Roll-Royc TAY-620-15

Service difficulty reports · 30

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 = 'TAY62015'
  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 YRRR201809260926Bearing · failedFAILURE OF REAR IP/LP COMPRESSOR BEARING.Sep 26, 2018 · Fokker F28MK0070 · Turbine Engine Compressor SectionSDR AU510001866Bolt · looseNR 1 LT LIFT DUMPER SYSTEM BELLCRANK SPIGOT ATTACHMENT BOLTS LOOSE.Dec 12, 2005 · Fokker F28MK0100 · Drag Control SystemSDR AU510001949Skin · lightning strikeEVIDENCE OF LIGHTNING STRIKE ON FUSELAGE AT STN 9305, STN 9805 AND STN 10253. INVESTIGATION CONTINUING.Dec 12, 2005 · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR AU510001861Bolt · shearedRT LIFT DUMPER SYSTEM NR 1 BELLCRANK INBOARD UPPER ATTACHMENT BOLT SHEARED.Dec 9, 2005 · Fokker F28MK0100 · Drag Control SystemSDR AU510001862Bearing · looseRT LIFT DUMPER NR 3 BELLCRANK HORIZONTAL ROD ATTACHMENT BEARING MIGRATED OF POSITION.Dec 9, 2005 · Fokker F28MK0100 · Drag Control SystemSDR AU510001864Rod · crackedRH LIFT DUMPER SYSTEM VERTICAL ROD CRACKED.Dec 9, 2005 · Fokker F28MK0100 · Drag Control SystemSDR AU510001867Bearing · wornLT WING TRAILING EDGE FLAP TRACK FORWARD SUPPORT BEARING WORN.Dec 9, 2005 · Fokker F28MK0100 · Trailing Edge FlapsSDR AU510001868Bearing · wornRT WING FLAP TRACK BEAM ASSEMBLY FORWARD SUPPORT BEARING WORN.Dec 9, 2005 · Fokker F28MK0100 · Trailing Edge FlapsSDR CA031209001Regulator · misinstalled(CAN) NR 2 ENGINE FAILED TO ACCELERATE AT ALTITUDE DURING ALPHA FLOOR PROTECTION TEST. (AIRCRAFT SLOWS TO MINIMUM SPEED. AUTO THROTTLE SHOULD KICK IN AND ACCELERATE AIRCRAFT.) INVESTIGATION OF THE CASC501 FUEL FLOW REGULATOR FROM THIS ENGINE SHOWED THAT IT HADAug 10, 2003 · Fokker F27MK100 · Fuel Controlling SystemSDR AALA20030545Engine · vibrationDURING LEVEL FLT AT 31,000 FT, AIRSPEED 270 KNTS, ON SELECTING 250 KNTS, NR 1 ENG INDICATED HIGH VIB ON MFDU ACCOMPANIED BY AUDIBLE NOISE & VIBRATION FELT THROUGH A/C. ATTEMPTED ICE CLEARING PROCEDURES WITH NO SUCCESS. ADVANCING THROTTLE ABOVE 1.14 EPR CAUSEMay 8, 2003 · N1427A · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR AUS20030420Brake · failed(AUS) BRAKE ROTOR AND STATOR INNER DRIVE LUGS FAILED. SEVERAL SMALL STONES WERE FOUND IN THE DEBRIS. SUSPECT CAUSED BY LOOSE GRAVEL FROM OUTBACK AIRSTRIPS.Apr 14, 2003 · Fokker F28MK0100 · BrakeSDR AUS20030450Stringer · corroded(AUS) RT CENTER WING STRINGER CONNECTING ANGLE LOCATED AT ZONE 138 STA 16511 CONTAINED EXFOLIATION CORROSION.Apr 9, 2003 · Fokker F28MK0100 · Wing, Longeron/StringerSDR AUS20030463Floorbeam · corroded(AUS) FORWARD FUSELAGE FLOORBEAMS CONTAINED EXFOLIATION CORROSION IN AREA BELOW THE FORWARD CABIN FLOOR PANELS. CORROSION WAS PRESENT AT SEVERAL FASTENER HOLES ON EACH OF THE FOUR FLOORBEAMS ATBL600L, BL600R AND BL 1127R. SUSPECT CAUSED BY GALLEY SPILLAGES.Apr 9, 2003 · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR AUS20030496Seat Track · corroded(AUS) AFT FLIGHT ATTENDANT SEAT SUPPORT BRACKET CORRODED.Apr 9, 2003 · Fokker F28MK0100 · Fuselage, Seat/Cargo Attach FittingsSDR AUS20030407Windshield · cracked(AUS) LT WINDSHIELD CRACKED. SUSPECT CAUSED BY MOISTURE INGRESS.Apr 5, 2003 · Fokker F28MK0100 · Flight Compartment WindowsSDR AUS20030381Spar Cap · corroded(AUS) LT WING FORWARD LOWER SPAR CAP CONTAINED TWO AREAS OF EXFOLIATION CORROSION LOCATED BETWEEN RIB 12375 AND RIB 12975. AREAS OF CORROSION APPROXIMATELY 50.8MM BY 25.4MM (2IN BY 1IN) AND 76.2MMBY 25.4MM (3IN BY 1IN).Apr 1, 2003 · Fokker F28MK0100 · Wing SparSDR AUS20030382Slide · faulty(AUS) ESCAPE SLIDE FAULTY. SLIDE DEPLOYED AND INFLATED CORRECTLY BUT FAILED TO DROP TO THE GROUND. THE RAFT WAS TWISTED APPROXIMATELY 45 DEGREES AROUND THE LONG AXIS WITH THE INBOARD END IN CONTACT WITH THE OUTSIDE OF THE DOOR FRAME/FUSELAGE.Mar 17, 2003 · Fokker F28MK0100 · Escape SlideSDR AUS20021420Windshield · cracked(AUS) RH WINDSHIELD CRACKED. SIGNS OF ELECTRICAL FAILURE. MANUFACTURERSUGGESTS PROBLEM COULD BE DUE TO MOISTURE INGRESS. SEE MDR02/1419 FOR FURTHER INFORMATION.Dec 7, 2002 · Fokker F28MK0100 · Flight Compartment WindowsSDR AUS20021114Servo · sticking(AUS) LH AUTO THROTTLE SERVO BINDING.Sep 14, 2002 · Fokker F28MK0100 · Power LeverSDR 2002FA0000151Pump · leakingAPPROX. 2 HOURS INTO FLIGHT FROM DTW TO SNA SYSTEM 1 PUMP 1 FAULT LIGHT ILLUMINATED. CREW FOLLOWED THE ABNORMAL PROCEDURES FOR HYDRAULIC SYSTEM 1 LOW PRESSURE. CREW NOTICE SYSTEM NR 1 QUANTITY BEGINING TO DROP. CREW DIVERTED HOPING TO GET ON THE GROUND BEFORE Jan 27, 2002 · N324K · Fokker F28MK0070 · Hydraulic Pump (Electric/Engine), MainSDR AUS20011054Line · failed(AUS) PRESSURISATION SYSTEM PRIMARY OUTFLOW VALVE SENSE LINE FROM THE MANUAL CONTROL TO THE SENSE PANEL IS CORRODED INTERNALLY CAUSING THE LINE TO SPLIT.Sep 30, 2001 · Fokker F28MK0100 · Cabin Pressure Control SystemSDR AUS20010879Spring · broken(AUS) LT MAIN LANDING GEAR DOOR FORWARD UPLOCK ASSEMBLY RETURN SPRING BROKEN.Aug 7, 2001 · Fokker F28MK0100 · Landing Gear Position and WarningSDR AUS20010561Switch · faulty(AUS) FUELLING CONTROL PANEL POWER SWITCH FAULTY. PANEL POWER REMAINEDON WITH THE SWITCH IN THE OFF' POSITION. INVESTIGATION FOUND THE ACCESS PANEL CAM OPERATING THE PANEL POWER SWITCH WHEN THE PANEL IS CLOSED WAS OUT OF ADJUSTMENT AND NOT OPERATING THESWITCHMay 27, 2001 · Fokker F28MK0100 · Aircraft Fuel Distribution SystemSDR AU010362Relay · failed(AUS) PRESSURISATION SYSTEM FAULTY. SUSPECT CAUSED BY HIGH RESISTANCE ACROSS CONTACTS IN RELAYS K1813, K1261, K1819 AND K1821 IN THEGROUND/FLIGHT RELAY BOX.Mar 31, 2001 · Fokker F28MK0100 · Cabin Pressure Control SystemSDR AU010365Indicator · faulty(AUS) NR 1 ENGINE OIL TEMPERATURE INDICATION SYSTEM FAULTY. WIRING AND INSULATION CHECKED WITH NO FURTHER PROBLEMS. CONNECTORS CLEANED AND INSPECTED. PROBLEM HAS NOT REOCCURRED.Mar 27, 2001 · Fokker F28MK0100 · Engine Oil TemperatureSDR AU010169Outflow Valve · failed(AUS) AVIONICS COOLING SYSTEM OUTFLOW VALVE FAILED.Feb 18, 2001 · Fokker F28MK0100 · Pressure Regulator/Outflow ValveSDR AU010115Connector · contaminated(AUS) NR 1 ENGINE OIL TEMPERATURE PROBE CONNECTOR PLUG LOOSE AND CONTAMINATED.Jan 29, 2001 · Fokker F28MK0100 · Engine Oil TemperatureSDR AU001231O-Ring · split(AUS) NR 1 HYDRAULIC SYSTEM PRESSURE SWITCH O-RING SEAL SPLIT.Dec 24, 2000 · Fokker F28MK0100 · Hydraulic System, MainSDR AU001232Computer · faulty(AUS) STALL PROTECTION COMPUTER FAULTY.Dec 17, 2000 · Fokker F28MK0100 · Stall Warning SystemSDR 99ZZZX2069Seal · failedTHE LP ROTOR WAS FREE TO ROTATE AND THE HP ROTOR WAS CONFIRMED AS BEING SEIZED. THERE WAS NO APPRECIABLE BACKLASH NOTED WHILE ATTEMPTING TO ROTATE THE HP ROTOR. THE HIGH SPEED GEARBOX MOUNTED ACCESSORIES WERE REMOVED AND ON COMPLETION, THE ROTOR WAS STILL NOApr 14, 1999 · Fokker F27MK100 · Turbine Section
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