# Rolls-Royce SPEY-511-8

- Type: Engine model (FAA registry)
- Registry code: 54069
- Manufacturer (registry): ROLLS-ROYC
- Model: SPEY 511-8
- Engine type: Turbo-jet
- Power: 11,400 lb thrust
- Data sheet: [TCDS E2EU](https://openairdocs.org/tcds/E2EU) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 15 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-spey-511-8

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2013-05-20](https://openairdocs.org/ad/2013-05-20): Bolts · Rolls-Royce Deutschland Spey 511-8. Effective Apr 24, 2013
- [AD 87-18-07](https://openairdocs.org/ad/87-18-07): Primary Airscoop · Rolls-Royce Deutschland Spey 506-14, Spey 506-14A, Spey 506-14D and 8 more. Effective Sep 28, 1987
- [AD 78-16-07](https://openairdocs.org/ad/78-16-07): High Pressure Fuel shutoff Valves · Rolls-Royce Deutschland Spey 511-8. Effective Aug 21, 1978
- [AD 68-17-05](https://openairdocs.org/ad/68-17-05): Air System Center Section Duct · Rolls-Royce Deutschland Spey 506-14, Spey 511-14 and Spey 511-8. Effective Jun 28, 1972

## Registered aircraft (15)

- [N105TB](https://openairdocs.org/aircraft/N105TB): [Air Force Material Command Esc/Dikl](https://openairdocs.org/faa-owner/AIR%20FORCE%20MATERIAL%20COMMAND%20ESC%2FDIKL), [Hanscom Afb, MA](https://openairdocs.org/faa-place/MA/Hanscom%20Afb), built 1968, S/N 31
- [N164PA](https://openairdocs.org/aircraft/N164PA): [Phoenix Air Group Inc](https://openairdocs.org/faa-owner/PHOENIX%20AIR%20GROUP%20INC), [Cartersville, GA](https://openairdocs.org/faa-place/GA/Cartersville), built 1979, S/N 257
- [N165PA](https://openairdocs.org/aircraft/N165PA): [Rca LLC](https://openairdocs.org/faa-owner/RCA%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1969, S/N 775
- [N178B](https://openairdocs.org/aircraft/N178B): [Missile Defense Agency (Mda)](https://openairdocs.org/faa-owner/MISSILE%20DEFENSE%20AGENCY%20(MDA)), [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa), built 1973, S/N 125
- [N17LK](https://openairdocs.org/aircraft/N17LK): [Aircraft Holding Solutions LLC Trustee](https://openairdocs.org/faa-owner/AIRCRAFT%20HOLDING%20SOLUTIONS%20LLC%20TRUSTEE), [Newark, DE](https://openairdocs.org/faa-place/DE/Newark), built 1984, S/N 431
- [N183PA](https://openairdocs.org/aircraft/N183PA): [Sandy Wings LLC](https://openairdocs.org/faa-owner/SANDY%20WINGS%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1984, S/N 385
- [N184PA](https://openairdocs.org/aircraft/N184PA): [Bartowjets LLC](https://openairdocs.org/faa-owner/BARTOWJETS%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1981, S/N 318
- [N218EE](https://openairdocs.org/aircraft/N218EE): [Solomon Mark Trustee](https://openairdocs.org/faa-owner/SOLOMON%20MARK%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1986, S/N 489
- [N305LR](https://openairdocs.org/aircraft/N305LR): [Aircraft Holding Solutions LLC Trustee](https://openairdocs.org/faa-owner/AIRCRAFT%20HOLDING%20SOLUTIONS%20LLC%20TRUSTEE), [Newark, DE](https://openairdocs.org/faa-place/DE/Newark), built 1980, S/N 305
- [N550JF](https://openairdocs.org/aircraft/N550JF): [Ts Aviation LLC](https://openairdocs.org/faa-owner/TS%20AVIATION%20LLC), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York), built 1985, S/N 472
- [N710CF](https://openairdocs.org/aircraft/N710CF): [Calspan Corp](https://openairdocs.org/faa-owner/CALSPAN%20CORP), [Niagara Falls, NY](https://openairdocs.org/faa-place/NY/Niagara%20Falls), built 1984, S/N 448
- [N721CF](https://openairdocs.org/aircraft/N721CF): [Calspan Corp](https://openairdocs.org/faa-owner/CALSPAN%20CORP), [Buffalo, NY](https://openairdocs.org/faa-place/NY/Buffalo), built 1984, S/N 429
- [N74A](https://openairdocs.org/aircraft/N74A): [Missile Defense Agency (Mda)](https://openairdocs.org/faa-owner/MISSILE%20DEFENSE%20AGENCY%20(MDA)), [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa), built 1968, S/N 36
- [N779LC](https://openairdocs.org/aircraft/N779LC): [Tulsa Technology Center School District No 18](https://openairdocs.org/faa-owner/TULSA%20TECHNOLOGY%20CENTER%20SCHOOL%20DISTRICT%20NO%2018), [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa), built 1970, S/N 88
- [N888WE](https://openairdocs.org/aircraft/N888WE): [Prime Aircraft & Aviation LLC](https://openairdocs.org/faa-owner/PRIME%20AIRCRAFT%20%26%20AVIATION%20LLC), [Edmond, OK](https://openairdocs.org/faa-place/OK/Edmond), S/N 394

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19940920035419I](https://openairdocs.org/incident/19940920035419I), Sep 20, 1994: Gulstm G1159 (N105TB), Portsmouth, NH, Minor damage. Two right main gear tires burst on takeoff near V1.aborted. Veered left. Nose gear left runway. Damaged prior stopping

## Service difficulty reports (80, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR ESPA2019F00223](https://openairdocs.org/sdr/ESPA2019F00223), May 17, 2019: SPAR. CORRODED. FOUND CORROSION ON WING AFT SPAR AT RBS 406.
- [SDR ESPA2019F00224](https://openairdocs.org/sdr/ESPA2019F00224), May 17, 2019: WING. CORRODED. RIGHT WING HAS CORROSION ON AFT SPAR AT RBS343.
- [SDR 2017F00013](https://openairdocs.org/sdr/2017F00013), Dec 27, 2016: ENGINE. MALFUNCTIONED. 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 FLI
- [SDR ESPA2016F00081](https://openairdocs.org/sdr/ESPA2016F00081), Mar 2, 2016: SEAL. LEAKING. 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 R
- [SDR 2014FA0000466](https://openairdocs.org/sdr/2014FA0000466), Jul 10, 2014: WINDOW. FAILED. 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 DIV
- [SDR 2014FA0000254](https://openairdocs.org/sdr/2014FA0000254), Apr 10, 2014: TURBINE NOZZLE. CRACKED. 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 INDI
- [SDR AOYA20140104001](https://openairdocs.org/sdr/AOYA20140104001), Jan 4, 2014: ENGINE. POWER LOSS. 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 DR
- [SDR 2013FA0000250](https://openairdocs.org/sdr/2013FA0000250), Apr 18, 2013: FLAPPER VALVE. FAILED. 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 SU
- [SDR 2012F00077](https://openairdocs.org/sdr/2012F00077), Apr 17, 2012: SKIN. DENTED. 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), Jan 16, 2011: ENGINE. FLAMED OUT. 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 DESCE
- [SDR EYDAN128KGC1FOD](https://openairdocs.org/sdr/EYDAN128KGC1FOD), Sep 10, 2009: COMPRESSOR. DISTORTED. 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
- [SDR WWQ2009F00000](https://openairdocs.org/sdr/WWQ2009F00000), Apr 19, 2009: ENGINE. FAILED. 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
- [SDR Y9PAN930LS82208](https://openairdocs.org/sdr/Y9PAN930LS82208), Aug 22, 2008: TRANSPONDER. INTERMITTENT. 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 PI
- [SDR YJU2008F00000](https://openairdocs.org/sdr/YJU2008F00000), Jul 7, 2008: TIRE. UNSERVICEABLE. 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 SEPARA
- [SDR ESPA100107](https://openairdocs.org/sdr/ESPA100107), Oct 17, 2007: WINDSHIELD. CRACKED. 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 DIVE
- [SDR 2007FA0000958](https://openairdocs.org/sdr/2007FA0000958), Sep 13, 2007: REGULATOR. FAILED. 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 
- [SDR Y9PAN818S83107](https://openairdocs.org/sdr/Y9PAN818S83107), Aug 31, 2007: SMOKE DETECTOR. MALFUNCTIONED. 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
- [SDR UG8A2007PA03S](https://openairdocs.org/sdr/UG8A2007PA03S), Jun 13, 2007: ATTACH FITTING. CORRODED. 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 FUSELAG
- [SDR BUE2006F00000](https://openairdocs.org/sdr/BUE2006F00000), Jul 27, 2006: ATTACH BRACKET. CRACKED. 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: INSPECT
- [SDR EW72006F00000](https://openairdocs.org/sdr/EW72006F00000), Jan 4, 2006: TURBINE. OVERTEMP. 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
- [SDR CA051014002](https://openairdocs.org/sdr/CA051014002), Oct 12, 2005: BLADES. DAMAGED. 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 
- [SDR 2005FA0001476](https://openairdocs.org/sdr/2005FA0001476), Sep 11, 2005: O-RING. LEAKING. 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 SH
- [SDR N382005F00004](https://openairdocs.org/sdr/N382005F00004), Jul 19, 2005: STARTER. MELTED. 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 I
- [SDR UG82005F00004](https://openairdocs.org/sdr/UG82005F00004), Jul 11, 2005: TIRE. MISMANUFACTURED. 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
- [SDR 2005FA0001034](https://openairdocs.org/sdr/2005FA0001034), Jun 11, 2005: PROXIMITY SWITCH. LOOSE. 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 AN
- [SDR O2G2004F00010](https://openairdocs.org/sdr/O2G2004F00010), Nov 21, 2004: WINDSHIELD. FAILED. RT WINDSHIELD OUTER PANE FAILED, DURING FLIGHT. REMOVED AND REPLACED WINDSHIELD. (NE03200504208)
- [SDR O2G2004F00006](https://openairdocs.org/sdr/O2G2004F00006), Oct 14, 2004: LINE. LEAKING. 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), Oct 11, 2004: CONVERTER. FAILED. 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), Sep 2, 2004: SKIN. CORRODED. DURING WING (RIGHT) NOT INSPECTION, EXFOLIATION CORROSION NOTED ON WING UPPER PLANK AND FRONT BEAM BETWEEN RBS 284 THRU 375. EXFOLIATION CORROSION REMOVED IAW S
- [SDR 2005FA0000104](https://openairdocs.org/sdr/2005FA0000104), Sep 2, 2004: COWLING. CORRODED. 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), Sep 2, 2004: BULKHEAD. CRACKED. 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), Sep 2, 2004: PANEL. CORRODED. 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. R
- [SDR 2005FA0000269](https://openairdocs.org/sdr/2005FA0000269), Sep 2, 2004: COWLING. CORRODED. 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), Aug 31, 2004: BEARING. FAILED. 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 FLUCTUATI
- [SDR N3B2004F00000](https://openairdocs.org/sdr/N3B2004F00000), Jul 16, 2004: TIRE. BLOWN. 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), Jul 7, 2004: WINDSCREEN. CRACKED. WINDSCREEN CRACK DURING FLIGHT.
- [SDR 2004F00233](https://openairdocs.org/sdr/2004F00233), Jul 2, 2004: DUCT. SEPARATED. COUPLING SEPARATED FROM END OF APU/GROUND START APU DUCT ASSY.
- [SDR PA04002](https://openairdocs.org/sdr/PA04002), Apr 19, 2004: CIRCUIT CARD. DIRTY. AURAL OVERSPEED WARNING CAME ON DURING TAKEOFF ROLL, LOW SPEED ABORT. THERE WAS A MALFUNCTION WITHIN THE OVERSPEED WARNING SYSTEM. THE AUDIBLE TONE GENERATOR WA
- [SDR ET72004F00000](https://openairdocs.org/sdr/ET72004F00000), Mar 31, 2004: HEAT SHIELD. DELAMINATED. 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 C
- [SDR 2003FA0001159](https://openairdocs.org/sdr/2003FA0001159), Oct 29, 2003: INDICATOR. MISREPAIRED. 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
- [SDR ZLW2004F00000](https://openairdocs.org/sdr/ZLW2004F00000), Sep 23, 2003: PITOT LINE. CLOGGED. 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 W
- [SDR 2003FA0001234](https://openairdocs.org/sdr/2003FA0001234), Sep 18, 2003: ACTUATOR. STUCK. 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 DISC
- [SDR CA030613001](https://openairdocs.org/sdr/CA030613001), Jun 11, 2003: TUBE. 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 FO
- [SDR CA030611004](https://openairdocs.org/sdr/CA030611004), Jun 11, 2003: RING. 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, ATTAC
- [SDR CA030409008](https://openairdocs.org/sdr/CA030409008), Apr 3, 2003: TUBE. 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 IDEN
- [SDR CA030507005](https://openairdocs.org/sdr/CA030507005), Apr 3, 2003: BOLT. 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 T
- [SDR CA030324010](https://openairdocs.org/sdr/CA030324010), Mar 24, 2003: BOLT. 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 
- [SDR VZG2003F00000](https://openairdocs.org/sdr/VZG2003F00000), Mar 12, 2003: CONTROL VALVE. INOPERATIVE. 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
- [SDR NASA51181](https://openairdocs.org/sdr/NASA51181), Mar 7, 2003: NUT. MISSING. 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
- [SDR ZLW2003F00000](https://openairdocs.org/sdr/ZLW2003F00000), Mar 4, 2003: FLOORBEAM. CRACKED. 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 I

All 80: https://openairdocs.org/engine/rolls-royce-spey-511-8/reports.md

## STCs that may be installed (OpenAirDocs) (3)

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SE01291LA](https://openairdocs.org/stc/SE01291LA): Installation of a Really Quiet LLC Internal Mixer Part Number RQ720100T, Revision B, dated January 25, 2000, or later FAA approved revisions, in accordance with Installation Instructions RQ73-3000-401/-402, Revision C, dated January 9, 2002, or later FAA approved revisions. This installation must be done concurrently with STC No. ST01292LA which modifies the airplane engine installation. Global United Capital LLC
- [STC SE994EA](https://openairdocs.org/stc/SE994EA): Manufacture of oil tank sight gage float. Airwork Service Division
- [STC SE748EA](https://openairdocs.org/stc/SE748EA): Installation of GLA ignition exciter. General Laboratory Association Inc

## PMA parts (OpenAirDocs) (12)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first.

- [383496-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161568686220241024194243.0001): Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces L922559 · Mar 28, 2023
- [383496-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113077720920241024194243.0001): Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 383496-1 · Mar 28, 2023
- [17343-83 860F](https://drs.faa.gov/browse/excelExternalWindow/CCBED10A550B46088525703F0054A71F.0001): Overheat Detector. Fenwal Safety Systems · Replaces 17343-83 860F · Nov 23, 2004
- [All parts listed on Dwg No. RQ720100T](https://drs.faa.gov/browse/excelExternalWindow/953EF4C1949D197E8525704A005910D5.0001): Internal Mixer. Really Quiet LLC · Modification part · Mar 21, 2002
- [1079-1](https://drs.faa.gov/browse/excelExternalWindow/2848AD6C96404FEE8525703B004FF3DB.0001): Sleeve Locating, LP Turbine. Air Concepts International · Replaces Rolls-Royce Limited EU.49442. · Dec 30, 1998
- [43503](https://drs.faa.gov/browse/excelExternalWindow/C6D504FE2AFEAE958525704C005D1172.0001): Exciter, Ignition. Unison Industries · Replaces RR 2-02J-89 · Jan 26, 1998
- [43663](https://drs.faa.gov/browse/excelExternalWindow/B9BA937D1B00E7A38525704C005D1176.0001): Exciter, Ignition. Unison Industries · Replaces RR 2-02J-089-001 · Jan 26, 1998
- [YW-90](https://drs.faa.gov/browse/excelExternalWindow/F354CDDDCBB790E88525703F004DD3D6.0001): Champion Spark Igniter. Champion Aerospace LLC · Replaces Rolls-Royce Spey L912017 · Oct 21, 1997
- [VB3402](https://drs.faa.gov/browse/excelExternalWindow/C443B12143532929852570500056B903.0001): Chip Collector. Vickers Inc, Systems Monitoring Div · Oct 13, 1997
- [43503](https://drs.faa.gov/browse/excelExternalWindow/4B3987F1CC7996D98525704C005D10A0.0001): Exciter. Unison Industries LLC · Dec 5, 1994
- [43663](https://drs.faa.gov/browse/excelExternalWindow/075D2CA77F8787088525704C005D10A2.0001): Exciter. Unison Industries LLC · Dec 5, 1994
- [FHE164E](https://drs.faa.gov/browse/excelExternalWindow/DE74B39A0183E23D8525703F004A6176.0001): Igniter. Champion Aerospace LLC · Replaces Rolls Royce CR114-2 · Dec 6, 1988

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