Vol. 74 No. 31. Wednesday Feb. 18, Pages

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1 Vol. 74 No. 31 Wednesday Feb. 18, 2009 Pages pwalker on PROD1PC71 with NOTICES VerDate Nov :31 Feb 17, 2009 Jkt PO Frm Fmt 4710 Sfmt 4710 E:\FR\FM\18FEWS.LOC 18FEWS

2 II Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 pwalker on PROD1PC71 with NOTICES The FEDERAL REGISTER (ISSN ) is published daily, Tuesday through Friday, except official holidays, by the Office of the Federal Register, National Archives and Records Administration, Washington, DC 20408, under the Federal Register Act (44 U.S.C. Ch. 15) and the regulations of the Administrative Committee of the Federal Register (1 CFR Ch. I). The Superintendent of Documents, U.S. Government Printing Office, Washington, DC is the exclusive distributor of the official edition. Periodicals postage is paid at Washington, DC. The FEDERAL REGISTER provides a uniform system for making available to the public regulations and legal notices issued by Federal agencies. 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To provide the public with access to information necessary to research Federal agency regulations which directly affect them. There will be no discussion of specific agency regulations. llllllllllllllllll WHEN: Tuesday, February 24, :00 a.m. 12:30 p.m. WHERE: Office of the Federal Register Conference Room, Suite North Capitol Street, NW. Washington, DC RESERVATIONS: (202) VerDate Nov :31 Feb 17, 2009 Jkt PO Frm Fmt 4710 Sfmt 4710 E:\FR\FM\18FEWS.LOC 18FEWS

3 Contents Federal Register Vol. 74, No. 31 Wednesday, February 18, 2009 III pwalker on PROD1PC71 with NOTICES2 Advisory Council on Historic Preservation See Historic Preservation, Advisory Council Agriculture Department See Forest Service See Natural Resources Conservation Service Broadcasting Board of Governors RULES Service of Process, 7562 Children and Families Administration NOTICES Statements of Organization, Functions and Delegations of Authority, 7603 Civil Rights Commission NOTICES Meetings; Sunshine Act, Coast Guard PROPOSED RULES Anchorage Regulations: Port of New York; Withdrawal, Passenger Weight and Inspected Vessel Stability Requirements, Commerce Department See International Trade Administration See National Oceanic and Atmospheric Administration Department of Transportation See Pipeline and Hazardous Materials Safety Administration Education Department NOTICES Charter School Programs: Reopening 2009 Fiscal Year (FY) Competition for Charter School Programs, Impact Aid Discretionary Construction Grant Program: Inviting Applications for New Awards for 2009 Fiscal Year (FY), Employment Standards Administration NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals, Energy Department See Federal Energy Regulatory Commission NOTICES Environmental Impact Statements; Intent: TX Energy, LLC, Industrial Gasification Facility, Beaumont, TX, Environmental Protection Agency NOTICES Pesticide Products; Registration Applications, Executive Office of the President See National Drug Control Policy Office Federal Aviation Administration RULES Airworthiness Directives: Airplanes; Airbus Model A and 300 SeriesAirplanes, and Airbus Model A Series, etc., Cessna Aircraft Co. Models 401, 401A, 401B, 402, 402A, and 402B Airplanes, Learjet Model 55, 55B, and 55C Airplanes, Class E Airspace; Amendment: Atlantic, IA, 7557 Corpus Christi, TX, Tulsa, OK, Class E Airspace; Revision: Galena, AK, Class E Airspace; Revocation: Rockport, TX, Establishment of Colored Federal Airways: Alaska, PROPOSED RULES Airworthiness Directives: BAE Systems (Operations) Limited Model BAe 146 and Avro 146 RJ Airplanes, Boeing Model and D Series Airplanes, Empresa Brasileira de Aeronautica S.A. (EMBRAER) Airplanes; Model EMB 135BJ, 135ER, et al., Saab AB, Saab Aerosystems Model SAAB 340A (SAAB/ SF340A) and SAAB 340B Airplanes, Turbofan Engines; Rolls Royce plc RB211 Trent 800 Series, NOTICES Meetings: National Parks Overflights Advisory Group Aviation Rulemaking Committee, Federal Energy Regulatory Commission NOTICES Meetings; Sunshine Act, Federal Reserve System NOTICES Meetings; Sunshine Act, 7601 Forest Service NOTICES Environmental Impact Statements; Availability, etc: Ochoco National Forest, Lookout Mountain Ranger District; Oregon; Big Summit Allotment Management Plan, Environmental Impact Statements; Intent: Ochoco National Forest, Lookout Mountain Ranger District; Oregon, Meetings: Fremont and Winema Resource Advisory Committee, 7587 Lake County Resource Advisory Committee, 7587 Ravalli County Resource Advisory Committee, 7587 Health and Human Services Department See Children and Families Administration VerDate Nov<24> :34 Feb 17, 2009 Jkt PO Frm Fmt 4748 Sfmt 4748 E:\FR\FM\18FECN.SGM 18FECN

4 IV Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 / Contents pwalker on PROD1PC71 with NOTICES2 See National Institutes of Health NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals, Historic Preservation, Advisory Council NOTICES Meetings: Advisory Council on Historic Preservation, 7584 Homeland Security Department See Coast Guard See Transportation Security Administration Internal Revenue Service PROPOSED RULES Further Guidance on the Application of Section 409A to Nonqualified Deferred Compensation Plans; Correction, 7575 International Trade Administration NOTICES Applications: Duty-Free Entry of Scientific Instruments, 7588 Labor Department See Employment Standards Administration Maritime Administration NOTICES Invitation for Public Comments: Requested Administrative Waiver of the Coastwise Trade Laws for the vessel WINDSONG, Requested Administrative Waiver of the Coastwise Trade Laws: HOLLYWOOD, 7635 L ATITUDE 32, National Drug Control Policy Office NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals, 7621 National Institutes of Health NOTICES Analysis of Comments and Implementation of the NIH Public Access Policy, Meetings: Center for Scientific Review, Center for Scientific Review Special Emphasis Panel; Amendment, 7615 National Cancer Institute Special Emphasis Panel, National Center for Research Resources Special Emphasis Panel, 7616 National Institute of Allergy and Infectious Diseases Special Emphasis Panel, National Institute of Child Health and Human Development Special Emphasis Panel, 7618 National Institute of Dental and Craniofacial Research Special Emphasis Panel, 7618 National Institute of Mental Health Special Emphasis Panel, 7617 National Institute of Neurological Disorders and Stroke Initial Review Group, National Institute on Aging Special Emphasis Panel, National Oceanic and Atmospheric Administration PROPOSED RULES Atlantic Highly Migratory Species: 2009 Atlantic Bluefin Tuna Quota Specifications and Effort Controls, NOTICES Applications: Seats for the Monterey Bay National Marine Sanctuary Advisory Council; Availability, Availability of Grant Funds for Fiscal Year 2009; Correction, 7588 Incidental Takes of Marine Mammals During Specified Activities: On-ice Marine Geophysical and Seismic Operations in State/OCS Waters of the U.S. Beaufort Sea off Alaska; Withdrawal, 7589 Taking and Importing Marine Mammals: U.S. Navy s Atlantic Fleet Active Sonar Training, 7590 Taking and Importing Marine Mammals; U.S. Navy Training in the Southern California Range Complex, Natural Resources Conservation Service PROPOSED RULES Healthy Forests Reserve Program, 7563 Nuclear Regulatory Commission RULES Regulatory Changes to Implement the Additional Protocol to the US/IAEA Safeguards Agreement; Correction, 7549 NOTICES Meetings; Sunshine Act, Pipeline and Hazardous Materials Safety Administration NOTICES Applications: Delays in Processing Special Permits, 7636 Modification of Special Permit, Securities and Exchange Commission NOTICES Meetings; Sunshine Act, 7622 Self-Regulatory Organizations; Proposed Rule Changes: NASDAQ Stock Market LLC, Small Business Administration NOTICES Disaster Declaration: Oregon, 7625 Social Security Administration NOTICES Title XVI: Determining Childhood Disability Documenting a Child s Impairment-Related Limitations, Title XVI; Determining Childhood Disability The Functional Equivalence Domain of Attending and Completing Tasks, Surface Transportation Board NOTICES Abandonment Exemptions: Illinois Central Railroad Co.; Grenada County, MS, Puget Sound & Pacific Railroad Co.; Grays Harbor County, WA, 7638 Discontinuance of Service Exemption: San Diego & Imperial Valley Railroad Co., Inc.; San Diego County, CA, 7639 VerDate Nov<24> :34 Feb 17, 2009 Jkt PO Frm Fmt 4748 Sfmt 4748 E:\FR\FM\18FECN.SGM 18FECN

5 Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 / Contents V Transportation Department See Federal Aviation Administration See Maritime Administration See Pipeline and Hazardous Materials Safety Administration See Surface Transportation Board See Transportation Security Administration Transportation Security Administration NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals, 7619 Treasury Department See Internal Revenue Service NOTICES Meetings: Community Development Advisory Board, 7639 Reader Aids Consult the Reader Aids section at the end of this page for phone numbers, online resources, finding aids, reminders, and notice of recently enacted public laws. To subscribe to the Federal Register Table of Contents LISTSERV electronic mailing list, go to listserv.access.gpo.gov and select Online mailing list archives, FEDREGTOC-L, Join or leave the list (or change settings); then follow the instructions. pwalker on PROD1PC71 with NOTICES2 VerDate Nov<24> :34 Feb 17, 2009 Jkt PO Frm Fmt 4748 Sfmt 4748 E:\FR\FM\18FECN.SGM 18FECN

6 VI Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 / Contents CFR PARTS AFFECTED IN THIS ISSUE A cumulative list of the parts affected this month can be found in the Reader Aids section at the end of this issue. 7 CFR Proposed Rules: CFR CFR 39 (3 documents) , 7552, (6 documents) , 7558, 7559, 7560, 7561 Proposed Rules: 39 (5 documents) , 7565, 7568, 7570, CFR CFR Proposed Rules: CFR Proposed Rules: CFR Proposed Rules: CFR Proposed Rules: pwalker on PROD1PC71 with NOTICES VerDate Nov :40 Feb 17, 2009 Jkt PO Frm Fmt 4711 Sfmt 4711 E:\FR\FM\18FELS.LOC 18FELS

7 7549 Rules and Regulations Federal Register Vol. 74, No. 31 Wednesday, February 18, 2009 cprice-sewell on PRODPC61 with RULES This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C The Code of Federal Regulations is sold by the Superintendent of Documents. Prices of new books are listed in the first FEDERAL REGISTER issue of each week. NUCLEAR REGULATORY COMMISSION 10 CFR Part 75 RIN 3150 AH38 [NRC ] Regulatory Changes To Implement the Additional Protocol to the US/IAEA Safeguards Agreement; Correction AGENCY: Nuclear Regulatory Commission. ACTION: Final rule; correcting amendment. SUMMARY: On December 23, 2008 (73 FR 78599), the Nuclear Regulatory Commission (NRC) published a final rule that amended the NRC s regulations to implement the requirements under the Protocol Additional to the Agreement between the United States of America and the International Atomic Energy Agency for the Application of Safeguards in the United States of America (Additional Protocol) for certain NRC and Agreement State licensees to report information on various nuclear fuel cycle-related activities and to provide the International Atomic Energy Agency (IAEA) with access to those locations. This document is necessary to correct an erroneous amendatory instruction which resulted in two undesignated center headings. DATES: The correction is effective February 18, 2009, and is applicable to December 23, 2008, the date the original rule became effective. ADDRESSES: You can access publicly available documents related to this document using the following methods: Federal e-rulemaking Portal: Go to and search for documents filed under Docket ID NRC Address questions about NRC dockets to Carol Gallagher ; Carol.Gallagher@nrc.gov. NRC s Public Document Room (PDR): The public may examine and have copied for a fee publicly available documents at the NRC s PDR, Public File Area O1 F21, One White Flint North, Rockville Pike, Rockville, Maryland. NRC s Agencywide Documents Access and Management System (ADAMS): Publicly available documents created or received at the NRC are available electronically at the NRC s electronic Reading Room at reading-rm/adams.html. From this page, the public can gain entry into ADAMS, which provides text and image files of NRC s public documents. If you do not have access to ADAMS or if there are problems in accessing the documents located in ADAMS, contact the NRC s PDR reference staff at , , or by to pdr.resource@nrc.gov. FOR FURTHER INFORMATION CONTACT: Michael T. Lesar, Chief, Rulemaking, Directives and Editing Branch, Office of Administration, Nuclear Regulatory Commission, Washington, DC , telephone , Michael.Lesar@nrc.gov. SUPPLEMENTARY INFORMATION: This document corrects an erroneous amendatory instruction which resulted in two undesignated center headings. List of Subjects in 10 CFR Part 75 Criminal penalties, Intergovernmental relations, Nuclear materials, Nuclear power plants and reactors, Reporting and recordkeeping requirements, Security measures. For the reasons set out in the preamble and under the authority of the Atomic Energy Act of 1954, as amended; the Energy Reorganization Act of 1974, as amended; and 5 U.S.C. 552 and 553, the NRC is adopting the following amendment to 10 CFR Part 75. PART 75 SAFEGUARDS ON NUCLEAR MATERIAL IMPLEMENTATION OF US/IAEA AGREEMENT 1. The authority citation for Part 75 continues to read as follows: Authority: Secs. 53, 63, 103, 104, 122, 161, 68 Stat. 930, 932, 936, 937, 939, 948, as amended (42 U.S.C. 2073, 2093, 2133, 2134, 2152, 2201); sec. 201, 88 Stat. 1242, as VerDate Nov<24> :38 Feb 17, 2009 Jkt PO Frm Fmt 4700 Sfmt 4700 E:\FR\FM\18FER1.SGM 18FER1 amended (42 U.S.C. 5841); sec. 1704, 112 Stat (44 U.S.C note). Section 75.4 also issued under secs. 135, 141, Public Law , 96 Stat. 2232, 2241 (42 U.S.C , On page 78613, in the third column, instruction 50 is corrected to read as follows: 50. Section and the undesignated center heading Installations Designated for IAEA Safeguards that follows are removed. Dated at Rockville, Maryland, this 10th day of February For the Nuclear Regulatory Commission. Michael T. Lesar, Chief, Rulemaking, Directives, and Editing Branch, Division of Administrative Services, Office of Administration. [FR Doc. E Filed ; 8:45 am] BILLING CODE P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA ; Directorate Identifier 2008 NM 223 AD; Amendment ; AD ] RIN 2120 AA64 Airworthiness Directives; Airbus Model A and 300 Series Airplanes, and Airbus Model A , 300, 500, and 600 Series Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; request for comments. SUMMARY: We are adopting a new airworthiness directive (AD) for the products listed above. This 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 A330 aircraft experienced a sudden [uncommanded] nose down order [event] while in cruise. This order was preceded by an automatic autopilot disconnection and triggering of the NAV IR1 FAULT Electronic Centralised Aircraft Monitor (ECAM) Caution. Investigations highlighted that at time of the event the Air Data Reference 1 (ADR) part

8 7550 Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 / Rules and Regulations cprice-sewell on PRODPC61 with RULES of ADIRU1 [Air Data Inertial Reference Unit] was providing erroneous and temporary wrong parameters in a random manner. This abnormal behaviour of the ADR1 led to several consequences such as unjustified stall and over speed warnings, loss of attitude information on Captain Primary Flight Display (PFD) and several ECAM warnings. Among the abnormal parameters, the provided Angle of Attack (AoA) value was such that the flight control computers commanded a sudden nose down aircraft movement, which constitutes an unsafe condition. * * * * * * * * These anomalies could result in high pilot workload, deviation from the intended flight path, and possible loss of control of the airplane. This AD requires actions that are intended to address the unsafe condition described in the MCAI. DATES: This AD becomes effective March 5, The Director of the Federal Register approved the incorporation by reference of certain publications, listed in the AD as of March 5, We must receive comments on this AD by March 20, ADDRESSES: You may send comments by any of the following methods: Federal erulemaking Portal: Go to Follow the instructions for submitting comments. Fax: (202) Mail: U.S. Department of Transportation, Docket Operations, M 30, West Building Ground Floor, Room W12 140, 1200 New Jersey Avenue, SE., Washington, DC Hand Delivery: U.S. Department of Transportation, Docket Operations, M 30, West Building Ground Floor, Room W12 40, 1200 New Jersey Avenue, SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. Examining the AD Docket You may examine the AD docket on the Internet at 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 AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone (800) ) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM 116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington ; telephone (425) ; fax (425) SUPPLEMENTARY INFORMATION: Discussion The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community, has issued EASA Emergency Airworthiness Directive E, dated January 15, 2009 (referred to after this as the MCAI ), to correct an unsafe condition for the specified products. The MCAI states: An A330 aircraft experienced a sudden [uncommanded] nose down order [event] while in cruise. This order was preceded by an automatic autopilot disconnection and triggering of the NAV IR1 FAULT Electronic Centralised Aircraft Monitor (ECAM) Caution. Investigations highlighted that at time of the event the Air Data Reference 1 (ADR) part of ADIRU1 [Air Data Inertial Reference Unit] was providing erroneous and temporary wrong parameters in a random manner. This abnormal behaviour of the ADR1 led to several consequences such as unjustified stall and over speed warnings, loss of attitude information on Captain Primary Flight Display (PFD) and several ECAM warnings. Among the abnormal parameters, the provided Angle of Attack (AoA) value was such that the flight control computers commanded a sudden [uncommanded] nose down aircraft movement, which constitutes an unsafe condition. At this stage of the investigation, the analysis of available data indicates that ADIRU1 abnormal behaviour is likely at the origin of the event. Due to similar design, the A340 aircraft are also impacted by this issue. In order to prevent the ADR from providing erroneous data to other aircraft systems, EASA [Emergency] AD E [dated November 19, 2008] was issued to require, in case faulty Inertial Reference (IR) is detected, to isolate both the IR and ADR by accomplishment of a modified Aircraft Flight Manual (AFM) operational procedure. Since that AD [EASA AD E, dated November 19, 2008] was issued, it has been reported that the OFF light did not illuminate in the cockpit after setting the IR and ADR pushbuttons to OFF. Investigation has determined that the ADIRU was indeed sometimes affected by another failure control. To prevent such a failure, the operational procedure has been updated to instruct the flight crew to de-energize the ADIRU if the OFF light is not illuminated after setting the IR and ADR pushbuttons to OFF. Consequently, [EASA Emergency] AD E [dated December 18, 2008], which superseded [EASA Emergency] AD E [dated November 19, 2008], requires accomplishment of the updated AFM operational procedure. Since this second AD was issued [EASA Emergency AD E, dated December 18, 2008], a new service event has been reported highlighting that, in some failure cases, even though the OFF light illuminates in the cockpit after setting the IR and ADR pushbuttons to OFF, the IR could VerDate Nov<24> :38 Feb 17, 2009 Jkt PO Frm Fmt 4700 Sfmt 4700 E:\FR\FM\18FER1.SGM 18FER1 keep providing erroneous data to other systems. In order to address all identified failure cases, de-energizing the affected ADIRU must be done by setting the IR mode rotary selector to OFF. Consequently, this AD, which supersedes AD E [dated December 18, 2008], requires accomplishment of the updated AFM operational procedure. The anomalies described above could result in high pilot workload, deviation from the intended flight path, and possible loss of control of the airplane. You may obtain further information by examining the MCAI in the AD docket. Relevant Service Information Airbus has issued A330 Temporary Revision /46, Issue 3, dated January 13, 2009, to the A330 (Airbus) Flight Manual; and A340 Temporary Revision /54, Issue 3, dated January 13, 2009, to the A340 (Airbus) Flight Manual. The actions described in this service information are intended to correct the unsafe condition identified in the MCAI. FAA s Determination and Requirements of This AD This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are issuing this AD because we evaluated all pertinent information and determined the unsafe condition exists and is likely to exist or develop on other products of the same type design. Differences Between the AD and the MCAI or Service Information We have reviewed the MCAI and related service information and, in general, agree with their substance. But we might have found it necessary to use different words from those in the MCAI to ensure the AD is clear for U.S. operators and is enforceable. In making these changes, we do not intend to differ substantively from the information provided in the MCAI and related service information. We might also have required different actions in this AD from those in the MCAI in order to follow FAA policies. Any such differences are highlighted in a Note within the AD. FAA s Determination of the Effective Date An unsafe condition exists that requires the immediate adoption of this AD. The FAA has found that the risk to

9 Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 / Rules and Regulations 7551 cprice-sewell on PRODPC61 with RULES the flying public justifies waiving notice and comment prior to adoption of this rule to prevent the ADR from providing erroneous data to other aircraft systems, which could result in high pilot workload, deviation from the intended flight path, and possible loss of control of the airplane. Therefore, we determined that notice and opportunity for public comment before issuing this AD are impracticable and that good cause exists for making this amendment effective in fewer than 30 days. Comments Invited This AD is a final rule that involves requirements affecting flight safety, and we did not precede it by notice and opportunity for public comment. We invite you to send any written relevant data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include Docket No. FAA ; Directorate Identifier 2008 NM 223 AD at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this AD because of those comments. We will post all comments we receive, without change, to including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD. Authority for This Rulemaking Title 49 of the United States Code specifies the FAA s authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency s authority. We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: General requirements. Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings We determined that this AD will not have federalism implications under Executive Order This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify this AD: 1. Is not a significant regulatory action under Executive Order 12866; 2. Is not a significant rule under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and 3. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. We prepared a regulatory evaluation of the estimated costs to comply with this AD and placed it in the AD docket. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39 AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, [Amended] 2. The FAA amends by adding the following new AD: Airbus: Amendment Docket No. FAA ; Directorate Identifier 2008 NM 223 AD. Effective Date (a) This airworthiness directive (AD) becomes effective March 5, Affected ADs (b) None. Applicability (c) This AD applies to Airbus Model A and 300; and A , 300, 500, and 600 series airplanes, certificated in any category, as listed in paragraphs (c)(1) and (c)(2) of this AD. (1) A , 202, 203, 223, 243, 301, 302, 303, 321, 322, 323, 341, 342, and 343 airplanes, all serial numbers, equipped with Northrop-Grumman (formerly Litton) Air Data Inertial Reference Units (ADIRUs), part number (P/N) ZZ (with ZZ from 09 up to 16 inclusive). (2) A , 212, 213, 311, 312, 313, 541, and 642 airplanes, all serial numbers, equipped with Northrop-Grumman VerDate Nov<24> :38 Feb 17, 2009 Jkt PO Frm Fmt 4700 Sfmt 4700 E:\FR\FM\18FER1.SGM 18FER1 (formerly Litton) ADIRUs, P/N ZZ (with ZZ from 09 up to 16 inclusive). Subject (d) Air Transport Association (ATA) of America Code 34: Navigation. Reason (e) The mandatory continued airworthiness information (MCAI) states: An A330 aircraft experienced a sudden [uncommanded] nose down order [event] while in cruise. This order was preceded by an automatic autopilot disconnection and triggering of the NAV IR1 FAULT Electronic Centralised Aircraft Monitor (ECAM) Caution. Investigations highlighted that at time of the event the Air Data Reference 1 (ADR) part of ADIRU1 [Air Data Inertial Reference Unit] was providing erroneous and temporary wrong parameters in a random manner. This abnormal behaviour of the ADR1 led to several consequences such as unjustified stall and over speed warnings, loss of attitude information on Captain Primary Flight Display (PFD) and several ECAM warnings. Among the abnormal parameters, the provided Angle of Attack (AoA) value was such that the flight control computers commanded a sudden [uncommanded] nose down aircraft movement, which constitutes an unsafe condition. At this stage of the investigation, the analysis of available data indicates that ADIRU1 abnormal behaviour is likely at the origin of the event. Due to similar design, the A340 aircraft are also impacted by this issue. In order to prevent the ADR from providing erroneous data to other aircraft systems, EASA [Emergency] AD E [dated November 19, 2008] was issued to require, in case faulty Inertial Reference (IR) is detected, to isolate both the IR and ADR by accomplishment of a modified Aircraft Flight Manual (AFM) operational procedure. Since that AD [EASA AD E, dated November 19, 2008] was issued, it has been reported that the OFF light did not illuminate in the cockpit after setting the IR and ADR pushbuttons to OFF. Investigation has determined that the ADIRU was indeed sometimes affected by another failure control. To prevent such a failure, the operational procedure has been updated to instruct the flight crew to de-energize the ADIRU if the OFF light is not illuminated after setting the IR and ADR pushbuttons to OFF. Consequently, [EASA Emergency] AD E [dated December 18, 2008], which superseded [EASA Emergency] AD E [dated November 19, 2008], requires accomplishment of the updated AFM operational procedure. Since this second AD was issued [EASA Emergency AD E, dated December 18, 2008], a new service event has been reported highlighting that, in some failure cases, even though the OFF light illuminates in the cockpit after setting the IR and ADR pushbuttons to OFF, the IR could keep providing erroneous data to other systems. In order to address all identified failure cases, de-energizing the affected ADIRU must

10 7552 Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 / Rules and Regulations cprice-sewell on PRODPC61 with RULES be done by setting the IR mode rotary selector to OFF. Consequently, this AD, which supersedes AD E [dated December 18, 2008], requires accomplishment of the updated AFM operational procedure. The anomalies described above could result in high pilot workload, deviation from the intended flight path, and possible loss of control of the airplane. Actions and Compliance (f) Unless already done: Within 14 days after the effective date of this AD, revise the applicable section of the A330 or A340 (Airbus) Flight Manual (FM) by inserting a copy of A330 (Airbus) Temporary Revision (TR) /46, or A340 (Airbus) TR / 54, both Issue 3, both dated January 13, 2009, as applicable. Thereafter, operate the airplane according to the limitations and procedures in the TRs. When information identical to that in the TR has been included in the general revisions of the FM, the general revisions may be inserted in the FM, and the TR may be removed. FAA AD Differences Note 1: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM 116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR Send information to ATTN: Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM 116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington ; telephone (425) ; fax (425) Before using any approved AMOC on any airplane to which the AMOC applies, notify your principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAAapproved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number Related Information (h) Refer to MCAI European Aviation Safety Agency Emergency Airworthiness Directive E, dated January 15, 2009; A330 (Airbus) TR /46, Issue 3, dated January 13, 2009; and A340 (Airbus) TR /54, Issue 3, dated January 13, 2009; for related information. Material Incorporated by Reference (i) You must use A330 (Airbus) Temporary Revision /46, Issue 3, dated January 13, 2009, to the A330 (Airbus) Flight Manual; or A340 (Airbus) Temporary Revision /54, Issue 3, dated January 13, 2009, to the A340 (Airbus) Flight Manual; as applicable; to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Airbus SAS Airworthiness Office EAL, 1 Rond Point Maurice Bellonte, Blagnac Cedex, France; fax ; airworthiness.a330- A340@airbus.com; Internet (3) You may review copies of the service information that is incorporated by reference at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call or (4) You may also review copies of the service information at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call , or go to: code_of_federal_regulations/ ibr_locations.html. Issued in Renton, Washington, on January 23, Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E Filed ; 8:45 am] BILLING CODE P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA ; Directorate Identifier 2008 CE 073 AD; Amendment ; AD ] RIN 2120 AA64 Airworthiness Directives; Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, and 402B Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 401, 401A, 401B, 402, 402A, and 402B airplanes. This AD requires an inspection of the auxiliary wing spar VerDate Nov<24> :38 Feb 17, 2009 Jkt PO Frm Fmt 4700 Sfmt 4700 E:\FR\FM\18FER1.SGM 18FER1 near the location where the main landing gear trunnion is mounted for cracks; immediate replacement if cracks of 0.5 inch or more are found; repetitive inspections with replacement at a later time as long as cracks of less than 0.5 inch are found; and a report to the FAA and Cessna if any cracks are found. This AD results from several reports of fatigue cracking on the affected airplanes in the auxiliary wing spar. We are issuing this AD to detect and correct such cracks, which, if not corrected, could result in failure of the wing auxiliary spar web and cause landing gear collapse during normal landing. This could lead to loss of control and passenger injury. DATES: This AD becomes effective on March 2, On March 2, 2009, the Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD. We must receive any comments on this AD by April 20, ADDRESSES: Use one of the following addresses to comment on this AD. Federal erulemaking Portal: Go to Follow the instructions for submitting comments. Fax: (202) Mail: U.S. Department of Transportation, Docket Operations, M 30, West Building Ground Floor, Room W12 140, 1200 New Jersey Avenue, SE., Washington, DC 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. To get the service information identified in this AD, contact Cessna Aircraft Company, P.O. Box 7704, Wichita, Kansas 67277; telephone: (800) or (316) ; Internet: To view the comments to this AD, go to The docket number is FAA ; Directorate Identifier 2008 CE 073 AD. FOR FURTHER INFORMATION CONTACT: Adam Neubauer, Aerospace Engineer, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) ; fax: (316) SUPPLEMENTARY INFORMATION: Discussion We have received several reports of fatigue cracking on Cessna Models 402A and 402B airplanes in the area of the auxiliary wing spar where the main landing gear trunnion is mounted. Other models with similar design that share

11 Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 / Rules and Regulations 7553 cprice-sewell on PRODPC61 with RULES the same risk of auxiliary wing spar cracking include Cessna Models 401, 401A, 401B, and 402. This condition, if not corrected, could result in failure of the wing auxiliary spar web and cause landing gear collapse during normal landing. This could lead to loss of control and passenger injury. Cessna has shown the FAA that parts with cracks in this area that are 0.5 inch or more need immediate replacement as they pose an immediate safety of flight issue. Cessna s analysis also shows that residual strength in the wing, up to ultimate design loads, will remain with cracks less than 0.5 inch, and the growth of these cracks is slow. Because analysis shows that a repetitive inspection program can provide an interim acceptable level of safety, the FAA will allow repetitive inspections when a crack less than 0.5 inch is found in the wing auxiliary spar during the initial inspection required by this action. Cracks need to be monitored (inspected every 50 hours time-inservice (TIS)) to show they do not reach 0.5 inch. If any crack reaches 0.5 inch or more, then the cracked part must be replaced before further flight. If no crack reaches 0.5 inch or more, then the cracked part must be replaced within 200 hours TIS or 12 months, whichever occurs first, regardless of crack growth. Relevant Service Information We reviewed Cessna Service Bulletin MEB08 8, dated December 23, The service information describes procedures for inspecting the wing auxiliary spar webs for cracks and replacing the left web/right web with a new left web/right web. FAA s Determination and Requirements of This AD We are issuing this AD because we evaluated all the information and determined the unsafe condition described previously is likely to exist or develop on other products of the same type design. This AD requires: An inspection of the auxiliary wing spar near the location where the main landing gear trunnion is mounted for cracks; Immediate replacement if cracks are 0.5 inch or more; Repetitive inspections (50 hours TIS) with replacement at 200 hours TIS or 12 months, whichever occurs first, if cracks are found that are less than 0.5 inch; and A report to the FAA and Cessna if any cracks are found. The FAA considers this interim action. We will work with Cessna and evaluate the crack reports and all other information. Based on this information, we may initiate additional rulemaking action. FAA s Determination of the Effective Date An unsafe condition exists that requires the immediate adoption of this AD. The FAA has found that the risk to the flying public justifies waiving notice and comment prior to adoption of this rule because cracks in the wing auxiliary spar web could lead to failure in this area and could cause landing gear collapse during normal landing. This could lead to loss of control and passenger injury. Some of the affected airplanes are operated 100 hours TIS or more monthly. Therefore, the repetitive inspections on these airplanes would occur in short intervals, and the replacement would be required within 2 months. Therefore, we determined that notice and opportunity for public comment before issuing this AD are impracticable and that good cause exists for making this amendment effective in fewer than 30 days. Comments Invited This AD is a final rule that involves requirements affecting flight safety, and we did not precede it by notice and an opportunity for public comment. We invite you to send any written relevant data, views, or arguments regarding this AD. Send your comments to an address listed under the ADDRESSES section. Include the docket number FAA ; Directorate Identifier 2008 CE 073 AD at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of the AD. We will consider all comments received by the closing date and may amend the AD in light of those comments. We will post all comments we receive, without change, to including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive concerning this AD. Authority for This Rulemaking Title 49 of the United States Code specifies the FAA s authority to issue rules on aviation safety. Subtitle I, Section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency s authority. VerDate Nov<24> :38 Feb 17, 2009 Jkt PO Frm Fmt 4700 Sfmt 4700 E:\FR\FM\18FER1.SGM 18FER1 We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701, General requirements. Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings We determined that this AD will not have federalism implications under Executive Order This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a significant regulatory action under Executive Order 12866; (2) Is not a significant rule under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and (3) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. We prepared a regulatory evaluation of the estimated costs to comply with this AD and placed it in the AD docket. Examining the AD Docket You may examine the AD docket that contains the AD, the regulatory evaluation, any comments received, and other information on the Internet at or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Office (telephone (800) ) is located at the street address stated in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: