Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines
airworthiness · Rule · Final rule; request for comments. · Published 2003-05-15 · Effective 2003-06-19 · 68 FR 26201
Document
Document number
03-11974
Federal Register citation
68 FR 26201
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Rolls-Royce plc RB211 Series Turbofan
Publication date
2003-05-15
Effective date
2003-06-19
FAA docket
Docket No. 2003-NE-15-AD
Abstract
The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce plc (RR) RB211-524C2-19 and RB211-524C2-B-19 series turbofan engines. This AD requires replacing the existing low pressure (LP) compressor location bearing assembly, intermediate pressure (IP) compressor location bearing, IP compressor bearing support housing, IP compressor rear stub shaft, LP compressor location bearing support, oil transfer connector assembly, hydraulic oil seal housing, and hydraulic oil seal with improved design parts. This AD is prompted by statistical analysis by the manufacturer of in-service premature bearing failures. The actions specified in this AD are intended to prevent LP compressor failure and uncontained disc failures, resulting in damage to the airplane.