Airworthiness Directives; BRP-Powertrain GmbH & Co KG Rotax Reciprocating Engines, 66534-66535 [2012-26772]

Download as PDF Federal Register / Vol. 77, No. 215 / Tuesday, November 6, 2012 / Rules and Regulations (b) The adjustments in paragraph (a) of this section apply to violations that occur after December 6, 2012. PART 109—RULES OF PRACTICE AND PROCEDURE IN ADJUDICATORY PROCEEDINGS 3. The authority citation for part 109 continues to read as follows: ■ Dated: October 26, 2012. Thomas J. Curry, Comptroller of the Currency. BILLING CODE 4810–33–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2012–0603; Directorate Identifier 2012–NE–17–AD; Amendment 39– 17160; AD 2012–16–13] erowe on DSK6TPTVN1PROD with RULES RIN 2120–AA64 Airworthiness Directives; BRPPowertrain GmbH & Co KG Rotax Reciprocating Engines Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. AGENCY: 14:24 Nov 05, 2012 Jkt 229001 § 109.103 Civil money penalties. * * * * * (c) * * * The amounts in this chart apply to violations that occur after December 6, 2012: 4. Section 109.103(c) is amended by revising the last sentence of the introductory text and the chart to read as follows: ■ The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to BRP-Powertrain GmbH & Co KG Rotax 912 F2; 912 F3; 912 F4; 912 S2; 912 S3; and 912 S4 reciprocating engines. The word ‘‘not’’ was improperly omitted from the Installation Prohibition section of the AD, thereby changing the prohibition in the AD. This correction reinserts ‘‘not’’ into the paragraph to correct the omission. In all other respects, the original document remains the same. SUMMARY: [FR Doc. 2012–27074 Filed 11–5–12; 8:45 am] VerDate Mar<15>2010 Authority: 5 U.S.C. 504, 554–557; 12 U.S.C. 1464, 1467, 1467a, 1468, 1817(j), 1818, 1820(k), 1829(e), 3349, 4717, 5412(b)(2)(B); 15 U.S.C. 78(l), 78o–5, 78u–2; 28 U.S.C. 2461 note; 31 U.S.C. 5321; and 42 U.S.C. 4012a. This final rule is effective November 6, 2012. The effective date for AD 2012–16–13 (77 FR 51462, August 24, 2012) remains September 10, 2012. DATES: You may examine the AD docket on the Internet at https:// 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 ADDRESSES: PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 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: Alan Strom, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; email: alan.strom@faa.gov; phone: 781– 238–7143; fax: 781–238–7199. SUPPLEMENTARY INFORMATION: Airworthiness Directive 2012–16–13, amendment 39–17160 (77 FR 51462, August 24, 2012), currently requires replacing the pressure side fuel hose on certain fuel pumps and inspecting the carburetors connected to those fuel pumps for contamination within 5 flight hours after the effective date of this AD E:\FR\FM\06NOR1.SGM 06NOR1 ER06NO12.003</GPH> 66534 Federal Register / Vol. 77, No. 215 / Tuesday, November 6, 2012 / Rules and Regulations for BRP-Powertrain GmbH & Co KG Rotax 912 F2; 912 F3; 912 F4; 912 S2; 912 S3; and 912 S4 reciprocating engines. As published, the text of paragraph (g)(3), Installation Prohibition, is incorrect. No other part of the preamble or regulatory information is in error; therefore, only the changed portion of the final rule is being published in the Federal Register. The effective date of this AD remains September 10, 2012. Correction of Regulatory Text § 39.13 [Corrected] In the Federal Register of August 24, 2012, on page 51464, in the 1st column, paragraph (g)(3) of AD 2012–16–13 is corrected to read as follows: * * * * * (3) After the effective date of this AD, do not approve for return to service any product or article with a fuel hose removed from a P/N 893114 fuel pump with an S/N listed in Table 1 to paragraph (c) of this AD. * * * * * ■ Issued in Burlington, Massachusetts, on October 24, 2012. Colleen M. D’Alessandro, Assistant Manager, Engine & Propeller Directorate, Aircraft Certification Service. [FR Doc. 2012–26772 Filed 11–5–12; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 97 [Docket No. 30866 ; Amdt. No. 3501] Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: This rule establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are erowe on DSK6TPTVN1PROD with RULES 14:24 Nov 05, 2012 This rule is effective November 6, 2012. The compliance date for each SIAP, associated Takeoff Minimums, and ODP is specified in the amendatory provisions. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of November 6, 2012. ADDRESSES: Availability of matters incorporated by reference in the amendment is as follows: For Examination— 1. FAA Rules Docket, FAA Headquarters Building, 800 Independence Avenue SW., Washington, DC 20591; 2. The FAA Regional Office of the region in which the affected airport is located; 3. The National Flight Procedures Office, 6500 South MacArthur Blvd., Oklahoma City, OK 73169 or, 4. The National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https://www.archives.gov/ federal_register/ code_of_federal_regulations/ ibr_locations.html. Availability—All SIAPs and Takeoff Minimums and ODPs are available online free of charge. Visit https:// www.nfdc.faa.gov to register. Additionally, individual SIAP and Takeoff Minimums and ODP copies may be obtained from: 1. FAA Public Inquiry Center (APA– 200), FAA Headquarters Building, 800 Independence Avenue SW., Washington, DC 20591; or 2. The FAA Regional Office of the region in which the affected airport is located. DATES: FOR FURTHER INFORMATION CONTACT: SUMMARY: VerDate Mar<15>2010 designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports. Jkt 229001 Richard A. Dunham III, Flight Procedure Standards Branch (AFS–420), Flight Technologies and Programs Divisions, Flight Standards Service, Federal Aviation Administration, Mike Monroney Aeronautical Center, 6500 South MacArthur Blvd. Oklahoma City, OK. 73169 (Mail Address: P.O. Box 25082, Oklahoma City, OK 73125) Telephone: (405) 954–4164. SUPPLEMENTARY INFORMATION: This rule amends Title 14 of the Code of Federal Regulations, Part 97 (14 CFR part 97), by establishing, amending, suspending, or revoking SIAPS, Takeoff Minimums PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 66535 and/or ODPS. The complete regulators description of each SIAP and its associated Takeoff Minimums or ODP for an identified airport is listed on FAA form documents which are incorporated by reference in this amendment under 5 U.S.C. 552(a), 1 CFR part 51, and 14 CFR part 97.20. The applicable FAA Forms are FAA Forms 8260–3, 8260–4, 8260–5, 8260–15A, and 8260–15B when required by an entry on 8260–15A. The large number of SIAPs, Takeoff Minimums and ODPs, in addition to their complex nature and the need for a special format make publication in the Federal Register expensive and impractical. Furthermore, airmen do not use the regulatory text of the SIAPs, Takeoff Minimums or ODPs, but instead refer to their depiction on charts printed by publishers of aeronautical materials. The advantages of incorporation by reference are realized and publication of the complete description of each SIAP, Takeoff Minimums and ODP listed on FAA forms is unnecessary. This amendment provides the affected CFR sections and specifies the types of SIAPs and the effective dates of the, associated Takeoff Minimums and ODPs. This amendment also identifies the airport and its location, the procedure, and the amendment number. The Rule This amendment to 14 CFR part 97 is effective upon publication of each separate SIAP, Takeoff Minimums and ODP as contained in the transmittal. Some SIAP and Takeoff Minimums and textual ODP amendments may have been issued previously by the FAA in a Flight Data Center (FDC) Notice to Airmen (NOTAM) as an emergency action of immediate flight safety relating directly to published aeronautical charts. The circumstances which created the need for some SIAP and Takeoff Minimums and ODP amendments may require making them effective in less than 30 days. For the remaining SIAPS and Takeoff Minimums and ODPS, an effective date at least 30 days after publication is provided. Further, the SIAPs and Takeoff Minimums and ODPS contained in this amendment are based on the criteria contained in the U.S. Standard for Terminal Instrument Procedures (TERPS). In developing these SIAPS and Takeoff Minimums and ODPs, the TERPS criteria were applied to the conditions existing or anticipated at the affected airports. Because of the close and immediate relationship between these SIAPs, Takeoff Minimums and ODPs, and safety in air commerce, I find that notice and public procedures before E:\FR\FM\06NOR1.SGM 06NOR1

Agencies

[Federal Register Volume 77, Number 215 (Tuesday, November 6, 2012)]
[Rules and Regulations]
[Pages 66534-66535]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2012-26772]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-0603; Directorate Identifier 2012-NE-17-AD; 
Amendment 39-17160; AD 2012-16-13]
RIN 2120-AA64


Airworthiness Directives; BRP-Powertrain GmbH & Co KG Rotax 
Reciprocating 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 was 
published in the Federal Register. That AD applies to BRP-Powertrain 
GmbH & Co KG Rotax 912 F2; 912 F3; 912 F4; 912 S2; 912 S3; and 912 S4 
reciprocating engines. The word ``not'' was improperly omitted from the 
Installation Prohibition section of the AD, thereby changing the 
prohibition in the AD. This correction reinserts ``not'' into the 
paragraph to correct the omission. In all other respects, the original 
document remains the same.

DATES: This final rule is effective November 6, 2012. The effective 
date for AD 2012-16-13 (77 FR 51462, August 24, 2012) remains September 
10, 2012.

ADDRESSES: You may examine the AD docket on the Internet at https://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: Alan Strom, Aerospace Engineer, Engine 
Certification Office, FAA, Engine & Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803; email: 
alan.strom@faa.gov; phone: 781-238-7143; fax: 781-238-7199.

SUPPLEMENTARY INFORMATION: Airworthiness Directive 2012-16-13, 
amendment 39-17160 (77 FR 51462, August 24, 2012), currently requires 
replacing the pressure side fuel hose on certain fuel pumps and 
inspecting the carburetors connected to those fuel pumps for 
contamination within 5 flight hours after the effective date of this AD

[[Page 66535]]

for BRP-Powertrain GmbH & Co KG Rotax 912 F2; 912 F3; 912 F4; 912 S2; 
912 S3; and 912 S4 reciprocating engines.
    As published, the text of paragraph (g)(3), Installation 
Prohibition, is incorrect.
    No other part of the preamble or regulatory information is in 
error; therefore, only the changed portion of the final rule is being 
published in the Federal Register.
    The effective date of this AD remains September 10, 2012.

Correction of Regulatory Text


Sec.  39.13  [Corrected]

0
In the Federal Register of August 24, 2012, on page 51464, in the 1st 
column, paragraph (g)(3) of AD 2012-16-13 is corrected to read as 
follows:
* * * * *
    (3) After the effective date of this AD, do not approve for return 
to service any product or article with a fuel hose removed from a P/N 
893114 fuel pump with an S/N listed in Table 1 to paragraph (c) of this 
AD.
* * * * *

    Issued in Burlington, Massachusetts, on October 24, 2012.
Colleen M. D'Alessandro,
Assistant Manager, Engine & Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 2012-26772 Filed 11-5-12; 8:45 am]
BILLING CODE 4910-13-P

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