Rolls-Royce SPEY-555-15

Service difficulty reports · 261

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 = 'SPEY55515'
  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 AUS20011420Pin · missing(AUS) RT ENGINE HP FUEL VALVE RELAY LEVER TO CONTROL ROD CONNECTION BOLT / NUT SPLIT PIN MISSING. NUT WAS LOOSE AND ALMOST SEPARATED FROM BOLT.Oct 21, 2001 · Fokker F28MK1000 · Engine ControlsSDR AUS20011431Line · cracked(AUS) PNEUMATIC SYSTEM BACKUP VALVE TO STUB WING SENSE LINE CRACKED AT FLARE.Oct 12, 2001 · Fokker F28MK1000 · Pneumatic Indicating SystemSDR AUS20011429Indicator · faulty(AUS) DME SYSTEM FAULTY.Oct 3, 2001 · Fokker F28MK1000 · DME/TACAN SystemSDR AUS20011430Spring · broken(AUS) RT MAIN LANDING GEAR DOOR UPLOCK LATCH OVERCENTRE SPRING BROKEN.Oct 3, 2001 · Fokker F28MK4000 · Landing Gear Retraction/Extension SystemSDR AUS20011433Switch · out of adjust(AUS) RT MAIN LANDING GEAR GROUND / FLIGHT SWITCH OUT OF ADJUSTMENT.Sep 30, 2001 · Fokker F28MK4000 · Landing Gear Position and WarningSDR CA010921008Indicator · false indication(CAN) AIRCRAFT WAS INVOLVED IN AN INFLIGHT PRECAUTIONARY SHUTDOWN OF ONE ENGINE DUE TO AN INDICATION OF OIL TEMP INDICATION TO RED LINE ENROUTE TO SANDSPIT. THE TROUBLESHOOTING PROVED THAT IT WAS AN INDICATION PROBLEMM ONLY.THE AIRCRAFT WAS RETURNED TO SERVICESep 19, 2001 · Fokker F28MK1000 · Engine Oil TemperatureSDR AUS20011302Duct · failed(AUS) APU AIR DUCT RUPTURED IN AREA DOWNSTREAM OF THE APU LOAD CONTROL AIR VALVE.Sep 17, 2001 · Fokker F28MK1000 · Engine Bleed Air SystemSDR CA011003005Control Unit · sticking(CAN) AIRCRAFT REPORTED TO HAVING THE FLIGHT MASTER CAUTION LIGHT ILLUMINATED ALONG WITH BOTH STAB CONTROL CAUTION LIGHTS ON TAKEOFF OUT OF TORONTO (YYZ). THE AIRCRAFT RETURNED TO TORONTO FOR AN UNEVENTFUL LANDING. THE HORIZONTAL STABILIZER CONTROL UNIT WAS RESep 14, 2001 · Fokker F28MK1000 · Stabilizer Control SystemSDR AUS20011300Pipe · cracked(AUS) RT AILERON ACTUATOR RETURN PIPE CRACKED AND LEAKING. LOSS OFHYDRAULIC FLUID.Sep 10, 2001 · Fokker F28MK1000 · Aileron Control SystemSDR AUS20011297Warning Light · faulty(AUS) FLIGHT CONTROL MASTER CAUTION LIGHT ILLUMINATED. NO CAUSE OF THE PROBLEM COULD BE FOUND BUT THE NR 1 AND NR 2 RUDDER BYPASS SWITCHES WERE REPLACED DUE TO PREVIOUS PROBLEMS.Sep 7, 2001 · Fokker F28MK4000 · Central WarningSDR AUS20011298Warning System · faulty(AUS) UNSAFE CONFIGURATION WARNING SOUNDED. INVESTIGATION COULD FIND NO CAUSE FOR THE PROBLEM. LH ELEVATOR BYPASS SWITCH CHANGED AS A PRECAUTION.Sep 4, 2001 · Fokker F28MK4000 · Central WarningSDR AUS20011428Wire · broken(AUS) LANDING GEAR ANTI-RETRACTION SUPPRESSION DIODE WIRE BROKEN OFF AND INSULATION WASHERS BADLY WORN.Sep 1, 2001 · Fokker F28MK1000 · Landing Gear Position and WarningSDR AUS20011426Bulb · unapproved part(AUS) LT MAIN LANDING GEAR DOWNLIGHT FITTED WITH INCORRECT PART NUMBER BULB. UNAPPROVED PART.Aug 30, 2001 · Fokker F28MK1000 · Landing Gear Position and WarningSDR AUS20011425Skin · cracked(AUS) FUSELAGE SKIN CRACKED AT THE 12 O'CLOCK POSITION BETWEEN STA 3845 AND STA 4875. CRACK LENGTH APPROXIMATELY 76.2MM (3IN).Aug 29, 2001 · Fokker F28MK1000 · Fuselage Main, Plate/SkinSDR AUS20011323Clamp · leaking(AUS) RT ENGINE BLEED AIR CROSSOVER DUCT CLAMP LEAKING.Aug 22, 2001 · Fokker F28MK4000 · Engine Bleed Air SystemSDR AUS20011325Fire Loop · faulty(AUS) APU FIRE WARNING SYSTEM LT SENSING ELEMENT FAULTY. FALSE FIRE WARNING RESULTED IN FIRE BOTTLE BEING FIRED.Aug 17, 2001 · Fokker F28MK1000 · Fire DetectionSDR AUS20011324Warning System · false activation(AUS) NR 2 GENERATOR HIGH INLET TEMPERATURE. INVESTIGATION COULD FIND NO CAUSE FOR THE PROBLEM. PLUGS AND CONNECTORS CLEANED.Aug 11, 2001 · Fokker F28MK1000 · AC Generator-AlternatorSDR AUS20011415Indicator · stuck(AUS) NR 1 HIGH PRESSURE VALVE SWITCH INDICATOR STICKING.Aug 11, 2001 · Fokker F28MK1000 · Pneumatic Indicating SystemSDR AUS20011416Downlock Switch · intermittent(AUS) NOSE LANDING GEAR DOOR DOWNLOCK MICROSWITCH INTERMITTENT IN OPERATION.Aug 8, 2001 · Fokker F28MK1000 · Landing Gear Position and WarningSDR AUS20011413Controller · faulty(AUS) LIFT DUMPER BARBER POLE REMAINED ON' AFTER LOCK SWITCH MOVED TO LOCKED POSITION. SUSPECT CAUSED BY FAULTY LIFT DUMPER CONTROL BOX.Aug 4, 2001 · Fokker F28MK1000 · Drag Control SystemSDR AUS20011409Pump · malfunctioned(AUS) NR 1 ENGINE NR 2 HYDRAULIC SYSTEM PUMP LOW PRESSURE.Aug 2, 2001 · Fokker F28MK1000 · Hydraulic Pump (Electric/Engine), MainSDR AUS20011408Line · leaking(AUS) TURBINE BYPASS VALVE DOWNSTREAM SENSE LINE LEAKING.Jul 27, 2001 · Fokker F28MK4000 · Cabin Temperature SensorSDR AUS20010787Boss · out of adj(AUS) SERVICE / EMERGENCY DOOR STRIKER BOSS LOOSE AND MISALIGNED.Jul 24, 2001 · Fokker F28MK1000 · Door Warning SystemSDR AUS20011407Csd · disconnected(AUS) NO1 CONSTANT SPEED DRIVE (CSD) DISCONNECTED IN FLIGHT.Jul 23, 2001 · Fokker F28MK4000 · Alternator-Generator DriveSDR AUS20010786Reducer · cracked(AUS) LANDING GEAR HYDRAULIC SYSTEM PRESSURE REDUCER CRACKED. LOSS OF HYDRAULIC FLUID.Jul 22, 2001 · Fokker F28MK1000 · Hydraulic System, MainSDR AUS20010760Engine · faulty(AUS) LT ENGINE OIL CONSUMPTION EXCESSIVE AT APPROXIMATELY 0.8 LITRES TO 1 LITRE PER HOUR.Jul 14, 2001 · Fokker F28MK4000 · Engine (Turbine/Turboprop)SDR AUS20010784Cable · broken(AUS) PASSENGER DOOR DECLUTCH CABLE TERMINAL END BROKEN.Jul 5, 2001 · Fokker F28MK4000 · Passenger/Crew DoorsSDR AUS20010782Drain Valve · stuck(AUS) PITOT STATIC SYSTEM DRAIN LINE VALVE STUCK IN OPEN POSITION.Jul 1, 2001 · Fokker F28MK1000 · Pitot/Static SystemSDR AUS20010781Actuator · leaking(AUS) STABILIZER ACTUATOR LEAKING. LOSS OF HYDRAULIC FLUID.Jun 26, 2001 · Fokker F28MK4000 · Stabilizer ActuatorSDR AUS20010898Lever · stuck(AUS) LANDING GEAR RETRACTION LEVER STUCK IN DOWN POSITION. CIRCUIT BREAKER L8 POPPED.Jun 21, 2001 · Fokker F28MK1000 · Landing Gear Retraction/Extension SystemSDR AUS20011451Blade · damaged(AUS) NR 1 ENGINE HP TURBINE BLADES (6OFF) DAMAGED.Jun 11, 2001 · Fokker F28MK1000 · Turbine SectionSDR AUS20010897Actuator · cracked(AUS) LT MAIN LANDING GEAR DOOR AFT ACTUATOR CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID.Jun 5, 2001 · Fokker F28MK1000 · Landing Gear Door ActuatorSDR AUS20010702Controller · erratic(AUS) PRESSURISATION SYSTEM ERRATIC IN OPERATION. INVESTIGATION FOUND THAT THE AIR FILTER AND VENTURI LINES WERE TRANSPOSED AT THE PRESSURISATION CONTROLLER CONNECTIONS. PERSONNEL/MAINTENANCEERROR.Jun 1, 2001 · Fokker F28MK1000 · Cabin Pressure Control SystemSDR AUS20010703Pipe · leaking(AUS) UTILITY HYDRAULIC SYSTEM SUCTION PIPE CONTAINED A PIN HOLE LEAK.LOSS OF HYDRAULIC FLUID.Jun 1, 2001 · Fokker F28MK1000 · Hydraulic System, MainSDR AUS20010704Lever · stuck(AUS) LANDING GEAR LEVER OBSTRUCTED IN DOWN POSITION.Jun 1, 2001 · Fokker F28MK1000 · Landing Gear SelectorSDR AUS20010895Line · loose(AUS) NO2 ENGINE THRUST FEED SENSE LINE TO GAUGE LOOSE.Jun 1, 2001 · Fokker F28MK1000 · Power Indicating SystemSDR AUS20010602Generator · failed(AUS) NO2 (RH) GENERATOR FAILED.May 30, 2001 · Fokker F28MK4000 · AC Generator-AlternatorSDR AUS20010705Duct · misaligned(AUS) LH BLEED AIR SYSTEM LEAKING AT ENGINE HP OUTLET CHECK VALVE DUCT. INVESTIGATION FOUND THE DUCT MATING SURFACES TO BE BADLY ALIGNED.May 27, 2001 · Fokker F28MK1000 · Pneumatic Distribution SystemSDR AUS20010601Generator · failed(AUS) NO1 GENERATOR FAILED. SUSPECT FAULTY CONSTANT SPEED DRIVE SWITCH.May 26, 2001 · Fokker F28MK4000 · Alternator-Generator DriveSDR AUS20010603Skin · cracked(AUS) TOP FUSELAGE SKIN CRACKED IN AREA BETWEEN STN3845 AND STN4875.CRACK LENGTH 406.4MM (16IN).May 26, 2001 · Fokker F28MK1000 · Fuselage Main, Plate/SkinSDR CA010626002Engine · failed(CAN) THE NR 2 ENGINE FAILED IN FLT ROUTE TO SAINT JOHN, NB. PILOTS RPT THAT IN LEVEL CRUISE FLT A LOUD BAND WAS HEARD, FOLLOWED BY SEVERE VIBRATIONS WHICH SUBSIDED WHEN ENGINE WAS BROUGHT BACK TO 80% NH TGT-OIL PRESSURE WAS NORMAL AT THIS POINT. DECISION WAS May 25, 2001 · Fokker F28MK1000 · Engine (Turbine/Turboprop)SDR AUS20010598Generator · faulty(AUS) RH INBOARD WHEEL SPEED GENERATOR FAULTY.May 19, 2001 · Fokker F28MK1000 · Brake Anti-Skid SectionSDR AUS20010595Switch · out of adj(AUS) LIFT DUMPER MANIFOLD NR 2 BYPASS SWITCH OUT OF ADJUSTMENT.May 17, 2001 · Fokker F28MK1000 · Drag Control SystemSDR AUS20010465Bolt · sheared(AUS) FLAP MOTOR ASSEMBLY BODY BOLT SHEARED AND BODY HALVES SEPARATED AT JOINT. LOSS OF HYDRAULIC FLUID.May 11, 2001 · Fokker F28MK4000 · Trailing Edge Flap ActuatorSDR AUS20010461Engine · malfunctioned(AUS) INCORRECT TAKEOFF THRUST SET BY PILOT. PERSONNEL ERROR.May 8, 2001 · Fokker F28MK4000 · Engine (Turbine/Turboprop)SDR AUS20010468Connector · loose(AUS) RH OUTBOARD LIFT DUMPER BELLCRANK INLOCK CONNECTOR LOOSE.May 7, 2001 · Fokker F28MK1000 · Drag Control SystemSDR AUS20010455Relay · faulty(AUS) RH GROUND/FLIGHT RELAY FAULTY. LH AND RH MLG GROUND FLIGHTSWITCHES CONTAMINATED.May 5, 2001 · Fokker F28MK1000 · Landing Gear Position and WarningSDR AUS20010459Switch · stuck(AUS) MAIN LANDING GEAR GROUND/FLIGHT SWITCHES STICKY.May 5, 2001 · Fokker F28MK1000 · Landing Gear Position and WarningSDR AUS20010464Landing Gear · faulty(AUS) LANDING GEAR WOULD NOT RETRACT.May 5, 2001 · Fokker F28MK1000 · Landing Gear Retraction/Extension SystemSDR AUS20010466Torque Link · cracked(AUS) NOSE LANDING GEAR LOWER TORQUE LINK CRACKED IN GREASE NIPPLEHOLE. FOUND USING VISUAL INSPECTION AND CONFIRMED USING EDDYCURRENT INSPECTION.May 5, 2001 · Fokker F28MK4000 · Nose/Tail Landing Gear
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