Airworthiness Directives; Cessna Aircraft Company Airplanes, 69123 [2011-28861]

Download as PDF Federal Register / Vol. 76, No. 216 / Tuesday, November 8, 2011 / Rules and Regulations delay in effective date for these same reasons. DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 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: 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 Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. AGENCY: 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, ■ 1. The authority citation for part 431 F150J, F150K, F150L, F150M, FA150K, continues to read as follows: FA150L, FRA150L, FA150M, FRA150M, Authority: 42 U.S.C. 6291–6317. 152, A152, F152, and FA152 airplanes. There is an error in the compliance ■ 2. Section 431.156 of subpart I is instructions. This document corrects revised to read as follows: that error. In all other respects, the § 431.156 Energy and water conservation original document remains the same. standards and effective dates. DATES: This final rule; correction, is effective November 8, 2011. The (a) Each commercial clothes washer effective date for AD 2009–10–09 R2 manufactured between January 1, 2007, remains September 12, 2011. and January 8, 2013, shall have— ADDRESSES: You may examine the AD (1) A modified energy factor of at least docket on the Internet at https:// 1.26; and www.regulations.gov; or in person at the (2) A water consumption factor of not Docket Management Facility between more than 9.5. 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD (b) Each commercial clothes washer docket contains this AD, the regulatory manufactured on or after January 8, evaluation, any comments received, and 2013, shall have a modified energy factor no less than and a water factor no other information. The address for the Docket Office (phone: (800) 647–5527) greater than: is Document Management Facility, U.S. Department of Transportation, Docket Modified Water energy Operations, M–30, West Building factor, Equipment class factor, Ground Floor, Room W12–140, 1200 gal./cu. ft./ cu. ft./kWh/ cycle New Jersey Avenue SE., Washington, cycle DC 20590. Top-Loading ...... 1.60 8.5 FOR FURTHER INFORMATION CONTACT: Ann Front-Loading ... 2.00 5.5 Johnson, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, Issued in Washington, DC, on November 1, 1801 Airport Road, Room 100, Wichita, Kansas 67209; phone: (316) 946–4105; 2011. fax: (316) 946–4107; email: Kathleen B. Hogan, ann.johnson@faa.gov. SUMMARY: PART 431—ENERGY EFFICIENCY PROGRAM FOR CERTAIN COMMERCIAL AND INDUSTRIAL EQUIPMENT tkelley on DSK3SPTVN1PROD with RULES 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 VerDate Mar<15>2010 16:08 Nov 07, 2011 Jkt 226001 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 PO 00000 Frm 00041 Fmt 4700 Sfmt 4700 69123 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 Federal Aviation Administration, DOT. ACTION: Final rule. AGENCY: E:\FR\FM\08NOR1.SGM 08NOR1

Agencies

[Federal Register Volume 76, Number 216 (Tuesday, November 8, 2011)]
[Rules and Regulations]
[Page 69123]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2011-28861]


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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.

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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 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: 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


Sec.  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
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