# Service difficulty reports: Roll-Royc TAY-620-15

A list on [Roll-Royc TAY-620-15](https://openairdocs.org/engine/roll-royc-tay-620-15.md).

Newest first. General aviation reporting is voluntary.

- [SDR YRRR201809260926](https://openairdocs.org/sdr/YRRR201809260926.md): Bearing · failed · Sep 26, 2018 · Fokker F28MK0070 · Turbine Engine Compressor Section
  > FAILURE OF REAR IP/LP COMPRESSOR BEARING.
- [SDR AU510001866](https://openairdocs.org/sdr/AU510001866.md): Bolt · loose · Dec 12, 2005 · Fokker F28MK0100 · Drag Control System
  > NR 1 LT LIFT DUMPER SYSTEM BELLCRANK SPIGOT ATTACHMENT BOLTS LOOSE.
- [SDR AU510001949](https://openairdocs.org/sdr/AU510001949.md): Skin · lightning strike · Dec 12, 2005 · Fokker F28MK0100 · Fuselage Main, Plate/Skin
  > EVIDENCE OF LIGHTNING STRIKE ON FUSELAGE AT STN 9305, STN 9805 AND STN 10253. INVESTIGATION CONTINUING.
- [SDR AU510001861](https://openairdocs.org/sdr/AU510001861.md): Bolt · sheared · Dec 9, 2005 · Fokker F28MK0100 · Drag Control System
  > RT LIFT DUMPER SYSTEM NR 1 BELLCRANK INBOARD UPPER ATTACHMENT BOLT SHEARED.
- [SDR AU510001862](https://openairdocs.org/sdr/AU510001862.md): Bearing · loose · Dec 9, 2005 · Fokker F28MK0100 · Drag Control System
  > RT LIFT DUMPER NR 3 BELLCRANK HORIZONTAL ROD ATTACHMENT BEARING MIGRATED OF POSITION.
- [SDR AU510001864](https://openairdocs.org/sdr/AU510001864.md): Rod · cracked · Dec 9, 2005 · Fokker F28MK0100 · Drag Control System
  > RH LIFT DUMPER SYSTEM VERTICAL ROD CRACKED.
- [SDR AU510001867](https://openairdocs.org/sdr/AU510001867.md): Bearing · worn · Dec 9, 2005 · Fokker F28MK0100 · Trailing Edge Flaps
  > LT WING TRAILING EDGE FLAP TRACK FORWARD SUPPORT BEARING WORN.
- [SDR AU510001868](https://openairdocs.org/sdr/AU510001868.md): Bearing · worn · Dec 9, 2005 · Fokker F28MK0100 · Trailing Edge Flaps
  > RT WING FLAP TRACK BEAM ASSEMBLY FORWARD SUPPORT BEARING WORN.
- [SDR CA031209001](https://openairdocs.org/sdr/CA031209001.md): Regulator · misinstalled · Aug 10, 2003 · Fokker F27MK100 · Fuel Controlling System
  > (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 HAD
- [SDR AALA20030545](https://openairdocs.org/sdr/AALA20030545.md): Engine · vibration · May 8, 2003 · N1427A · Fokker F28MK0100 · Engine (Turbine/Turboprop)
  > DURING 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 CAUSE
- [SDR AUS20030420](https://openairdocs.org/sdr/AUS20030420.md): Brake · failed · Apr 14, 2003 · Fokker F28MK0100 · Brake
  > (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.
- [SDR AUS20030450](https://openairdocs.org/sdr/AUS20030450.md): Stringer · corroded · Apr 9, 2003 · Fokker F28MK0100 · Wing, Longeron/Stringer
  > (AUS) RT CENTER WING STRINGER CONNECTING ANGLE LOCATED AT ZONE 138 STA 16511 CONTAINED EXFOLIATION CORROSION.
- [SDR AUS20030463](https://openairdocs.org/sdr/AUS20030463.md): Floorbeam · corroded · Apr 9, 2003 · Fokker F28MK0100 · Fuselage Main, Floor Beam
  > (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.
- [SDR AUS20030496](https://openairdocs.org/sdr/AUS20030496.md): Seat Track · corroded · Apr 9, 2003 · Fokker F28MK0100 · Fuselage, Seat/Cargo Attach Fittings
  > (AUS) AFT FLIGHT ATTENDANT SEAT SUPPORT BRACKET CORRODED.
- [SDR AUS20030407](https://openairdocs.org/sdr/AUS20030407.md): Windshield · cracked · Apr 5, 2003 · Fokker F28MK0100 · Flight Compartment Windows
  > (AUS) LT WINDSHIELD CRACKED. SUSPECT CAUSED BY MOISTURE INGRESS.
- [SDR AUS20030381](https://openairdocs.org/sdr/AUS20030381.md): Spar Cap · corroded · Apr 1, 2003 · Fokker F28MK0100 · Wing Spar
  > (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).
- [SDR AUS20030382](https://openairdocs.org/sdr/AUS20030382.md): Slide · faulty · Mar 17, 2003 · Fokker F28MK0100 · Escape Slide
  > (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.
- [SDR AUS20021420](https://openairdocs.org/sdr/AUS20021420.md): Windshield · cracked · Dec 7, 2002 · Fokker F28MK0100 · Flight Compartment Windows
  > (AUS) RH WINDSHIELD CRACKED. SIGNS OF ELECTRICAL FAILURE. MANUFACTURERSUGGESTS PROBLEM COULD BE DUE TO MOISTURE INGRESS. SEE MDR02/1419 FOR FURTHER INFORMATION.
- [SDR AUS20021114](https://openairdocs.org/sdr/AUS20021114.md): Servo · sticking · Sep 14, 2002 · Fokker F28MK0100 · Power Lever
  > (AUS) LH AUTO THROTTLE SERVO BINDING.
- [SDR 2002FA0000151](https://openairdocs.org/sdr/2002FA0000151.md): Pump · leaking · Jan 27, 2002 · N324K · Fokker F28MK0070 · Hydraulic Pump (Electric/Engine), Main
  > APPROX. 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
- [SDR AUS20011054](https://openairdocs.org/sdr/AUS20011054.md): Line · failed · Sep 30, 2001 · Fokker F28MK0100 · Cabin Pressure Control System
  > (AUS) PRESSURISATION SYSTEM PRIMARY OUTFLOW VALVE SENSE LINE FROM THE MANUAL CONTROL TO THE SENSE PANEL IS CORRODED INTERNALLY CAUSING THE LINE TO SPLIT.
- [SDR AUS20010879](https://openairdocs.org/sdr/AUS20010879.md): Spring · broken · Aug 7, 2001 · Fokker F28MK0100 · Landing Gear Position and Warning
  > (AUS) LT MAIN LANDING GEAR DOOR FORWARD UPLOCK ASSEMBLY RETURN SPRING BROKEN.
- [SDR AUS20010561](https://openairdocs.org/sdr/AUS20010561.md): Switch · faulty · May 27, 2001 · Fokker F28MK0100 · Aircraft Fuel Distribution System
  > (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 THESWITCH
- [SDR AU010362](https://openairdocs.org/sdr/AU010362.md): Relay · failed · Mar 31, 2001 · Fokker F28MK0100 · Cabin Pressure Control System
  > (AUS) PRESSURISATION SYSTEM FAULTY. SUSPECT CAUSED BY HIGH RESISTANCE ACROSS CONTACTS IN RELAYS K1813, K1261, K1819 AND K1821 IN THEGROUND/FLIGHT RELAY BOX.
- [SDR AU010365](https://openairdocs.org/sdr/AU010365.md): Indicator · faulty · Mar 27, 2001 · Fokker F28MK0100 · Engine Oil Temperature
  > (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.
- [SDR AU010169](https://openairdocs.org/sdr/AU010169.md): Outflow Valve · failed · Feb 18, 2001 · Fokker F28MK0100 · Pressure Regulator/Outflow Valve
  > (AUS) AVIONICS COOLING SYSTEM OUTFLOW VALVE FAILED.
- [SDR AU010115](https://openairdocs.org/sdr/AU010115.md): Connector · contaminated · Jan 29, 2001 · Fokker F28MK0100 · Engine Oil Temperature
  > (AUS) NR 1 ENGINE OIL TEMPERATURE PROBE CONNECTOR PLUG LOOSE AND CONTAMINATED.
- [SDR AU001231](https://openairdocs.org/sdr/AU001231.md): O-Ring · split · Dec 24, 2000 · Fokker F28MK0100 · Hydraulic System, Main
  > (AUS) NR 1 HYDRAULIC SYSTEM PRESSURE SWITCH O-RING SEAL SPLIT.
- [SDR AU001232](https://openairdocs.org/sdr/AU001232.md): Computer · faulty · Dec 17, 2000 · Fokker F28MK0100 · Stall Warning System
  > (AUS) STALL PROTECTION COMPUTER FAULTY.
- [SDR 99ZZZX2069](https://openairdocs.org/sdr/99ZZZX2069.md): Seal · failed · Apr 14, 1999 · Fokker F27MK100 · Turbine Section
  > THE 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 NO

## 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 = 'TAY62015'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/roll-royc-tay-620-15/reports

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