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

airworthiness · Rule · Final rule; request for comments. · Published 2019-08-27 · Effective 2019-09-11 · 84 FR 44683

Document

Document number
2019-18340
Federal Register citation
84 FR 44683
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Rolls-Royce Deutschland Ltd & Co KG Turbofan
Publication date
2019-08-27
Effective date
2019-09-11
FAA docket
Docket No. FAA-2019-0528

Abstract

The FAA is superseding airworthiness directive (AD) 2018-25-01 for all Rolls-Royce plc (RR) Trent 1000-A, Trent 1000-C, Trent 1000-D, Trent 1000-E, Trent 1000-G, and Trent 1000-H turbofan model engines. AD 2018-25-01 required initial and repetitive inspections of the intermediate-pressure compressor (IPC) stage 1 rotor (R1) blades, IPC stage 2 rotor (R2) blades, and IPC shaft stage 2 dovetail posts, and removing any cracked parts from service. This AD retains those inspections, revises certain reinspection intervals, and adds certain engine models to the applicability. This AD was prompted by a determination by the manufacturer of the need to revise inspection intervals for certain affected engines. In addition, the FAA added recently validated additional engine models to the applicability. The FAA is issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
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