Federal Aviation Administration, DOT.
Final rule; correction.
This document makes a correction to Airworthiness Directive (AD) 2004-05-22. That AD applies to certain RRD TAY 611-8, TAY 620-15, TAY 650-15, and TAY 651-54 series turbofan engines with ice-impact panels installed in the low pressure (LP) compressor case. We published AD 2004-05-22 in the Federal Register on March 10, 2004, (69 FR 11305). The AD number in the Amendatory Language is incorrect. This document corrects that AD number. In all other respects, the original document remains the same.
Effective March 25, 2004.Start Further Info
FOR FURTHER INFORMATION CONTACT:
Jason Yang, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7747; fax (781) 238-7199.End Further Info End Preamble Start Supplemental Information
A final rule AD, FR Doc, 04-5263 that applies to certain RRD TAY 611-8, TAY 620-15, TAY 650-15, and TAY 651-54 series turbofan engines with ice-impact panels installed in the LP compressor case, was published in the Federal Register on March 10, 2004, (69 FR 11305). The following correction is needed:
On page 11307, in the second column, in the Amendatory Language, in the third paragraph, in the first line, “200X-05-22” is corrected to read “2004-05-22”.End Amendment Part Start Signature
Issued in Burlington, MA, on March 18, 2004.
Mark C. Fulmer,
Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service.
[FR Doc. 04-6577 Filed 3-24-04; 8:45 am]
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