AD 2006-11-05

final rule

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

AD Number
2006-11-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-NE-12-AD
FR Citation
71 FR 58254
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

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

Unsafe Condition

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 "-52...

Affected Aircraft

Rolls-Royce plc 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 LK46210, LK58278, LK67634, LK76036, UL11706, UL15358, UL22577, UL22578, and UL24738 installed.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register 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.

Document Text

Show stored source text (verify against official source)
[Federal Register Volume 71, Number 191 (Tuesday, October 3, 2006)]
[Rules and Regulations]
[Page 58254]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: E6-16235]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-NE-12-AD; Amendment 39-14609; AD 2006-11-05]
RIN 2120-AA64


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

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: 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.

DATES: Effective Date: October 3, 2006.

FOR FURTHER INFORMATION CONTACT: Ian Dargin, Aerospace Engineer, Engine 
Certification Office, FAA, Engine and Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803; telephone (781) 238-7178; 
fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD FR Doc, 06-4713 applicable 
to 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, was published in the Federal Register 
on May 23, 2006 (71 FR 29586). The following correction is needed:


Sec.  39.13  [Corrected]

    On page 29587, in the first column of Table 1, in the second row, 
in the third line, ``-524B-02, B-B-02, B3-02, and B4 series, Pre SB No. 
72-7730'' is corrected to read ``-524B-02, B-B-02, B3-02, and B4 
series, Pre and Post accomplishment of SB No. 72-7730''.

    Issued in Burlington, Massachusetts, on September 26, 2006.
Peter A. White,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
 [FR Doc. E6-16235 Filed 10-2-06; 8:45 am]
BILLING CODE 4910-13-P

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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