Airworthiness directives: General Electric Co.; correction,

[Federal Register: March 4, 2005 (Volume 70, Number 42)]

[Rules and Regulations]

[Page 10485]

From the Federal Register Online via GPO Access [wais.access.gpo.gov]

[DOCID:fr04mr05-1]

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[[Page 10485]]

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-NE-43-AD; Amendment 39-13835; AD 2004-22-07]

RIN 2120-AA64

Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

SUMMARY: This document makes a correction to Airworthiness Directive (AD) 2004-22-07. That AD applies to GE CF6-80C2 turbofan engines with certain part number (P/N) high pressure turbine stage 2 nozzle guide vanes (HPT S2 NGVs) installed. That AD was published in the Federal Register on October 27, 2004 (69 FR 62571). The phrase ``5.0 or more cycles per flight leg'' in the Compliance section is incorrect. This document corrects that phrase. In all other respects, the original document remains the same.

EFFECTIVE DATE: Effective March 4, 2005.

FOR FURTHER INFORMATION CONTACT: Eugene Triozzi, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA; telephone (781) 238-7148; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 04-23929 that applies to GE CF6-80C2 turbofan engines with certain P/N HPT S2 NGVs installed, was published in the Federal Register on October 27, 2004 (69 FR 62571). The following correction is needed:

PART 39--[CORRECTED]

Sec. 39.13 [Corrected]

0 On page 62574, in the first column, in paragraph (h)(1), in the second line, ``more cycles per flight leg,'' is corrected to read ``more hours per flight leg,''

Issued in Burlington, MA, on February 24, 2005. Jay J. Pardee, Manager, Engine and Propeller Directorate, Aircraft Certification Service.

[FR Doc. 05-4072 Filed 3-3-05; 8:45 am]

BILLING CODE 4910-13-U