AD 2004-26-05

[Federal Register Volume 71, Number 238 (Tuesday, December 12, 2006)]
[Rules and Regulations]
[Page 74466]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: E6-21122]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2004-NE-19-AD; Amendment 39-13197; AD 2004-26-05]
RIN 2120-AA64


Airworthiness Directives; Rolls-Royce plc RB211-524 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) 2004-26-05 applicable to certain Rolls-Royce plc (RR) RB211-524 
series turbofan engines that was published in the Federal Register on 
January 5, 2005. The part number UL29916 in the Applicability section 
is incorrect. This document corrects that part number. In all other 
respects, the original document remains the same.

DATES: Effective Date: December 12, 2006.

FOR FURTHER INFORMATION CONTACT: Ian Dargin, Aerospace Engineer, Engine 
Certification Office, FAA, Engine and Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-
7178; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule airworthiness directive FR Doc, 
05-85 applicable to RR RB211-524 series turbofan engines, was published 
in the Federal Register on January 5, 2005 (70 FR 681). The following 
correction is needed:


Sec.  39.13  [Corrected]

0
On page 682, in the first column, in the PART 39--AIRWORTHINESS 
DIRECTIVES Section, in the Applicability paragraph, in the second line, 
``UL29916'' is corrected to read ``UL26916''.

    Issued in Burlington, Massachusetts, on December 5, 2006.
Diane M. Cook,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
 [FR Doc. E6-21122 Filed 12-11-06; 8:45 am]
BILLING CODE 4910-13-P