Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
airworthiness · Rule · Final rule; request for comments. · Published 2024-04-09 · Effective 2024-04-15 · 89 FR 24691
Document
Document number
2024-07433
Federal Register citation
89 FR 24691
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Rolls-Royce Deutschland Ltd & Co KG
Publication date
2024-04-09
Effective date
2024-04-15
FAA docket
Docket No. FAA-2024-0993
Abstract
The FAA is adopting a new airworthiness directive (AD) for all Rolls-Royce Deutschland Ltd & Co KG (RRD) Model RB211-524H-36 and RB211-524H-T-36 engines. This AD was prompted by reports of engine surges and a subsequent investigation which found that the surges may have been caused by material loss on the high-pressure compressor (HPC) stage 1 and stage 2 rotor path liners. This AD requires borescope inspections (BSIs) of the HPC stage 1 and stage 2 rotor path liners for material loss, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.