Rolls-Royce TAY-650-15

Service difficulty reports · 164

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 = 'TAY65015'
  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 JBXA000211Connector · dirtyFLT 7 RDU/BOS - NR 1 ENG TGT INDICATES LARGE FLUCTUATIONS IN ALL PHASES OF FLIGHT. FUEL FLOW ON NR 1 INDICATES 300 - 400 LBS HIGHER THAN NR 2 ON HIGH POWER SETTINGS. CLEANED TGT TEST PORT CANNON PLUG IAW F100 MM 77-45-00. PERFORMED ENGINE POWER RUN IAW F1Nov 2, 2000 · N104ML · Fokker F28MK0100 · Engine Temperature Indicating SystemSDR JBXA000208Shaft · shearedNR 1 ENGINE WOULD NOT SPOOL BEYOND 10 PERCENT N2. REPLACED NR 1 STARTER IAW AMM 80-11-01,OPS CK BAD. SHEARED STARTER SHAFT. NR 1 ENGINE GEARBOX JAMMED. REMOVED AND REPLACED NR 1 ENGINE IAW MIDWAY WORK PACKAGE WORK CARD F4604, LEAK AND OPS CK GOOD.Oct 18, 2000 · N108ML · Fokker F28MK0100 · Starter-GeneratorSDR USAAF00073Engine · failedIND - FLT 1193 - EN ROUTE PHL-MCI, THE NR 2 ENGINE SHUT DOWN IN CRUISE FLIGHT, AT FL 350 AND .72 MACH. THE ATTEMPT TO RESTART THE ENGINE WAS UNSUCCESSFUL. AN EMERGENCY WAS DECLARED, AND THE FLIGHT WAS DIVERTED TO IND, WHERE IT LANDED WITHOUT INCIDENT. TOTALOct 1, 2000 · N896US · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR JBXA0000194Engine · overtempABORTED TAKEOFF FLL, NR 2 ENGINE TGT WARNING TEMP WAS APPROX 875 PULLED BACK THRUST LEVERS TO 1.5 EPR TO ALLOW TGT TO DECREASE TO BELOW 735. PERFORMED OVER TEMPERATURE INSPECTION OF NR 2 ENGINE IAW AMM 71-00-00, NO DEFECTS NOTED.Aug 6, 2000 · N104ML · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR USAAF00016Engine · malfunctionedCLE-CLT - FLT 2173, AT FL270, NEAR CLT, THE CREW GOT A HIGH VIBRATION MESSAGE FOR THE NR 2 ENGINE. THE POWER WAS REDUCED TO IDLE AND BROUGHT BACK UP TO SEE IF THE VIBRATION WOULD GO AWAY. NO CHANGE. THE CAPTAIN THEN DECLARED AN EMERGENCY. THE FLIGHT LANDEDFeb 18, 2000 · N861US · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR AALA991992Fuel Transfer · malfunctionedSDF - FLT 1827 - SHORTLY AFTER TAKEOFF, CENTER FUEL TANK FUEL OF APPROXIMATELY 700 POUNDS WENT TO ZERO POUNDS. RIGHT WING TANK READING 700 POUNDS HIGHER THAN LEFT. SLIGHT FUEL SMELL IN COCKPIT. ACCOMPLISHED AUTOMATIC AND MANUAL CENTER FUEL AUTOFEED. COULD Dec 30, 1999 · N1401G · Fokker F28MK0100 · Engine Fuel DistributionSDR JBXA9900128Transducer · failedFLT 9 RDU - BOS, ON TAKEOFF AT APPROX 75 KTS HAD LIFT DUMPER FAULT ON LEFT MFDU. ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED OPS CHECK OF PSEU, NO FAULT NOTED. LIFT DUMPERS CHECKED GOOD IAW AMM 31-41-01. REMOVED AND REPLACED NR 4 WHEEL SPEED TRANSDUCERDec 13, 1999 · N109ML · Fokker F28MK0100 · Drag Control SystemSDR JBXA9900127Transducer · failedRDU - LIFT-DUMPER UNSAFE FAULT ON LEFT MFDU AT 75 KTS (ABORTED TAKEOFF). REMOVED AND REPLACED RT INBOARD WHEEL SPEED SENSOR (TRANSDUCER) IAW F-100 AMM 32-45-02. OPERATIONAL TEST GOOD.Dec 2, 1999 · N103ML · Fokker F28MK0100 · Drag Control SystemSDR AALA991093Air Flow Control · defectiveJFK - FLT 763 - DURING TAKEOFF ISP/ORD, NR 2 ENGINE FAILED. ENGINE WAS RESTARTED IN-FLIGHT. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED JFK WITHOUT INCIDENT. REPLACED AIR FLOW CONTROL REGULATOR ON NR 2 ENGINE. ALSO REPLACED NR 2 ENGINE FUEL FLOW REGULATOR AJul 23, 1999 · N1407D · Fokker F28MK0100 · Fuel Controlling SystemSDR USAAF99006Engine · lightning strikePIT - FLT 717 - DURING DESCENT INTO PIT, AT AN ALTITUDE OF 7,000 FEET, THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. NUMEROUS FAULT MESSAGES ILLUMINATED. THE RIGHT ENGINE OIL PRESSURE INDICATOR DROPPED TO ZERO. AT THIS TIME, THE CREW MOVED THE RIGHT ENGINE THRJan 18, 1999 · N855US · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR USAAF00002Engine · vibrationIND-PIT - FLT 430 - ON DESCENT, ENGINE 1 HIGH VIBRATION CAUTION WAS INDICATED ON THE MFDU. VIBRATION FELL WITHIN LIMITS ONCE THRUST LEVER WAS RETARDED TO THE IDLE POSITION. AN EMERGENCY WAS DECLARED FOLLOWED BY AN UNEVENTFUL LANDING. THE ENGINE WAS NOT SHUTJan 3, 1999 · N851US · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR CA990430052Shaft · worn(CAN) AIRCRAFT RETURNED TO DEPARTURE POINT AFTER HIGH ENGINE VIBRATIONS. MAINTENANCE CONFIRMED VIBRATIONS AT 0.5 IPS STARTING AT 57 PERCENT UP TO TAKEOFF POWER. ENGINE DISASSEMBLY FOUND WEAR ON THE HP TURBINE SHAFT SPLINES END FACES, WHICH ALLOWED THE HP TUDec 28, 1998 · Turbine SectionSDR CA990430055Bevel Gear · stripped(CAN) ON CLIMB-OUT AT FL 220, THE NR 2 ENGINE GENERATOR LIGHT CAME ON AND THE ENGINE SURGED, THE ENGINE THEN ROLLED BACK TO IDLE FOR 3-5 SECONDS BEFORE FLAMING OUT. THE ENGINE WAS SECURED AND THE AIRCRAFT DIVERTED. POST-FLIGHT AN ENGINE START WAS ATTEMPTED Dec 28, 1998 · Turbine Engine Accessory DriveSDR JBXA970015Lift Dumper · failedLIFT DUMPER FAULTED ON TAKEOFF. INSPECTED AND DEFERRED AS PER DMI NR 0423 RELEASED PER MEL NR 27-63-1.May 4, 1997 · N103ML · Fokker F28MK0100 · Drag Control System
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