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Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Turbofan Engines

airworthiness · Rule · Final rule; request for comments. · Published 2012-03-23 · Effective 2012-03-23 · 77 FR 16917

Document

Document number
2012-6995
Federal Register citation
77 FR 16917
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Rolls-Royce Deutschland Ltd & Co KG Turbofan
Publication date
2012-03-23
Effective date
2012-03-23
FAA docket
Docket No. FAA-2012-0288

Abstract

We are adopting a new airworthiness directive (AD) for certain Rolls-Royce Deutschland (RRD) Models Tay 611-8 and Tay 611-8C turbofan engines. This AD requires replacement of the high-pressure (HP) turbine spanner retaining nut. This AD was prompted by the discovery that certain HP turbine spanner retaining nuts were improperly heat treated after application of silver plating. We are issuing this AD to prevent failure of the HP turbine stage 2 disc, uncontained engine failure, and damage to the airplane.

Source

Authoritative
Federal Register document
Machine
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