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Airworthiness Directives; Rolls-Royce plc RB211-524D4 Series Turbofan Engines

airworthiness · Rule · Final rule; request for comments. · Published 2000-09-07 · Effective 2000-09-22 · 65 FR 54143

Document

Document number
00-22610
Federal Register citation
65 FR 54143
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Rolls-Royce plc RB211-524D4 Series Turbofan
Publication date
2000-09-07
Effective date
2000-09-22
FAA docket
Docket No. 2000-NE-23-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to Rolls-Royce plc models RB211-524D4-19, -524D4-B-19, - 524D4-B-39, -524D4X-19, and 524D4X-B-19 turbofan engines with a cold stream nozzle assembly Part Number (PN) LJ32826 installed. This action requires inspection for cracks and repair of the cold stream nozzle assembly longitudinal flange. This amendment is prompted by a report of the loss of a large section of cold stream nozzle assembly in flight. The actions specified in this AD are intended to detect cracks that could result in failure of the cold stream nozzle assembly, possible release of cold stream nozzle debris from the engine, and possible damage to airplane control surfaces.

Source

Authoritative
Federal Register document
Machine
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