Federal Register / Vol. 76, No. 216 / Tuesday, November 8, 2011 / Rules and Regulations 69123 

delay in effective date for these same 

reasons. 

List of Subjects in 10 CFR Part 431 

Administrative practice and 

procedure, Confidential business 

information, Energy conservation, 

Household appliances, Imports, 

Intragovernmental relations, Reporting 

and recordkeeping requirements, and 

Small businesses. 

Accordingly, part 431 of chapter II, 

subchapter D, of title 10 of the Code of 

Federal Regulations, is corrected by 

making the following correcting 

amendments: 

PART 431—ENERGY EFFICIENCY 

PROGRAM FOR CERTAIN 

COMMERCIAL AND INDUSTRIAL 

EQUIPMENT 

■ 1. The authority citation for part 431 

continues to read as follows: 

Authority: 42 U.S.C. 6291–6317. 

■ 2. Section 431.156 of subpart I is 

revised to read as follows: 

§ 431.156 Energy and water conservation 

standards and effective dates. 

(a) Each commercial clothes washer 

manufactured between January 1, 2007, 

and January 8, 2013, shall have— 

(1) A modified energy factor of at least 

1.26; and 

(2) A water consumption factor of not 

more than 9.5. 

(b) Each commercial clothes washer 

manufactured on or after January 8, 

2013, shall have a modified energy 

factor no less than and a water factor no 

greater than: 

Equipment class 

Modified 

energy 

factor, 

cu. ft./kWh/ 

cycle 

Water 

factor, 

gal./cu. ft./ 

cycle 

Top-Loading ...... 1.60 8.5 

Front-Loading ... 2.00 5.5 

Issued in Washington, DC, on November 1, 

2011. 

Kathleen B. Hogan, 

Deputy Assistant Secretary for Energy 

Efficiency, Energy Efficiency and Renewable 

Energy. 

[FR Doc. 2011–28920 Filed 11–7–11; 8:45 am] 

BILLING CODE 6450–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2007–27747; Directorate 

Identifier 2007–CE–030–AD; Amendment 

39–16782; AD 2009–10–09 R2] 

RIN 2120–AA64 

Airworthiness Directives; Cessna 

Aircraft Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting an 

airworthiness directive (AD) that 

published in the Federal Register. That 

AD applies to certain Cessna Aircraft 

Company (Cessna) Models 150F, 150G, 

150H, 150J, 150K, 150L, 150M, A150K, 

A150L, A150M, F150F, F150G, F150H, 

F150J, F150K, F150L, F150M, FA150K, 

FA150L, FRA150L, FA150M, FRA150M, 

152, A152, F152, and FA152 airplanes. 

There is an error in the compliance 

instructions. This document corrects 

that error. In all other respects, the 

original document remains the same. 

DATES: This final rule; correction, is 

effective November 8, 2011. The 

effective date for AD 2009–10–09 R2 

remains September 12, 2011. 

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: Ann 

Johnson, Aerospace Engineer, FAA, 

Wichita Aircraft Certification Office, 

1801 Airport Road, Room 100, Wichita, 

Kansas 67209; phone: (316) 946–4105; 

fax: (316) 946–4107; email: 

ann.johnson@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Airworthiness Directive 2009–10–09 R2, 

Amendment 39–16782 (76 FR 53308, 

August 26, 2011), currently requires 

either installing a placard prohibiting 

spins and other acrobatic maneuvers in 

the airplane or replacing the rudder 

stop, the rudder stop bumper, and the 

attachment hardware with a new rudder 

stop modification kit for certain Cessna 

Models 150F, 150G, 150H, 150J, 150K, 

150L, 150M, A150K, A150L, A150M, 

F150F, F150G, F150H, F150J, F150K, 

F150L, F150M, FA150K, FA150L, 

FRA150L, FA150M, FRA150M, 152, 

A152, F152, and FA152 airplanes. 

As published, the text in the 

Procedures column of Table 2 in 

paragraph (g)(1) of this AD incorrectly 

states ‘‘* * * fabricate the placard 

required in paragraph (g)(1)(i) of this AD 

* * *’’, and the text should refer to 

paragraph (g)(1)(ii). 

No other part of the preamble or 

regulatory information has been 

changed; therefore, only the changed 

portion of the final rule is being 

published in the Federal Register. 

The effective date of this AD remains 

September 12, 2011. 

Correction of Regulatory Text 

§ 39.13 [Corrected] 

In the Federal Register of August 26, 

2011, on page 53311, in the 3rd column, 

Procedures, paragraph (g)(1), Table 2— 

Actions, Compliance and Procedures, of 

AD 2009–10–09 R2 is corrected to read 

as follows: 

* * * * * 

A person authorized to perform 

maintenance as specified in 14 CFR 43.3 of 

the Federal Aviation Administration 

Regulations (14 CFR 43.3) is required to make 

the AFM and POH changes, fabricate the 

placard required in paragraph (g)(1)(ii) of this 

AD, and make an entry into the aircraft 

logbook showing compliance with the 

portion of the AD per compliance with 14 

CFR 43.9. 

* * * * * 

Issued in Kansas City, Missouri, on 

November 2, 2011. 

John R. Colomy, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2011–28861 Filed 11–7–11; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–1301; Directorate 

Identifier 2010–SW–008–AD; Amendment 

39–16851; AD 2011–22–08] 

RIN 2120–AA64 

Airworthiness Directives; MD 

Helicopters, Inc. Model MD900 

Helicopters 

AGENCY: Federal Aviation 

Administration, DOT. 

ACTION: Final rule. 


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