# Service difficulty reports: Rolls-Royce SPEY-511-8

A list on [Rolls-Royce SPEY-511-8](https://openairdocs.org/engine/rolls-royce-spey-511-8.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 80 reports

- [SDR ESPA2019F00223](https://openairdocs.org/sdr/ESPA2019F00223.md): Spar · corroded · May 17, 2019 · N163PA · Gulstm G1159A · Wing Spar
  > FOUND CORROSION ON WING AFT SPAR AT RBS 406.
- [SDR ESPA2019F00224](https://openairdocs.org/sdr/ESPA2019F00224.md): Wing · corroded · May 17, 2019 · N163PA · Gulstm G1159A · Wing Spar
  > RIGHT WING HAS CORROSION ON AFT SPAR AT RBS343.
- [SDR 2017F00013](https://openairdocs.org/sdr/2017F00013.md): Engine · malfunctioned · Dec 27, 2016 · N901EH · Engine (Turbine/Turboprop)
  > DURING 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, N
- [SDR ESPA2016F00081](https://openairdocs.org/sdr/ESPA2016F00081.md): Seal · leaking · Mar 2, 2016 · N183PA · Gulstm G1159 · Passenger/Crew Doors
  > ENROUTE 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 ALT
- [SDR 2014FA0000466](https://openairdocs.org/sdr/2014FA0000466.md): Window · failed · Jul 10, 2014 · Gulstm G1159A · Passenger Compartment Windows
  > WHILE 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 FURTHER
- [SDR 2014FA0000254](https://openairdocs.org/sdr/2014FA0000254.md): Turbine Nozzle · cracked · Apr 10, 2014 · Turbine Section
  > ENGINE 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 INSPECTION
- [SDR AOYA20140104001](https://openairdocs.org/sdr/AOYA20140104001.md): Engine · power loss · Jan 4, 2014 · N55ME · Gulstm G1159A · Engine (Turbine/Turboprop)
  > ENGINE 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 T
- [SDR 2013FA0000250](https://openairdocs.org/sdr/2013FA0000250.md): Flapper Valve · failed · Apr 18, 2013 · N10123 · Gulstm G1159 · Aircraft Fuel Distribution System
  > OVER 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
- [SDR 2012F00077](https://openairdocs.org/sdr/2012F00077.md): Skin · dented · Apr 17, 2012 · N477WG · Gulstm G1159A · Wing, Plate/Skin
  > DURING POST FLIGHT WALK-AROUND BY FLIGHT CREW NOTICED A POSSIBLE BIRD STRIKE AND DENT ON LT OTBD L/E.
- [SDR 2011F00019](https://openairdocs.org/sdr/2011F00019.md): Engine · flamed out · Jan 16, 2011 · N918BG · Gulstm G1159A · Engine (Turbine/Turboprop)
  > AT 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 DESTINA
- [SDR EYDAN128KGC1FOD](https://openairdocs.org/sdr/EYDAN128KGC1FOD.md): Compressor · distorted · Sep 10, 2009 · N128KG · Gulstm G1159 · Turbine Engine Compressor Section
  > ON 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 INSPEC
- [SDR WWQ2009F00000](https://openairdocs.org/sdr/WWQ2009F00000.md): Engine · failed · Apr 19, 2009 · N366JA · Gulstm G1159A · Engine (Turbine/Turboprop)
  > DURING 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 PERCEN
- [SDR Y9PAN930LS82208](https://openairdocs.org/sdr/Y9PAN930LS82208.md): Transponder · intermittent · Aug 22, 2008 · N930LS · Gulstm G1159 · ATC Transponder System
  > MODE 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 INDIC
- [SDR YJU2008F00000](https://openairdocs.org/sdr/YJU2008F00000.md): Tire · unserviceable · Jul 7, 2008 · N797BD · Gulstm G1159A · Tire
  > PILOTS 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, SEVERE
- [SDR ESPA100107](https://openairdocs.org/sdr/ESPA100107.md): Windshield · cracked · Oct 17, 2007 · N183PA · Gulstm G1159 · Flight Compartment Windows
  > DURING 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 VISUALLY
- [SDR 2007FA0000958](https://openairdocs.org/sdr/2007FA0000958.md): Regulator · failed · Sep 13, 2007 · N776MA · Gulstm G1159A · Engine Fuel Distribution
  > PILOTS 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
- [SDR Y9PAN818S83107](https://openairdocs.org/sdr/Y9PAN818S83107.md): Smoke Detector · malfunctioned · Aug 31, 2007 · N818S · Gulstm G1159A · Smoke Detection
  > AFTER 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 ST
- [SDR UG8A2007PA03S](https://openairdocs.org/sdr/UG8A2007PA03S.md): Attach Fitting · corroded · Jun 13, 2007 · N473KT · Gulstm G1159A · Wing, Attach Fittings
  > LT 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 SERVI
- [SDR BUE2006F00000](https://openairdocs.org/sdr/BUE2006F00000.md): Attach Bracket · cracked · Jul 27, 2006 · N416WM · Gulstm G1159A · Fuselage Main, Attach Fittings
  > MAIN 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-
- [SDR EW72006F00000](https://openairdocs.org/sdr/EW72006F00000.md): Turbine · overtemp · Jan 4, 2006 · N888LV · Gulstm G1159A · Turbine Section
  > DURING 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)
- [SDR CA051014002](https://openairdocs.org/sdr/CA051014002.md): Blades · damaged · Oct 12, 2005 · Gulstm G1159 · Turbine Engine Compressor Section
  > GII 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 NU
- [SDR 2005FA0001476](https://openairdocs.org/sdr/2005FA0001476.md): O-Ring · leaking · Sep 11, 2005 · N165ST · Gulstm GIV · Hydraulic System, Main
  > HYD 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 NOT
- [SDR N382005F00004](https://openairdocs.org/sdr/N382005F00004.md): Starter · melted · Jul 19, 2005 · N95SJ · Gulstm G1159B · Engine Starter
  > LT 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)
- [SDR UG82005F00004](https://openairdocs.org/sdr/UG82005F00004.md): Tire · mismanufactured · Jul 11, 2005 · N473KT · Gulstm G1159A · Tire
  > NR 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 W
- [SDR 2005FA0001034](https://openairdocs.org/sdr/2005FA0001034.md): Proximity Switch · loose · Jun 11, 2005 · N900DH · Gulstm G1159 · Landing Gear Position and Warning
  > AC 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.
- [SDR O2G2004F00010](https://openairdocs.org/sdr/O2G2004F00010.md): Windshield · failed · Nov 21, 2004 · N590DA · Gulstm G1159A · Flight Compartment Windows
  > RT WINDSHIELD OUTER PANE FAILED, DURING FLIGHT. REMOVED AND REPLACED WINDSHIELD. (NE03200504208)
- [SDR O2G2004F00006](https://openairdocs.org/sdr/O2G2004F00006.md): Line · leaking · Oct 14, 2004 · N624BP · Gulstm GIV · Engine Pressure Ratio (EPR)
  > RT ENGINE WOULD NOT MAKE EPR OF THE DAY, RETORQUE P3 SPLITTER. PERFORMED ENGINE POWER RUN, OPS CK GOOD.
- [SDR O2G2004F00005](https://openairdocs.org/sdr/O2G2004F00005.md): Converter · failed · Oct 11, 2004 · N590DA · Gulstm G1159A · Cabin Pressure Control System
  > RT CONVERTER FAILED AND LOST AUTO CONTROL OF PRESSUREIZATION. RAN CHECKLIST SEVERAL TIMES WITH NO EFFECT. REMOVE AND REPLACED CONVERTER.
- [SDR 2005FA0000103](https://openairdocs.org/sdr/2005FA0000103.md): Skin · corroded · Sep 2, 2004 · N826GW · Gulstm G1159 · Wing, Plate/Skin
  > DURING 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.
- [SDR 2005FA0000104](https://openairdocs.org/sdr/2005FA0000104.md): Cowling · corroded · Sep 2, 2004 · N826GW · Gulstm G1159 · Nacelle/Pylon, Plate/Skin
  > DURING LT ENGINE MID-LIFE UPDATES, LT FIXED COWL WAS INSPECTED AND CORROSION WAS NOTED. FIXED COWL WAS REPAIRED.
- [SDR 2005FA0000267](https://openairdocs.org/sdr/2005FA0000267.md): Bulkhead · cracked · Sep 2, 2004 · N826GW · Gulstm G1159 · Fuselage Main, Bulkhead
  > DURING 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.
- [SDR 2005FA0000268](https://openairdocs.org/sdr/2005FA0000268.md): Panel · corroded · Sep 2, 2004 · N826GW · Gulstm G1159 · Wing, Plate/Skin
  > DURING 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.
- [SDR 2005FA0000269](https://openairdocs.org/sdr/2005FA0000269.md): Cowling · corroded · Sep 2, 2004 · N826GW · Gulstm G1159 · Nacelle/Pylon, Plate/Skin
  > DURING RT ENGINE MID-LIFE UPDATES, RT FIXED COWL WAS INSPECTED AND CORROSION WAS NOTED. FIXED COWL WAS REPAIRED.
- [SDR IV42004F00000](https://openairdocs.org/sdr/IV42004F00000.md): Bearing · failed · Aug 31, 2004 · N949NA · Gulstm G1159 · DC Generating System
  > DURING 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 AP
- [SDR N3B2004F00000](https://openairdocs.org/sdr/N3B2004F00000.md): Tire · blown · Jul 16, 2004 · N510SR · Gulstm G1159B · Tire
  > LT 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.
- [SDR 2004F00234](https://openairdocs.org/sdr/2004F00234.md): Windscreen · cracked · Jul 7, 2004 · N1NA · Gulstm G1159A · Flight Compartment Windows
  > WINDSCREEN CRACK DURING FLIGHT.
- [SDR 2004F00233](https://openairdocs.org/sdr/2004F00233.md): Duct · separated · Jul 2, 2004 · N1NA · Gulstm G1159A · Pneumatic Distribution System
  > COUPLING SEPARATED FROM END OF APU/GROUND START APU DUCT ASSY.
- [SDR PA04002](https://openairdocs.org/sdr/PA04002.md): Circuit Card · dirty · Apr 19, 2004 · N473KT · Gulstm G1159A · Central Warning
  > AURAL 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
- [SDR ET72004F00000](https://openairdocs.org/sdr/ET72004F00000.md): Heat Shield · delaminated · Mar 31, 2004 · N668JT · Gulstm G1159 · Engine Cowling System
  > NOTED 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 COR
- [SDR 2003FA0001159](https://openairdocs.org/sdr/2003FA0001159.md): Indicator · misrepaired · Oct 29, 2003 · N80J · Gulstm G1159A · Engine Bleed Air System
  > EVERYTIME 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)
- [SDR ZLW2004F00000](https://openairdocs.org/sdr/ZLW2004F00000.md): Pitot Line · clogged · Sep 23, 2003 · N36MW · Gulstm G1159 · Pitot/Static System
  > AC 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 NIT
- [SDR 2003FA0001234](https://openairdocs.org/sdr/2003FA0001234.md): Actuator · stuck · Sep 18, 2003 · N388CW · Gulstm G1159A · Stabilizer Actuator
  > DURING 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) W
- [SDR CA030613001](https://openairdocs.org/sdr/CA030613001.md): Tube · sheared · Jun 11, 2003 · Gulstm G1159A · Trailing Edge Flap Actuator
  > (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.
- [SDR CA030611004](https://openairdocs.org/sdr/CA030611004.md): Ring · cracked · Jun 11, 2003 · Gulstm G1159 · Engine Mount Section
  > (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 TR
- [SDR CA030409008](https://openairdocs.org/sdr/CA030409008.md): Tube · chafed · Apr 3, 2003 · Gulstm G1159A · Hydraulic System, Main
  > (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 SHO
- [SDR CA030507005](https://openairdocs.org/sdr/CA030507005.md): Bolt · broken · Apr 3, 2003 · Gulstm G1159B · Turbine Section
  > (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
- [SDR CA030324010](https://openairdocs.org/sdr/CA030324010.md): Bolt · failed · Mar 24, 2003 · Gulstm G1159 · Turbine Engine Compressor Section
  > (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. MI
- [SDR VZG2003F00000](https://openairdocs.org/sdr/VZG2003F00000.md): Control Valve · inoperative · Mar 12, 2003 · N444GA · Gulstm G1159A · Landing Gear Door Retract Section
  > NOSE 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 WAS
- [SDR NASA51181](https://openairdocs.org/sdr/NASA51181.md): Nut · missing · Mar 7, 2003 · N848NA · Gulstm G1159 · Engine (Turbine/Turboprop)
  > IN 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 F
- [SDR ZLW2003F00000](https://openairdocs.org/sdr/ZLW2003F00000.md): Floorbeam · cracked · Mar 4, 2003 · N622RR · Gulstm G1159 · Fuselage Main, Floor Beam
  > DURING 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.

Next page: https://openairdocs.org/engine/rolls-royce-spey-511-8/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/rolls-royce-spey-511-8/reports

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