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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

airworthiness · Rule · Final rule. · Published 2008-01-07 · Effective 2008-02-11 · 73 FR 1048

Document

Document number
E7-25497
Federal Register citation
73 FR 1048
Type
Rule
Action
Final rule.
Category
airworthiness
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

Authoritative
Federal Register document
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