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

airworthiness · Rule · Final rule; request for comments. · Published 2026-01-12 · Effective 2026-01-27 · 91 FR 1082

Document

Document number
2026-00333
Federal Register citation
91 FR 1082
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Rolls-Royce Deutschland Ltd & Co KG
Publication date
2026-01-12
Effective date
2026-01-27
FAA docket
Docket No. FAA-2025-5398

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Rolls-Royce Deutschland Ltd & Co KG (RRD) Model Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE, Trent 1000-D, Trent 1000-E, Trent 1000-G, and Trent 1000-H engines. This AD was prompted by a determination made by the manufacturer that a high-pressure compressor (HPC) mini-disc anti-rotation block could possibly release into the HPC assembly stage 5 and 6 discs and the cone rotor rear shaft (HPC rear drum) during an engine operation. This AD requires repetitive borescope inspections (BSIs) of the HPC rear drum cavity and cavities between each HPC rotor disc, and depending on the results of inspection, removal of the engine from service. This AD also allows an alternative method of complying with the repetitive BSIs if certain actions are accomplished. The FAA is issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
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