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 AALA20040937Battery Pack · dischargedFORWARD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION.Sep 6, 2004 · N1421K · Fokker F28MK0100 · Emergency LightingSDR CA040826001Frame · cracked(CAN) DURING INSPECTION, AD 2001-21-04 WAS PERFORMED ON FUSELAGE FRAME STRIPS AT STA 3820 THRU STA 3870 AT THE AFT SIDE OF THE NLG BAY IAW NDTM PART 6 AND AD2001-21-04. 2 CRACKS WERE FOUND, RT 0.650 LONG AND LT 0.600 INCH LONG.Aug 24, 2004 · Fokker F28MK0100 · Fuselage Main, FrameSDR CA040827005Connector · misinstalled(CAN) DURING TAKE OFF, TOWER REPORTED VAPOR TRAILING FROM WING. AC BACK FROM DEPARTURE. APROX 2000 LBS OF FUEL LOST. MAINT FOUND AUTO FEED SYS IN FAULT, CAUSING FUEL FROM CENTER TANK TRANSFERRED TO WING. A CONNECTOR AT REAR SPAR FOR PILOT VALVE FOUND NOT PAug 23, 2004 · Fokker F28MK0100 · Engine Fuel and ControlSDR CA040819010Probe · unserviceable(CAN) NO AIRSPEED INDICATION ON F/O SIDE DURING T/O. T/O REJECTED. MAINTENANCE DID A PITOT/STATIC TESTED AND SYSTEM FOUND NORMAL. BOTH ADC COMPUTER INTERCHANGED FORT/S. THE FOLLOWING T/O WAS ALSO REJECTED FOR THE SAME REASON. MAINTENANCE FOUND THE RT F/O INTEAug 18, 2004 · Fokker F28MK0100 · Pitot/Static SystemSDR CA040803009Vent Line · disconnected(CAN) DEFECT WAS RECORDED, RT FUEL LEAK REPORTED FROM RT NACA FUEL VENT . THIS WAS SECOND OCCURRENCE. AFTER INSPECTION, MAINT DISCOVERED THAT FUEL VENT LINE WAS DISCONNECTED (SEPARATED) AND NOT LINED UP, (TO SHORT). PROBLEM WAS RELATED TO THE MFG NOT DELIVERJul 29, 2004 · Fokker F28MK0100 · Engine Fuel DistributionSDR CA040727002Case · damaged(CAN) UNDERWATER ACOUSTIC BEACON DK100, S/N DJ6834, HAS BEEN ALTERED TO REPLACE BATTERY, BY DRILLING HOLES IN BATTERY COVER END CAP (TO RECEIVE A SPANNER WRENCH). THIS ALTERATION HAS UNDERMINED INTEGRITY OF BEACON. REPLACEMENT BATTERY KITS SUPPLIED BY OEM AREJul 21, 2004 · Fokker F28MK0100 · Emergency Locator BeaconSDR AUS20040509Valve · faulty(AUS) LT BLEED AIR VALVE FAULTY.Jun 11, 2004 · Fokker F28MK0100 · Pneumatic Distribution SystemSDR AUS20040370Tank · corroded(AUS) RT WING FUEL SYSTEM COLLECTOR TANK CONTAINED LEVEL 3 CORROSION ON LOWER INTERNAL SURFACE.May 10, 2004 · Fokker F28MK0100 · Fuel StorageSDR AUS20040371Tank · corroded(AUS) LT WING FUEL SYSTEM COLLECTOR TANK CONTAINED LEVEL 3 CORROSION ON LOWER INTERNAL SURFACE.May 10, 2004 · Fokker F28MK0100 · Fuel StorageSDR AUS20040380Roller · mismanufactured(AUS) MAIN DOOR LOCKING ROLLER INTERNAL DIAMETER WAS TOO SMALL TO FIT OVER THE STEEL STUD IN THE DOOR FRAME. ROLLER WAS A NEW ITEM AND WAS BEING FITTED TO THE DOOR. SUSPECT FAULTY MANUFACTURE.May 10, 2004 · Fokker F28MK0100 · Landing Gear DoorsSDR AUS20040381Stringer · cracked(AUS) STRINGER 68 CRACKED.May 7, 2004 · Fokker F28MK0100 · Fuselage Main, Longeron/StringerSDR AUS20040346Skin · corroded(AUS) WING TRAILING EDGE CONTAINED CORROSION ON BOTH SIDES.May 6, 2004 · Fokker F28MK0100 · Wing Main, Frame StructureSDR AUS20040347Floorbeam · corroded(AUS) CABIN FLOOR PANEL SUPPORT BEAMS (2OFF) CORRODED. SUSPECT CAUSED BY INCORRECT REMOVAL OF FLOOR PANEL AND GAP SEALANT USING A SHARP EDGED TOOL WHICH SCORED THE BEAMS. CORROSION INITIATED AT THE SCORE MARKS. PERSONNEL/MAINTENANCE ERROR.May 6, 2004 · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR AUS20040348Stringer · corroded(AUS) CENTER CARGO COMPARTMENT CORRODED ON FORWARD FACE OF DOOR SILL BEAM AND LOWER SHELL STRINGERS.May 6, 2004 · Fokker F28MK0100 · Fuselage Main, Longeron/StringerSDR AUS20040354Skin · corroded(AUS) RT WING TIP TRAILING EDGE CORRODED. CORROSION ALSO FOUND UNDERSTATIC DISCHARGER BASE.May 6, 2004 · Fokker F28MK0100 · Wing, Plate/SkinSDR AUS20040355Stringer · corroded(AUS) WING CENTER SECTION EXTERNAL LOWER SURFACE Z SECTION STRINGERS CONTAINED LEVEL 3 CORROSION.May 6, 2004 · Fokker F28MK0100 · Wing, Center BoxSDR AUS20040356Bracket · corroded(AUS) AILERON TAB BEARING BRACKET CONTAINED LEVEL 3 CORROSION.May 6, 2004 · Fokker F28MK0100 · Aileron TabsSDR AUS20040316Pump · broken(AUS) RT AFT BOOST PUMP INLET CHECK VALVE FLAP SEPARATED AT PIVOT POINT.Apr 30, 2004 · Fokker F28MK0100 · Fuel Boost PumpSDR AUS20040300Bracket · misinstalled(AUS) LT ELEVATOR CONTROL ROD LOCK BRACKET INCORRECTLY INSTALLED AND FOULING ON LT ELEVATOR ROD CAUSING RESTRICTION IN ELEVATOR MOVEMENT. PERSONNEL/MAINTENANCE ERROR.Apr 28, 2004 · Fokker F28MK0100 · Elevator Control SystemSDR AUS20040301Door Frame · corroded(AUS) SERVICE DOOR FRAME CONTAINED LEVEL 3 CORROSION LOCATED AT THE BOTTOM FORWARD CORNER.Apr 28, 2004 · Fokker F28MK0100 · Fuselage Main, StructureSDR AUS20040291Skin · corroded(AUS) WING STRUCTURE CONTAINED LEVEL 3 CORROSION IN THE FOLLOWING AREAS: CORROSION FOUND ON FORWARD FACE OF FORWARD MAIN SPAR AT RIB STATION 129752. ACCESS PANEL Z536FB MOUNTING FLANGE HAD EVIDENCE OF SURFACE AND DEEPER CORROSION AT RIB 11974-12795. FORWARD FApr 22, 2004 · Fokker F28MK0100 · Wing, Plate/SkinSDR AUS20040152Duct · cracked(AUS) NR 2 BLEED AIR SYSTEM BIFURCATED DUCT CRACKED IN AREA OF SUPPORT ATTACHING BRACKET ADJACENT TO THE PRSOV. CRACK LENGTH APPROXIMATELY 25MM (0.984IN).Mar 2, 2004 · Fokker F28MK0100 · Pneumatic Distribution SystemSDR AUS20040061Valve · faulty(AUS) PNEUMATIC SYSTEM SHUTOFF VALVE FAULTY. LIMITED INFORMATION PROVIDED.Feb 3, 2004 · Fokker F28MK0100 · Pneumatic Distribution SystemSDR AUS20031335Brake Assy · broken(AUS) NR 1 BRAKE ASSEMBLY FAILED. INSPECTION FOUND THAT THE PISTONS HAD HOLED THE CARBON DISK PRESSURE PLATE CAUSING IT TO DELAMINATE AND THEN ALLOW THE PISTONS TO CONTACT THE FIRST ROTATING DISK R1 CAUSING SEVERE WEAR TO R1 AND THE PISTONS.Dec 29, 2003 · Fokker F28MK0100 · BrakeSDR AUS20031286Clamp · wrong part(AUS) ENGINE ANTI-ICE VALVE PIPE PN 1159P41706-7 WORN AND BROKEN BY CLAMP. CLAMP WAS INCORRECT PART PN S230SST (CORRECT CLAMP PN GC500BV04CTN). THE TEFLON SLEEVE ON THE CLAMP HAD WORN AWAY RESULTING IN METAL TO METAL CONTACT BETWEEN THE CLAMP AND PIPE WHICH WDec 22, 2003 · Fokker F28MK0100 · Air Intake Anti/De-Ice SystemSDR AUS20031284Sensor · failed(AUS) LT LANDING GEAR UPLOCK SENSOR FAILED. SEE ALSO MDR 03/1273 FOR ASSOCIATED DEFECT.Dec 16, 2003 · Fokker F28MK0100 · Landing Gear Position and WarningSDR AUS20031273Drain Line · failed(AUS) DRAIN TUBE CONNECTION LOCATED BELOW WINDSCREEN FAILED ALLOWING WATER TO LEAK ONTO AND CONTAMINATE LANDING GEAR LOCK HANDLE SOLENOID.Dec 15, 2003 · Fokker F28MK0100 · Flight Compartment WindowsSDR AUS20031290Wire · damaged(AUS) FORWARD AVIONICS BAY WIRING DAMAGED. EFIS FAN CIRCUIT BREAKER FAILED AND COULD NOT BE RESET.Dec 14, 2003 · Fokker F28MK0100 · Air Conditioning System WiringSDR AALA20031413Light · brokenDFW) EMERGENCY LIGHT FORWARD OF FORWARD SERVICE DOOR IS BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FORWARD OF FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--Dec 10, 2003 · N1425A · Fokker F28MK0100 · Emergency LightingSDR AALA20031028Regulator · failedORD - FLT 1988 - AIRCRAFT EN ROUTE XNA TO ORD, THROTTLE STUCK IN THE CRUISE POWER SETTING. EMERGENCY DECLARED AND SHUTDOWN NR 2 ENGINE PRIOR TO LANDING. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE FUEL FLOW REGULATOR. LEAK AND SYSTEM GROUND CHECKED NSep 18, 2003 · N1409B · Fokker F28MK0100 · Fuel Controlling SystemSDR AALA20030963Engine · bird ingestionSHORTLY AFTER TAKEOFF, AIRCRAFT HIT A FLOCK OF BIRDS. ENGINE NR 2 FAILED. FOLLOWED CHECKLIST, SHUTDOWN NR 2 ENGINE, AIRCRAFT HAD SEVERE VIBRATION. COMPLIED WITH PROCEDURE TO PULL FIRE HANDLE AND DISCHARGE FIRE BOTTLE. LANDED AT JFK APPROX 79,000 LBS WEIGHTSep 4, 2003 · N1450A · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR AUS20030497Cowling · bird strike(AUS) BIRDSTRIKE ON LT SIDE OF FUSELAGE NOSE CONE. INSPECTION FOUND NR 1 ENGINE INTAKE AUCOUSTIC LINER LOWER PANEL DELAMINATED. SOME SHREDDED STRANDS OF THE LINER WERE FOUND ON THE FAN BLADES ANDTHE BYPASS DUCT. A BORESCOPE INSPECTION OF ALL STAGES OF THECOMPRMay 11, 2003 · Fokker F28MK0100 · Engine Cowling SystemSDR AALA20021208Floorbeam · corrodedFLOORBEAM CAP CORRODED. BL1127L, STA 3845-4850. REMOVED AND REPLACED TEE-CAP, STA 4175-4575.Aug 21, 2002 · N1436A · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR AALA20021207Floorbeam · corrodedFLOORBEAM CAP CORRODED. (PL600L, STA 3845-4850). CUTOUT CORROSION, INSTALLED FLOORBEAM CAP STA 4175-4575 PER AARD.Aug 21, 2002 · N1436A · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR AALA20021206Floorbeam · corrodedFLOORBEAM, BL600R, CAP CORRODED, STA 3845-4850. CUTOUT CORROSION, INSTALLED FLOORBEAM CAP 3845-4850 PER SRM.Aug 21, 2002 · N1436A · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR AALA20021205Floorbeam · corrodedFLOORBEAM CAP CORRODED BLO, STA 4610-4710. CUTOUT CORROSION, INSTALLED STRAP AND DOUBLER IAW AARD.Aug 21, 2002 · N1436A · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR AALA20021204Fitting · corrodedFORWARD GIRT BAR BLOCK FITTING CORRODED AT FORWARD ENTRY. STA3850 FLOORBEAM 1420L. REMOVED AND REPLACED GIRT BAR BLOCK FITTING IAW SRM.Aug 21, 2002 · N1436A · Fokker F28MK0100 · Fuselage Main, Attach FittingsSDR AALA20021175Separator · crackedON TAKEOFF ROLL ORD, PACK ONE TEMPERATURE WENT TO 145 DEGREES. FLIGHT ATTENDANT AND PASSENGER REPORTED SMOKE IN CABIN. PACK ONE FAULTED ON OVERHEAD. RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT PACK SEPARATOR. SYSTEM GROUND CHECKED NORMAL OPERAAug 16, 2002 · N1417D · Fokker F28MK0100 · Cabin Cooling SystemSDR AALA20021176Connector · damagedDURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTING AT 11 AND 12 DIM. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING CONNECTOR AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.Aug 15, 2002 · N1430D · Fokker F28MK0100 · Light System WiringSDR USA2002F00077Wire · brokenMAINTENANCE FOUND THE EMERGENCY LIGHT ON SEAT ROW 13 ABC INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT ROW 13 ABC. OPERATIONAL CHECK NORMAL.Aug 3, 2002 · N585US · Boeing 737301 · Light System WiringSDR AALA20021079Rudder · faultyAFTER TAKEOFF BOTH STABILIZER TRIM FAULTED, BOTH YAW DAMPER AND NR 2 RUDDER SYSTEM FAULTED. STABILIZER TRIM AND YAW DAMPER WERE RESET. LANDED WITHOUT INCIDENT. REPLACED RUDDER LIMITER MONITOR. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 23, 2002 · N1427A · Fokker F28MK0100 · Stabilizer Control SystemSDR AALA20020628Engine · vibrationEN ROUTE, NR 2 ENGINE, SEVERE VIBRATION, VIBRATION HIGH NR 2 ON MFDU, CONFIRMED WITH ALTERNATE VIBRATION SWITCH. AT IDLE, VIBRATION STILL IN RED BAND OUT OF LIMITS. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. OIL AND HYDRAULIC ODORS ON TOUCHDOWN. REPLAMay 5, 2002 · N1447L · Fokker F28MK0100 · Turbine Engine Compressor SectionSDR JBXA000315Powerplant · overtemp#1 ENGINE OVERTEMPERATURE/860 DEGREE'S FARENHEIT. CORRECTIVE ACTION: PERFORMED TAY SB 77-1454 IAW TAY 77-1454. CHANGE RESISTOR AFROM CM TO CK. PERFORMED ACCEL AND DECELL CHECKS AND IGV SCHEDULING CHECK IAW TAY 71-00-00.Aug 8, 2001 · N110ML · Fokker F28MK0100 · Engine Temperature Indicating SystemSDR JBXA000297Engine · malfunctionedHIGH EGT APPROACHING REDLINE DURING TOGA TAKEOFF RDU. PEAK TGT 850 FOR 1 SECOND. PERFORMED OPS CHECK OF NR 1 ENGINE TOGA EGT IAW AMM 71-00-00, NO FAULTS NOTED EGT WITHIN LIMITS. OPS CHECK GOOD.Jun 22, 2001 · N110ML · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR AUS20010520Gearbox · making metal(AUS) LH ENGINE HIGH SPEED GEARBOX CHIP DETECTOR AND OIL FILTER CONTAMINATED WITH FINE METAL PARTICLES. FILTER DIFFERENTIAL PRESSURE POP-UP INDICATOR OPERATED.May 19, 2001 · Fokker F28MK0100 · Turbine Engine Accessory DriveSDR AUS20010499Guide Vane · out of adj(AUS) RT ENGINE VIBRATION. POWER INCREASE LED TO HIGH ITT WITH LOW N1 AND LOW EPR WITH LOW N2. INVESTIGATION FOUND THE ACCELERATION TIME SLOW DUE TO IGV SCHEDULING OUT OF ADJUSTMENT.May 10, 2001 · Fokker F28MK0100 · Turbine Engine Compressor SectionSDR USAAF01009Engine · failedPIT-TOL - FLT 841 - WHILE CLIMBING THROUGH FL180, THE CREW FELT A VIBRATION IN THE AIRCRAFT. THEN, RECEIVED A VIBRATION WARNING INDICATION FOR THE LEFT ENGINE. POWER WAS PULLED BACK ON THE LEFT ENGINE. WHILE THE POWER WAS BEING REMOVED, THE LEFT ENGINE FAILMar 19, 2001 · N893US · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR JBXA00240Blade · nickedNICK FOUND IN NR 2 ENGINE FAN BLADE ON POST FLIGHT INSPECTION. REMOVED AND REPLACED NR 2 ENGINE IAW MIDWAY AIRLINES WORKCARDS F4624 AND 4622.Feb 24, 2001 · N109ML · Fokker F28MK0100 · Turbine Engine Compressor SectionSDR CA010103009Turbine · damaged(CAN) U.S. AIRWAYS ESN 17339 WAS REMOVED FOR HIGH VIBRATION UPON STRIP. THE FOLLOWING WAS NOTED.1. HP TURBINE MIGRATED AXIALLY REARWARDS TO THE EXTENT THE HP1 TURBINE BLADE INNER PLATFORM REAR FACES CONTACTED THE HP2 NGV INNER PLATFORM FRONT FACES.2. THE ASSOCNov 24, 2000 · Turbine SectionSDR AU001106Engine · vibrates(AUS) NR 1 ENGINE VIBRATION. INSPECTION COULD FIND NO CAUSE OR DAMAGE AND IT IS SUSPECTED THAT ICE FORMATION ON THE FAN BLADES WAS THE CAUSE OF THE PROBLEM.Nov 17, 2000 · Fokker F28MK0100 · Engine (Turbine/Turboprop)
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