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Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines; Correction

airworthiness · Rule · Final rule; correction. · Published 2006-10-03 · Effective 2006-10-03 · 71 FR 58254

Document

Document number
E6-16235
Federal Register citation
71 FR 58254
Type
Rule
Action
Final rule; correction.
Category
airworthiness
Manufacturer
Rolls-Royce plc RB211 Series Turbofan
Publication date
2006-10-03
Effective date
2006-10-03
FAA docket
Docket No. 2003-NE-12-AD

Abstract

This document makes a correction to Airworthiness Directive (AD) 2006-11-05 applicable to Rolls-Royce plc (RR) RB211-22B series, RB211-524B, -524C2, -524D4, -524G2, -524G3, and -524H series, and RB211-535C and -535E series turbofan engines with high pressure compressor (HPC) stage 3 disc assemblies, part numbers (P/Ns) LK46210, LK58278, LK67634, LK76036, UL11706, UL15358, UL22577, UL22578, and UL24738 installed. That AD published in the Federal Register on May 23, 2006 (71 FR 29586). The "-524B-02, B-B-02, B3-02, and B4 series, Pre SB No. 72-7730" in the Regulatory section is incorrect. This document corrects that requirement. In all other respects, the original document remains the same.

Source

Authoritative
Federal Register document
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