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Airworthiness Directives; General Electric Company (GE) CF6-80A1/A3 and CF6-80C2A Series Turbofan Engines, Installed on Airbus Industrie A300-600 and A310 Series Airplanes; Correction

Document Details

Information about this document as published in the Federal Register.

Published Document

This document has been published in the Federal Register. Use the PDF linked in the document sidebar for the official electronic format.

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AGENCY:

Federal Aviation Administration, DOT.

ACTION:

Final rule; correction

SUMMARY:

This document makes a correction to Airworthiness Directive (AD) 2005-06-07. That AD applies to GE CF6-80A1/A3 and CF6-80C2A series turbofan engines. We published AD 2005-06-07 in the Federal Register on March 21, 2005, (70 FR 13365). A service bulletin number in the compliance section is incorrect. This document corrects that service bulletin number. In all other respects, the original document remains the same.

EFFECTIVE DATE:

Effective May 5, 2005.

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FOR FURTHER INFORMATION CONTACT:

Karen Curtis, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7192; fax (781) 238-7199.

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SUPPLEMENTARY INFORMATION:

A final rule AD, FR Doc. 05-5299, that applies to GE CF6-80A1/A3 and CF6-80C2A series turbofan engines, was published in the Federal Register on March 21, 2005, (70 FR 13365). The following correction is needed:

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PART 39—[CORRECTED]

[Corrected]
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On page 13368, in the first column, in compliance section paragraph (i)(2), in the sixth line, “No. CF6-80C2A SB 78A4022, Revision 2,” is corrected to read “No. CF6-80C2A SB 78A1081, Revision 2”.

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Start Printed Page 23784

Issued in Burlington, MA, on April 26, 2005.

Jay J. Pardee,

Manager, Engine and Propeller Directorate, Aircraft Certification Service.

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[FR Doc. 05-8883 Filed 5-4-05; 8:45 am]

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