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Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW535A Turbofan Engines; Correction

Document Details

Information about this document as published in the Federal Register.

Published Document

This document has been published in the Federal Register. Use the PDF linked in the document sidebar for the official electronic format.

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AGENCY:

Federal Aviation Administration (FAA), Department of Transportation (DOT).

ACTION:

Final rule; correction.

SUMMARY:

The FAA is correcting airworthiness directive (AD) 2006-24-08. That AD applies to Pratt & Whitney Canada (P&WC) PW535A turbofan engines. We published that AD in the Federal Register on December 4, 2006 (71 FR 70284). The fuel manifold part number (P/N) 3025267-01 listed in paragraph (c) is incorrect. This document corrects that P/N. In all other respects, the original document remains the same.

EFFECTIVE DATE:

Effective May 22, 2007.

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FOR FURTHER INFORMATION CONTACT:

Ian Dargin, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA, 01803; telephone (781) 238-7178; fax (781) 238-7199.

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SUPPLEMENTARY INFORMATION:

On December 4, 2006 (71 FR 70284), we published a final rule AD, FR Doc, E6-20204, in the Federal Register. That AD applies to P&WC PW535A turbofan engines. We need to make the following correction:

[Corrected]

On page 70286, in the second column, in paragraph (c), in the fourth line, “3025267-01” is corrected to read “3052627-01”.

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Issued in Burlington, Massachusetts, on May 14, 2007.

Peter A. White,

Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service.

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[FR Doc. E7-9719 Filed 5-21-07; 8:45 am]

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