# Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Tay 611-8, Tay 611-8C, Tay 620-15, Tay 650-15, and Tay 651-54 Turbofan Engines
> **Rule** · Final rule. · Published 2008-01-07 · Effective 2008-02-11 · 73 FR 1048
## Document
- **Document number:** E7-25497
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 73 FR 1048
- **Publication date:** 2008-01-07
- **Effective date:** 2008-02-11
- **FAA docket:** Docket No. FAA-2007-27811
## Abstract

The FAA is superseding an existing airworthiness directive (AD) for Rolls-Royce Deutschland Ltd & Co KG (RRD) Tay 611-8, Tay 620- 15, Tay 650-15, and Tay 651-54 turbofan engines. That AD currently requires initial and repetitive visual inspections of all ice-impact panels and fillers in the low pressure (LP) compressor case for certain conditions and replacing, as necessary, any or all panels. This AD requires the same actions, provides terminating action to those repetitive actions, and adds the Tay 611-8C turbofan engine to the applicability. This AD results from RRD introducing new LP compressor case ice-impact panels with additional retention features to these Tay turbofan engines. We are issuing this AD to prevent release of ice- impact panels due to improper bonding that can result in loss of thrust in both engines.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2008/01/07/E7-25497/airworthiness-directives-rolls-royce-deutschland-ltd-and-co-kg-tay-611-8-tay-611-8c-tay-620-15-tay)
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