Airworthiness Directives; General Electric Company CF6-45A, CF6-50A, CF6-50C, and CF6-50E Series Turbofan Engines; Correction

[Federal Register Volume 70, Number 110 (Thursday, June 9, 2005)]
[Rules and Regulations]
[Page 33692]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-11442]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2004-19463; Directorate Identifier 2004-NE-14-AD; 
Amendment 39-14029; AD 2005-07-05]
RIN 2120-AA64


Airworthiness Directives; General Electric Company CF6-45A, CF6-
50A, CF6-50C, and CF6-50E 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) 2005-07-05. That AD applies to General Electric Company (GE) CF6-
45A, CF6-50A, CF6-50C, and CF6-50E series turbofan engines that have 
not incorporated GE Service Bulletin (SB) No. CF6-50 S/B 72-1239, 
Revision 1, dated September 24, 2003, or that have not incorporated 
paragraph 3.B. of GE SB No. CF6-50 S/B 72-1239, original issue, dated 
May 29, 2003. We published AD 2005-07-05 in the Federal Register on 
March 30, 2005, (70 FR 16096). A descriptive phrase was inadvertently 
left out of compliance paragraph (f). This document corrects compliance 
paragraph (f). In all other respects, the original document remains the 
same.

DATES: Effective June 9, 2005.

FOR FURTHER INFORMATION CONTACT: Karen Curtis, Aerospace Engineer, 
Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803; telephone (781) 238-
7192; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 05-6107, that 
applies to (GE) CF6-45A, CF6-50A, CF6-50C, and CF6-50E series turbofan 
engines that have not incorporated GE Service Bulletin (SB) No. CF6-50 
S/B 72-1239, Revision 1, dated September 24, 2003, or that have not 
incorporated paragraph 3.B. of GE SB No. CF6-50 S/B 72-1239, original 
issue, dated May 29, 2003, was published in the Federal Register on 
March 30, 2005, (70 FR 16096). The following correction is needed:


Sec.  39.13  [Corrected]

0
On page 16098, in the first column, in compliance paragraph (f), the 
third line, ``cycles-since-new (CSN), or 3,000 cycles-'' is corrected 
to read ``cycles-since-new (CSN) on the TMF assembly, or 3,000 cycles-
''.

    Issued in Burlington, MA, on June 2, 2005.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 05-11442 Filed 6-8-05; 8:45 am]
BILLING CODE 4910-13-P

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