# [Corrected]
**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.
**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.
**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:
**39 CFR Part 13**
**PART 39—[CORRECTED]**
§ 39.13
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”.
Issued in Burlington, MA, on April 26, 2005.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification Service.