# Service difficulty reports: Rolls-Royce DART-532-7R

A list on [Rolls-Royce DART-532-7R](https://openairdocs.org/engine/rolls-royce-dart-532-7r.md).

Newest first. General aviation reporting is voluntary.

- [SDR COEA0802703](https://openairdocs.org/sdr/COEA0802703.md): Alternator · failed · Mar 19, 2008 · N703FE · Fokker F27MK600 · AC Generation System
  > RETURN TO BLOCKS. FLT NR7276, DURING TAXI TO THE RUNWAY, THE LT ALTERNATOR FAILED. THE AC RETURNED TO THE RAMP (BLOCKS) WITHOUT ANY FURTHUR INCIDENT. LT ALTERNATOR WAS REPLACED ON THE LT ENGINE.
- [SDR COEA0801702](https://openairdocs.org/sdr/COEA0801702.md): Gyro · failed · Mar 14, 2008 · N702FE · Fokker F27MK600 · Attitude Gyro and Indicating System
  > RETURN TO BLOCKS. FLIGHT NR 7276 ITC TO AFW. WHILE PREPAIRING FOR DEPARTURE THE CREW DISCOVERED THE CAPT HEADING AND SITUATION INDICATOR (HSI) COMPASS CARD WAS SPINNING ERRATICALLY. THE CREW REQUESTED TO RETURN TO THE RAMP, UPON WHICH TIME THE HSI COMPASS C
- [SDR COE2005F00002](https://openairdocs.org/sdr/COE2005F00002.md): Inverter · inoperative · Oct 3, 2005 · N741FE · Fokker F27MK600 · AC Inverter
  > DEPARTURE, ENROUTE, NR 1 INVERTER WENT OFF LINE AND WOULD NOT COME BACK ON. CREW REPORTED A STRONG BURNING ODOR BUT NO SMOKE. AIRCRAFT DIVERTED. THE NR 1 INVERTER CB WAS POPPED. THE NR 1 INVERTER WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERV
- [SDR COE2005F00000](https://openairdocs.org/sdr/COE2005F00000.md): Wire Harness · inoperative · Jan 20, 2005 · N741FE · Fokker F27MK600 · Engine Indicating System Wiring
  > NR 2 TGT FLUCUTATED BETWEEN 0 AND 600 DEGREES IN FLIGHT. AIRCRAFT RETURNED TO AIRPORT. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. FOUND BROKEN WIRE ON CONNECTOR PLUG BACKSHELL AT FIREWALL. ENTIRE HARNESS WAS REPLACED. AIRCRAFT WA
- [SDR COE2004F00001](https://openairdocs.org/sdr/COE2004F00001.md): Alternator · failed · Nov 3, 2004 · N702FE · Fokker F27MK600 · AC Generation System
  > ON CLIMB OUT, RT ALTERNATOR FAIL LIGHT CAME ON. AIRCRAFT RETURNED TO DEPARTURE. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT ALTERNATOR. AIRCRAFT WAS RETURNED TO SERIVCE.
- [SDR COE2004F00000](https://openairdocs.org/sdr/COE2004F00000.md): Control Panel · failed · Mar 4, 2004 · N741FE · Fokker F27MK600 · DC Generating System
  > AFTER TAKEOFF, LEFT ENGINE GENERATOR WOULD NOT CARRY A LOAD. CREW TURNED BACK WHERE MAINTNANCE WAS AVAILABLE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT GENERATOR CONTROL PANEL. AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR MTNA20032](https://openairdocs.org/sdr/MTNA20032.md): Propeller · malfunctioned · Apr 2, 2003 · N728FE · Fokker F27MK500 · Propeller Feathering/Reversing
  > IN FLIGHT FROM CRW TO LCK THE LEFT ENGINE AUTO-FEATHERED. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED UNEVENTFULLY AT LCK. THE CAUSE IS UNKNOWN AT THIS TIME.
- [SDR AU000155](https://openairdocs.org/sdr/AU000155.md): Compressor · failed · Mar 23, 2000 · Fokker F27MK600 · Pneumatic Distribution System
  > (AUS) LH ENGINE DRIVEN PNEUMATIC COMPRESSOR FAILED. OIL LINE FOUNDBROKEN AT BRAZED FITTING.
- [SDR 99ZZZX2119](https://openairdocs.org/sdr/99ZZZX2119.md): Skin · corroded · Mar 25, 1999 · N76753 · Boeing 727227 · Fuselage Main, Plate/Skin
  > DURING A C-CHECK, CORROSION WAS NOTED ON EXTERIOR SKIN STA 1050 - STA 1070, STR 29R.
- [SDR AU990148](https://openairdocs.org/sdr/AU990148.md): Seal · failed · Feb 11, 1999 · Fokker F27MK600 · Turbine Engine Accessory Drive
  > (AUS) NR 2 ENGINE AUXILIARY GEARBOX OUTPUT SHAFT SEAL LEAKING. ENGINE HAD SUFFERED A PREVIOUS AUXILIARY GEARBOX DRIVESHAFT FAILURE WHICH MAY HAVE CONTRIBUTED TO THE DEFECT.
- [SDR COEA9901701](https://openairdocs.org/sdr/COEA9901701.md): Engine · failed · Jan 14, 1999 · N701FE · Fokker F27MK600 · Engine (Turbine/Turboprop)
  > EN ROUTE TO OAK FOM YVR FLT 7525, PILOTS REPORTED HAVING A LOW TORQUE INDICATION ON NR 1 ENGINE. MAINTENANCE WAS ADVISED UPON ARRIVAL IN OAK. WHEN THE MECHANIC OPENED THE LOWER COWLING ON THE ENGINE A PIECE OF METAL THAT LOOKED LIKE A PIECE OF HOUSING FELL O
- [SDR AU980886](https://openairdocs.org/sdr/AU980886.md): Driveshaft · failed · Jul 23, 1998 · Fokker F27MK600 · Turbine Engine Accessory Drive
  > (AUS) RIGHT ENGINE GEARBOX DRIVESHAFT FAILED AT THE FORWARD UNIVERSAL JOINT DAMAGING THE ENGINE `W' STRUT AND NR 1 AND NR 2 COMBUSTION CHAMBERS.
- [SDR 98ZZZM565](https://openairdocs.org/sdr/98ZZZM565.md): Line · loose · Jul 10, 1998 · N284MA · Fokker F27MK500 · Turbine Engine Oil System
  > DURING CRUISE, LEFT GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED. (M)
- [SDR AU981017](https://openairdocs.org/sdr/AU981017.md): Switch · leaking · Jul 1, 1998 · Fokker F27MK600 · Propeller Controlling System
  > (AUS) NR 2 ENGINE PROPELLER CONTROL UNIT PRESSURE SWITCH LEAKING OIL.
- [SDR 98ZZZX2571](https://openairdocs.org/sdr/98ZZZX2571.md): Combustion Can · cracked · Jun 21, 1998 · N284MA · Fokker F27MK500 · Turbine Engine Combustion Section
  > DURING A SCHEUDLED INSPECTION, THE NR 1 COMBUSTION CAN ASSY ON THE LEFT ENGINE WAS REJECTED DUE TO AN OUTER CASING BURN-THROUGH NEAR THE AFT END. UPON CAN REMOVAL, THE FLAME TUBE WAS FOUND CRACKED 360 DEGREES AND SEPARATED APPROXIMATELY 4 INCHES - 5 INCHES FR
- [SDR AU971553](https://openairdocs.org/sdr/AU971553.md): Transceiver · failed · Dec 10, 1997 · Fokker F27MK600 · Weather Radar System
  > (AUS) RADAR TRANSMITTER/RECEIVER FAILED.
- [SDR COEA9701701](https://openairdocs.org/sdr/COEA9701701.md): Engine · failed · Dec 1, 1997 · N701FE · Fokker F27MK600 · Engine (Turbine/Turboprop)
  > UPON START OF THE NR 2 ENGINE (S/N 14211), FLIGHT CREW EXPERIENCED MODERATE VIBRATION EMANATING FROM THE ENGINE. CREW SHUT DOWN ENGINE AFTER LOW IDLE WAS ATTAINED. MAINTENANCE INVESTIGATED NR 2 ENGINE AND DISCOVERED THE LOW PRESSURE TURBINE DISK (NR 3) HAD S
- [SDR 97ZZZM1065](https://openairdocs.org/sdr/97ZZZM1065.md): Turbine Blade · broken · Sep 10, 1997 · N280EA · Fokker F27MK600 · Turbine Section
  > THE FLIGHT CREW NOTED THAT THE NR 2 ENGINE WAS RUNNING ABOVE THE NORMAL EGT AT TAKEOFF POWER. VISUAL INSPECTION OF THE ENGINES TURBINE SECTION REVEALED IMPACT DISTRESS TO THE LPT BLADES AND STATORS. BORESCOPE INSPECTION REVEALED ON IP TURBINE BLADE SEPARATED
- [SDR COEA9702740](https://openairdocs.org/sdr/COEA9702740.md): Oil Seal · worn · Jul 17, 1997 · N740FE · Fokker F27MK600 · Turbine Engine Accessory Drive
  > AFTER DEPARTURE FROM LBB, CAPTAIN REPORTS RT ENGINE GEARBOX OIL PRESSURE LIGHT ILLUMINATED. PILOT FEATHERED ENGINE AND RETURNED TO LBB. MX DISPATCHED. UPON INSPECTION, MX FOUND OIL SEAL ON THE GEARBOX SIDE OF DRIVE SHAFT HAD FAILED. MX REMOVED DRIVE SH
- [SDR COEA9701740](https://openairdocs.org/sdr/COEA9701740.md): B Nut · loose · Jul 16, 1997 · N740FE · Fokker F27MK600 · Turbine Engine Accessory Drive
  > AFTER DEPARTURE FROM LBB, PILOT REPORTED LOW PRESSURE LIGHT FOR RIGHT GEARBOX ILLUMINATED. THE CAPTAIN OBTAINED CLEARANCE AND ELECTED TO SHUT DOWN RIGHT ENGINE AND RETURN TO THE LBB AIRPORT. LANDING WAS MADE WITHOUT FURTHER INCIDENT. M/C CONTACT LBB AERO, A
- [SDR 97ZZZX2093](https://openairdocs.org/sdr/97ZZZX2093.md): Fuel Pump · shaft sheared · Apr 29, 1997 · N709FE · Fokker F27MK500 · Engine Fuel Pump
  > ON CLIMB-OUT OF LCK, THE LEFT ENGINE AUTOFEATHERED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO LCK WITH NO FURTHER PROBLEMS. THE MECHANIC FOUND A SHEARED SHAFT ON THE FUEL PUMP. THE ENGINE CHECKED GOOD IAW THE FOKKER MM AFTER THE FUEL PUMP WAS REPLACED.
- [SDR 97ZZZX2094](https://openairdocs.org/sdr/97ZZZX2094.md): Engine · damaged · Feb 6, 1997 · N721FE · Fokker F27MK500 · Turbine Section
  > EWR/YMX - EN ROUTE, THE LEFT ENGINE STARTED TO AUTOFEATHER. THE LEFT ENGINE TEMP STARTED TO RISE, THE FLIGHT CREW THEN MANUALLY FEATHERED THE PROP. THE CREW DECLARED AN EMERGENCY AND WAS CLEARED TO LAND IN ALB. THE PILOT TRIED TO RESTART THE ENGINE, BUT IT W
- [SDR 96ZZZX5461](https://openairdocs.org/sdr/96ZZZX5461.md): Drive Shaft · sheared · Apr 17, 1996 · N718FE · Fokker F27MK500 · Turbine Engine Accessory Drive
  > GRR - ON DEPARTING REACHING 5,000 FEET ALTITUDE, THE RIGHT GEARBOX OIL PRESSURE LIGHT, ALTERNATOR LIGHT, GENERATOR FAIL LIGHT CAME ON AT THE SAME TIME. THE FLIGHT CREW DID A PRECAUTIONARY ENGINE SHUT DOWN AND RETURNED TO GRR. THE AIRCRAFT LANDED WITHOUT ANY
- [SDR 96ZZZX458](https://openairdocs.org/sdr/96ZZZX458.md): Gearbox · failed · Jan 12, 1996 · N722FE · Fokker F27MK500 · Turbine Engine Reduction Gear
  > RIC - ON CLIMB-OUT, THE LEFT ENGINE INDICATED A POWER LOSS (RPM DROPPED TO 13,800 AT MAX). THE CREW DECLARED AN EMERGENCY AND RETURNED TO RIC. DURING DESCENT, LEFT GENERATOR LIGHT, LEFT ALTERNATOR LIGHT, AND LEFT GEARBOX OIL PRESSURE LIGHT CAME ON. ALL TEMP
- [SDR 96ZZZX185](https://openairdocs.org/sdr/96ZZZX185.md): Bearing · failed · Oct 9, 1995 · N2FOR · Fokker F27MK600 · Turbine Engine Compressor Section
  > CREW NOTED REDUCED TORQUE INDICATED ON TAKEOFF. CLIMB TORQUE INDICATED NORMAL. PCU AND FCU WERE CHANGED WITH NO EFFECT. WET TAKEOFF POWER NORMAL. ENGINE WAS REMOVED AND SENT TO ROLLS ROYCE CANADA. TEAR DOWN INDICATES FAILURE OF LAY SHAFT FRONT BEARING ROL

## 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 = 'DART5327R'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/rolls-royce-dart-532-7r/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.