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.
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
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 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.SDR AUS20011431Line · cracked(AUS) PNEUMATIC SYSTEM BACKUP VALVE TO STUB WING SENSE LINE CRACKED AT FLARE.SDR AUS20011429Indicator · faulty(AUS) DME SYSTEM FAULTY.SDR AUS20011430Spring · broken(AUS) RT MAIN LANDING GEAR DOOR UPLOCK LATCH OVERCENTRE SPRING BROKEN.SDR AUS20011433Switch · out of adjust(AUS) RT MAIN LANDING GEAR GROUND / FLIGHT SWITCH OUT OF ADJUSTMENT.SDR 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 SERVICESDR AUS20011302Duct · failed(AUS) APU AIR DUCT RUPTURED IN AREA DOWNSTREAM OF THE APU LOAD CONTROL AIR VALVE.SDR 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 RESDR AUS20011300Pipe · cracked(AUS) RT AILERON ACTUATOR RETURN PIPE CRACKED AND LEAKING. LOSS OFHYDRAULIC FLUID.SDR 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.SDR AUS20011298Warning System · faulty(AUS) UNSAFE CONFIGURATION WARNING SOUNDED. INVESTIGATION COULD FIND NO CAUSE FOR THE PROBLEM. LH ELEVATOR BYPASS SWITCH CHANGED AS A PRECAUTION.SDR AUS20011428Wire · broken(AUS) LANDING GEAR ANTI-RETRACTION SUPPRESSION DIODE WIRE BROKEN OFF AND INSULATION WASHERS BADLY WORN.SDR AUS20011426Bulb · unapproved part(AUS) LT MAIN LANDING GEAR DOWNLIGHT FITTED WITH INCORRECT PART NUMBER BULB. UNAPPROVED PART.SDR AUS20011425Skin · cracked(AUS) FUSELAGE SKIN CRACKED AT THE 12 O'CLOCK POSITION BETWEEN STA 3845 AND STA 4875. CRACK LENGTH APPROXIMATELY 76.2MM (3IN).SDR AUS20011323Clamp · leaking(AUS) RT ENGINE BLEED AIR CROSSOVER DUCT CLAMP LEAKING.SDR AUS20011325Fire Loop · faulty(AUS) APU FIRE WARNING SYSTEM LT SENSING ELEMENT FAULTY. FALSE FIRE WARNING RESULTED IN FIRE BOTTLE BEING FIRED.SDR AUS20011324Warning System · false activation(AUS) NR 2 GENERATOR HIGH INLET TEMPERATURE. INVESTIGATION COULD FIND NO CAUSE FOR THE PROBLEM. PLUGS AND CONNECTORS CLEANED.SDR AUS20011415Indicator · stuck(AUS) NR 1 HIGH PRESSURE VALVE SWITCH INDICATOR STICKING.SDR AUS20011416Downlock Switch · intermittent(AUS) NOSE LANDING GEAR DOOR DOWNLOCK MICROSWITCH INTERMITTENT IN OPERATION.SDR AUS20011413Controller · faulty(AUS) LIFT DUMPER BARBER POLE REMAINED ON' AFTER LOCK SWITCH MOVED TO LOCKED POSITION. SUSPECT CAUSED BY FAULTY LIFT DUMPER CONTROL BOX.SDR AUS20011409Pump · malfunctioned(AUS) NR 1 ENGINE NR 2 HYDRAULIC SYSTEM PUMP LOW PRESSURE.SDR AUS20011408Line · leaking(AUS) TURBINE BYPASS VALVE DOWNSTREAM SENSE LINE LEAKING.SDR AUS20010787Boss · out of adj(AUS) SERVICE / EMERGENCY DOOR STRIKER BOSS LOOSE AND MISALIGNED.SDR AUS20011407Csd · disconnected(AUS) NO1 CONSTANT SPEED DRIVE (CSD) DISCONNECTED IN FLIGHT.SDR AUS20010786Reducer · cracked(AUS) LANDING GEAR HYDRAULIC SYSTEM PRESSURE REDUCER CRACKED. LOSS OF HYDRAULIC FLUID.SDR AUS20010760Engine · faulty(AUS) LT ENGINE OIL CONSUMPTION EXCESSIVE AT APPROXIMATELY 0.8 LITRES TO 1 LITRE PER HOUR.SDR AUS20010784Cable · broken(AUS) PASSENGER DOOR DECLUTCH CABLE TERMINAL END BROKEN.SDR AUS20010782Drain Valve · stuck(AUS) PITOT STATIC SYSTEM DRAIN LINE VALVE STUCK IN OPEN POSITION.SDR AUS20010781Actuator · leaking(AUS) STABILIZER ACTUATOR LEAKING. LOSS OF HYDRAULIC FLUID.SDR AUS20010898Lever · stuck(AUS) LANDING GEAR RETRACTION LEVER STUCK IN DOWN POSITION. CIRCUIT BREAKER L8 POPPED.SDR AUS20011451Blade · damaged(AUS) NR 1 ENGINE HP TURBINE BLADES (6OFF) DAMAGED.SDR AUS20010897Actuator · cracked(AUS) LT MAIN LANDING GEAR DOOR AFT ACTUATOR CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID.SDR 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.SDR AUS20010703Pipe · leaking(AUS) UTILITY HYDRAULIC SYSTEM SUCTION PIPE CONTAINED A PIN HOLE LEAK.LOSS OF HYDRAULIC FLUID.SDR AUS20010704Lever · stuck(AUS) LANDING GEAR LEVER OBSTRUCTED IN DOWN POSITION.SDR AUS20010895Line · loose(AUS) NO2 ENGINE THRUST FEED SENSE LINE TO GAUGE LOOSE.SDR AUS20010602Generator · failed(AUS) NO2 (RH) GENERATOR FAILED.SDR 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.SDR AUS20010601Generator · failed(AUS) NO1 GENERATOR FAILED. SUSPECT FAULTY CONSTANT SPEED DRIVE SWITCH.SDR AUS20010603Skin · cracked(AUS) TOP FUSELAGE SKIN CRACKED IN AREA BETWEEN STN3845 AND STN4875.CRACK LENGTH 406.4MM (16IN).SDR 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 SDR AUS20010598Generator · faulty(AUS) RH INBOARD WHEEL SPEED GENERATOR FAULTY.SDR AUS20010595Switch · out of adj(AUS) LIFT DUMPER MANIFOLD NR 2 BYPASS SWITCH OUT OF ADJUSTMENT.SDR AUS20010465Bolt · sheared(AUS) FLAP MOTOR ASSEMBLY BODY BOLT SHEARED AND BODY HALVES SEPARATED AT JOINT. LOSS OF HYDRAULIC FLUID.SDR AUS20010461Engine · malfunctioned(AUS) INCORRECT TAKEOFF THRUST SET BY PILOT. PERSONNEL ERROR.SDR AUS20010468Connector · loose(AUS) RH OUTBOARD LIFT DUMPER BELLCRANK INLOCK CONNECTOR LOOSE.SDR AUS20010455Relay · faulty(AUS) RH GROUND/FLIGHT RELAY FAULTY. LH AND RH MLG GROUND FLIGHTSWITCHES CONTAMINATED.SDR AUS20010459Switch · stuck(AUS) MAIN LANDING GEAR GROUND/FLIGHT SWITCHES STICKY.SDR AUS20010464Landing Gear · faulty(AUS) LANDING GEAR WOULD NOT RETRACT.SDR AUS20010466Torque Link · cracked(AUS) NOSE LANDING GEAR LOWER TORQUE LINK CRACKED IN GREASE NIPPLEHOLE. FOUND USING VISUAL INSPECTION AND CONFIRMED USING EDDYCURRENT INSPECTION.
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