Federal Aviation Administration, DOT.
Final rule; correction
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 May 5, 2005.Start Further Info
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.End Further Info End Preamble Start Supplemental 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:Start Part
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”.End Amendment Part Start Signature
Issued in Burlington, MA, on April 26, 2005.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification Service.
[FR Doc. 05-8883 Filed 5-4-05; 8:45 am]
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