[Federal Register Volume 76, Number 2 (Tuesday, January 4, 2011)]
[Rules and Regulations]
[Page 255]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-33171]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-0829; Directorate Identifier 2010-NE-23-AD;
Amendment 39-16524; AD 2010-24-05]
RIN 2120-AA64
Airworthiness Directives; Pratt & Whitney Canada Corp. (P&WC)
PW305A and PW305B Turbofan Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
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SUMMARY: The FAA is correcting an airworthiness directive (AD) that
published in the Federal Register. That AD applies to the products
listed above. The agency docket No. and the engine type in the subject
heading and paragraph (c) in the Summary section and the Regulatory
text are incorrect. This document corrects that error. In all other
respects, the original document remains the same.
DATES: This final rule is effective January 3, 2011.
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (phone: 800-647-5527) is Document Management Facility,
U.S. Department of Transportation, Docket Operations, M-30, West
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: James Lawrence, Aerospace Engineer,
Engine Certification Office, FAA, 12 New England Executive Park,
Burlington, MA 01803; phone: (781) 238-7176; fax: (781) 238-7199; e-
mail: [email protected].
SUPPLEMENTARY INFORMATION: Airworthiness Directive 2010-24-05,
amendment 39-16524 (75 FR 72653, November 26, 2010), currently requires
updating the airworthiness limitations section of the engine
maintenance manuals for Pratt & Whitney Canada (P&WC) PW305A and PW305B
turbofan engines.
As published, the agency docket No. in the Summary section and the
engine type in the Summary section and in the Regulatory text are
incorrect.
No other part of the preamble or regulatory information has been
changed; therefore, only the changed portion of the final rule is being
published in the Federal Register.
The effective date of this AD remains January 3, 2011.
Correction of Non-Regulatory Text
In the Federal Register of November 26, 2010, AD 2010-24-05;
Amendment 39-16524 is corrected as follows:
On page 72653, in the third column, on line 19 under 14 CFR Part
39, change ``Docket No. FAA-2010-0892'' to ``Docket No. FAA-2010-
0829''.
On page 72653, in the third column, on line 25 under 14 CFR Part
39, change ``PW305A and PW305B Turboprop'' to ``PW305A and PW305B
Turbofan''.
Correction of Regulatory Text
Sec. 39.13 [Corrected]
0
In the Federal Register of November 26, 2010, on page 72655, in the
first column, paragraph (c) of AD 2010-24-05 is corrected to read as
follows:
* * * * *
(c) This AD applies to Pratt & Whitney Canada Corp. (P&WC)
PW305A and PW305B turbofan engines with certain impellers, part
numbers (P/Ns) 30B2185, 30B2486, 30B2858-01, or 30B4565-01
installed. These engines are installed on, but not limited to,
Hawker-Beech Corporation BAe.125 series 1000A, 1000B, and Hawker
1000 airplanes and Learjet Inc. Learjet 60 airplanes.
* * * * *
Issued in Burlington, Massachusetts, on December 22, 2010.
Peter A. White,
Assistant Manager, Engine & Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 2010-33171 Filed 1-3-11; 8:45 am]
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