# Service difficulty reports: Rolls-Royce TAY-650-15

A list on [Rolls-Royce TAY-650-15](https://openairdocs.org/engine/rolls-royce-tay-650-15.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 164 reports

- [SDR 2010FA0000216](https://openairdocs.org/sdr/2010FA0000216.md): Turbine Blades · fractured · Sep 9, 2009 · Turbine Section
  > THE REPORT SUGGEST THAT THE LPT3 BLADE HAD FRACTURED IN HIGH CYCLE FATIGUE THAT HAD PROPAGATED FROM AN INTERGRANULAR CRACK ON THE AIRFOIL T/E.
- [SDR CA070109005](https://openairdocs.org/sdr/CA070109005.md): Valve · malfunctioned · Nov 8, 2006 · Fokker F28MK0100 · Fuel Storage
  > (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
- [SDR CA070110005](https://openairdocs.org/sdr/CA070110005.md): Warning System · malfunctioned · Oct 9, 2006 · Fokker F28MK0100 · Interphone/Passenger Announcement (PA) System
  > (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 LA
- [SDR CA060919005](https://openairdocs.org/sdr/CA060919005.md): Actuator · malfunctioned · Sep 10, 2006 · Fokker F28MK0100 · Drag Control System
  > (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.
- [SDR AU510001439](https://openairdocs.org/sdr/AU510001439.md): Microphone · faulty · Dec 12, 2005 · Fokker F28MK0100 · Audio Integrating System
  > (AUS) HAND MICROPHONE SWITCH STICKING.(OTHER CAUSE: STICKY SWITCH - MATERIAL) (CASA# 510001439)
- [SDR AU510001481](https://openairdocs.org/sdr/AU510001481.md): Nipple · missing · Dec 12, 2005 · Fokker F28MK0100 · Trailing Edge Flaps
  > (AUS) FLAP BALL NUT GREASE NIPPLE MISSING.(OTHER CAUSE: UNKNOWN) (CASA# 510001481)
- [SDR AU510001497](https://openairdocs.org/sdr/AU510001497.md): Strut · faulty · Dec 12, 2005 · Fokker F28MK0100 · Main Landing Gear Strut/Axle/Truck
  > LT MAIN LANDING GEAR STRUT INTERNAL SLEEVE MIGRATED OUT OF POSITION AND BLOCKED BLEED PLUG HOLE, FOUND DURING INSPECTION IAW AD/F100/64.
- [SDR AU510001498](https://openairdocs.org/sdr/AU510001498.md): Strut · cracked · Dec 12, 2005 · Fokker F28MK0100 · Main Landing Gear Strut/Axle/Truck
  > RT MAIN LANDING GEAR STRUT BLEED PORT CRACKED, FOUND DURING INSPECTION IAW AD/F100/64.
- [SDR AU510001521](https://openairdocs.org/sdr/AU510001521.md): Igniter · failed · Dec 12, 2005 · Fokker F28MK0100 · APU Start/Ignition System
  > APU 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 W
- [SDR AU510001534](https://openairdocs.org/sdr/AU510001534.md): Connector · loose · Dec 12, 2005 · Fokker F28MK0100 · Engine Indicating System Wiring
  > ENGINE INDICATION SYSTEM PRESSURE BULKHEAD CONNECTOR P2874 LOOSE.
- [SDR AU510001540](https://openairdocs.org/sdr/AU510001540.md): Pressure Switch · faulty · Dec 12, 2005 · Fokker F28MK0100 · Fuel Pressure Indicating
  > RT ENGINE LP FUEL PRESSURE SWITCH FAULTY.
- [SDR AU510001648](https://openairdocs.org/sdr/AU510001648.md): Pitot Head · faulty · Dec 12, 2005 · Fokker F28MK0100 · Pitot/Static System
  > NR 3 PITOT HEAD HEATING SYSTEM FAILED.
- [SDR AU510001654](https://openairdocs.org/sdr/AU510001654.md): Bearing · worn · Dec 12, 2005 · Fokker F28MK0100 · Turbine Engine Air Inlet Section
  > LT ENGINE INLET GUIDE VANE BEARINGS PNO UP60336 (1OFF) AND PNO EU61711 (2OFF) WORN. FOUND DURING INSPECTION IAW SB TAY-75-1655.
- [SDR AU510001655](https://openairdocs.org/sdr/AU510001655.md): Connector · leaking · Dec 12, 2005 · Fokker F28MK0100 · Crew Oxygen System
  > CREW OXYGEN MASK BOX ASSEMBLY CONNECTOR LEAKING. LOSS OF OXYGEN.
- [SDR AU510001667](https://openairdocs.org/sdr/AU510001667.md): Smoke Detector · faulty · Dec 12, 2005 · Fokker F28MK0100 · Smoke Detection
  > REPORT OF CIGARETTE SMOKE SMELL IN CABIN. TOILET SMOKE DETECTOR DID NOT ACTIVATE ALARM. INVESTIGATION CONTINUING.
- [SDR AU510001721](https://openairdocs.org/sdr/AU510001721.md): Hose · failed · Dec 12, 2005 · Fokker F28MK0100 · Smoke Detection
  > LT 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.
- [SDR AU510001726](https://openairdocs.org/sdr/AU510001726.md): Pipe · fractured · Dec 12, 2005 · Fokker F28MK0100 · Hydraulic System, Main
  > HYDRAULIC PIPE LOCATED ON THE FORWARD WALL OF THE REAR CARGO HOLD LEAKING. INVESTIGATION FOUND A FRACTURED FLARE. PIPE WAS A -4 STAINLESS STEEL TYPE.
- [SDR AU510001740](https://openairdocs.org/sdr/AU510001740.md): Exciter · faulty · Dec 12, 2005 · Fokker F28MK0100 · APU Start/Ignition System
  > APU IGNITION EXCITER UNIT FAULTY.
- [SDR AU510001751](https://openairdocs.org/sdr/AU510001751.md): Fuel Control · failed · Dec 12, 2005 · Fokker F28MK0100 · APU Engine Fuel and Control
  > (AUS) APU AUTO-SHUTDOWN IN FLIGHT. INVESTIGATION FOUND A FAULTY FUEL CONTROL UNIT. (CASA NR 510001751)
- [SDR AU510001802](https://openairdocs.org/sdr/AU510001802.md): Motor · sheared · Dec 12, 2005 · Fokker F28MK0100 · APU Start/Ignition System
  > APU STARTER MOTOR DRIVE SHAFT SHEARED.
- [SDR AU510001804](https://openairdocs.org/sdr/AU510001804.md): Bolt · broken · Dec 12, 2005 · Fokker F28MK0100 · Wheel/Ski/Float
  > NR 2 MAIN WHEEL TIE BOLT BROKEN. BOLT HEAD MISSING. INVESTIGATION CONTINUING.
- [SDR AU510001805](https://openairdocs.org/sdr/AU510001805.md): Iru · failed · Dec 12, 2005 · Fokker F28MK0100 · Inertial Guidance System
  > NR 2 INERTIAL REFERENCE UNIT (IRU) INTERMITTENTLY FAILS CODE 2. INVESTIGATION CONTINUING.
- [SDR AU510001887](https://openairdocs.org/sdr/AU510001887.md): Switch · faulty · Dec 12, 2005 · Fokker F28MK0100 · Air Intake Anti/De-Ice System
  > NR 1 ENGINE ANTI-ICE SWITCH FAULTY.
- [SDR AU510001903](https://openairdocs.org/sdr/AU510001903.md): Drive Shaft · sheared · Dec 12, 2005 · Fokker F28MK0100 · APU Start/Ignition System
  > (AUS) APU STARTER MOTOR DRIVESHAFT SHEARED. INVESTIGATION FOUND THAT THE BROKEN END WAS JAMMED IN THE CLUTCH ASSEMBLY. (CASA NR 510001903)
- [SDR AU510001914](https://openairdocs.org/sdr/AU510001914.md): Bolt · loose · Dec 12, 2005 · Fokker F28MK0100 · Ailerons
  > (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)
- [SDR AU510001915](https://openairdocs.org/sdr/AU510001915.md): Control Cable · misrigged · Dec 12, 2005 · Fokker F28MK0100 · Trailing Edge Flap Control System
  > (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)
- [SDR AU510001923](https://openairdocs.org/sdr/AU510001923.md): Cooling Fan · faulty · Dec 12, 2005 · Fokker F28MK0100 · Air Distribution Fan
  > (AUS) AVIONICS COOLING FAN NOISY IN OPERATION.
- [SDR AU510001935](https://openairdocs.org/sdr/AU510001935.md): Stringer · corroded · Dec 12, 2005 · Fokker F28MK0100 · Fuselage Main, Longeron/Stringer
  > NR 3 LT STRINGER LOCATED AT STN 13851 IN THE FORWARD CARGO COMPARTMENT CORRODED.
- [SDR AU510001947](https://openairdocs.org/sdr/AU510001947.md): Shutoff Valve · failed · Dec 12, 2005 · Fokker F28MK0100 · Air Intake Anti/De-Ice System
  > LT ENGINE ANTI-ICE PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) FAILED.
- [SDR AU510001948](https://openairdocs.org/sdr/AU510001948.md): Motor · faulty · Dec 12, 2005 · Fokker F28MK0100 · Fuel Transfer Valve
  > FUEL SYSTEM RT CROSS FLOW VALVE MOTOR FAULTY. VALVE STUCK IN CLOSED POSITION.
- [SDR AU510002018](https://openairdocs.org/sdr/AU510002018.md): Igniter · worn · Dec 12, 2005 · Fokker F28MK0100 · Spark Plug/Igniter
  > NR 2 ENGINE IGNITER WORN.
- [SDR AU510002019](https://openairdocs.org/sdr/AU510002019.md): Solenoid · faulty · Dec 12, 2005 · Fokker F28MK0100 · Engine Thrust Reverser
  > NR 2 ENGINE THRUST REVERSER INTERMITTENT WARNING. INVESTIGATION FOUND THE SECONDARY LOCK SOLENOID HAD A FAULTY INTERNAL SWITCH.
- [SDR AU510002024](https://openairdocs.org/sdr/AU510002024.md): Fairing · cracked · Dec 12, 2005 · Fokker F28MK0100 · Engine Collector/Tailpipe/Nozzle
  > ENGINE EXHAUST SPOKE FAIRING CRACKED IN TWO PLACES AT THE 7:30 O`CLOCK AND 9 O`CLOCK POSITIONS.
- [SDR AU510002107](https://openairdocs.org/sdr/AU510002107.md): Shutoff Valve · faulty · Dec 12, 2005 · Fokker F28MK0100 · Pneumatic Distribution System
  > RT BLEED AIR PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) FAULTY.
- [SDR AU510002112](https://openairdocs.org/sdr/AU510002112.md): Transponder · failed · Dec 12, 2005 · Fokker F28MK0100 · ATC Transponder System
  > NR 2 ATC TRANSPONDER FAILED. INVESTIGATION CONTINUING.
- [SDR AU510002116](https://openairdocs.org/sdr/AU510002116.md): Control Panel · faulty · Dec 12, 2005 · Fokker F28MK0100 · ATC Transponder System
  > NR 2 ATC TRANSPONDER SYSTEM CONTROL PANEL DISPLAY DIGITS NOT VISIBLE.
- [SDR AU510002130](https://openairdocs.org/sdr/AU510002130.md): Oxygen Bottle · leaking · Dec 12, 2005 · Fokker F28MK0100 · Crew Oxygen System
  > COCKPIT OXYGEN BOTTLE LEAKING FROM VALVE.
- [SDR AU510001987](https://openairdocs.org/sdr/AU510001987.md): Igniter · failed · Dec 10, 2005 · Fokker F28MK0100 · Spark Plug/Igniter
  > NR 1 ENGINE IGNITER PLUG FAILED.
- [SDR AU510001988](https://openairdocs.org/sdr/AU510001988.md): Apu · failed · Dec 10, 2005 · Fokker F28MK0100 · APU Core Engine
  > APU AUTO SHUTDOWN. INVESTIGATION COULD FIND NO FAULTS. DURING TEST FLIGHT THE APU AGAIN SHUT DOWN. INVESTIGATION CONTINUING.
- [SDR AU510001708](https://openairdocs.org/sdr/AU510001708.md): Apu · inoperative · Dec 8, 2005 · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) System
  > APU FAILED TO START. INVESTIGATION CONTINUING.
- [SDR AU510001579](https://openairdocs.org/sdr/AU510001579.md): Shutoff Valve · faulty · Dec 7, 2005 · Fokker F28MK0100 · Pneumatic Distribution System
  > (AUS) PNEUMATIC SYSTEM PRESSURE REGULATING SHUTOFF VALVE (PRSOV) FAULTY. (CASA NR 510001579)
- [SDR AU510001587](https://openairdocs.org/sdr/AU510001587.md): Computer · faulty · Dec 7, 2005 · Fokker F28MK0100 · Autopilot Computer
  > (AUS) AUTOPILOT COMPUTER SUSPECT FAULTY. (CASA NR 510001587)
- [SDR AU510001588](https://openairdocs.org/sdr/AU510001588.md): Slide · faulty · Dec 7, 2005 · Fokker F28MK0100 · Escape Slide
  > (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)
- [SDR AU510002078](https://openairdocs.org/sdr/AU510002078.md): Line · cracked · Nov 11, 2005 · Fokker F28MK0100 · Hydraulic System, Main
  > (AUS) HYDRAULIC PIPE CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID. (CASA NR 510002078)
- [SDR AU510001989](https://openairdocs.org/sdr/AU510001989.md): Pump · failed · Nov 10, 2005 · Fokker F28MK0100 · Hydraulic Pump, Auxiliary
  > NR 2 SYSTEM HYDRAULIC PUMP FAILED. INVESTIGATION CONTINUING.
- [SDR AU510001518](https://openairdocs.org/sdr/AU510001518.md): Computer · faulty · Nov 6, 2005 · Fokker F28MK0100 · Autopilot Computer
  > AUTOPILOT COMPUTER INTERMITTENT FAULT.
- [SDR AU510002087](https://openairdocs.org/sdr/AU510002087.md): Pressure Switch · faulty · Oct 11, 2005 · Fokker F28MK0100 · Fuel Pressure Indicator
  > FUEL TRANSFER PUMP PRESSURE SWITCH FAULTY.
- [SDR AU510002126](https://openairdocs.org/sdr/AU510002126.md): Pressure Switch · failed · Oct 11, 2005 · Fokker F28MK0100 · Hydraulic Indicating System
  > LT AND RT HYDRAULIC PRESSURE SWITCHES FOR THE NR 2 STABILIZER SYSTEM FAULTY.
- [SDR AU510002127](https://openairdocs.org/sdr/AU510002127.md): Totalizer · faulty · Oct 11, 2005 · Fokker F28MK0100 · Fuel Indicating System
  > FUEL INDICATING SYSTEM COMBINED PROCESSOR TOTALIZER UNIT (CPT) FAULTY.
- [SDR AU510002086](https://openairdocs.org/sdr/AU510002086.md): Idg · faulty · Sep 11, 2005 · Fokker F28MK0100 · AC Generator-Alternator
  > LT ENGINE INTEGRATED DRIVE GENERATOR (IDG) FAULTY. LT GENERATOR LINE CONTACTOR P/N S6002206 ALSO CHANGED.

Next page: https://openairdocs.org/engine/rolls-royce-tay-650-15/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/rolls-royce-tay-650-15/reports

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