Rolls-Royce TAY-611-8
Service difficulty reports · 213
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 = 'TAY6118' 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 = 'TAY6118' 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 CA120417020Connector · burned(CAN) BURNED WIRES WERE FOUND ON CONNECTOR PLUG 400P17 IN THE TAIL COMPARTMENT FUSE BS 603. THE WIRES IN THIS PLUG ARE FOR THE FIRE DETECTION LIGHT WARNING ON FIRE T-HANDLE. NO EVIDENCE OF FLUIDS IN THAT AREA, NO EVIDENCE OF RUBBING/CHAFING ON ANY OF THE SURSDR CA120417017Drive Shaft · gouged(CAN) DURING A ROUTINE INSPECTION THE LT AND RT OTBD FLAP DRIVE SHAFTS WERE FOUND TO HAVE GOUGES LOCATED RT WERE THEY PASS THROUGH A LIGHTNING HOLE AT RBS 230 OF IT`S RESPECTIVE WING. DRIVE SHAFTS TO BE REPLACED. UNSURE OF CAUSE.SDR CA120417018Cable · worn(CAN) DURING ELEVATOR AND RUDDER MAIN CABLE INSPECTION, ALL 4 CABLES WERE FOUND TO HAVE WEAR, BLENCHED CABLES, IN THE AREA WHERE THE CABLES RUN THROUGH GAMMA TUBES, BS 498-596, FURTHER INVESTIGATION FOUND THAT GAMMA TUBES WERE BOWING AND CAUSING CABLES TO RUB SDR DXTA2012022704888Engine · vibrationNR 1 ENGINE DISPLAYED HIGH VIBRATION, IE LP 2.25, IN FLIGHT. PRECAUTIONARY SHUTDOWN AND LANDING WITHOUT FURTHER INCIDENT. INSPECTED AIRCRAFT, NO DEFECTS NOTED.SDR AOYA2011121500001Landing Gear · malfunctionedAFTER DEPARTURE, NOSE LANDING GEAR FAILED TO RETRACT. SEVERAL ATTEMPTS TO RETRACT WERE MADE WITH NO SUCCESS. AN UNEVENTFUL NORMAL LANDING WAS MADE. AFTER LANDING, GEAR PINNED AND A VISUAL INSPECTION MADE. MAIN GEAR DOORS WERE OPEN AND THE NOSE GEAR DOORS SDR AMCR201105Tire · blisteredAFTER FLIGHT, POSTFLIGHT INSPECTION REVEALED A BLISTER ON THE SIDEWALL OF THE NR1 MAIN TIRE. THIS TIRE HAS ONLY 4 LANDINGS ON IT SINCE NEW. BLISTER WAS APPROX .5"D AND PROTUDING .7500", ABOUT 1" DOWN PAST THE CROWN OF THE SIDEWALL.SDR 2011FA0000444Wire Harness · defectiveDURING DESCENT, THE RED AND YELLOW WARNING MESSAGES DISPLAY: "L THRUST REVERSER DEPLOY" AND "LT THRUST REVERSER UNLOCK". AFTER LANDING VISUAL INSPECTION, THE LT THRUST REVERSER WAS AUTO MOVING BACK AND CAN NOT DEPLOY. DURING TROUBLESHOOTING, THE LT THRUST REVESDR 2011F00026Pump · damagedWHILE ON OUTBOUND FLIGHT, THE PILOT REPORTED LOSS OF THE COMBINED HYD PRESSURE AND FLUID; AUXILIARY PUMP TEMPORARILY FAILED, TOO. PILOT MADE UNSCHEDULED LANDING. ON GROUND, THE NR 1 ENGINE DRIVEN PUMP, FOUND WITH BLOWN-OUT GASKET CAUSING HYD LOSS AND DAMAGE SDR 2011F00022Electronic Unit · intermittentIMMEDIATELY AFTER REACHING CRUISING ALTITUDE OF FL410, THE CREW NOTICED THE LT AUTOTHROTTLE ADVANCING FOLLOWED IMMEDIATELY BY A MASTER CAUTION CHIME/LIGHT. CAS MESSAGES OF LT FUEL PRESS LOW (RED CAPTION), LT MAIN FUEL FAIL (AMBER), LT ALT FUEL FAIL (AMBER). SDR DXTA2010122304273Pump · leakingPASSING 15000 FT ON DECENT THE "CHECK HYD QUANTITY" MESSAGE ILLUMINATED AND HYD SYNOPSIS PAGE SHOWED THE FLIGHT HYD SYS QUANTITY OF ZERO. ABOUT 1 MINUTE LATER THE FLIGHT HYD PRESSURE DECREASED TO 0. AND THE FLT HYD FAIL MESSAGE ILLUMINATED. RAN APPROPRIATED CHSDR DXTA2010122004369Hydraulic System · warning lightAFTER APPROX 50 MINUTES IN FLT, DURING CRUISE AT FL 380, AMBER HYD QTY LOW CAS ILLUMINATED. HYD PAGE QTY SHOWED COMBINED QTY JUST ABOVE LOW MARK. OVER THE NEXT 50 MIN IT SLOWLY DECREASED BELOW THE LOW MARK & WENT FROM WHITE TO RED. DURING APPROACH & LANDING, SDR 2010F00230Windshield · crackedWHILE IN CRUZ THE RT WINDSHIELD OUTTER PLY CRACKED. THE CREW LANDED THE ACFT TO VERIFY IT WAS ONLY THE OUTER PLY. THE CREW THEN WROTE A DISCREPANCY AND DEFERED IT USING THE CDL FROM THE FLIGHT MANUAL 56-1 AND CONTIUED IT FLIGHT, WHERE THE WINDSHIELD WAS CHANGESDR WWQA110110Windshield · crackedWHILE IN CRUISE, THE RT WINDSHIELD OUTER PLY CRACKED. THE CREW LANDED THE ACFT AT TO VERIFY IT WAS ONLY THE OUTER PLY. THE CREW THEN WROTE A DISCREPANCY AND DEFERRED IT USING THE CDL FROM THE FLIGHT MANUAL CDL 56-1 AND CONTINUED ITS FLIGHT WHERE THE WINDSHIELSDR N93A10282010Angle · crackedDURING INSP OF ACFT FOR CONDITION SURVEY IT WAS NOTED THAT THE 793 BULKHEAD CAP ANGLE WAS CRACKED.SDR AMCR201008Mask · wrong partFOUND PORTABLE O2 MASK TO BE THE INCORRECT TYPE. EVEN THOUGH CUSTOMER BULLETIN 213 DID NOT LIST THIS ACFT IN THE EFFECTIVITY SECTION, AN INSP REVEALED THE WRONG MASK ANYWAY. ANOTHER BAD MASK WAS FOUND ON ANOTHER ACFT IN THE FLEET ALSO NOT LISTED IN THE BULLETISDR N93A07232010Oven · odorABOUT 30 MINUTES INTO FLIGHT, THE F/A TURNED THE OVEN ON TO WARM SOME BREAD. WITHIN A FEW MINUTES SHE NOTICED THE AREA HAD AN ELECTRICAL BURNING ODOR AND AN ODOR OTHER THAN BURNED FOOD. SHE ALSO STATED SHE NOTICED SMOKE INSIDE THE OVEN DOOR WINDOW. THE OVEN SDR N93A06142010Rib · corrodedDURING REMOVAL OF MLG FOR O/H, NOTED SIGNIFICANT CORROSION IN MLG ATTACH BORES OF THE LT WING SPONSON RIB.SDR N93A06142010AAttach Fitting · corrodedDURING REMOVAL OF MLG FOR O/H, NOTED SIGNIFICANT CORROSION IN MLG ATTACH BORES OF THE RT WING SPONSON RIB.SDR N93A06142010BLug · corrodedDURING REMOVAL OF HORIZONTAL STABILIZER, NOTED SIGNIFICANT CORROSION IN LT HORIZ STABILZER TO VERT STABILZER ATTACH LUGS (VERT STAB SIDE).SDR N93A06142010CLug · corrodedDURING REMOVAL OF HORIZONTAL STABILIZER NOTED SIGNIFICANT CORROSION IN RIGHT HORIZONTAL STABILZER TO VERTICAL STABILZER ATTACH LUGS (VERTICAL STAB SIDE).SDR N93A04032010Connector · looseDURING CLIMB, LT ENGINE TGT EXCEEDANCE WAS NOTED. MX FOUND CONNECTORS 900A1P16 AND 900A1P17 LOOSE. BOTH CONNECTORS ARE LOCATED AT THE ENGINE PYLON JUST AFT OF THE FIXED COWL AND CONNECT TO THE THRUST REVERSER. RATCHETING TYPE CONNECTORS WERE SECURED AND OPSSDR N93A03222010Throttle Cable · brokenCREW REPORTED LT THROTTLE IS LOOSE AND INOPERATIVE. MX FOUND LT THROTTLE CABLE BROKEN UNDER FLOOR IN AFT LAV JUST FWD OF WHERE CABLE TURNS UPWARD AT AFT LAV AFT WALL. CABLE APPARENTLY HAD BEEN FRAYING ON STRUCTURE PRIOR TO BREAKING.SDR 2010F00048Skin · corrodedREPAIR SURFACE AND INNER GRANULAR CORROSION LOCATED ON FWD WING PLANK IN THE AREA OF THE LT LOWER REBATE AT WING BL19.0 TO B.L.21.0. REF GDAS-BAF W/O SC3925.12.12 FOR FURTHER DETAILS. RECEIVED ENGINEERING DISPOSITION DATED 02/11/2010, W/O SC19577 STATING REPAISDR 2010F00047Skin · corrodedREPAIRED SURFACE AND INNER GRANULAR CORROSION LOCATED FWD WING PLANK IN AREA OF FUEL ACCESS DOOR. REF: GDAS-BAF W/O SC3925 FOR FURTHER DETAILS. RECEIVED ENGINEERING DISPOSITION DATED 02/05/2010, W/O CS197059 STATING REPAIR IAW BLUE PRINT SE45803171-1 REV.-, PSDR Y9PA663P112508Hydraulic System · low pressureENROUTE, THE CREW DECLARED AN EMERGENCY AND LANDED. THE REPORT IS BOTH HYDR SYS QUANTITY WAS INDICATING LOW, LOCATED A LOCAL TECH IAW AIR CARRIER MM SECTION 3.02. CHECKED THE QUANTITY IN THE HYDR RESERVOIRS AND VERIFIED THAT THEY WHERE LOW, SERVICED IAW COMPUSDR Y9PAN663P102908Washer · wrong partUPON THE MID-LIFE REMOVAL OF NR1 ENG FOUND THAT THE WASHER USED AT THE TRUNNION TIE BOLT HAD A O/D THAT WAS TO LARGE FOR THE USE OF TOOL (T900175-1). THIS TOOL IS USED TO PREVENT THE TRUNNION CANISTER FROM MOVING. IAW CAUTION FOUND IN MM 71-00-00 PG. 405 B. 2SDR N932008F00002Regulator · malfunctionedAFTER TAKEOFF RT ENG WOULD NOT RESPOND TO THROTTLE SETTING AND REMAINED AT TAKEOFF POWER. ENG WAS SHUTDOWN. (S)SDR WWQ2008F00001Starter · wornRT ENG FAILED TO START. FOUND THAT THE STARTER WAS BAD. DURING THE STARTER REPLACEMENT NOTICED ABNORMAL WEAR ON THE ENG GEAR BOX STARTER GEAR. CONTACTED ENGINEERING DEPARTMENTS TO ASK FOR LIMITATIONS. AFTER ENGINEERING DEPARTMENTS REVIEWED THE PICTURES, DESDR WWQ2008F00002Gear · wornRT ENGINE FAILED TO START, FOUND THAT THE STARTER WAS BAD. DURING THE STARTER REPLACEMENT, NOTICED ABNORMAL WEAR ON THE ENGINE GEAR BOX STARTER GEAR. CONTACTED ENGINEERING DEPARTMENTS TO AS FOR LIMITATIONS. AFTER ENGINEERING DEPARTMENTS REVIEWED PICTURES, THEYSDR 2008FA0000494Water Separator · damagedBOTH UNITS O/H AT MFG. WHEN CHANGING SOCK, FOUND RUST STAINS ON SOCK. REMOVED AND FOUND RETAINING CHAIN PN 834639 RUSTED. CHAIN WAS WRONG MATERIAL (METAL) AND INCORRECT LENGTH (9.5 INCHES). REPLACEMENT UNIT WAS SS WITH A TOTAL LENGTH OF (6 INCHES). ALSO OSDR 2008FA0000506Transmitter · malfunctionedTRANSMITTER CAUSED LT ENGINE TO SPOOL BACK TO IDLE, AC RETURNED TO AIRPORT AND LANDED WITH NO INCIDENT. (K)SDR N93A01042008Shuttle Valve · malfunctionedAFTER TAKEOFF, CREW RECEIVED 'CHK HYD QTY" CAS MESSAGE AND VERIFIED BY QUANTITY LEVEL BEING LOW. MAINTENANCE FOUND THAT HYDRAULIC SHUTTLE VALVE ACTUATED DURING GEAR BLOW DOWN ON PREVIOUS FLIGHT AND DID NOT FULLY RESEAT.SDR N93A29032008Connector · looseAFTER GEAR WAS EXTENDED FOR LANDING, RT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. FOUND RT MLG DOWNLOCK SWITCH CONNECTOR NOT FULLY SEATED. RESEATED CONNECTOR, OPS CHECKS WERE ACCOMPLISHED SUCESSFULLY.SDR 2008FA0000226Sight Glass · crackedSIGHT GLASS CRACKED IN SEVERAL LOCATIONS AND LEAKS HYDRAULIC FLUID, THIS TANK IS ONE OF SEVERAL RETURNED FOR THE SAME DEFECT. (K)SDR N382008F00001Pulley · obstructedAT PREFLIGHT, THE PILOT NOTICED THAT THE SPEED BRAKES DID NOT CLOSE COMPLETELY. MAINT WAS CALLED AND AFTER SOME OPERATIONAL CHECKS AND A VISUAL INSPECTION OF THE CONTROL SYS AT THE LT MAIN GEAR WHEEL WELL A STONE WAS FOUND AT A CONTROL CABLE PULLEY AND THE STSDR BKE2008F00003Windshield · crackedPILOT REPORTED, IN FLIGHT, THAT THE CO-PILOTS WINDSHIELD OUTER PANE CRACKED AND SHATTERED. THE INNER PANE HELD. PILOT DIVERTED AND REPAIRS ARE IN PROGRESS. SUSPECT THE THE WINDSHIELD HEAT FAILED. (K)SDR N93A23032008Unknown · malfunctionedFLYING THRU MODERATE TURBULENCE THE AUTO PILOT , YAW DAMPENER, FLIGHT GUIDANCE COMPUTER, AND MACH TRIM. ALSO, STICK SHAKER ACTIVATED ALTHOUGH AIRCRAFT WAS TRAVELING AT 270 KNOTS. AIRCRAFT WAS INSPECTED AND SYSTEM OPS CHECKS COMPLETED. NO DEFECTS FOUND.SDR FAA011808002Oil System · low pressure30 MINUTE INTO THE FLIGHT OIL PRESSURE DROPPED TO 7 PSI. NO ASSOCIATED CAS MESSAGE. OIL TEMP WAS SLIGHTLY HIGHER THAN LT ENGINE. FUEL TEMP WAS 19 DEGREES HIGHER THAN LT. DURING DESCENT OIL PRESSURE CAME BACK TO 47 PSI.SDR FAA011808001Fuel Control · inoperativeON APPROACH TO TTN THE AUTO THROTTLES DISENGAGED. THE RT LEVER KNOB WAS ONE KNOB AFT OF THE LT. WHEN RT LEVER WAS ADVANCED FORWARD THE RT ENGINE DID NOT RESPOND TO THROTTLE MOVEMENT.SDR N93A10102007Pressure Switch · unknownAFTER TAKEOFF, STEER BY WIRE FAIL LIGHT, ILLUMINATED THEN WENT OUT AFTER 5 MINUTESSDR N93A29092007Steering Sys · malfunctionedNOSE STEERING PULLS TO RIGHT WHEN HANDWHEEL IS CENTERED. (OPEN)SDR N93A12092007Steering Sys · failedAFTER LANDING AIRCRAFT, STEERING MADE AN UNCOMMANDED TURN TO THE RIGHT.SDR N93A28082007Attach Fitting · corrodedDURING 5000 LANDING INSPECTION FOUND 714 BULKHEAD VERTICAL STAB ATTACH FITTINGS CORRODED.SDR N93A28082007AAngle · crackedDURING 5000 LANDING INSPECTION FOUND 793 BULKHEAD VERTICAL STAB CAP ANGLE CRACKED.SDR N93A12082007Valve · failedNOSE WHEEL STEERING FAILURE DURING START UP.SDR N93A09082007Fitting · corrodedDURING INSPECTION FOUND ON VERTICAL STAB ATTACH BULKHEAD AND FITTING CORRODED.SDR WWQ2007F00000Drive Shaft · looseON AUG 7, 2007 UPON LANDING, THE CREW CALLED MAINT AND REPORTED THAT UPON DESCENT FROM 41,000 FT, THEY GOT A FGC1 FAIL MESSAGE ALONG WITH A FWD TRIM LIMIT MESSAGE. THEY WERE UNABLE TO TRIM THE AIRCRAFT ELEVATORS. THEY COMPLIED WITH THE AC CHECKLIST TO RESET SDR Y9PAN663P8707Unknown · odorCREW REPORTED SMOKE IN THE CABIN ON DESCENT INTO LGA, CREW MENTIONED THAT IT WAS EMITTING FROM THE BAGGAGE BAY AREA WITH AN ELECTRICAL SMELL. INSPECTED ACFT BAGGAGE BAY AREA BY REMOVING FLOORBOARD ACCESS PANELS, BAGGAGE BAY SIDE WALL PANELS AT LGA WITH REPRESSDR N93A25072007Engine · shutdownAFTER TAKEOFF CREW RECEIVED LP EXCEEDANCE CAS MESSAGE WHEN THROTTLES WERE RETARDED ENGINE DID NOT RESPOND TO MOVEMENT. CREW SHUTDOWN ENGINE AND RETURNED TO DEPARTURE AIRPORT.SDR 93A19072007Unknown · warning lightAFTER TAKEOFF, NOSE WHEEL STEERING FAIL MESSAGE ILLUMINATED. OPEN
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