Rolls-Royce Spey 555-15
Rolls-Royce Spey 555-15 is the baseline Spey 500-series turbofan model, distinct from the uprated 555-15H, 555-15N, and 555-15P variants. EASA.E.064 records a two-spool architecture with one five-stage low-pressure compressor and one twelve-stage high-pressure compressor, a 43.81 kN maximum take-off static rating, and a 42.12 kN maximum continuous rating under sea-level ISA test conditions. EASA.A.037 records the exact twin-engine F28 installation for Mark 1000/1000C, 2000, and 3000R/RC aircraft; lifecycle remains unknown because certification and continuing-airworthiness records do not establish current production or universal in-service status.
Identity
- Aliases
- Spey 555-15RB.183 Mk 555-15RB 183 Mk 555-15
- Domains
- aviation
- Identity Level
- model
- Kind
- turbofan
- Name
- Rolls-Royce Spey 555-15
- Status
- unknown
Details
- Air Breathing Specs
- Max Thrust Kn
- 43.81
- Sea Level Static Thrust Kn
- 43.81
- Spool Count
- 2
- Description
- Rolls-Royce Spey 555-15 is the baseline Spey 500-series turbofan model, distinct from the uprated 555-15H, 555-15N, and 555-15P variants. EASA.E.064 records a two-spool architecture with one five-stage low-pressure compressor and one twelve-stage high-pressure compressor, a 43.81 kN maximum take-off static rating, and a 42.12 kN maximum continuous rating under sea-level ISA test conditions. EASA.A.037 records the exact twin-engine F28 installation for Mark 1000/1000C, 2000, and 3000R/RC aircraft; lifecycle remains unknown because certification and continuing-airworthiness records do not establish current production or universal in-service status.
- Developers
- Family
- Manufacturers
Links
Assets & Meta
- Creation Time
- July 30, 2026 at 04:11:19 UTC
- Updated Time
- August 21, 2026 at 00:50:05 UTC
Other
- Sources
- Accessed Date
- 2026-07-29
- Note
- Establishes Spey 555-15, 555-15H, 555-15N, and 555-15P as separate certified Spey 500-series models.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.E.064 — Rolls-Royce Deutschland Spey 500 series engines
- Accessed Date
- 2026-07-29
- Note
- Maps every F28 Fellowship mark to exact twin Spey 555-15, 555-15N, 555-15H, or 555-15P installations and identifies the service-bulletin modification paths.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.A.037 — Fokker F28
- Accessed Date
- 2026-08-20
- Note
- EASA.E.064 Issue 02 identifies the Spey 555-15 type-certification date, two-spool compressor/turbine architecture, 43.81 kN maximum take-off static rating, 42.12 kN maximum continuous rating, and 555-15-specific operating, maintenance, overhaul, and life-limited-parts manual references.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.E.064 Issue 02 — Spey 500 series engines (direct TCDS PDF)