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[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 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: 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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