Rolls-Royce SPEY-555-15

Service difficulty reports · 261

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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 AU990694Bleed Valve · faulty(AUS) PRESSURIZATION SYSTEM BLEED AIR SHUTOFF VALVES FAULTY.Mar 23, 1999 · Fokker F28MK4000 · Cabin Pressure Control SystemSDR AU990141Diffuser · cracked(AUS) NR 2 ENGINE DIFFUSER CASE CRACKED IN SEVERAL PLACES AT THE 6:30 O'CLOCK POSITION.Feb 10, 1999 · Fokker F28MK4000 · Turbine Engine Combustion SectionSDR AU990297Diffuser · cracked(AUS) NR 2 ENGINE DIFFUSER CASE ASSEMBLY CRACKED IN SEVERAL PLACES AT THE 6:30 O'CLOCK POSITION.Feb 10, 1999 · Fokker F28MK4000 · Turbine Engine Combustion SectionSDR CA990310095Engine · failed(CAN) NR 2 ENGINE FAILED ON CLIMB-OUT, A SEVERE VIBRATION WAS FELT THROUGHOUT THE AIRCRAFT. THE ENGINE WAS SHUTDOWN, THE FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT DIVERTED. THE AIRCRAFT LANDED SAFELY. INITIAL INSPECTION FOUND THE OIL TANK COMPLETELY EMPFeb 1, 1999 · Fokker F28MK1000 · Engine (Turbine/Turboprop)SDR CA990310093Pump · failed(CAN) THERE WAS SIGNIFICANT DROP IN HYDRAULIC QUANTITY FROM THE UTILITY SYSTEM IN-FLIGHT. PER THE CHECK LIST THE PUMPS WERE OFF LOADED. RE-ENGAGING THE PUMPS PRIOR TO LANDING, THE NR 2 UTILITY SYSTEM DID NOT COME BACK ON LINE. LOSS OF ALL HYDRAULIC SYSTEMS.Jan 15, 1999 · Fokker F28MK1000 · Hydraulic Pump (Electric/Engine), MainSDR CA990310088Blade · separated(CAN) DURING FLIGHT AT FL 300, THE NR 1 ENGINE FLAMED OUT AND THE HP FUEL LEVER MOVED TO THE SHUTOFF POSITION UNINITIATED. AIRCRAFT LANDED WITHOUT INCIDENT AND THE ENGINE WAS REPLACED. THE AIRCRAFT RETURNED TO SERVICE. OBSERVATIONS ON THE REPLACED ENGINE WEJan 1, 1999 · Fokker F28MK1000 · Turbine SectionSDR CA990318068Blade · failed(CAN) DURING CRUISE AT FL 300, NR 1 ENGINE FLAMED OUT. PILOT REPORTED NR 1 ENGINE HP FUEL LEVER MOVING UNCOMMANDED TO SHUT-OFF POSITION. FLIGHT CREW ATTEMPTED RE-START, BUT VIBRATIONS WERE EXCESSIVE SO ENGINE WAS SHUT DOWN. POST- FLIGHT INSPECTION AT DESTINJan 1, 1999 · Fokker F28MK1000 · Turbine SectionSDR AU981686Rod · out of adjust(AUS) DURING TAKEOFF, NR 2 ENGINE FAILED TO REACH 100 PERCENT THRUST. GROUND INVESTIGATION FOUND THE ENGINE CONTROL ROD 'D' OUT OF ADJUSTMENT, I.E. OFF THE MAXIMUM STOP. 34,454.Dec 31, 1998 · Fokker F28MK4000 · Power LeverSDR CA990115013Turbine · damaged(CAN) TAKEOFF WAS ABORTED DUE TO ENGINE VIBRATION, WHICH WAS HEAVIEST AT 92% N2, AND UNSTABLE ENGINE PARAMETERS. ICING CONDITIONS WERE PRESENT. NEITHER CLEANING NOR FUEL BLEED CLEARED THE PROBLEM. VISUAL INSPECTION FOUND THE LOW PRESSURE TURBINE DAMAGED, WITH Dec 18, 1998 · Fokker F28FOKKER* · Turbine SectionSDR CA990310086Blade · missing(CAN) NR 1 ENGINE WAS VIBRATING AT TAKEOFF POWER WHILE TAXIING. THE AIRCRAFT RETURNED TO THE GATE WHERE THE ENGINE WAS INSPECTED AND THE LP COMPRESSOR WAS LUBRICATED. DURING SUBSEQUENT RUN-UP, ALL ENGINE PARAMETERS WERE NORMAL, BUT WHEN TAKEOFF POWER WAS APPDec 18, 1998 · Fokker F28MK1000 · Turbine SectionSDR CA981207005Blade · bent(CAN) ON CLIMB-OUT, THE AIRCRAFT EXPERIENCED A SEVERE VIBRATION FOLLOWED BY A LOUD BANG. AT THIS TIME THE PILOTS NOTICED THE NR 2 ENGINE STARTING TO SPOOL DOWN AND TEMP OUT. THE CREW ELECTED TO SHUT THE NR 2 ENGINE DOWN AND RETURN TO THE DEPARTURE POINT. PONov 18, 1998 · Fokker F28MK1000 · Engine (Turbine/Turboprop)SDR CA990115025Blade · failed(CAN) PROVISIONAL ASSESSMENT IS THE LP TURBINE HAD A BLADE FAILURE.Nov 18, 1998 · Fokker F28MK1000 · Turbine SectionSDR AU981529Angle · broken(AUS) LEFT MAIN LANDING GEAR DOOR FORWARD MICROSWITCH ATTACHMENT ANGLE BROKEN. PART TC: 35,926.Nov 11, 1998 · Fokker F28MK4000 · Fuselage Miscellaneous StructureSDR AU981550Seal · worn(AUS) LEFT ENGINE DRIVEN HYDRAULIC PUMP SHAFT SEAL FAILED. LOSS OF HYDRAULIC FLUID.Nov 8, 1998 · Fokker F28MK4000 · Hydraulic Pump (Electric/Engine), MainSDR AU981552Seal · worn(AUS) LEFT ENGINE DRIVEN HYDRAULIC PUMP SHAFT SEAL LEAKING. LOSS OF HYDRAULIC FLUID. SEE ALSO OPERATOR CONTROL NR AU981550.Nov 8, 1998 · Fokker F28MK4000 · Hydraulic Pump (Electric/Engine), MainSDR AU981436Line · leaking(AUS) PITOT SYSTEM LEAKING FROM SPEED COMM AND AIR SPEED TRANSDUCER.Oct 20, 1998 · Fokker F28MK4000 · Pitot/Static SystemSDR AU981306Compressor · damaged(AUS) NR 2 ENGINE N2 COMPRESSOR REAR STAGE COMPRESSOR BLADES SEVERELY DAMAGED.Oct 1, 1998 · Fokker F28MK4000 · Turbine Engine Compressor SectionSDR AU981239Skin · delaminated(AUS) RUDDER TRAILING EDGE DELAMINATED. THE DELAMINATION STARTED APPROXIMATELY 145 MM (5.7 INCHES) UP FROM THE BOTTOM AND EXTENDED UP FOR A FURTHER 710 MM (27.9 INCHES). THE WIDTH OF THE DELAMINATION WAS APPROXIMATELY 135 MM (5.3 INCHES).Sep 3, 1998 · Fokker F28MK4000 · Rudder, Plate/SkinSDR CA980916030Actuator · jammed(CAN) HORIZONTAL STAB JAMMED ON APPROACH. BOTH STAB CAUTION LIGHTS COME ON ON THE HYDRAULIC FLIGHT CONTROL PANEL. ALTERNATE SYSTEM TRIED BUT NOT OPERATIONAL. EMERGENCY DECLARED AND PASSENGERS ASKED TO MOVE TO REAR OF AIRCRAFT. CFR CALLED OUT. UNEVENTFUL LAAug 25, 1998 · Fokker F28MK1000 · Stabilizer ActuatorSDR AU981148Support · corroded(AUS) LEFT MAIN LANDING GEAR SUPPORT STRUCTURE CORRODED.Aug 8, 1998 · Fokker F28MK4000 · Wing, Landing Gear Attach FittingsSDR AU981157Actuator · leaking(AUS) RIGHT MAIN LANDING GEAR DOWNLOCK ACTUATOR LEAKING. LOSS OF SYSTEM 1 HYDRAULIC FLUID. INVESTIGATION FOUND SPRING ACTUATOR BACKUP RING P/N 130036365 DAMAGED. PART TC: 55,277.Jun 14, 1998 · Fokker F28MK4000 · Landing Gear Retraction/Extension SystemSDR AU981158Washer · failed(AUS) FLAP DRIVE CENTER GEARBOX CONE CLUTCH POSITION WASHERS FAILED. PART TC: 62,175.Jun 14, 1998 · Fokker F28MK4000 · Trailing Edge Flap Control SystemSDR AU980918Ballast · failed(AUS) LEFT GLARESHIELD RED FLUORESCENT TUBE BALLAST UNIT (LG16) INTERNAL SHORT CIRCUIT.May 9, 1998 · Fokker F28MK4000 · Flight Compartment LightingSDR AU971542Beam · cracked(AUS) FLOOR BEAM CRACKED AT EDGE OF PREVIOUS REPAIR IN AREA BENEATH GALLEY AND FIRST CONSOLE. CRACK LENGTH 20MM (0.787IN). FOUND DURING CORROSION CONTROL PROGRAMME WHICH CONSTITUTES PART OFAD/F28/66.Dec 3, 1997 · Fokker F28MK1000 · Fuselage Main, Floor BeamSDR AU971461Web · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN TWO PLACES:- 1. WEB AT HORIZONTAL BEAM 7 LOCATED OUTBOARD OF VERTICAL BEAM BL325L 2. WEB AT HORIZONTAL BEAM 8 LOCATED OUTBOARD OF VERTICAL BEAM BL325L FOUND DURING VISUAL INSPECTION IAW ER F28-53-10-20G.Aug 19, 1997 · Fokker F28MK4000 · Fuselage Main, BulkheadSDR AU971463Door · cracked(AUS) RH SERVICE/EMERGENCY DOOR CONTAINED TWO CRACKS IN THE LOWER AFT CORNER RUNNING UNDER THE REPAIR DOUBLERS. CRACK LENGTHS 5MM AND 6MM (0.19IN AND 0.23IN). FOUND DURING EDDY CURRENT INSPECTION IAW ER F28/53/30/18C.Aug 6, 1997 · Fokker F28MK4000 · Service DoorsSDR CA970807047Inverter · shorting out(CAN) AFTER LANDING THE FLIGHT ATTENDANT CALL CHIMES STARTED SOUNDING CONTINUOUSLY, ACCOMPANIED BY STATIC IN THE INTERPHONE SYSTEM. AFTER THE MAJORITY OF THE PASSENGERS WERE OFF, THE FLIGHT ATTENDANT NOTICED SMOKE IN THE FORWARD CABIN AREA. THE REMAINING PASSEJul 25, 1997 · Fokker F28MK1000 · AC InverterSDR CA970807046Fuel Flow Reg · faulty(CAN) TAKEOFF REJECTED DUE TO INSUFFICIENT THRUST ON NR1 ENGINE. MAINTENANCE RPLACED THE NR1 ENGINE FUEL FLOW REGULATOR. ENGINE GROUND RUN AND LEAK CHECK CARRIED OUT SERVICEABLE AND THE AIRCRAFT RETURNED TO SERVICE.Jul 19, 1997 · Fokker F28MK1000 · Fuel Flow SensorSDR AU971035Quadrant · contaminated(AUS) RH WING OUTBOARD AILERON LOWER QUADRANT BEARING WATER INGRESSJun 21, 1997 · Fokker F28MK4000 · Aileron Control SystemSDR CA970604001Sense Line · worn(CAN) AFTER TAKEOFF CREW NOTED LIMITED AIRFLOW FROM THE AIR CONDITIONING PACKS AND NO PRESSURIZATION. AIRCRAFT RETURNED TO BASE. INSPECTION FOUND A BLEED SENSE LINE CHAFED AND WORN THROUGH AT A CLAMP LOCATION. THE LINE WAS REPLACED AND THE AIRCRAFT RETURNED TOMay 21, 1997 · Fokker F28MK1000 · Pneumatic Distribution SystemSDR AU970510Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THREE AREAS:-1. FORWARD PRESSURE BULKHEAD REAR SIDE AT HORIZONTAL BEAM 7 LEFT OF BL325L - CRACK LENGTH 76.2MM (3IN)2. FORWARD PRESSURE BULKHEAD REAR SIDE AT HORIZONTAL BEAM 7 RIGHT OF BL325R - CRACK LENGTH 127MM (5INMay 18, 1997 · Fokker F28MK4000 · Fuselage Main, BulkheadSDR AU970533Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THREE PLACES:- 1. REAR SIDE OF FORWARD PRESSURE BULKHEAD WEB AT HORIZONTAL BEAM NO7 LEFT OF BL325L - CRACK LENGTH 76.2MM (3IN) 2. REAR SIDE OF FORWARD PRESSURE BULKHEAD WEB AT HORIZONTAL BEAM NO7 RIGHT OF BL325R - CRAMay 18, 1997 · Fokker F28MK4000 · Fuselage Main, BulkheadSDR USAAF97040Engine · vibrationBHM/CLT - FLT 1480 - WHLE IN HOLDING PATTERN OVER CLT DUE TO WEATHER CONDITIONS, VIBRATION WAS EXPERIENCED ON RIGHT ENGINE. CREW WENT TO ALTERNATE PROCEDURES. INDICATION STILL EXCEEDED LIMITATIONS. THE RIGHT ENGINE WAS PUT TO IDLE. THE CREW DECLARED AN EMEApr 22, 1997 · N868US · Fokker F28MK1000 · Engine (Turbine/Turboprop)SDR CA970422001Blade · dented(CAN) DURING A GROUND RUN TO INVESTIGATE A REPORTED IN-FLIGHT VIBRATION, THE ENGINE SURGED AND WAS SHUTDOWN. INITIAL REPORT WAS A FAILED LOW PRESSURE (LP2) TURBINE BLADE, SINCE AMENDED TO A "DENTED" LP2 TURBINE BLADE. METAL SPLATTER WAS ALSO REPORTED IN THE TAApr 10, 1997 · Fokker F28MK1000 · Turbine SectionSDR CA970401007Switch · req adjustment(CAN) AFTER DEPARTURE CARGO DOOR WARNING LIGHT CAME ON. AIRCRAFT RETURNED. AFT CARGO DOOR MICROSWITCH OUT OF ADJUSTMENT, ADJUSTED.Mar 4, 1997 · Fokker F28MK1000 · Door Warning SystemSDR CA970206021Blade · missing(CAN) DURING CLIMB THROUGH FL270 THE CREW HEARD A "BANG" AND FELT A VIBRATION FROM #2 ENGINE, WHILE THE ENGINE WAS STILL MAKING POWER. AIRCRAFT RETURNED TO THE POINT OF DEPARTURE. INITIAL INSPECTION REVEALED A LOW PRESSURE TURBINE BLADE MISSING. THIS ENGINE SUJan 31, 1997 · Fokker F28MK1000 · Turbine SectionSDR AU970096Drain Valve · leaking(AUS) LH ENGINE LP FUEL FILTER DRAIN VALVE LEAKING FROM FLANGE AREAJan 30, 1997 · Fokker F28MK1000 · Engine Fuel DistributionSDR CA970219011Turbine Blade · missing(CAN) #2 ENGINE EXPERIENCED SUDDEN VIBRATIONS THROUGH FL270. ALL ENGINE PARAMETERS WERE FINE BUT VIBRATIONS COULD BE FELT THROUGH THE AIRCRAFT AND POWER LEVERS. ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO ITS POINT OF DEPARTURE. POST FLIGHT INSPECTION FOUJan 29, 1997 · Fokker F28MK1000 · Turbine SectionSDR CA970206002Thrust Meter · stuck(CAN) CREW REJECTED TAKEOFF DUE TO #1 ENGINE THRUST INDEX ON LEFT HAND THRUST METER BEING STUCK AT 85 PERCENT AND UNABLE TO ADJUST. AIRCRAFT RETURNED TO BASE AND THE THRUST INDICATOR WAS REPLACED.Jan 27, 1997 · Fokker F28MK1000 · Engine Indicating SystemSDR CA970206003Regulator · faulty(CAN) ON TAKEOFF ROLL THE #2 ENGINE DID NOT PRODUCE TAKEOFF RATED THRUST. THE TAKEOFF WAS REJECTED. MAINTENANCE FOUND THE PROBLEM TO BE AN AIR LEAK. CORR UJOINT AND 3 GASKETS WERE REPLACED ON THE #2 ENGINE FUEL FLOW REGULATOR AT THE P3 CONNECTION. ENGINE WAS GJan 20, 1997 · Fokker F28MK1000 · Fuel Controlling SystemSDR CA970121005Fuelflow Reg · faulty(CAN) ON TAKEOFF ROLL THE #1 ENGINE WOULD NOT SPOOL UP TO FULL POWER. AIRCRAFT RETURNED TO GATE. MAINTENANCE FOUND THE FUEL FLOW REGULATOR TO BE FAULTY. THE FUEL FLOW REGULATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Jan 1, 1997 · Fokker F28MK1000 · Fuel Controlling SystemSDR USAAF96126Fuel Flow · failedFLT 284 - BWI-IND - WHILE EN ROUTE OVER PIT, CAPT REPORTED LT ENG DID NOT RESPOND. UPON DESCENT NR 1 EPR WOULD NT GO TO IDLE, 85 PERCENT N2. TRIED TO ADVANCE THROTTLES SEVERAL TIMES. FLIGHT DIVERTED TO PIT AND AN EMERGENCY WAS DECLARED. ENGINE WAS DOWN TO Dec 12, 1996 · N888AU · Fokker F28MK0100 · Fuel Controlling SystemSDR CA961230003Control Unit · faulty(CAN) #2 ENGINE HAD A FIRE WARNING INDICATION IN FLIGHT. #2 ENGINE WAS SHUTDOWN AND FIRE WARNING WENT OUT, SO FIRE BOTTLES WERE NOT ACTIVATED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE FAULT ON THE GROUND. ALL SYSTEMS CHECKED NODec 10, 1996 · Fokker F28MK1000 · Fire DetectionSDR QXEA9600480Engine Oil · over servicedSMOKE SMELL IN AFT AREA OF CABIN REPORTED BY A PASSENGER AND LEFT LAV SMOKE DETECTOR ALARM SOUNDED ON TAXI OUT. AIRCRAFT RETURNED TO GATE. NUMBER TWO ENGINE FOUND OVER SERVICED BY TWO QUARTS ON THE ENGINE OIL. ENGINE OIL SERVICED TO NORMAL LEVEL. ENGINE GRDec 4, 1996 · N478US · Fokker F28MK4000 · Turbine Engine Oil SystemSDR CA961112021Bracket · cracked(CAN) AFTER LANDING LE FLAP #1 AND #2 LIFTDUMPER PANELS WOULD NOT RETRACT ENTIRELY. THE LIFTDUMPER WAS BARBER POLED AND THERE WAS NO LIFTDUMPER MASTER WARNING INDICATION. LH SUPPORT LEVER BRACKET PARTIALLY BROKEN AND TWO BOLTS SHEARED OFF. REPAIRED OR REPLACEDDec 1, 1996 · Fokker F28MK1000 · Leading Edge Slat Control SystemSDR USAAF96102Fuel Contl Reg · failedRIC-PHL - FLT 1150 - AFTER TAKEOFF, NR 2 ENGINE REMAINED AT TAKEOFF POWER. CAPTAIN DISCONNECTED THE AUTOTHROTTLE AND ATTEMPTED TO SLOW ENGINE WITH THROTTLE. THIS DID NOT WORK. ENGINE EXCEEDED N2 LIMIT SO CAPTAIN SHUTDOWN THE ENGINE. FLIGHT RETURNED TO RIC Sep 22, 1996 · N893US · Fokker F28MK0100 · Fuel Controlling SystemSDR CA960909020Acm · cabin smoke(CAN) ON CLIMB OUT CREW REPORTED SMOKE IN CABIN. FOUND OIL AT #1 AIR CYCLE MACHINE. REPLACED.Aug 9, 1996 · Fokker F28MK1000 · Cabin Cooling SystemSDR CA960909016Controller · failure(CAN) AIRCRAFT ENCOUNTERED PRESSURIZATION PROBLEMS SPIKING UP TO 2000 FEET MIN. IN ASSOCIATION WITH POWER LEVER MOVEMENT. HIGH BLEED CYCLING ON AND OFF. TURNING RATE KNOB TO MINIMUM HAD NO EFFECT. PRESSURE CONTROLLER REPLACED.Aug 5, 1996 · Fokker F28MK1000 · Cabin Pressure ControllerSDR CA960826025Apu · cabin smoke(CAN) ON DEPARTURE SMOKE IN CABIN AND COCKPIT AND SMOKE DETECTOR IN LAVATORY WAS ACTIVATED. AIRCRAFT COMPLETED OVERWEIGHT WITHOUT INCIDENT. SECOND OCCURRENCE OF SAME PROBLEM. OVERWEIGHT LANDING CHECK REVEALED CRACK AT RETENTION ACTUATOR AND LEG. GEAR REPLACED.Jul 31, 1996 · Fokker F28MK1000 · APU Cowling/ContainmentSDR AU961099Regulator · faulty(AUS) NO2 ENGINE FUEL FLOW REGULATOR (FFR) SUSPECT FAULTYJul 30, 1996 · Fokker F28MK4000 · Fuel Controlling System
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