Rolls-Royce SPEY-511-8

Service difficulty reports · 80

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 = 'SPEY5118'
  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 ESPA2019F00223Spar · corrodedFOUND CORROSION ON WING AFT SPAR AT RBS 406.May 17, 2019 · N163PA · Gulstm G1159A · Wing SparSDR ESPA2019F00224Wing · corrodedRIGHT WING HAS CORROSION ON AFT SPAR AT RBS343.May 17, 2019 · N163PA · Gulstm G1159A · Wing SparSDR 2017F00013Engine · malfunctionedDURING LANDING, THE CREW REPORTED THAT THE NR 1 ENGINE STAYED AT IDLE AND FAILED TO RESPOND TO THROTTLE INPUTS. THE AIRCRAFT WAS ON A COMPANY REQUIRED CHECK FLIGHT FOR AN UNRELATED ISSUE AND NO PASSENGERS WERE ON BOARD. THE AIRCRAFT LANDED WITH OUT INCIDENT, NDec 27, 2016 · N901EH · Engine (Turbine/Turboprop)SDR ESPA2016F00081Seal · leakingENROUTE AT FL410 . HEARD A LOUD NOISE COMING FROM THE FRONT ENTRANCE DOOR AND SUSPECTED A DOOR SEAL LEAK. THE CABIN BEGAN TO CLIMB AT A RAPID RATE. ELECTED TO REQUEST A LOWER ALTITUDE WITH ATC WHILE WORKING ON THE ISSUE. BEGAN A DESCENT TO THE ASSIGNED ALTMar 2, 2016 · N183PA · Gulstm G1159 · Passenger/Crew DoorsSDR 2014FA0000466Window · failedWHILE CLIMBING THROUGH 390 TO FL430 THE RT AFT-MOST PASSENGER WINDOW CRACKED AND BLEW OUT. THEN THE RT ENGINE FLAMED OUT. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO LAND. AIRPORT FIRE AND RESCUE DISPATCHED AND THE ACFT TAXIED TO THE RAMP WITHOUT FURTHERJul 10, 2014 · Gulstm G1159A · Passenger Compartment WindowsSDR 2014FA0000254Turbine Nozzle · crackedENGINE WAS REMOVED FOR O/H, INSPECTION IAW O-SP4-G AND NMSB72-666. DURING THE CRACK TEST INSPECTION IAW 72-50 OF THE HPT 2 DISC, THE DISC EXHIBITED A CRACK INDICATION IN THE DISC WEB THAT HELD PENETRANT AND WAS FURTHER VERIFIED WITH THE STEREO FOCUS INSPECTIONApr 10, 2014 · Turbine SectionSDR AOYA20140104001Engine · power lossENGINE START & TAXI CHECKS WERE NORMAL. A ROLLING TAKEOFF WAS PERFORMED TO COMPUTED EPR'S. ALL ENG PARAMETERS WERE NORMAL DURING TAKEOFF ACCELERATION UNTIL A DROP IN THE LT ENG EPR TO APPROXIMATELY 1.9. THE LT ENG THRUST LEVER DID NOT RESPOND TO AN ATTEMPT TJan 4, 2014 · N55ME · Gulstm G1159A · Engine (Turbine/Turboprop)SDR 2013FA0000250Flapper Valve · failedOVER A 4 YEAR PERIOD, THIS ACFT HAS EXPERIENCED 2 INSTANCES OF IN-FLIGHT ROLL BACK AND SHUTDOWN OF THE RT ENGINE. IN BOTH CASES ENGINE COULD BE RESTARTED AND SUBSEQUENT EXTENSIVE EVALUATION AND INSPECTION REVEALED NO DEFECTS. ACFT OPERATED WITHOUT INCIDENT Apr 18, 2013 · N10123 · Gulstm G1159 · Aircraft Fuel Distribution SystemSDR 2012F00077Skin · dentedDURING POST FLIGHT WALK-AROUND BY FLIGHT CREW NOTICED A POSSIBLE BIRD STRIKE AND DENT ON LT OTBD L/E.Apr 17, 2012 · N477WG · Gulstm G1159A · Wing, Plate/SkinSDR 2011F00019Engine · flamed outAT FL 430, ENCOUNTERED MODERATED MOUNTAIN WAVE WITH AIRSPEED FLUXUATION OF MACH .80 TO .72. AT THIS TIME WE HAD THE NR 2 ENGINE FLAMEOUT. PERFORMED NORMAL DESCENT TO AIRSTART ENVELOPE, COMPLIED WITH AIRSTART CHECKLIST, NO DEFECTS NOTED, CONTINUED TO DESTINAJan 16, 2011 · N918BG · Gulstm G1159A · Engine (Turbine/Turboprop)SDR EYDAN128KGC1FODCompressor · distortedON 09/10/09 THE AIRCRAFT DEPARTED EWR ENROUTE TO OPF, DURING CLIMB IN ICING CONDITIONS; AT 33,400 FT, THE NR 1 ENGINE HAD A COMPRESSOR STALL AND STARTED TO ROLL BACK. THE CREW INITIATED A RELIGHT AND THE ENGINE RETURNED TO NORMAL OPERATION. MAINTENANCE INSPECSep 10, 2009 · N128KG · Gulstm G1159 · Turbine Engine Compressor SectionSDR WWQ2009F00000Engine · failedDURING CLIMB OUT, AFTER TAKEOFF, APPROXIMATELY 5K FEET THE CREW HEARD A LOUD BANG FROM THE LT ENGINE. THE CREW CHECKED THE ENGINE PARAMETERS AND FOUND 0 EPR AND NOTICED THAT THE POWER LEVER WAS UNRESPONSIVE ON THE LT ENGINE. LP HP WAS APPROXIMATELY 30 PERCENApr 19, 2009 · N366JA · Gulstm G1159A · Engine (Turbine/Turboprop)SDR Y9PAN930LS82208Transponder · intermittentMODE C TRANSPONDERS READ 500 FT HIGH 99 PERCENT OF THE TIME (IN CRUISE). TROUBLESHOOTING IN PROCESS, WILL AMEND FORM WHEN DETERMINATION OF CAUSE 8/22/08. RAN PITOT/STATIC SYS TO 45,000 FT AND CHECKED OUT PUT OF TRANSPONDER SYS WITH ATC601 TEST SET AND INDICAug 22, 2008 · N930LS · Gulstm G1159 · ATC Transponder SystemSDR YJU2008F00000Tire · unserviceablePILOTS REPORTED THAT ON TAKEOFF, THEY FELT A BUMP FOLLOWING THE VR CALLOUT. AFTER LANDING, IT WAS DISCOVERED THAT THE NR 3 MAIN TIRE TREAD HAD COMPLETELY SEPARATED FROM THE TIRE DOWN TO THE CORD AREA. THE TREAD COMING OFF DAMAGED THE FLAP TORQUE TUBE, SEVEREJul 7, 2008 · N797BD · Gulstm G1159A · TireSDR ESPA100107Windshield · crackedDURING DECENT AT 20,000 FEET THE CO-PILOTS WINDSHIELD DEVELOPED CRACK STARTING FROM THE RT SIDE BOLT PATTERN AND EXTENDING DOWN AND ACROSS. CREW DECIDED TO DIVERT, AS THE CRACK HAD SPLIT INTO (2) CRACKS. ALSO, DECLARED AN EMERGENCY TO ATC PROCEEDING VISUALLYOct 17, 2007 · N183PA · Gulstm G1159 · Flight Compartment WindowsSDR 2007FA0000958Regulator · failedPILOTS REPORT FELT HEAVY VIBRATION FOR 3 TO 4 SECONDS, THEN HEARD A LOUD BANG FOLLOWED BY LT ENGINE SPOOLING DOWN. AIRCRAFT SAFELY LANDED AT AIRPORT. CONTACTED MFG, WHO DISPATCHED A RESPONSE CREW TO AIRPORT. FOUND THAT THE FUEL FLOW REGULATOR HAD FAILED IN Sep 13, 2007 · N776MA · Gulstm G1159A · Engine Fuel DistributionSDR Y9PAN818S83107Smoke Detector · malfunctionedAFTER TAKEOFF, LAV SMOKE ALARM ANNUNCATOR ILLUMINATED, CREW REPORTED THAT THEY INSPECTED THE LAV AREA FOR SIGNS OF SMOKE AND FIRE, NONE OBSERVED. THE ANNUNCATOR WENT OUT AND THEN CAME BACK ON. THE CREW THEN ELECTED TO DIVERT. UPON LANDING, THE APU WOULD NOT STAug 31, 2007 · N818S · Gulstm G1159A · Smoke DetectionSDR UG8A2007PA03SAttach Fitting · corrodedLT AFT IB WING ATTACH FITTING HAS CORROSION AT OB EDGE AT FS 452, BL 33.COMPLIED WITH AIRCRAFT SERVICE CHANGE 229, WING TO FUSELAGE IB ATTACH CONNECTION FUSELAGE STATION 452 LT SIDE, REPLACEMENT/MODIFICATION. GENERATED FAA FORM 337. AIRCRAFT RETURNED TO SERVIJun 13, 2007 · N473KT · Gulstm G1159A · Wing, Attach FittingsSDR BUE2006F00000Attach Bracket · crackedMAIN ENTRY DOOR IS NOT CLOSING CORRECTLY (STOPS 12 INCHES TO 16 INCHES SHORT OF NORMAL WHEN BEING CLOSED WITH THE AUXILIARY HYDRAULIC PUMP). RESOLUTION: INSPECTED AND FOUND MAIN ENTRY DOOR ACTUATOR ATTACH BRACKET( PN 1159BM50216-1), INTERCOSTAL (PN 159B10456-Jul 27, 2006 · N416WM · Gulstm G1159A · Fuselage Main, Attach FittingsSDR EW72006F00000Turbine · overtempDURING TAKEOFF AT ROTATION, LOUD SERIES OF BOOMS HEARD. CREW CONDUCTED FLY BY AND ADVISED BY CONTROL TOWER TO LAND. AIRCRAFT LANDED SAFELY. SUBSEQUENT BOROSCOPE INSPECTION OF NR 2 ENGINE REVEALED HEAT DAMAGE TO MULTIPLE STAGES OF TURBINE SECTION. (K)Jan 4, 2006 · N888LV · Gulstm G1159A · Turbine SectionSDR CA051014002Blades · damagedGII SERIAL 236 IN NR 1 POSITION HAS EXPERIENCED FOD DAMAGE. THE DAMAGE HAS BEEN FOUND TO THE LPC5 BLADES AND HPC1 BLADES. THE REST OF THE HP COMPRESSOR HAS YET TO BE INSPECTED. THE DAMAGE HAS BEEN CAUSED BY THE RELEASE OF ONE LP OGV INNER BOLT WASHER AND NUOct 12, 2005 · Gulstm G1159 · Turbine Engine Compressor SectionSDR 2005FA0001476O-Ring · leakingHYD LINE WAS REPLACED DUE TO CRACK IN FLARE AT TEE FITTING. REPLACEMENT OF LINE REQUIRED INSTALL OF NEW O-RING, WHERE TEE FITTING ATTACHES TO FLIGHT CTRL HYD SHUT OFF VALVE. AFTER INSTALL OF HYD LINE AND O-RING, A LEAK CHECK WAS PERFORMED. NO LEAKS WERE NOTSep 11, 2005 · N165ST · Gulstm GIV · Hydraulic System, MainSDR N382005F00004Starter · meltedLT ENGINE WILL NOT START; NO START VALVE OR IGNITION LIGHT WHEN STARTER BUTTON PRESSED. A REPLACEMENT STARTER WAS INSTALLED AND THE AIRCRAFT WAS FLOWN BACK TO ITS HOME BASE. (K)Jul 19, 2005 · N95SJ · Gulstm G1159B · Engine StarterSDR UG82005F00004Tire · mismanufacturedNR 2 NOSE LANDING GEAR TIRE HAS A BULGE (INDICATING TREAD SEPARATION) BETWEEN THE SIDEWALL CHINE AND THE TREAD OF THE TIRE. BULGE IS APPROXIMATELY 7 INCHES LONG. SUSPECT MANUFACTURING DEFECT IN TIRE. TIRE AND WHEEL ASSY REMOVED FROM AIRCRAT AND OVERHAULED WJul 11, 2005 · N473KT · Gulstm G1159A · TireSDR 2005FA0001034Proximity Switch · looseAC DEPARTED FOR 3 DAY TRIP. AC MADE A STOP TO PICK UP 1 PASSENGER, THEN TOOK OFF AND HEADED TO PICK UP ANOTHER PASSENGER. ON EXTENDING THE GEAR, LT GEAR DOWN AND LOCKED LIGHT FAILED TO LITE. CREW TRIED 6 TIMES BY RETRACTING AND EXTENDING GEAR TO NO AVIAL. Jun 11, 2005 · N900DH · Gulstm G1159 · Landing Gear Position and WarningSDR O2G2004F00010Windshield · failedRT WINDSHIELD OUTER PANE FAILED, DURING FLIGHT. REMOVED AND REPLACED WINDSHIELD. (NE03200504208)Nov 21, 2004 · N590DA · Gulstm G1159A · Flight Compartment WindowsSDR O2G2004F00006Line · leakingRT ENGINE WOULD NOT MAKE EPR OF THE DAY, RETORQUE P3 SPLITTER. PERFORMED ENGINE POWER RUN, OPS CK GOOD.Oct 14, 2004 · N624BP · Gulstm GIV · Engine Pressure Ratio (EPR)SDR O2G2004F00005Converter · failedRT CONVERTER FAILED AND LOST AUTO CONTROL OF PRESSUREIZATION. RAN CHECKLIST SEVERAL TIMES WITH NO EFFECT. REMOVE AND REPLACED CONVERTER.Oct 11, 2004 · N590DA · Gulstm G1159A · Cabin Pressure Control SystemSDR 2005FA0000103Skin · corrodedDURING WING (RIGHT) NOT INSPECTION, EXFOLIATION CORROSION NOTED ON WING UPPER PLANK AND FRONT BEAM BETWEEN RBS 284 THRU 375. EXFOLIATION CORROSION REMOVED IAW SRM. REPAIRS COMPLETED.Sep 2, 2004 · N826GW · Gulstm G1159 · Wing, Plate/SkinSDR 2005FA0000104Cowling · corrodedDURING LT ENGINE MID-LIFE UPDATES, LT FIXED COWL WAS INSPECTED AND CORROSION WAS NOTED. FIXED COWL WAS REPAIRED.Sep 2, 2004 · N826GW · Gulstm G1159 · Nacelle/Pylon, Plate/SkinSDR 2005FA0000267Bulkhead · crackedDURING COMPLIANCE OF NDT EDDY CURRENT INSP OF FS-793.75 BULKHEAD, CAP ANGLE WAS FOUND CRACKED. NEW CAP ANGLE WAS INSTALLED IAW DWG NR SE20000210, REV. D.Sep 2, 2004 · N826GW · Gulstm G1159 · Fuselage Main, BulkheadSDR 2005FA0000268Panel · corrodedDURING WIG (LT) NDT INSPECTION EXFOLIATION CORROSION NOTED ON WING UPPER PLANK AND FRONT BEAM BETWEEN RBS 284 THRU 375. REMOVED EXFOLIATION CORROSION IAW SRM. REPAIRS COMPLETED.Sep 2, 2004 · N826GW · Gulstm G1159 · Wing, Plate/SkinSDR 2005FA0000269Cowling · corrodedDURING RT ENGINE MID-LIFE UPDATES, RT FIXED COWL WAS INSPECTED AND CORROSION WAS NOTED. FIXED COWL WAS REPAIRED.Sep 2, 2004 · N826GW · Gulstm G1159 · Nacelle/Pylon, Plate/SkinSDR IV42004F00000Bearing · failedDURING CLIMBOUT, 2 HIGH TVI INDICATION ON NR 1 END AFT WAS OBSERVED (APPROX 2.5). AFTER POWER WAS REDUCED, TVI INDICATION REDUCED TO APPROX (.7), SOME FLUCTUATION ON TVI INDICATOR. GEN VOLTAGE WAS NORMAL BUT HAD SPLIT IN GEN AMPERAGE WITH NR 1 GEN SHOWING APAug 31, 2004 · N949NA · Gulstm G1159 · DC Generating SystemSDR N3B2004F00000Tire · blownLT MAIN GEAR TIRE BLEW OUT ON TAKEOFF. DAMAGE TO LT WING, LT GEAR HARNESS, BRAKE LINES, AND A DENT IN THE LT LOWER ENGINE COWL.Jul 16, 2004 · N510SR · Gulstm G1159B · TireSDR 2004F00234Windscreen · crackedWINDSCREEN CRACK DURING FLIGHT.Jul 7, 2004 · N1NA · Gulstm G1159A · Flight Compartment WindowsSDR 2004F00233Duct · separatedCOUPLING SEPARATED FROM END OF APU/GROUND START APU DUCT ASSY.Jul 2, 2004 · N1NA · Gulstm G1159A · Pneumatic Distribution SystemSDR PA04002Circuit Card · dirtyAURAL OVERSPEED WARNING CAME ON DURING TAKEOFF ROLL, LOW SPEED ABORT. THERE WAS A MALFUNCTION WITHIN THE OVERSPEED WARNING SYSTEM. THE AUDIBLE TONE GENERATOR WAS REMOVED. THE NR 2 CHANNEL CARD WAS REMOVED, INSPECTED, CLEANED AND REINSTALLED. THE OVERSPEED Apr 19, 2004 · N473KT · Gulstm G1159A · Central WarningSDR ET72004F00000Heat Shield · delaminatedNOTED HEAT SHIELD HAS DISBONDED FROM RT FIX COWL OUTER SKIN AT APPROX FS 596.0 TO NACELLE STATION 179.0 (OIL CAN). INSPECTION OF FIX COWL INTERIOR (INNER SKIN CORE) AT FS 596.0 TO NACELLE STATION 179.0. NO DEFECTS NOTED. FOUND DELAMINATION ON INNER SKIN CORMar 31, 2004 · N668JT · Gulstm G1159 · Engine Cowling SystemSDR 2003FA0001159Indicator · misrepairedEVERYTIME WE HAVE SENT ONE OF THESE UNITS TO THE MANUFACTURER, WE RECEIVE IT BACK IN AN UNSATISFACTORY WORKING CONDITION. THIS UNIT HAS A CABIN RATE OF CLIMB OF +50, SITTING ON THE GROUND WITH NO AIR APPLIED.(K)Oct 29, 2003 · N80J · Gulstm G1159A · Engine Bleed Air SystemSDR ZLW2004F00000Pitot Line · cloggedAC WAS ON TAKEOFF ROLL WHEN THE FLIGHT CREW NOTED A SUBSTANTIAL SPLIT BETWEEN AIRSPEED INDICATORS. AC WAS TAXIED BACK FOR TROUBLESHOOTING. PITOT/STATIC CHECKS WERE ACCOMPLISHED AND DISCREPANCY DUPLICATED. ALL PITOT AND STATIC LINES WERE DISCONNECTED AND NITSep 23, 2003 · N36MW · Gulstm G1159 · Pitot/Static SystemSDR 2003FA0001234Actuator · stuckDURING FINAL APPROACH, FLAPS WOULD NOT EXTEND BEYOND 35 DEGREES TO THE NORMAL 39 DEGREES, NOR COULD THE FLAPS RETRACT. LANDING WAS UNEVENTFUL. IT WAS LATER DISCOVERED THAT HORIZ STAB ACT (WHICH BEGINS TO MOVE HORZ STAB DOWN WHEN FLAPS GO BEYOND 10 DEGREES) WSep 18, 2003 · N388CW · Gulstm G1159A · Stabilizer ActuatorSDR CA030613001Tube · sheared(CAN) AFTER REMOVING THE FLAPS TO REPAIR THE D TRACK WEB IAW AIRCRAFT SERVICE CHANGE 318B. THE LT OUTBOARD FLAP ACTUATOR SCREWJACK BALL RETURN TUBE COVER WAS FOUND SHEARED OFF (SUSPECT IMPROPER INSTALLATION). REPAIRED IAW CUSTOMER BULLETIN NR 99.Jun 11, 2003 · Gulstm G1159A · Trailing Edge Flap ActuatorSDR CA030611004Ring · cracked(CAN) TIME SHOWN ABOVE IS ENGINE TIME. PART IS OVERHAULED AT ENGINE INSTALLATION. THE TRUNNION ASSEMBLY ATTACHED TO THE FORWARD ENGINE MOUNTING BEAM LINK, ATTACHING ENGINE TO AIRCRAFT, WAS RECEIVED AT RRC WITH ENGINE 8841 FOR REVISION. THE RING NUT LOCKING TRJun 11, 2003 · Gulstm G1159 · Engine Mount SectionSDR CA030409008Tube · chafed(CAN) HUDRAULIC TUBES WERE FOUND TO BE CHAFFED BEYOND LIMITS DURING THE PYLON INTERIOR SCHEDULE INSPECTION. BOTH LEFT & RIGHT TUBES SHOWED DAMAGE IN NEARLY IDENTICAL SPOTS, CAUSED BYCHAFFING ON A ELECTRICALWIRE THAT HAD BEEN CLAMPPED NOT PROPERLY. THE WIRE SHOApr 3, 2003 · Gulstm G1159A · Hydraulic System, MainSDR CA030507005Bolt · broken(CAN) ENGINE IS AT RRC FOR REPAIR DUE TO HIGH VIBRATION ON WING. VIBRATION ON THE REAR PICK UP WAS CONFIRMED ON A TEST BED RUN AT RRC. DURING THE STRIP OF THE TURBINE SECTION IT WAS NOTED THAT 2 OF BOLTS HAVE RELEASE THEMSELVES FROM THE LP TURBINE INNER SEAL Apr 3, 2003 · Gulstm G1159B · Turbine SectionSDR CA030324010Bolt · failed(CAN) LP OGV S BOLT FAILED DURING GROUND RUN. THE DAMAGED WAS CONTAINED WITHIN THE ENG. ENG SUFFERED FROM HIGH VIBRATION AND THEN A BOROSCOPE WAS PERFORMED AND THE LP COMPRESSOR ROTOR WAS FOUND DAMAGED. ENG STRIP CONFIRMED THAT ONE OFF OGV BOLT WAS MISSING. MIMar 24, 2003 · Gulstm G1159 · Turbine Engine Compressor SectionSDR VZG2003F00000Control Valve · inoperativeNOSE LANDING GEAR WOULD NOT EXTEND WITH THE LANDING GEAR HANDLE PLACED IN THE DOWN POSITION. TROUBLESHOT LANDING GEAR AND FOUND THE NOSE GEAR DOOR CONTROL VALVE INOPERATIVE NOT ALLOWING THE GEAR DOOR TO OPEN. NOSE GEAR DOORS WOULD OPEN WHEN GROUND HANDLE WASMar 12, 2003 · N444GA · Gulstm G1159A · Landing Gear Door Retract SectionSDR NASA51181Nut · missingIN JUNE 2000 DURING A ROUTINE POSTFLIGHT INSPECTION FOD WAS DISCOVERED ON THE LP COMPRESSOR 5TH STAGE BLADES. DURING A SUBSQUENT TEARDOWN IT WAS DISCOVERED THAT A LP COMPRESSOR OGV BOLT AND NUT AND CAME LOOSE AND CAUSED THE DAMAGE TO THE ENGINE. THE BOLT WAS FMar 7, 2003 · N848NA · Gulstm G1159 · Engine (Turbine/Turboprop)SDR ZLW2003F00000Floorbeam · crackedDURING A ROUTINE CABIN BELOW FLOOR INSPECTION, IT WAS FOUND THAT THE AFT FLOORBEAM SECONDARY SUPPORT WAS CRACKED. A NEW PART IS AVAILABLE FROM MFG AND WILL BE INSTALLED PRIOR TO FURTHER FLIGHT.Mar 4, 2003 · N622RR · Gulstm G1159 · Fuselage Main, Floor Beam
Back to Rolls-Royce SPEY-511-8