[Federal Register: May 5, 2005 (Volume 70, Number 86)]
[Rules and Regulations]
[Page 23783-23784]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr05my05-2]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 99-NE-41-AD; Amendment 39-14015; AD 2005-06-07]
RIN 2120-AA64
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
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction
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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:
PART 39--[CORRECTED]
Sec. 39.13 [Corrected]
0
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''.
[[Page 23784]]
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]
BILLING CODE 4910-13-P