYSTEM TESTED SERVICEABLE AFTER REPLACEMENT. Sep 10, 2006 · Fokker F28MK0100 · Drag Control SystemSDR AU510001439Microphone · faulty(AUS) HAND MICROPHONE SWITCH STICKING.(OTHER CAUSE: STICKY SWITCH - MATERIAL ) (CASA# 510001439)Dec 12, 2005 · Fokker F28MK0100 · Audio Integrating SystemSDR AU510001481Nipple · missing(AUS) FLAP BALL NUT GREASE NIPPLE MISSING.(OTHER CAUSE: UNKNOWN ) (CASA# 510001481)Dec 12, 2005 · Fokker F28MK0100 · Trailing Edge FlapsSDR AU510001497Strut · faultyLT MAIN LANDING GEAR STRUT INTERNAL SLEEVE MIGRATED OUT OF POSITION AND BLOCKED BLEED PLUG HOLE, FOUND DURING INSPECTION IAW AD/F100/64.Dec 12, 2005 · Fokker F28MK0100 · Main Landing Gear Strut/Axle/TruckSDR AU510001498Strut · crackedRT MAIN LANDING GEAR STRUT BLEED PORT CRACKED, FOUND DURING INSPECTION IAW AD/F100/64.Dec 12, 2005 · Fokker F28MK0100 · Main Landing Gear Strut/Axle/TruckSDR AU510001521Igniter · failedAPU IGNITER PLUG FAILED. WORKSHOP INVESTIGATION FOUND THAT ONLY APPARENT FAULT WAS SLIGHT SOILING ON THE CERAMIC INSIDE OF THE CONNECTOR END OF THE IGNITER. THERE WAS NO OBVIOUS SIGN OF ARCING ACROSS THE CERAMIC SURFACE. WHEN THE IGNITER WAS CLEANED, THERE WDec 12, 2005 · Fokker F28MK0100 · APU Start/Ignition SystemSDR AU510001534Connector · looseENGINE INDICATION SYSTEM PRESSURE BULKHEAD CONNECTOR P2874 LOOSE.Dec 12, 2005 · Fokker F28MK0100 · Engine Indicating System WiringSDR AU510001540Pressure Switch · faultyRT ENGINE LP FUEL PRESSURE SWITCH FAULTY.Dec 12, 2005 · Fokker F28MK0100 · Fuel Pressure IndicatingSDR AU510001648Pitot Head · faultyNR 3 PITOT HEAD HEATING SYSTEM FAILED.Dec 12, 2005 · Fokker F28MK0100 · Pitot/Static SystemSDR AU510001654Bearing · wornLT ENGINE INLET GUIDE VANE BEARINGS PNO UP60336 (1OFF) AND PNO EU61711 (2OFF) WORN. FOUND DURING INSPECTION IAW SB TAY-75-1655.Dec 12, 2005 · Fokker F28MK0100 · Turbine Engine Air Inlet SectionSDR AU510001655Connector · leakingCREW OXYGEN MASK BOX ASSEMBLY CONNECTOR LEAKING. LOSS OF OXYGEN.Dec 12, 2005 · Fokker F28MK0100 · Crew Oxygen SystemSDR AU510001667Smoke Detector · faultyREPORT OF CIGARETTE SMOKE SMELL IN CABIN. TOILET SMOKE DETECTOR DID NOT ACTIVATE ALARM. INVESTIGATION CONTINUING.Dec 12, 2005 · Fokker F28MK0100 · Smoke DetectionSDR AU510001721Hose · failedLT TOILET SMOKE DETECTOR TO AIR EJECTOR HOSE SPLIT AT EJECTOR END. RT SMOKE DETECTOR TO AIR EJECTOR TUBE SIDEWALL COLLAPSED. HOSES ALLOW FOR AIRFLOW THROUGH SMOKE DETECTORS.Dec 12, 2005 · Fokker F28MK0100 · Smoke DetectionSDR AU510001726Pipe · fracturedHYDRAULIC PIPE LOCATED ON THE FORWARD WALL OF THE REAR CARGO HOLD LEAKING. INVESTIGATION FOUND A FRACTURED FLARE. PIPE WAS A -4 STAINLESS STEEL TYPE.Dec 12, 2005 · Fokker F28MK0100 · Hydraulic System, MainSDR AU510001740Exciter · faultyAPU IGNITION EXCITER UNIT FAULTY.Dec 12, 2005 · Fokker F28MK0100 · APU Start/Ignition SystemSDR AU510001751Fuel Control · failed(AUS) APU AUTO-SHUTDOWN IN FLIGHT. INVESTIGATION FOUND A FAULTY FUEL CONTROL UNIT. (CASA NR 510001751)Dec 12, 2005 · Fokker F28MK0100 · APU Engine Fuel and ControlSDR AU510001802Motor · shearedAPU STARTER MOTOR DRIVE SHAFT SHEARED.Dec 12, 2005 · Fokker F28MK0100 · APU Start/Ignition SystemSDR AU510001804Bolt · brokenNR 2 MAIN WHEEL TIE BOLT BROKEN. BOLT HEAD MISSING. INVESTIGATION CONTINUING.Dec 12, 2005 · Fokker F28MK0100 · Wheel/Ski/FloatSDR AU510001805Iru · failedNR 2 INERTIAL REFERENCE UNIT (IRU) INTERMITTENTLY FAILS CODE 2. INVESTIGATION CONTINUING.Dec 12, 2005 · Fokker F28MK0100 · Inertial Guidance SystemSDR AU510001887Switch · faultyNR 1 ENGINE ANTI-ICE SWITCH FAULTY.Dec 12, 2005 · Fokker F28MK0100 · Air Intake Anti/De-Ice SystemSDR AU510001903Drive Shaft · sheared(AUS) APU STARTER MOTOR DRIVESHAFT SHEARED. INVESTIGATION FOUND THAT THE BROKEN END WAS JAMMED IN THE CLUTCH ASSEMBLY. (CASA NR 510001903)Dec 12, 2005 · Fokker F28MK0100 · APU Start/Ignition SystemSDR AU510001914Bolt · loose(AUS) LT AILERON TAB OB HINGE BRACKET ATTACHMENT BOLTS LOOSE. BOLTS WERE THREADBOUND IN ANCHOR NUTS. INVESTIGATION FOUND INCORRECT BOLTS WERE FITTED BY A PREVIOUS OPERATOR IN THE US. (CASA NR 510001914)Dec 12, 2005 · Fokker F28MK0100 · AileronsSDR AU510001915Control Cable · misrigged(AUS) CONTROL CABLES FOR FLAPS ( F1 AND F2) WERE FOUND TO BE 43LB LOW IN TENSION. THE LT AILERON WING CABLE WAS 30LB LOW. THE LT AND RT AILERON UPFLOAT CABLES WERE 45LB LOW. (CASA NR 510001915)Dec 12, 2005 · Fokker F28MK0100 · Trailing Edge Flap Control SystemSDR AU510001923Cooling Fan · faulty(AUS) AVIONICS COOLING FAN NOISY IN OPERATION.Dec 12, 2005 · Fokker F28MK0100 · Air Distribution FanSDR AU510001935Stringer · corrodedNR 3 LT STRINGER LOCATED AT STN 13851 IN THE FORWARD CARGO COMPARTMENT CORRODED.Dec 12, 2005 · Fokker F28MK0100 · Fuselage Main, Longeron/StringerSDR AU510001947Shutoff Valve · failedLT ENGINE ANTI-ICE PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) FAILED.Dec 12, 2005 · Fokker F28MK0100 · Air Intake Anti/De-Ice SystemSDR AU510001948Motor · faultyFUEL SYSTEM RT CROSS FLOW VALVE MOTOR FAULTY. VALVE STUCK IN CLOSED POSITION.Dec 12, 2005 · Fokker F28MK0100 · Fuel Transfer ValveSDR AU510002018Igniter · wornNR 2 ENGINE IGNITER WORN.Dec 12, 2005 · Fokker F28MK0100 · Spark Plug/IgniterSDR AU510002019Solenoid · faultyNR 2 ENGINE THRUST REVERSER INTERMITTENT WARNING. INVESTIGATION FOUND THE SECONDARY LOCK SOLENOID HAD A FAULTY INTERNAL SWITCH.Dec 12, 2005 · Fokker F28MK0100 · Engine Thrust ReverserSDR AU510002024Fairing · crackedENGINE EXHAUST SPOKE FAIRING CRACKED IN TWO PLACES AT THE 7:30 O`CLOCK AND 9 O`CLOCK POSITIONS.Dec 12, 2005 · Fokker F28MK0100 · Engine Collector/Tailpipe/NozzleSDR AU510002107Shutoff Valve · faultyRT BLEED AIR PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) FAULTY.Dec 12, 2005 · Fokker F28MK0100 · Pneumatic Distribution SystemSDR AU510002112Transponder · failedNR 2 ATC TRANSPONDER FAILED. INVESTIGATION CONTINUING.Dec 12, 2005 · Fokker F28MK0100 · ATC Transponder SystemSDR AU510002116Control Panel · faultyNR 2 ATC TRANSPONDER SYSTEM CONTROL PANEL DISPLAY DIGITS NOT VISIBLE.Dec 12, 2005 · Fokker F28MK0100 · ATC Transponder SystemSDR AU510002130Oxygen Bottle · leakingCOCKPIT OXYGEN BOTTLE LEAKING FROM VALVE.Dec 12, 2005 · Fokker F28MK0100 · Crew Oxygen SystemSDR AU510001987Igniter · failedNR 1 ENGINE IGNITER PLUG FAILED.Dec 10, 2005 · Fokker F28MK0100 · Spark Plug/IgniterSDR AU510001988Apu · failedAPU AUTO SHUTDOWN. INVESTIGATION COULD FIND NO FAULTS. DURING TEST FLIGHT THE APU AGAIN SHUT DOWN. INVESTIGATION CONTINUING.Dec 10, 2005 · Fokker F28MK0100 · APU Core EngineSDR AU510001708Apu · inoperativeAPU FAILED TO START. INVESTIGATION CONTINUING.Dec 8, 2005 · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) SystemSDR AU510001579Shutoff Valve · faulty(AUS) PNEUMATIC SYSTEM PRESSURE REGULATING SHUTOFF VALVE (PRSOV) FAULTY. (CASA NR 510001579)Dec 7, 2005 · Fokker F28MK0100 · Pneumatic Distribution SystemSDR AU510001587Computer · faulty(AUS) AUTOPILOT COMPUTER SUSPECT FAULTY. (CASA NR 510001587)Dec 7, 2005 · Fokker F28MK0100 · Autopilot ComputerSDR AU510001588Slide · faulty(AUS) RT ESCAPE SLIDE FAILED TO DEPLOY CORRECTLY. FOLLOWING MANUAL OPERATION THE SLIDE INFLATED BUT WAS NOT CORRECTLY ORIENTATED TO THE DOOR OPENING. SUSPECT CAUSED BY FAULTY PACKING OF THE SLIDE AT THE LAST OVERHAUL. (CASA NR 510001588)Dec 7, 2005 · Fokker F28MK0100 · Escape SlideSDR AU510002078Line · cracked(AUS) HYDRAULIC PIPE CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID. (CASA NR 510002078)Nov 11, 2005 · Fokker F28MK0100 · Hydraulic System, MainSDR AU510001989Pump · failedNR 2 SYSTEM HYDRAULIC PUMP FAILED. INVESTIGATION CONTINUING.Nov 10, 2005 · Fokker F28MK0100 · Hydraulic Pump, AuxiliarySDR AU510001518Computer · faultyAUTOPILOT COMPUTER INTERMITTENT FAULT.Nov 6, 2005 · Fokker F28MK0100 · Autopilot ComputerSDR AU510002087Pressure Switch · faultyFUEL TRANSFER PUMP PRESSURE SWITCH FAULTY.Oct 11, 2005 · Fokker F28MK0100 · Fuel Pressure IndicatorSDR AU510002126Pressure Switch · failedLT AND RT HYDRAULIC PRESSURE SWITCHES FOR THE NR 2 STABILIZER SYSTEM FAULTY.Oct 11, 2005 · Fokker F28MK0100 · Hydraulic Indicating SystemSDR AU510002127Totalizer · faultyFUEL INDICATING SYSTEM COMBINED PROCESSOR TOTALIZER UNIT (CPT) FAULTY.Oct 11, 2005 · Fokker F28MK0100 · Fuel Indicating SystemSDR AU510002086Idg · faultyLT ENGINE INTEGRATED DRIVE GENERATOR (IDG) FAULTY. LT GENERATOR LINE CONTACTOR P/N S6002206 ALSO CHANGED.Sep 11, 2005 · Fokker F28MK0100 · AC Generator-Alternator
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