Airworthiness Directives: Pratt & Whitney Canada (PWC) PW206A, PW206B, et al.; Correction
Federal Register: July 27, 2009 (Volume 74, Number 142)
Rules and Regulations
Page 36925
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
DOCID:fr27jy09-1
Rules and Regulations
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Page 36925
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA-2007-0219; Directorate Identifier 2007-NE-46-AD;
Amendment 39-15806; AD 2009-03-05
RIN 2120-AA64
Airworthiness Directives; Pratt & Whitney Canada (PWC) PW206A,
PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and PW207E Turboshaft
Engines; Correction
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
SUMMARY: 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.
DATES: Effective Date: Effective July 27, 2009.
FOR FURTHER INFORMATION CONTACT: Ian Dargin, Aerospace Engineer, Engine
Certification Office, FAA, Engine and Propeller Directorate, 12 New
England Executive Park; Burlington, MA 01803; e-mail: ian.dargin@faa.gov; telephone (781) 238-7178; fax (781) 238-7199.
SUPPLEMENTARY INFORMATION: 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:
Sec. 39.13 [Corrected] 0
On page 7795, in the third column, in the regulatory text, in the 10th paragraph, in the fourth line, delete ``Bell 429,''.
Issued in Burlington, Massachusetts, on July 20, 2009.
Peter A. White,
Assistant Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
FR Doc. E9-17599 Filed 7-24-09; 8:45 am
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