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Airworthiness Directives; Pratt & Whitney Canada (PWC) PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and PW207E Turboshaft Engines; Correction

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Information about this document as published in the Federal Register.

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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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Federal Aviation Administration (FAA), DOT.


Final rule; correction.


The FAA is correcting airworthiness directive (AD) 2009-03-05. That AD applies to PWC PW206 and PW207 series turboshaft engines. We published that AD in the Federal Register on February 20, 2009 (74 FR 7794). Paragraph (d) in the regulatory text is incorrect. This document corrects that paragraph. In all other respects, the original document remains the same.


Effective Date: Effective July 27, 2009.

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

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On February 20, 2009 (74 FR 7794), we published a final rule AD, FR Doc E9-3046, in the Federal Register. That AD applies to PWC PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and PW207E turboshaft engines. We need to make the following correction:

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On page 7795, in the third column, in the regulatory text, in the 10th paragraph, in the fourth line, delete “Bell 429,”.

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Issued in Burlington, Massachusetts, on July 20, 2009.

Peter A. White,

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

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[FR Doc. E9-17599 Filed 7-24-09; 8:45 am]