Rolls-Royce DART-532-7R

Service difficulty reports · 25

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 = 'DART5327R'
  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 COEA0802703Alternator · failedRETURN 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.Mar 19, 2008 · N703FE · Fokker F27MK600 · AC Generation SystemSDR COEA0801702Gyro · failedRETURN 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 CMar 14, 2008 · N702FE · Fokker F27MK600 · Attitude Gyro and Indicating SystemSDR COE2005F00002Inverter · inoperativeDEPARTURE, 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 SERVOct 3, 2005 · N741FE · Fokker F27MK600 · AC InverterSDR COE2005F00000Wire Harness · inoperativeNR 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 WAJan 20, 2005 · N741FE · Fokker F27MK600 · Engine Indicating System WiringSDR COE2004F00001Alternator · failedON 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.Nov 3, 2004 · N702FE · Fokker F27MK600 · AC Generation SystemSDR COE2004F00000Control Panel · failedAFTER 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.Mar 4, 2004 · N741FE · Fokker F27MK600 · DC Generating SystemSDR MTNA20032Propeller · malfunctionedIN 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.Apr 2, 2003 · N728FE · Fokker F27MK500 · Propeller Feathering/ReversingSDR AU000155Compressor · failed(AUS) LH ENGINE DRIVEN PNEUMATIC COMPRESSOR FAILED. OIL LINE FOUNDBROKEN AT BRAZED FITTING.Mar 23, 2000 · Fokker F27MK600 · Pneumatic Distribution SystemSDR 99ZZZX2119Skin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON EXTERIOR SKIN STA 1050 - STA 1070, STR 29R.Mar 25, 1999 · N76753 · Boeing 727227 · Fuselage Main, Plate/SkinSDR AU990148Seal · failed(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.Feb 11, 1999 · Fokker F27MK600 · Turbine Engine Accessory DriveSDR COEA9901701Engine · failedEN 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 OJan 14, 1999 · N701FE · Fokker F27MK600 · Engine (Turbine/Turboprop)SDR AU980886Driveshaft · failed(AUS) RIGHT ENGINE GEARBOX DRIVESHAFT FAILED AT THE FORWARD UNIVERSAL JOINT DAMAGING THE ENGINE `W' STRUT AND NR 1 AND NR 2 COMBUSTION CHAMBERS.Jul 23, 1998 · Fokker F27MK600 · Turbine Engine Accessory DriveSDR 98ZZZM565Line · looseDURING CRUISE, LEFT GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED. (M)Jul 10, 1998 · N284MA · Fokker F27MK500 · Turbine Engine Oil SystemSDR AU981017Switch · leaking(AUS) NR 2 ENGINE PROPELLER CONTROL UNIT PRESSURE SWITCH LEAKING OIL.Jul 1, 1998 · Fokker F27MK600 · Propeller Controlling SystemSDR 98ZZZX2571Combustion Can · crackedDURING 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 FRJun 21, 1998 · N284MA · Fokker F27MK500 · Turbine Engine Combustion SectionSDR AU971553Transceiver · failed(AUS) RADAR TRANSMITTER/RECEIVER FAILED.Dec 10, 1997 · Fokker F27MK600 · Weather Radar SystemSDR COEA9701701Engine · failedUPON 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 SDec 1, 1997 · N701FE · Fokker F27MK600 · Engine (Turbine/Turboprop)SDR 97ZZZM1065Turbine Blade · brokenTHE 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 SEPARATEDSep 10, 1997 · N280EA · Fokker F27MK600 · Turbine SectionSDR COEA9702740Oil Seal · wornAFTER 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 SHJul 17, 1997 · N740FE · Fokker F27MK600 · Turbine Engine Accessory DriveSDR COEA9701740B Nut · looseAFTER 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, AJul 16, 1997 · N740FE · Fokker F27MK600 · Turbine Engine Accessory DriveSDR 97ZZZX2093Fuel Pump · shaft shearedON 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.Apr 29, 1997 · N709FE · Fokker F27MK500 · Engine Fuel PumpSDR 97ZZZX2094Engine · damagedEWR/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 WFeb 6, 1997 · N721FE · Fokker F27MK500 · Turbine SectionSDR 96ZZZX5461Drive Shaft · shearedGRR - 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 Apr 17, 1996 · N718FE · Fokker F27MK500 · Turbine Engine Accessory DriveSDR 96ZZZX458Gearbox · failedRIC - 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 TEMPJan 12, 1996 · N722FE · Fokker F27MK500 · Turbine Engine Reduction GearSDR 96ZZZX185Bearing · failedCREW 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 ROLOct 9, 1995 · N2FOR · Fokker F27MK600 · Turbine Engine Compressor Section
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