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

61361 

Vol. 75, No. 192 

Tuesday, October 5, 2010 

DEPARTMENT OF ENERGY 

10 CFR Part 429 

[Docket No. EERE–2010–BT–CE–0014] 

RIN 1904–AC24 

Energy Conservation Program: 

Certification, Compliance, and 

Enforcement for Consumer Products 

and Commercial and Industrial 

Equipment 

Correction 

In proposed rule document 2010– 

22353 beginning on page 56796 in the 

issue of Thursday, September 16, 2010 

make the following correction: 

§429.9 [Corrected] 

On page 56816, in §429.9(c), in the 

first column, §429.9(c)(9) through (10) is 

being printed in its entirety: 

(9)(i) For each basic model of direct 

heating equipment (not including 

furnaces) a sample of sufficient size 

shall be tested to insure that– 

(A) Any represented value of 

estimated annual operating cost, energy 

consumption or other measure of energy 

consumption of a basic model for which 

consumers would favor lower values 

shall be no less than the higher of: 

(1) The mean of the sample, or 

(2) The upper 971⁄2 percent 

confidence limit of the true mean 

divided by 1.05, and 

(B) Any represented value of the fuel 

utilization efficiency or other measure 

of energy consumption of a basic model 

for which consumers would favor 

higher values shall be no greater than 

the lower of: 

(1) The mean of the sample or 

(2) The lower 971⁄2 percent confidence 

limit of the true mean divided by 0.95. 

(ii) In calculating the measures of 

energy consumption for each unit 

tested, use the design heating 

requirement corresponding to the mean 

of the capacities of the units of the 

sample. 

(10) For each basic model of 

conventional cooking tops, conventional 

ovens and microwave ovens a sample of 

sufficient size shall be tested to insure 

that– 

(i) Any represented value of estimated 

annual operating cost, energy 

consumption or other measure of energy 

consumption of a basic model for which 

consumers would favor lower values 

shall be no less than the higher of: 

(A) The mean of the sample, or 

(B) The upper 971⁄2 percent 

confidence limit of the true mean 

divided by 1.05, and 

(ii) Any represented value of the 

energy factor or other measure of energy 

consumption of a basic model for which 

consumers would favor higher values 

shall be no greater than the lower of: 

(A) The mean of the sample, or 

(B) The lower 971⁄2 percent 

confidence limit of the true mean 

divided by 0.95. 

[FR Doc. C1–2010–22353 Filed 10–4–10; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–0994; Directorate 

Identifier 2009–NE–39–AD] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

plc (RR) RB211–535 Series Turbofan 

Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for the 

products listed above. This proposed 

AD results from mandatory continuing 

airworthiness information (MCAI) 

issued 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: 

There have been several findings of 

cracking at the firtrees of LP Turbine discs. 

Fatigue crack initiation and subsequent crack 

propagation at the firtree may result in 

multiple LP Turbine blade release. The latter 

may potentially be beyond the containment 

capabilities of the engine casings. Thus, 

cracking at the firtrees of LP Turbine discs 

constitutes a potentially unsafe condition. 

We are proposing this AD to detect 

cracks in the low-pressure turbine stage 

1, 2, and 3 discs, which could result in 

an uncontained release of LP turbine 

blades and damage to the airplane. 

DATES: We must receive comments on 

this proposed AD by November 19, 

2010. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov and follow 

the instructions for sending your 

comments electronically. 

• Mail: Docket Management Facility, 

U.S. Department of Transportation, 1200 

New Jersey Avenue SE., West Building 

Ground Floor, Room W12–140, 

Washington, DC 20590–0001. 

• Hand Delivery: Deliver to Mail 

address above between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

• Fax: (202) 493–2251. 

Contact Rolls-Royce plc., P.O. Box 31, 

Derby, DE24 8BJ, United Kingdom; 

Telephone: 011 44 1332 242424, Fax: 

011 44 1332 249936; e-mail: 

tech.help@rolls-royce.com for the 

service information identified in this 

proposed AD or download the 

publication from https:// 

www.aeromanager.com/. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; or in person at the 

Docket Operations office 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 Operations 

office (telephone (800) 647–5527) is the 

same as the Mail address provided in 

the ADDRESSES section. Comments will 

be available in the AD docket shortly 

after receipt. 

FOR FURTHER INFORMATION CONTACT: Ian 

Dargin, Aerospace Engineer, Engine 

Certification Office, FAA, Engine and 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

e-mail: ian.dargin@faa.gov; telephone 

(781) 238–7178; fax (781) 238–7199. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 


hsrobinson on DSK69SOYB1PROD with PROPOSALS-1