# Rolls-Royce SPEY-555-15P

- Type: Engine model (FAA registry)
- Registry code: 54065
- Manufacturer (registry): ROLLS-ROYC
- Model: SPEY 555-15P
- Engine type: Turbo-jet
- Power: 9,900 hp
- Data sheet: [TCDS E2EU](https://openairdocs.org/tcds/E2EU) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-spey-555-15p

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 2017-10-25](https://openairdocs.org/ad/2017-10-25): Turbine Engine Compressor · Rolls-Royce Deutschland Spey 506-14A, Spey 555-15, Spey 555-15H and 2 more. Effective Jun 12, 2017
- [AD 2004-24-05](https://openairdocs.org/ad/2004-24-05): Split low pressure (LP) compressor case · Rolls-Royce Deutschland Spey 555-15, Spey 555-15H, Spey 555-15N and 1 more. Effective Dec 29, 2004
- [AD 2002-18-03](https://openairdocs.org/ad/2002-18-03): Stage 2 LPT Blades · Rolls-Royce Deutschland Spey 506-14A, Spey 555-15, Spey 555-15H and 2 more. Effective Oct 16, 2002
- [AD 2000-23-11](https://openairdocs.org/ad/2000-23-11): Disk Drive Arm · Rolls-Royce Deutschland Spey 555-15, Spey 555-15H, Spey 555-15N and 1 more. Effective Dec 20, 2000
- [AD 94-25-09](https://openairdocs.org/ad/94-25-09): High Pressure Compressor Disk · Rolls-Royce Deutschland Spey 506-14, Spey 506-14A, Spey 506-14D and 6 more. Effective Feb 17, 1995
- [AD 94-23-09](https://openairdocs.org/ad/94-23-09): High Pressure Compressor Disks · Rolls-Royce Deutschland Spey 506-14, Spey 506-14A, Spey 506-14D and 6 more. Effective Jan 6, 1995
- [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 86-11-03](https://openairdocs.org/ad/86-11-03): Stage 12 HPC Disks And Rotor Seals, And LPC Drive Shafts · Rolls-Royce Deutschland Spey 555-15, Spey 555-15H, Spey 555-15N and 1 more. Effective Jun 20, 1986
- [AD 72-20-07](https://openairdocs.org/ad/72-20-07): Fuel Tubes · Rolls-Royce Deutschland Spey 555-15, Spey 555-15H, Spey 555-15N and 1 more. Effective Oct 2, 1972

## Registered aircraft

None registered with this engine model now.

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (20)

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

- [SDR YRRR2016FA0000052](https://openairdocs.org/sdr/YRRR2016FA0000052), Jan 22, 2016: BLADE. FAILED. UPON DISASSEMBLY OF ENGINE POST TEST RUN, DAMAGE TO THE LPT MODULE WAS NOTICED. IT APPEARS THAT THE LPT2 BLADE FAILED CAUSING SUBSTANTIAL DAMAGE TO THE SET, 79 
- [SDR CA070613001](https://openairdocs.org/sdr/CA070613001), Jun 12, 2007: DUCT. MISREPAIRED. (CAN) ENGINE FRONT BYPASS DUCT FOUND AT INSPECTION WITH NON STANDARD REPAIR OUTSIDE OEM LIMITATION. PATCH REPAIR ON OUTSIDE WALL 8 INCH LONG BY 2.5 INCH WIDE OU
- [SDR BUE2007F00002](https://openairdocs.org/sdr/BUE2007F00002), Feb 8, 2007: BOLT. SHEARED. ( REF NR: 287N416WM) DURING INSPECTION FOUND THE RT EJECTOR OB BEARING FITTING UPPER BOLT SHEARED, LOWER BOLT BENT/BEGINNING TO SHEAR, IB BEARING FITTING UPPER 
- [SDR BUE2005F00000](https://openairdocs.org/sdr/BUE2005F00000), Nov 1, 2004: ENGINE. VIBRATION. NR 1 ENGINE VIBRATION THEN EGT STARTED RAISING TOWARD UPPER LIMITS, ENGINE DID NOT RESPOND TO ENGINE EGT CHECK LIST, SO THE ENGINE WAS SHUT DOWN.
- [SDR QXEA0101419](https://openairdocs.org/sdr/QXEA0101419), Aug 29, 2001: FIRE LOOP. SHORTED. BIL - ENROUTE FROM BIL TO SEA THE NR 2 FIRE WARNING SOUNDED AND LIGHT UP. PERFORMED ENGINE FIRE CHECK LIST, SHUTING DOWN NR 2 ENGINE. AFTER PULLING THE FIRE CON
- [SDR QXEA0100625](https://openairdocs.org/sdr/QXEA0100625), Apr 20, 2001: ENGINE. VIBRATION. YYC - ON CLIMBOUT FROM YYC ENGINE VIBRATION AND CABIN FILLED WITH SMOKE. RETURNED TO FIELD. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE. OPERATIONAL CH
- [SDR CA001005009](https://openairdocs.org/sdr/CA001005009), Aug 8, 2000: REGULATOR. FAILED. (CAN) AFTER TAKEOFF, THE FLIGHT CREW WAS UNABLE TO THROTTLE BACK THE ENGINE. THEY SUBSEQUENTLY SHUT THE ENGINE DOWN AND RETURNED TO FIELD. REPLACEMENT OF FUEL F
- [SDR QXEA9900509](https://openairdocs.org/sdr/QXEA9900509), Mar 20, 1999: TURBINE BLADE. FAILED. MWH - A/C EN ROUTE FROM SEA TO BIL, WHILE CLIMBING THROUGH 26,000 FT HEARD A BANG AND RIGHT ENGINE BEGAN TO VIBRATE, TGT ON RISE. SHUT DOWN ENGINE AND DIVERTED 
- [SDR CA990318012](https://openairdocs.org/sdr/CA990318012), Mar 7, 1999: BLADE. FAILED. (CAN) IN CRUISE AT FL 325, THE CREW HEARD A LOUD BANG FROM NR 1 ENGINE, FOLLOWED BY ALL ENGINE PARAMETERS DROPPING OFF. ENGINE WAS SHUTDOWN AND AIRCRAFT CONTINU
- [SDR CA990318070](https://openairdocs.org/sdr/CA990318070), Mar 7, 1999: TURBINE BLADE. FAILED. (CAN) NR 1 ENGINE SHUTDOWN IN-FLIGHT, REPORTED LP TURBINE BLADE FAILURE. NO OTHER INFO AVAILABLE. FURTHER REPORT TO FOLLOW.
- [SDR QXEA9700578](https://openairdocs.org/sdr/QXEA9700578), Sep 19, 1997: ENGINE. SMOKING. PDX- TOWER REPORTED SMOKE FROM AIRCRAFT DURING FIRST 300 TO 400 FEET OF TAKEOFF. GROUND RAN ENGINE AT HIGH POWER FOR SEVERAL MINUTES, NO EXCESSIVE SMOKE NOTED. 
- [SDR QXEA9700570](https://openairdocs.org/sdr/QXEA9700570), Sep 16, 1997: FIRE LOOP. MALFUNCTION. BOI- NR 1 ENGINE FIRE WARNING ON CLIMBOUT AT 15,000 FEET. FOLLOWED FIRE PROCEDURE CHECKLIST. DISCHARGED FIRE BOTTLE. WARNING LIGHT WENT OUT 3 SECONDS AFTER BOTT
- [SDR QXEA9700426](https://openairdocs.org/sdr/QXEA9700426), Aug 3, 1997: ENGINE. SMOKING. CONTROL TOWER REPORTED EXCESSIVE SMOKE FROM THE NR 2 ENGINE ON TAKEOFF ROLL. THE SMOKE THEN DISIPATED. ABORTED TAKEOFF AND RETURNED TO THE GATE. ENGINE OIL LEVE
- [SDR A21A9649001](https://openairdocs.org/sdr/A21A9649001), Jul 31, 1996: OIL TANK. LEAKING. TEAR DOWN REPORT CONFIRMS MULTIPLE OIL LEAKS IN AREA OF OIL TANK POSSIBLY MIGRATING INTO INLET PLENNUM WHICH CAUSED SMOKE OUT THE BLEED AIR AND TAILPIPE. (M)
- [SDR USAAF96065](https://openairdocs.org/sdr/USAAF96065), Jun 24, 1996: FUEL NOZZLE. BURNED. CLT - FLT 464 - AFTER TAKEOFF, THE NR 1 ENGINE WOULD NOT ADVANCE TO FULL THROTTLE AFTER REACHING 8000 FEET. ENGINE SURGED AFTER 8000 FEET. FLIGHT RETURNED TO CL
- [SDR CA960123027](https://openairdocs.org/sdr/CA960123027), Jan 2, 1996: ENGINE. MAKING METAL. (CAN)VIBRATIONS FELT AT FL250. POWER REDUCED FROM 94 PERCENT TO 91 PERCENT & VIBRATIONS INCREASED. ENGINE WAS SHUTDOWN & FLIGHT DIVERTED. POST FLIGHT INSPECTION
- [SDR USAAF95009](https://openairdocs.org/sdr/USAAF95009), Dec 31, 1995: ENGINE. VIBRATING. CRW - FL 551 - EN ROUTE CLE-CLT, CREW EXPERIENCED VIBRATION FROM RIGHT ENGINE. UPON POWER REDUCTION, THE VIBRATION BECAME SEVERE. CREW SHUT DOWN ENGINE (SET 12 
- [SDR USAAF95003](https://openairdocs.org/sdr/USAAF95003), Oct 22, 1995: FUEL FLOW REG. FAILED. CLT - FLT NR 379 - AFTER TAKEOFF, CLIMBING THROUGH FL 100, THE CREW FELT AND ENGINE VIBRATION. THERE WAS A DROP IN EGT, DROP IN FUEL FLOW AND A DROP IN LP RPM. 
- [SDR USAA951041](https://openairdocs.org/sdr/USAA951041), Sep 28, 1995: O-RING. CUT. GSO - FLT NR 735 - NR 1 ENGINE SHUT DOWN ON SHORT FINAL DUE TO CSD LIGHT, LOW OIL PRESSURE AND DECAYING RPM TO 38 PERCENT HP RPM. FOUND O-RING CUT AND LEAKING F
- [SDR USAA950576](https://openairdocs.org/sdr/USAA950576), Jun 8, 1995: COMPRESSOR. STALLED. CLT - FLT 0456 - WHILE CLIMBING OUT OF CLT, FLIGHT ENCOUNTERED A COMPERSSOR STALL. THE CAPTAIN POWERED BACK TO IDLE THEN UP AGAIN AND GOT ANOTHER COMPRESSOR STA

## PMA parts (OpenAirDocs) (2)

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

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