Rolls-Royce TAY-650-15

Service difficulty reports · 164

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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 AU510001833Fan Blade · damagedENGINE LP FAN BLADE CONTAINED NICKS IN THE LEADING EDGE. THE DAMAGE WAS BLENDED OUT AND AN EDDY CURRENT INSPECTION IS DUE WITHIN 50 HOURS. INVESTIGATION CONTINUING.Sep 9, 2005 · Fokker F28MK0100 · Turbine Engine Compressor SectionSDR AU510001972Drive Shaft · shearedNR 1 ENGINE STARTER DRIVESHAFT SHEARED. SUSPECT CAUSED BY ERRATIC PRESSURE PULSES FROM APU AIR SUPPLY.Aug 10, 2005 · Fokker F28MK0100 · Engine StarterSDR AU510001973Thermocouple · brokenAPU AIR SUPPLY ERRATIC WITH PULSES CAUSING FAILURE OF THREE AIRSTARTERS. INVESTIGATION FOUND APU THERMOCOUPLE BREAKING DOWN.Aug 10, 2005 · Fokker F28MK0100 · APU Indicating SystemSDR AU510001834Pump · obstructedRT ENGINE ENVIRONMENTAL DRAIN TANK EJECTOR PUMP BLOCKED.Aug 9, 2005 · Fokker F28MK0100 · Engine Fuel DistributionSDR AU510001438Relay · failed(AUS) EMERGENCY INVERTER SYSTEM TRANSFER RELAY FAILED.(OTHER CAUSE: MATERIAL ) (CASA# 510001438)Aug 6, 2005 · Fokker F28MK0100 · AC InverterSDR AU510001515Skin · lightning strikeLIGHTNING STRIKE ON FUSELAGE WITH EXIT HOLE FOUND IN RT ELEVATOR TRAILING EDGE.Aug 6, 2005 · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR AU510001516Relay · faultyNR 2 THRUST REVERSER RELAY FAULTY.Aug 6, 2005 · Fokker F28MK0100 · Engine Thrust ReverserSDR AU510001517Pseu · faultyPROXIMITY SYSTEM ELECTRONIC UNIT (PSEU) INTERMITTENT OPERATION.Aug 6, 2005 · Fokker F28MK0100 · Landing Gear Position and WarningSDR AU510001961Drive Shaft · sheared(AUS) NR 2 ENGINE AIR STARTER DRIVESHAFT SHEARED. (OTHER CAUSE: AWAITING STRIP REPORT ) (CASA NR 510001961)Jul 10, 2005 · Fokker F28MK0100 · Engine StarterSDR AU510001963Drive Shaft · shearedNR 2 ENGINE AIR STARTER DRIVE SHAFT SHEARED.Jul 10, 2005 · Fokker F28MK0100 · Engine StarterSDR AU510002219Control System · faultyELEVATOR CONTROL SYSTEM MESSAGE ON MULTI FUNCTION DISPLAY UNIT (MFDU).May 12, 2005 · Fokker F28MK0100 · Elevator Control SystemSDR AU510001953Gcu · failedNR 2 GENERATOR CONTROL UNIT (GCU) FAILED. NR 2 GENERATOR TRIPPED OFF LINE.May 10, 2005 · Fokker F28MK0100 · AC RegulatorSDR AU510001959Bolt · incorrect(AUS) LT LIFT DUMPER ACTUATOR NR 3 AND NR 4 ATTACHMENT BOLTS NOT LOCKWIRED. PERSONNEL/MAINTENANCE ERROR. (CASA NR 510001959)May 10, 2005 · Fokker F28MK0100 · Drag Control ActuatorSDR AU510002102Pseu · faultyPROXIMITY SENSING ELECTRONIC UNIT (PSEU) FAULTY.Apr 11, 2005 · Fokker F28MK0100 · Landing Gear Position and WarningSDR AU510001544Windshield · crackedNR 1 WINDSHIELD CRACKED. CRACK ORIGINATES NEAR ELEMENT.Apr 7, 2005 · Fokker F28MK0100 · Flight Compartment WindowsSDR AU510001513Trim Switch · faultyNR 2 TRIM SWITCH FAULTY.Apr 6, 2005 · Fokker F28MK0100 · Autopilot SystemSDR AU510001974Trim Switch · faultySTABILIZER TRIM SWITCH INTERMITTENT DUE TO FAULTY WIRE TERMINATION.Mar 10, 2005 · Fokker F28MK0100 · Stabilizer Position IndicatingSDR AU510001542Display · faultyMULTI FUNCTION DISPLAY UNIT (MFDU) SUSPECT FAULTY.Mar 7, 2005 · Fokker F28MK0100 · Central ComputersSDR CA050302001Windshield · cracked(CAN) DURING ENROUTE, THE CAPTAIN OBSERVED HIS SIDE WINDSHIELD ASSY WAS CRACKED. THE AIRCRAFT WAS DIVERTED AND LANDED WITHOUT INCIDENT. THE CAPT'S SIDE WINDSHIELD ASSY WAS REPLACED IAW MM 56-11-00. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT.Mar 1, 2005 · Fokker F28MK0100 · Flight Compartment WindowsSDR CA050301007A/C Pack · smoke(CAN) WHILE AT CRUISE, THE CABIN CREW INFORMED THE FLIGHT DECK THERE WAS SMOKE IN THE CABIN. THE AIRCRAFT MADE AN UNSCHEDULED LANDING RETURNING TO BASE AND LANDED WITHOUT INCIDENT. NR 2 PACK WAS TURNED OFF AND SMOKE DISSIPATED. MAINTENANCE OPERATED THE NR 2Feb 25, 2005 · Fokker F28MK0100 · Cabin Cooling SystemSDR CA050225001Gasket · damaged(CAN) DURING CLIMB, THE CREW OBSERVED NR1 ANTI-ICE INDICATION FOLLOWED BY A BLEED DUCT FAULT. THE AIRCRAFT MADE AN UNSCHEDULED LANDING WITHOUT INCIDENT. THE ORIGINAL SNAG WAS CLEARED WITH NO FAULT FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE WITH THE SNAG RFeb 21, 2005 · Fokker F28MK0100 · Engine Bleed Air SystemSDR CA050218007Switch · inoperative(CAN) DURING CLIMB, NR1 ENGINE BLEED FAULT ILLUMINATED. AT CRUISE, THE BLEED WAS RESET RESULTING IN THE SAME BLEED DUCT LEAK ALERT. THE AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. MAINTENANCE REPLACED THE LT SHROUD OVERHEAT SWITCH IAW MM 36-11-11 AND TESTEDFeb 16, 2005 · Fokker F28MK0100 · Bleed Air Indicating SystemSDR CA050214004Engine · smoke(CAN) DURING PUSH BACK, SMOKE WAS OBSERVED IN THE CABIN AREA WHILE ENGINES WERE BEING STARTED. THE AIRCRAFT RETURNED TO THE GATE. ENGINE STARTS WERE CARRIED OUT AT THE GATE AND THE SMOKE WAS NO LONGER OBSERVED IN THE CABIN. DE-ICING FLUID WAS SUSPECTED. NOFeb 11, 2005 · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR AU510002106Pump · low pressureNR 1 CENTER WING TANK BOOST PUMP LOW PRESSURE.Feb 11, 2005 · Fokker F28MK0100 · Fuel Boost PumpSDR CA050209003Indicator · failed(CAN) DURING TAXI, THE CREW OBSERVED THE WING ANTI-ICE FAIL LIGHT CAME ON WITH THE ENGINE ANTI-ICE SELECTED ON. THE AIRCRAFT RETURNED TO THE GATE. MAINT PERFORMED THE CONTROL UNIT BITE TEST. THE OPERATIONAL TEST WAS CARRIED OUT IAW MM 30-11-00 WITH NO FAULTFeb 7, 2005 · Fokker F28MK0100 · Bleed Air Indicating SystemSDR CA050208005Control Unit · failed(CAN) DURING TAKE-OFF, THE CREW OBSERVED NR2 ELEVATOR FAULT, LEVEL 3 ALERT ON THE MFDS. THE CREW INITIATED A REJECTED TAKE-OFF SUCCESSFULLY AND RETURNED TO THE GATE. MAINTENANCE CONFIRMED THE ELEVATOR BOOSTER CONTROL UNIT WAS SUSPECT. THE UNIT WAS REPLACED AFeb 6, 2005 · Fokker F28MK0100 · Elevator Control SystemSDR CA050201006Windshield · cracked(CAN) DURING FLIGHT IT WAS OBSERVED THE RT WINDSHIELD OUTER PANE WAS CRACKED. CREW INITIATED QRH PROCEDURES AND FLIGHT WAS CONTINUED. AIRCRAFT LANDED WITHOUT INCIDENT. RT WINDSHIELD WAS REPLACED IAW MM 56-11-00. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHTJan 30, 2005 · Fokker F28MK0100 · Flight Compartment WindowsSDR CA050125005Apu · smoke(CAN) AFTER START SEQUENCE AND COMMENCE TAXI, THE CABIN CREW OBSERVED A LIGHT SMOKE COMING THROUGH THE AIR VENT. THE APU WAS SHUTDOWN WHICH SEEMED TO DISSAPATE THE SMOKE. AS A PRECAUTION THE AIRCRAFT RETURNED TO THE GATE AND PASSENGERS DISEMBARKED. MAINTENAJan 24, 2005 · Fokker F28MK0100 · APU Bleed Air SystemSDR CA050125004Line · burst(CAN) IT WAS OBSERVED BY THE FLIGHT ATTENDANTS THAT A WATER LEAK WAS FOUND COMING FROM THE FWD GALLEY AREA. THE MANUAL SHUT-OFF VALVE WAS CLOSED BUT THE LEAK WAS STILL OBSERVED. THE AIRCRAFT RETURNED TO THE GATE AND A WATER LINE UNDER THE FWD GALLEY HAD BURSJan 23, 2005 · Fokker F28MK0100 · Potable Water SystemSDR CA050124003Motor · contaminated(CAN) DURING CLIMB, IT WAS REPORTED BY THE CREW THAT ELEVATOR PITCH CONTROL WAS VERY HARD TO OPERATE. THE AUTO PILOT WAS DISENGAGED AND IN MANUAL OPERATION IT WAS STILL VERY HARD TO OPERATE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT.Jan 20, 2005 · Fokker F28MK0100 · Elevator Control SystemSDR CA050119005Computer · failed(CAN) DURING CLIMB, IT WAS OBSERVED THAT THE MFDS FAILED. FLIGHT WARNING COMPUTER WAS SUSPECTED. AIRCRAFT RETURNED TO BASE AND LANDED WITHOUT INCIDENT. THE FLT WARNING COMPUTER WAS REPLACED AND CHECKED SERVICEABLE IAW MM 31-51-00. THERE WAS NO PROBLEM WITHJan 17, 2005 · Fokker F28MK0100 · Integrated Flight SystemSDR CA050119006Display · failed(CAN) DURING CLIMB, IT WAS OBSERVED THAT THE NR1 AND NR2 EMUX SINGLE CHANNELS FAILED. THE AIRCRAFT RETURNED TO BASE AND LANDED WITHOUT INCIDENT. THE NR1 AND NR2 MAIN FLIGHT DISPLAY UNITS WERE REPLACED AND CHECKED SERVICEABLE IAW MM 31-61-01. NO FURTHER INCIDJan 17, 2005 · Fokker F28MK0100 · Integrated Flight SystemSDR AU510001807Indicator · faultySTANDBY ARTIFICIAL HORIZON (AH) FAULTY. AH HAS A SLIGHT TILT TO THE LEFT.Jan 9, 2005 · Fokker F28MK0100 · Attitude Gyro and Indicating SystemSDR AU510001533Pushrod · crackedNR 1 RT INBOARD LIFT DUMPER BELLCRANK PUSHROD CRACKED IN TWO PLACES.Jan 7, 2005 · Fokker F28MK0100 · Drag Control SystemSDR AU510001541Target · debondedRT MLG LWR TOGGLE TARGET PARTIALLY DISBONDED. LANDING GEAR WAS BEING FITTED TO A/C AFTER BEING IN STORAGE FOR SEVERAL YEARS.Jan 7, 2005 · Fokker F28MK0100 · Landing Gear Position and WarningSDR AU510001549Bearing · wornLIFT DUMPER ACTUATOR RODEND BEARING WORN.Jan 7, 2005 · Fokker F28MK0100 · Drag Control SystemSDR AU510001512Solenoid · stickingNR 2 ENGINE THRUST REVERSER SECONDARY LOCK SOLENOID BINDING IN LAST 2MM (0.078IN) OF TRAVEL.Jan 6, 2005 · Fokker F28MK0100 · Engine Thrust ReverserSDR AU510001514Display · faultyMULTI FUNCTION DISPLAY UNIT (MFDU) FAULTY.Jan 6, 2005 · Fokker F28MK0100 · Central DisplaySDR CA050104001Packing · failed(CAN) HYDRAULIC SYSTEM NR 1 FAILED IN FLT (AFTER TAKE OFF), LOW QUANTITY. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO PLACE OF DEPARTURE. MAINTENANCE FOUND THAT THE HYDRAULIC SYSTEM FAILURE WAS CAUSED BY A PACKING FAILURE OF THE THERMAL RELIEF VALVE Jan 3, 2005 · Fokker F28MK0100 · Hydraulic System, MainSDR CA041231002Line · burst(CAN) AFTER TAKE OFF, COULD NOT GET AIRCRAFT TO PRESSURIZE. AIRCRAFT LANDED BACK TO DEPARTURE AIRPORT. MAINTENANCE FOUND BOTH PRIMARY AND SECONDARY OUTFLOW VALVES AND OUTFLOW VALVE DRAIN LINE CONTAMINATED WITH ICE. WATER CAME FROM POTABLE WATER SYSTEM. A Dec 30, 2004 · Fokker F28MK0100 · Potable Water SystemSDR CA041224009Fuel Sys · malfunctioned(CAN) AFTER DEPARTURE DURING CRUISE, A FUEL UNBALANCE WAS NOTICED AND LEAK SUSPECTED FROM NR 1 ENGINE. ENGINE NR 1 WAS SECURED AND AIRCRAFT LANDED BACK TO DEPARTURE AIRPORT. BOTH ENGINES WERE RAN AND NO LEAK WAS FOUND. THE AUTO FEED SYSTEM WAS PUT INOPERATIDec 23, 2004 · Fokker F28MK0100 · Aircraft Fuel Distribution SystemSDR CA041216002Connector · burned(CAN) FOLLOWING A DISCREPANCY WITH THE LAVATORY DRAINING, MAINTENANCE FOUND THE HEATER ASSY FOR STATIC VENTILATION (REAR DRAIN MAST) NOT WORKING. ONE OF THE 2 CONNECTORS AT THE HEATER WAS FOUND BURNED. THE INSULATION BLANKET AROUND THE HEATER WAS FOUND CARBDec 13, 2004 · Fokker F28MK0100 · Water Line Anti-Ice SystemSDR CA041207005Line · leaking(CAN) DURING CLIMB, CANNOT PRESSURIZE ACRFT. ACRFT RETURNED TO DEPARTURE AIRPORT. MX FOUND CABIN AIR FILTER FOR OUTFLOW VALVES FULLY ICE COVERED DUE TO POTABLE WATER TANK LINE LEAKING AND DRIPPING OVER FILTER. FILL WATER LINE FITTING AT THE TANK CONNECTION TDec 2, 2004 · Fokker F28MK0100 · Potable Water SystemSDR CA041129013Sensor · malfunctioned(CAN) NOV 25TH 2004, AIRCRAFT HAD A STALL COMPUTER FAULT, MFDU MESSAGE ON TAKEOFF ROLL. REJECTED THE TAKEOFF AT 90 KTS INDICATED. A DMI (DEFERRED MAINTENANCE ITEM) 14809 WAS RAISED IAW MEL 27-35-3, FOR A STALL WARNING COMPUTER TO BE REPLACED, IT WAS REPLACENov 25, 2004 · Fokker F28MK0100 · Stall Warning SystemSDR CA041124005Windshield · cracked(CAN) NOV 23RD 2004, RT FLIGHT OFFICER WINDSHIELD CRACKED IN FLIGHT DURING CLIMB. AIRCRAFT C/OUT AN AIR TURN BACK. MAINTENANCE REPLACED THE WINDSHIELD (P/NOFF, D20543-406, S/N OFF, 01303H2172 - P/N ON D20543-406, S/N ON 04198H1107) IAW AMM 56-11-00.Nov 23, 2004 · Fokker F28MK0100 · Flight Compartment WindowsSDR CA041124004Proximity Switch · faulty(CAN) AC DIVERTED, AFTER HAVING A HYDR STAB NR 1 FAULT IN FLIGHT (LOST FAULT ON LANDING). MAINT C/OUT A HYDR CONTROL STABILIZER OPS CHECK IAW AMM 27-42-01, NO FAULT FOUND. ON FOLLOWING FLIGHT, SAME MESSAGE REAPPEARED ON THE MSDS (MULTI FUNCTIONAL DISPLAY SYNov 21, 2004 · Fokker F28MK0100 · Stabilizer Control SystemSDR CA041122010Indicator · inoperative(CAN) PILOT DECLARED AN EMERGENCY LANDING BECAUSE HE HAD NO GREEN LIGHT ON HIS LANDING INDICATOR, BUT HAD NO MESSAGE ON MFDU, THAT THE GEAR WAS UNSAFE. NOTE: IN REFERENCE TO THE QRH (QUICK REFERENCE HANDBOOK, ABNORMAL PROCEDURES,6.09 PAGE2, THE FLIGHT CREW WASNov 19, 2004 · Fokker F28MK0100 · Landing Gear Position and WarningSDR CA041122009Engine · vibration(CAN) AIRCRAFT ENCOUNTERED HI VIBRATION IN CLIMB ON NR2 ENGINE GAUGE, MFDS MESSAGE ALERT (REF JOURNEY LOG PAGE 031117). UNABLE TO MAINTAIN THRUST. THRUST WAS REDUCED BY .15 TO CLEAR ALERT. AIRCRAFT RETURNED TO BASE. MAINTENANCE TROUBLESHOT IAW AMM 71-00-0Nov 18, 2004 · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR CA040917002Autothrottle Sys · malfunctioned(CAN) DURING CLIMB, AIRCRAFT HAD NR 2 AUTO THROTTLE (A/T) AFCAS FAULT, FOLLOWED BY NR 1 AND 2 STAB TRIM DOUBLE CHANNEL IN FAULT. AIRCRAFT LANDED BACK TO DEPARTUREAIRPORT. THE A/T DEFECT WAS DISPATCHED AS PER MEL AND RECTIFIED THE DAY AFTER B Y ADJUSTING THE Sep 15, 2004 · Fokker F28MK0100 · Auto Throttle SystemSDR CA040914007Landing Gear · out of position(CAN) MAIN GEAR UNSAFE APPEARED ON MFDS AFTER GEAR RETRACTION. AIRCRAFT LANDED BACK TO DEPARTURE AIRPORT. MAINTENANCE FOUND THE LANDING HYDRAULIC TEST VALVE LT IN (GROUND ONLY) POSITION. THE VALVE WAS LEFT IN THAT POSITION FOLLOWING A GEAR RETRACTION/EXTENSSep 13, 2004 · Fokker F28MK0100 · Main Landing Gear
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