This section of the FEDERAL REGISTER

contains notices to the public of the proposed

issuance of rules and regulations. The

purpose of these notices is to give interested

persons an opportunity to participate in the

rule making prior to the adoption of the final

rules.

Proposed Rules Federal Register

14467 

Vol. 78, No. 44 

Wednesday, March 6, 2013 

DEPARTMENT OF ENERGY 

10 CFR Part 430 

[Docket No. EERE–2011–BT–STD–0006] 

RIN 1904–AC43 

Energy Conservation Program: 

Availability of the Preliminary 

Technical Support Document for 

General Service Fluorescent Lamps 

and Incandescent Reflector Lamps 

Correction 

In proposed rule document 2013– 

04711, appearing on pages 13563–13566 

in the issue of Thursday, February 28, 

2013, make the following correction: 

On page 13563, in the second column, 

in the sixth paragraph, on the first and 

second lines, ‘‘GSFL-IRL_2011-STD0006@ee.doe.gov’’ should read ‘‘GSFLIRL_2011-STD-0006@ee.doe.gov’’. 

[FR Doc. C1–2013–04711 Filed 3–5–13; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0220; Directorate 

Identifier 2013–CE–002–AD] 

RIN 2120–AA64 

Airworthiness Directives; Slingsby 

Sailplanes Ltd. Sailplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for all 

Slingsby Sailplanes Ltd. Models Dart 

T.51, Dart T.51/17, and Dart T.51/17R 

sailplanes equipped with aluminum 

alloy spar booms that would supersede 

an existing AD. This proposed AD 

results from mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as an incident of glue joint 

failure on a starboard wing caused by 

water entering the area of the airbrake 

box that resulted in delamination and 

corrosion in the area of the aluminum 

alloy spar booms and the wing attach 

fittings. We are issuing this proposed 

AD to require actions to address the 

unsafe condition on these products. 

DATES: We must receive comments on 

this proposed AD by April 22, 2013. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: (202) 493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590, between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. 

For service information identified in 

this proposed AD, contact Slingsby 

Advanced Composites Ltd., Ings Lane, 

Kirkbymoorside, North Yorkshire, 

England YO62 6EZ; telephone: 

+44(0)1751 432474; Internet: none. You 

may review copies of the referenced 

service information at the FAA, Small 

Airplane Directorate, 901 Locust, 

Kansas City, Missouri 64106. For 

information on the availability of this 

material at the FAA, call (816) 329– 

4148. 

Examining the AD Docket 

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 proposed AD, the 

regulatory evaluation, any comments 

received, and other information. The 

street address for the Docket Office 

(telephone (800) 647–5527) is in the 

ADDRESSES section. Comments will be 

available in the AD docket shortly after 

receipt. 

FOR FURTHER INFORMATION CONTACT: Jim 

Rutherford, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4165; fax: (816) 

329–4090; email: 

jim.rutherford@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 

this proposed AD. Send your comments 

to an address listed under the 

ADDRESSES section. Include ‘‘Docket No. 

FAA–2013–0220; Directorate Identifier 

2013–CE–002–AD’’ at the beginning of 

your comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this proposed AD. We will 

consider all comments received by the 

closing date and may amend this 

proposed AD because of those 

comments. 

We will post all comments we 

receive, without change, to http:// 

regulations.gov, including any personal 

information you provide. We will also 

post a report summarizing each 

substantive verbal contact we receive 

about this proposed AD. 

Discussion 

On October 22, 1998, we issued AD 

98–22–15, Amendment 39–10863 (63 

FR 58624, November 2, 1998). That AD 

required actions intended to address an 

unsafe condition on the products listed 

above. 

Since we issued AD 98–22–15, 

Amendment 39–10863 (63 FR 58624, 

November 2, 1998), Slingsby Aviation 

Ltd. has revised the related service 

information to remove the 5-year 

repetitive ‘‘cutout’’ inspection and to 

add a repetitive annual inspection using 

an endoscope. The endoscope 

inspection method would be done using 

existing drain holes in the lower wing 

skin. 

Using revised service information is 

mandatory within the United Kingdom 

airworthiness system. It is not necessary 

for the Civil Aviation Authority (CAA), 

which is the aviation authority for the 

United Kingdom, to issue an AD to 

mandate the use of new service 

information. 

Proposing AD action is the only way 

the FAA can mandate the use of new 

service information; however, owners/ 


TKELLEY on DSK3SPTVN1PROD with PROPOSALS