# Proposed AD FAA-2007-0037: Rolls-Royce Deutschland Ltd. & Co. KG (RRD) Models Tay 650-15 and Tay 651-54 Turbofan Engines

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2008-10-14
- Products: Rolls-Royce Deutschland
- Product type: Engine
- Action: Notice of proposed rulemaking (NPRM).
- Published: May 6, 2010, 75 FR 24825
- Comments due: June 21, 2010
- Became: [AD 2008-10-14](https://openairdocs.org/ad/2008-10-14)
- Docket: FAA-2007-0037 (https://www.regulations.gov/docket/FAA-2007-0037, where comments are filed)
- Project: 2007-NE-41-AD
- FR document: 2010-10739
- Official PDF: https://openairdocs.org/files/sha256/d2/01/d2014c5a3faa0ed92f834e57df85612e5bb854e0894fa45900da1f8dfcb738b3 (from https://www.govinfo.gov/content/pkg/FR-2010-05-06/pdf/2010-10739.pdf)
- Federal Register: https://www.federalregister.gov/documents/2010/05/06/2010-10739/airworthiness-directives-rolls-royce-deutschland-ltd-and-co-kg-rrd-models-tay-650-15-and-tay-651-54
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AF7331DF95265FB98625771B0051DC92.0001
- Page: https://openairdocs.org/proposed/FAA-2007-0037

## Summary

We propose to supersede an existing airworthiness directive (AD) for Tay 650-15 turbofan engines. That AD currently requires initial and repetitive inspections of the low-pressure (LP) turbine discs stage 2 and stage 3 for corrosion, on certain Tay 650-15 serial number engines. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: Strip results from some of the engines listed in the applicability section of this AD revealed excessively corroded low-pressure turbine disks stage 2 and stage 3. The corrosion is considered to be caused by the environment in which these engines are operated. Following a life assessment based on the strip findings it is concluded that inspections for corrosion attack are required. The action specified by this European Aviation Safety Agency (EASA) AD 2008-0122was intended to avoid a failure of a low- pressure turbine disk stage 2 or stage 3 due to potential corrosion problems which could result in uncontained engine failure and damage to the airplane. It has been later realized that the same unsafe condition could potentially occur on more serial numbers for the Tay 650-15 engines and on the Tay 651-54 engines. This AD, superseding EASA AD 2008-0122, retaining its requirements, is therefore issued to expand the Applicability in adding further engine serial numbers for the Tay 650-15 engines and in adding the Tay 651-54 engines. We are proposing this AD to detect corrosion that could cause the stage 2 or stage 3 disk of the LP turbine to fail and result in an uncontained failure of the engine.

## Notices in this docket

- Jan 2, 2008: Notice of proposed rulemaking (NPRM). (first notice), FR document E7-25457, comments due Feb 1, 2008 (https://www.federalregister.gov/documents/2008/01/02/E7-25457/airworthiness-directives-rolls-royce-deutschland-ltd-and-co-kg-rrd-tay-650-15-turbofan-engines)
- May 6, 2010: Notice of proposed rulemaking (NPRM)., FR document 2010-10739, comments due Jun 21, 2010 (https://www.federalregister.gov/documents/2010/05/06/2010-10739/airworthiness-directives-rolls-royce-deutschland-ltd-and-co-kg-rrd-models-tay-650-15-and-tay-651-54)

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