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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AALA20040937Battery Pack · dischargedFORWARD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR 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.SDR 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 PSDR 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 INTESDR 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 DELIVERSDR 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 ARESDR AUS20040509Valve · faulty(AUS) LT BLEED AIR VALVE FAULTY.SDR AUS20040370Tank · corroded(AUS) RT WING FUEL SYSTEM COLLECTOR TANK CONTAINED LEVEL 3 CORROSION ON LOWER INTERNAL SURFACE.SDR AUS20040371Tank · corroded(AUS) LT WING FUEL SYSTEM COLLECTOR TANK CONTAINED LEVEL 3 CORROSION ON LOWER INTERNAL SURFACE.SDR 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.SDR AUS20040381Stringer · cracked(AUS) STRINGER 68 CRACKED.SDR AUS20040346Skin · corroded(AUS) WING TRAILING EDGE CONTAINED CORROSION ON BOTH SIDES.SDR 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.SDR AUS20040348Stringer · corroded(AUS) CENTER CARGO COMPARTMENT CORRODED ON FORWARD FACE OF DOOR SILL BEAM AND LOWER SHELL STRINGERS.SDR AUS20040354Skin · corroded(AUS) RT WING TIP TRAILING EDGE CORRODED. CORROSION ALSO FOUND UNDERSTATIC DISCHARGER BASE.SDR AUS20040355Stringer · corroded(AUS) WING CENTER SECTION EXTERNAL LOWER SURFACE Z SECTION STRINGERS CONTAINED LEVEL 3 CORROSION.SDR AUS20040356Bracket · corroded(AUS) AILERON TAB BEARING BRACKET CONTAINED LEVEL 3 CORROSION.SDR AUS20040316Pump · broken(AUS) RT AFT BOOST PUMP INLET CHECK VALVE FLAP SEPARATED AT PIVOT POINT.SDR 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.SDR AUS20040301Door Frame · corroded(AUS) SERVICE DOOR FRAME CONTAINED LEVEL 3 CORROSION LOCATED AT THE BOTTOM FORWARD CORNER.SDR 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 FSDR 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).SDR AUS20040061Valve · faulty(AUS) PNEUMATIC SYSTEM SHUTOFF VALVE FAULTY. LIMITED INFORMATION PROVIDED.SDR 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.SDR 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 WSDR AUS20031284Sensor · failed(AUS) LT LANDING GEAR UPLOCK SENSOR FAILED. SEE ALSO MDR 03/1273 FOR ASSOCIATED DEFECT.SDR AUS20031273Drain Line · failed(AUS) DRAIN TUBE CONNECTION LOCATED BELOW WINDSCREEN FAILED ALLOWING WATER TO LEAK ONTO AND CONTAMINATE LANDING GEAR LOCK HANDLE SOLENOID.SDR AUS20031290Wire · damaged(AUS) FORWARD AVIONICS BAY WIRING DAMAGED. EFIS FAN CIRCUIT BREAKER FAILED AND COULD NOT BE RESET.SDR 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--SDR 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 NSDR 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 WEIGHTSDR 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 THECOMPRSDR AALA20021208Floorbeam · corrodedFLOORBEAM CAP CORRODED. BL1127L, STA 3845-4850. REMOVED AND REPLACED TEE-CAP, STA 4175-4575.SDR AALA20021207Floorbeam · corrodedFLOORBEAM CAP CORRODED. (PL600L, STA 3845-4850). CUTOUT CORROSION, INSTALLED FLOORBEAM CAP STA 4175-4575 PER AARD.SDR AALA20021206Floorbeam · corrodedFLOORBEAM, BL600R, CAP CORRODED, STA 3845-4850. CUTOUT CORROSION, INSTALLED FLOORBEAM CAP 3845-4850 PER SRM.SDR AALA20021205Floorbeam · corrodedFLOORBEAM CAP CORRODED BLO, STA 4610-4710. CUTOUT CORROSION, INSTALLED STRAP AND DOUBLER IAW AARD.SDR AALA20021204Fitting · corrodedFORWARD GIRT BAR BLOCK FITTING CORRODED AT FORWARD ENTRY. STA3850 FLOORBEAM 1420L. REMOVED AND REPLACED GIRT BAR BLOCK FITTING IAW SRM.SDR 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 OPERASDR 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.SDR USA2002F00077Wire · brokenMAINTENANCE FOUND THE EMERGENCY LIGHT ON SEAT ROW 13 ABC INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT ROW 13 ABC. OPERATIONAL CHECK NORMAL.SDR 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.SDR 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. REPLASDR 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.SDR 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.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.SDR 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.SDR 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 FAILSDR 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.SDR 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 ASSOCSDR 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.
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