# Airworthiness Directives; Rolls-Royce Deutschland (RRD) (Formerly Rolls-Royce, plc) Tay 611-8, Tay 620-15, Tay 620-15/20, Tay 650-15, Tay 650-15/10, and Tay 651-54 Turbofan Engines; Correction
> **Rule** · Final rule; correction. · Published 2005-01-26 · Effective 2005-01-26 · 70 FR 3614
## Document
- **Document number:** 05-1392
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 70 FR 3614
- **Publication date:** 2005-01-26
- **Effective date:** 2005-01-26
- **FAA docket:** Docket No. 2004-NE-11-AD
## Abstract

This document makes corrections to Airworthiness Directive (AD) 2004-26-10. That AD applies to certain RRD Tay 611-8, Tay 620-15, Tay 620-15/20, Tay 650-15, Tay 650-15/10, and Tay 651-54 turbofan engines with ice-impact panels installed in the low pressure (LP) compressor case. That AD was published in the Federal Register on January 6, 2005 (70 FR 1172). This document corrects the same service bulletin paragraph number reference in 17 locations of the compliance section. This document also corrects an inspection limit and a service bulletin number in the compliance section. In all other respects, the original document remains the same.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2005/01/26/05-1392/airworthiness-directives-rolls-royce-deutschland-rrd-formerly-rolls-royce-plc-tay-611-8-tay-620-15)
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