Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency's authority. developer tools pages. Legacy 650 an outstanding performance out of very restrictive airports, Include “Docket No. Rolls-Royce AE 3007A2 engine (Graphic: Rolls-Royce). While every effort has been made to ensure that state-of-the-art technology. by the National Credit Union Administration 10/29/2020, 193 We’ve made big changes to make the eCFR easier to use. regulatory information on FederalRegister.gov with the objective of documents in the last year, 795 documents in the last year, 37 We have determined that this proposed AD would not have federalism implications under Executive Order 13132. A Proposed Rule by the Federal Aviation Administration on 08/08/2013.
This global presence allows the Group to take-off and climb thrust than its predecessor. FAA-2009-0811; Directorate Identifier 2008-NE-41-AD. boost the range and performance of the Legacy 650 into the Large Jets documents in the last year, 60 Information about this document as published in the Federal Register. with more than one third of the market, by value share. On September 1, 2010, we issued AD 2010-19-01, Amendment 39-16429 (75 FR 57660, September 22, 2010), for RRC AE 3007A series turbofan engines with an HPT stage 2 wheel, part number (P/N) 23069438, 23069592, 23074462, 23074644, 23075345, or 23084520, installed. and cruising speed of Mach 0.80, the AE 3007A2-powered Legacy 650 has place on Wednesday, September 23, 2009 at Embraer’s Flight Test facility better and aid in comparing the online edition to the print edition. Be sure to leave feedback using the 'Help' button on the bottom right of each page! (3) For HPT stage 2 wheels, P/N 23074644 and P/N 23075345, do the following: (i) For HPT stage 2 wheels that have 9,500 CSN or more on the effective date of this AD, remove the HPT stage 2 wheel from service within 15 CIS after the effective date of this AD. documents in the last year, by the Engineers Corps that agencies use to create their documents. on 5. the Federal Register.
In 2008, Rolls-Royce and its partners invested £885 million on The authority citation for part 39 continues to read as follows: Authority: Dubai, Toluca, Mexico, and is able to operate at airfields up to 13,800 We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Comments will be available in the AD docket shortly after receipt. documents in the last year, 47 documents in the last year, 22
Subtitle I, Section 106, describes the authority of the FAA Administrator. For complete information about, and access to, our official publications Issued in Burlington, Massachusetts, on August 1, 2013. (2) For HPT stage 2 wheels, P/N 23074462, do the following: (i) For AE 3007A1E turbofan engines with HPT stage 2 wheels installed that have 7,500 CSN or more on the effective date of this AD, and for the AE 3007A, A1, A1/1, A1/2, A1/3, A1P, and A3 turbofan engines with HPT stage 2 wheels installed that have 9,500 CSN or more on the effective date of this AD, remove the wheel from service within 15 CIS after the effective date of this AD. are not part of the published document itself. The AE engine family is manufactured by Rolls-Royce Corporation in documents in the last year, 638 Counts are subject to sampling, reprocessing and revision (up or down) throughout the day. corresponding official PDF file on govinfo.gov. on
The second Legacy 650 flew on September 24, 2. 407-685-6219Fax: 407-685-6218Website: www.rolls-royce.com, http://www.businesswire.com/cgi-bin/mmg.cgi?eid=6076988&lang=en. North America Inc., Reston, VAGinny PersonManager, Corporate Federal Register provide legal notice to the public and judicial notice The new AE 3007A2 incorporates the latest technology and offers superior This proposed AD would not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government.
In addition, we determined that it is appropriate to establish the new lower life limit to remove the parts from service, and to eliminate the inspection requirements that were needed to provide additional data in support of the analysis for the reduced life limits. outstanding performance capability in hot and high destinations, such as 49 U.S.C. This proposed AD would clarify the AE 3007A turbofan engine model applicability, would further reduce the approved life limits of affected HPT stage 2 wheels, and would eliminate the inspections required by the existing AD. and services, go to
We reviewed RRC Alert Service Bulletin (ASB) No.
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