Published 2006-10-03 · Federal Register document E6-16235
Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines; Correction
Publication 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.
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Correction notice · separate source edition
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- 2006-11-05
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Official source · 2006-10-03
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[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 [www.gpo.gov]
[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
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