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--- schema: federal-register doc_type: fedreg source_file: FR-2014-03-18.xml --- 79 52 Tuesday, March 18, 2014 Contents Agricultural Marketing Agricultural Marketing Service PROPOSED RULES Pistachios Grown in California, Arizona, and New Mexico: Aflatoxin Regulations, 15050-15052 2014-05834 Agriculture Agriculture Department See Agricultural Marketing Service See Animal and Plant Health Inspection Service See Farm Service Agency See Food and Nutrition Service See Rural Business-Cooperative Service See Rural Housing Service See Rural Utilities Service Animal Animal and Plant Health Inspection Service NOTICES Determinations of Nonregulated Status:

BASF Plant Sciences, LP, 15095-15096 2014-06016 Dow AgroSciences, LLC, 15096-15097 2014-06013 Census Bureau Census Bureau NOTICES Meetings: Census Scientific Advisory Committee, 15097-15098 2014-05914 Centers Disease Centers for Disease Control and Prevention NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals, 15127-15129 2014-05880 Centers Medicare Centers for Medicare & Medicaid Services RULES Medicare Program: Extension of the Payment Adjustment for Low-Volume Hospitals and the Medicare-dependent Hospital Program under the Hospital Inpatient Prospective Payment Systems for Acute Care Hospitals for Fiscal Year 2014, 15022-15030 2014-05922 Hospital Inpatient Prospective Payment Systems for Acute Care Hospitals and the Long Term Care Hospital Prospective Payment System and Fiscal Year 2013 Rates;

Hospitals' Resident Caps for Graduate Medical Education Payment Purposes, etc.; Corrections, 15032-15033 2014-05836 Hospital Inpatient Prospective Payment Systems for Acute Care Hospitals and the Long Term Care Hospital Prospective Payment System and Fiscal Year 2014 Rates, etc.; Corrections, 15030-15031 2014-05837 Children Children and Families Administration NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals: Federal Strategic Action Plan on Services for Victims of Human Trafficking, etc., 15129 2014-05824 Coast Guard Coast Guard RULES Safety Zones:

Sea World San Diego Fireworks, Mission Bay, San Diego, CA, 15010-15012 2014-05722 PROPOSED RULES Special Local Regulations: 38th Annual Swim around Key West, Atlantic Ocean and Gulf of Mexico, Key West, FL, 15071-15074 2014-05864 Choptank River, between Cambridge, MD and Trappe, MD, 15068-15071 2014-05963 Commerce Commerce Department See Census Bureau See Foreign-Trade Zones Board See International Trade Administration See National Institute of Standards and Technology See National Oceanic and Atmospheric Administration See Patent and Trademark Office Defense Department Defense Department See Navy Department Department of Transportation See Pipeline and Hazardous Materials Safety Administration Education Department Education Department PROPOSED RULES Priorities:

Centers for International Business Education Program, 15084-15087 2014-05941 Foreign Language and Area Studies Fellowships Program, 15081-15083 2014-05863 Language Resource Centers Program, 15074-15077 2014-05937 National Resource Centers Program, 15077-15081 2014-05927 Undergraduate International Studies and Foreign Language Program, 15087-15090 2014-05855 NOTICES Applications for New Awards: Professional Development for Arts Educators Program, 15103-15110 2014-05934 Energy Department Energy Department See Energy Efficiency and Renewable Energy Office See Federal Energy Regulatory Commission PROPOSED RULES Energy Conservation Program:

Data Collection, Comparison with Forecasted Unit Sales of Five Lamp Types, 15058-15061 2014-05776 Energy Efficiency Programs for Consumer Products: Energy Conservation Standards for Commercial and Industrial Air Compressors, 15061-15062 2014-05933 NOTICES Meetings: Environmental Management Site-Specific Advisory Board, Portsmouth, 15110 2014-05973 Fusion Energy Sciences Advisory Committee, 15110-15111 2014-05976 Proposed Arrangements, 15111 2014-05953 Energy Efficiency Energy Efficiency and Renewable Energy Office NOTICES Energy Conservation Program for Consumer Products:

Representative Average Unit Costs of Energy, 15111-15112 2014-05949 Guidance for Industry: Department of Energy Support for Building Energy Code Compliance Software, 15112-15113 2014-05952 Environmental Protection Environmental Protection Agency RULES Air Quality State Implementation Plans; Approvals and Promulgations: Missouri, 15017-15019 2014-05821 Virginia; 2010 Nitrogen Dioxide National Ambient Air Quality Standards, 15012-15016 2014-05808 West Virginia; Steubenville-Weirton, OH-WV Nonattainment Area, 15019-15021 2014-05807 PROPOSED RULES Air Quality State Implementation Plans;

Approvals and Promulgations: Missouri, 15092 2014-05823 Clean Air Act Grant: South Coast Air Quality Management District; Opportunity for Public Hearing, 15090-15092 2014-05906 NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals: Land Disposal Restrictions, 15116 2014-05917 NESHAP for Clay Ceramics Manufacturing, Glass Manufacturing and Secondary Nonferrous Metals Processing Area Sources, 15116-15117 2014-05886 NSPS for Commercial and Industrial Solid Waste Incineration Units, 15117-15118 2014-05884 Nominations:

Human Studies Review Board Advisory Committee, 15118-15119 2014-05907 Petitions for Reconsiderations: Michigan; Regional Haze State Implementation Plan, 15119 2014-05905 Executive Office of the President See Presidential Documents See Science and Technology Policy Office See Trade Representative, Office of United States Export Import Export-Import Bank NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals, 15119-15121 2014-05862 Meetings; Sunshine Act, 15121 2014-06086 Farm Service Farm Service Agency PROPOSED RULES Methodology and Formulas for Allocation of Loan and Grant Program Funds, 15052-15058 2014-05491 Federal Aviation Federal Aviation Administration RULES Airworthiness Directives:

Bombardier, Inc., 14997-14999 2014-04851 The Boeing Company Airplanes, 14977-14996 2014-04819 2014-04826 2014-04838 2014-04843 IFR Altitudes, 14999-15009 2014-05765 PROPOSED RULES Amendment of Class E Airspace: Bridgeport, CT, 15064-15065 2014-05889 Elkin, NC, 15067-15068 2014-05890 Newnan, GA, 15065-15067 2014-05888 Special Conditions: Extra Flugzeugproduktions and Vertriebs [Extra] GmbH, EA-300/LC; Acrobatic Category Aerodynamic Stability, 15062-15064 2014-05951 NOTICES Grant Acquired Property Releases:

Asheville Regional Airport, Asheville, NC, 15203-15204 2014-05898 Federal Communications Federal Communications Commission PROPOSED RULES Radio Broadcasting Services: Haynesville, LA, 15094 2014-05948 Special Access Proceeding, 15092-15093 2014-05940 NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals, 15121-15122 2014-05916 Performance Review Board; Appointments, 15122 2014-05942 Federal Deposit Federal Deposit Insurance Corporation NOTICES Agency Information Collection Activities;

Proposals, Submissions, and Approvals: Retail Foreign Exchange Transactions, 15122 2014-05816 Federal Energy Federal Energy Regulatory Commission NOTICES Meetings; Sunshine Act, 15113-15115 2014-05978 Federal Highway Federal Highway Administration NOTICES Environmental Impact Statements; Availability, etc.: Hawaii, HI, 15204 2014-05899 Federal Reserve Federal Reserve System NOTICES Formations of, Acquisitions by, and Mergers of Bank Holding Companies, 15122-15123 2014-05853 Federal Trade Federal Trade Commission NOTICES Agency Information Collection Activities;

Proposals, Submissions, and Approvals, 15123-15126 2014-05844 2014-05847 Financial Crimes Financial Crimes Enforcement Network NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals: Renewal without Change to the Bank Secrecy Act, Designation of Exempt Person Report, 15204-15205 2014-05965 Fish Fish and Wildlife Service NOTICES Endangered Species Recovery Permit Applications, 15138-15140 2014-05902 Food and Drug Food and Drug Administration NOTICES Agency Information Collection Activities;

Proposals, Submissions, and Approvals: Premarket Notification for a New Dietary Ingredient, 15129-15130 2014-05876 Preparing a Claim of Categorical Exclusion or an Environmental Assessment for Submission to the Center for Food Safety and Applied Nutrition, 15130 2014-05848 Draft Guidance for Industry and Staff: Humanitarian Device Exemption, Questions and Answers, 15130-15131 2014-05900 Draft Guidance for Industry: Bioavailability and Bioequivalence Studies Submitted in New Drug Applications or Investigational New Drug Applications, 15131-15132 2014-05849 Food and Nutrition Food and Nutrition Service RULES WIC Food Packages:

Special Supplemental Nutrition Program; Correction, 15214-15215 C2--2014--04105 Foreign Trade Foreign-Trade Zones Board NOTICES Production Activities: Phillips 66 Co., Foreign-Trade Zone 3, San Francisco, CA, 15098 2014-05970 Reorganizations under Alternative Site Frameworks: Foreign-Trade Zone 60, Nogales, AZ, 15098-15099 2014-05968 Health and Human Health and Human Services Department See Centers for Disease Control and Prevention See Centers for Medicare & Medicaid Services See Children and Families Administration See Food and Drug Administration See Health Resources and Services Administration See National Institutes of Health NOTICES Findings of Research Misconduct, 15127 2014-05921 Health Resources Health Resources and Services Administration NOTICES Meetings:

National Advisory Committee on Rural Health and Human Services, 15132-15133 2014-05950 Homeland Homeland Security Department See Coast Guard See U.S. Customs and Border Protection Interior Interior Department See Fish and Wildlife Service International Trade Adm International Trade Administration NOTICES Antidumping and Countervailing Duty Administrative Reviews; Results, Extensions, Amendments, etc.: Narrow Woven Ribbons with Woven Selvedge from Taiwan; Partial Rescission, 15099-15100 2014-05971 Antidumping and Countervailing Duty Investigations;

Results, Extensions, Amendments, etc.: Grain-Oriented Electrical Steel from the People's Republic of China, 15100 C1--2014--05259 Meetings: United States Travel and Tourism Advisory Board, 15100 2014-06078 International Trade Com International Trade Commission NOTICES Investigations; Determinations, Modifications, Rulings, etc.: Laminated Woven Sacks from China, 15140 2014-05852 Justice Department Justice Department See Justice Programs Office NOTICES Agency Information Collection Activities;

Proposals, Submissions, and Approvals: 2013 National Survey of Prosecutors, 15140-15141 2014-05910 Proposed Settlement Agreements under CERCLA, 15141 2014-05887 Proposed Settlement Agreements under CERCLA and the Resource Conservation and Recovery Act, 15142 2014-05815 Justice Programs Justice Programs Office NOTICES Draft Reports and Recommendations: Research Committee of the Scientific Working Group on Disaster Victim Identification, 15142 2014-05893 Meetings: Coordinating Council on Juvenile Justice and Delinquency Prevention, 15142-15143 2014-05892 Labor Department Labor Department See Workers Compensation Programs Office National Institute National Institute of Standards and Technology NOTICES National Cybersecurity Center of Excellence and Electric Power Sector Identity and Access Management Use Case, 15100-15102 2014-05960 National Institute National Institutes of Health NOTICES Agency Information Collection Activities;

Proposals, Submissions, and Approvals: Qualitative Feedback on Agency Service Delivery; Generic Clearance, 15133 2014-05962 Meetings: Center for Scientific Review, 15133-15135 2014-05870 2014-05871 2014-05872 Draft National Toxicology Program Technical Reports, 15135-15136 2014-05895 National Heart, Lung, and Blood Institute, 15134-15135 2014-05868 2014-05869 Start-Up Exclusive Patent License Agreements: Treatment of Breast Cancer, Prostate Cancer, Ewing Sarcoma, and Thymoma, 15136-15137 2014-05867 National Oceanic National Oceanic and Atmospheric Administration RULES Fisheries of the Exclusive Economic Zone Off Alaska:

Pacific Cod by Catcher Vessels Using Hook-and-Line Gear in the Central Regulatory Area of the Gulf of Alaska, 15048-15049 2014-05919 Pacific Cod by Catcher Vessels Using Hook-and-Line Gear in the Western Regulatory Area of the Gulf of Alask, 15047-15048 2014-05918 Fisheries of the Northeastern United States: Atlantic Mackerel, Squid, and Butterfish Fisheries; Butterfish Trip Limit Reduction, 15046-15047 2014-05920 National Science National Science Foundation NOTICES Permit Applications Received under the Antarctic Conservation Act, 15144 2014-05881 Navy Navy Department NOTICES Privacy Act;

Systems of Records, 15102-15103 2014-05850 Nuclear Regulatory Nuclear Regulatory Commission NOTICES Facility Operating Licenses: Applications and Amendments Involving Proposed No Significant Hazards Considerations, etc., 15144-15157 2014-05645 Inspections, Tests, Analyses, and Acceptance Criteria: Virgil C. Summer Unit 2 Combined License, 15157-15158 2014-05936 License Amendment Applications: Palo Verde Nuclear Generating Station, 15159 2014-05935 Prairie Island Independent Spent Fuel Storage Installation, Northern States Power Co., 15158-15159 2014-05938 Requests for Alternate Decommissioning Schedules:

Department of the Navy Space and Naval Warfare Centers Pacific, 15159-15162 2014-05982 Office of United States Trade Representative See Trade Representative, Office of United States Patent Patent and Trademark Office NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals, 15102 2014-05877 Pension Benefit Pension Benefit Guaranty Corporation RULES Allocation of Assets in Single-Employer Plans; Benefits Payable in Terminated Single-Employer Plans:

Interest Assumptions for Valuing and Paying Benefits, 15009-15010 2014-05854 Pipeline Pipeline and Hazardous Materials Safety Administration RULES Hazardous Materials: Adoption of Certain Special Permits and Competent Authorities into Regulations, 15033-15046 2014-05630 Presidential Documents Presidential Documents ADMINISTRATIVE ORDERS Overtime Pay Regulations; Modernization Efforts (Memorandum of March 13, 2014), 15209-15212 2014-06138 Rural Business Rural Business-Cooperative Service PROPOSED RULES Methodology and Formulas for Allocation of Loan and Grant Program Funds, 15052-15058 2014-05491 Rural Housing Service Rural Housing Service PROPOSED RULES Methodology and Formulas for Allocation of Loan and Grant Program Funds, 15052-15058 2014-05491 Rural Utilities Rural Utilities Service PROPOSED RULES Methodology and Formulas for Allocation of Loan and Grant Program Funds, 15052-15058 2014-05491 Science Technology Science and Technology Policy Office NOTICES Requests for Information:

Interagency Funding for Research and Engineering Projects Conducted by Federal Researchers, 15162-15163 2014-06036 Securities Securities and Exchange Commission NOTICES Meetings; Sunshine Act, 15163 2014-06012 Self-Regulatory Organizations; Proposed Rule Changes: BOX Options Exchange, LLC, 15180-15183 2014-05860 EDGA Exchange, Inc., 15168-15170 2014-05839 EDGX Exchange, Inc., 15166-15168 2014-05840 Financial Industry Regulatory Authority, Inc., 15185 C1--2014--04792 International Securities Exchange, LLC, 15170-15172 2014-05873 Miami International Securities Exchange, LLC, 15183-15190 2014-05858 2014-05859 2014-05874 NASDAQ OMX BX, Inc., 15163-15166 2014-05856 NYSE Arca, Inc., 15191-15198 2014-05861 NYSE MKT, LLC, 15185 C1--2014--05179 The NASDAQ Stock Market, LLC, 15172-15179, 15198-15201 2014-05857 2014-05875 Trading Suspension Orders:

Petrotech Oil and Gas, Inc., 15201 2014-06005 Small Business Small Business Administration NOTICES Disaster Declarations: Georgia, 15201 2014-05851 Trade Representative Trade Representative, Office of United States NOTICES Request for Nominations: Charter Renewal of the Trade Advisory Committee on Africa, 15201-15203 2014-05923 Transportation Department Transportation Department See Federal Aviation Administration See Federal Highway Administration See Pipeline and Hazardous Materials Safety Administration NOTICES Meetings:

Data Capture and Management Research Program, 15203 2014-05865 Treasury Treasury Department See Financial Crimes Enforcement Network See United States Mint Customs U.S. Customs and Border Protection NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals: Documents Required Aboard Private Aircraft, 15137-15138 2014-05866 U.S. Mint United States Mint NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals: Application for Intellectual Property Use Form, 15206-15207 2014-05977 Customer Satisfaction and Opinion Surveys and Focus Group Interviews, 15205-15206 2014-05979 Quantitative Public Opinion Research for Circulating Coins - Surveys and Focus Group Interviews, 15206 2014-05980 Veteran Affairs Veterans Affairs Department NOTICES Meetings:

Genomic Medicine Program Advisory Committee, 15207 2014-05901 Workers' Workers Compensation Programs Office NOTICES Agency Information Collection Activities; Proposals, Submissions, and Approvals, 15143-15144 2014-05981 Separate Parts In This Issue Part II Presidential Documents, 15209-15212 2014-06138 Part III Agriculture Department, Food and Nutrition Service, 15214-15215 C2--2014--04105 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 http://listserv.access.gpo.gov and select Online mailing list archives, FEDREGTOC-L, Join or leave the list (or change settings); then follow the instructions. 79 52 Tuesday, March 18, 2014 Rules and Regulations DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2013-0542; Directorate Identifier 2011-NM-162-AD; Amendment 39-17785 AD 2014-05-12] RIN 2120-AA64 Airworthiness Directives;

The Boeing Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: We are superseding Airworthiness Directive

(AD)2010-15-08 for all The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. AD 2010-15-08 required repetitive inspections for discrepancies of each carriage spindle of the outboard mid-flaps; repetitive gap checks of the inboard and outboard carriages of the outboard mid-flaps to detect fractured carriage spindles; measuring to ensure that any new or serviceable carriage spindle meets minimum allowable diameter measurements taken at three locations; repetitive inspections, measurements, and overhaul of the carriage spindles; replacement of any carriage spindle when it has reached its maximum life limit; and corrective actions if necessary. This new AD requires reducing the life limit of the carriages, reducing the repetitive interval for certain inspections and gap checks for certain carriages. This new AD also adds an option, for certain replacements, of doing an inspection, and related investigative and corrective actions if necessary. This AD was prompted by a report of failure of both flap carriages. We are issuing this AD to detect and correct cracked, corroded, or fractured carriage spindles, which could lead to severe flap asymmetry, and could result in reduced control or loss of controllability of the airplane. DATES: This AD is effective April 22, 2014. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of April 22, 2014. The Director of the Federal Register approved the incorporation by reference of certain other publications listed in this AD as of August 31, 2010 (75 FR 43803, July 27, 2010). ADDRESSES: For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206-544-5000, extension 1; fax 206-766-5680; Internet *https://www.myboeingfleet.com.* You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. Examining the AD Docket You may examine the AD docket on the Internet at *http://www.regulations.gov* by searching for and locating Docket No. FAA-2014-05-12 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 Docket 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: Nancy Marsh, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone:

(425)917-6440; fax:

(425)917-6590; email: *nancy.marsh@faa.gov.* SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking

(NPRM)to amend 14 CFR part 39 to supersede AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010). AD 2010-15-08 applied to all The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. The NPRM published in the **Federal Register** on July 1, 2013 (78 FR 39193). The NPRM was prompted by a report of failure of both flap carriages. The NPRM proposed to continue to require repetitive inspections for discrepancies of each carriage spindle of the outboard mid-flaps; repetitive gap checks of the inboard and outboard carriages of the outboard mid-flaps to detect fractured carriage spindles; measuring to ensure that any new or serviceable carriage spindle meets minimum allowable diameter measurements taken at three locations; repetitive inspections, measurements, and overhaul of the carriage spindles; replacement of any carriage spindle when it has reached its maximum life limit; and corrective actions if necessary. The NPRM also proposed to require reducing the life limit of the carriages, reducing the repetitive interval for certain inspections and gap checks for certain carriages. The NPRM also proposed to add an option, for certain replacements, of doing an inspection, and related investigative and corrective actions if necessary. We are issuing this AD to detect and correct cracked, corroded, or fractured carriage spindles, which could lead to severe flap asymmetry, and could result in reduced control or loss of controllability of the airplane. Comments We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the proposal (78 FR 39193, July 1, 2013) and the FAA's response to each comment. Request to Revise Note Boeing requested we revise note 1 to paragraph

(m)of the NPRM (78 FR 39193, July 1, 2013) to read, “. . . Boeing

(737)Standard Overhaul Practices Manual (SOPM), Revision 25 or later.” Boeing stated that as its production standard changes, the SOPM is revised each time the SOPM is updated. Boeing stated that a global alternative method of compliance

(AMOC)is required each time the SOPM is revised and this generates AMOC activity that does not enhance fleet safety. We disagree to revise Note 1 to paragraph

(m)of this final rule because the text in Note 1 is informational guidance and does not relieve the requirement in paragraph

(m)to obtain approval for the method used to apply plating, regardless of what revision of the SOPM is specified. We have not changed this final rule in this regard. Request to Revise Requirement for Plating Boeing requested the following requirement in paragraph (m)(3) of the NPRM (78 FR 39193, July 1, 2013) be removed, “The carriage must not be plated using any high velocity oxygen fuel

(HVOF)thermal spray process.” Boeing stated AD 2011-04-10, Amendment 39-16609 (76 FR 9498, February 18, 2011), and AD 2012-13-07, Amendment 39-17109 (77 FR 39153, July 2, 2012), required diligent inspection of HVOF coated carriages. Boeing stated that inspections to date have only found minor corrosion, well in advance of a potential unsafe condition. Boeing stated requiring carriages to be converted to nickel [plating] does not enhance fleet safety. We disagree to remove the requested phrase. The restriction against future application of HVOF plating of the flap carriages was coordinated and agreed to by The Boeing Company prior to issuance of the NPRM (78 FR 39193, July 1, 2013). Service experience has shown that the HVOF coating has insufficient reliability, therefore the restriction is necessary. We have not changed this final rule in this regard. Clarification Regarding the Installation of Winglets Aviation Partners Boeing

(APB)stated the installation of winglets per Supplemental Type Certificate

(STC)ST01219SE ( *http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/BE866B732F6CF31086257B9700692796?OpenDocument&Highlight=st01219se* ) does not affect the accomplishment of the manufacturer's service instructions. We agree with APB's statement that the installation of winglets as specified in STC ST01219SE ( *http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/BE866B732F6CF31086257B9700692796?OpenDocument&Highlight=st01219se* ) does not affect accomplishment of the requirements of this AD, and for airplanes on which STC ST01219SE is installed, a “change in product”

(AMOC)approval request is not necessary to comply with the requirements of section 39.17 of the Federal Aviation Regulations (14 CFR 39.17). We have redesignated paragraph

(c)of the NPRM (78 FR 39193, July 1, 2013) as (c)(1) and added this provision in new paragraph (c)(2) of this final rule. Conclusion We reviewed the relevant data, considered the comments received, and determined that air safety and the public interest require adopting this AD with the changes described previously and minor editorial changes. We have determined that these minor changes: • Are consistent with the intent that was proposed in the NPRM (78 FR 39193, July 1, 2013) for correcting the unsafe condition; and • Do not add any additional burden upon the public than was already proposed in the NPRM (78 FR 39193, July 1, 2013). We also determined that these changes will not increase the economic burden on any operator or increase the scope of this AD. Costs of Compliance We estimate that this AD affects 652 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs Action Labor cost Parts cost Cost per product Cost on U.S. operators Inspections [actions retained from existing AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010)] 12 work-hours × $85 per hour = $1,020 $0 $1,020 per inspection cycle $665,040 per inspection cycle. Inspections and measurements [actions retained from existing AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010)] 2 work-hours × $85 per hour = $170 $0 $170 per inspection and measurement cycle $110,840 per inspection and measurement cycle. Overhauls [actions retained from existing AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010)] 16 work-hours × $85 per hour = $1,360 1 $28,000 $29,360 per overhaul cycle $19,142,720 per overhaul cycle. Replacements [actions retained from existing AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010)] 16 work-hours × $85 per hour = $1,360 2 $60,000 $61,360 per replacement cycle $40,006,720 per replacement cycle. 1 $7,000 per spindle; 4 spindles per airplane. 2 $15,000 per spindle; 4 spindles per airplane. The new requirements of this AD add no additional economic burden. 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 have determined that this AD will not have federalism implications under Executive Order 13132. 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),

(3)Will not affect intrastate aviation in Alaska, and

(4)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. 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, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by removing Airworthiness Directive

(AD)2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010), and adding the following new AD: **2014-05-12 The Boeing Company:** Amendment 39-17785; Docket No. FAA-2013-0542; Directorate Identifier 2011-NM-162-AD.

(a)Effective Date This AD is effective April 22, 2014.

(b)Affected ADs This AD supersedes AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010).

(c)Applicability

(1)This AD applies to all The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any category.

(2)Installation of Supplemental Type Certificate

(STC)ST01219SE ( *http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/BE866B732F6CF31086257B9700692796?OpenDocument&Highlight=st01219se* ) does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST01219SE is installed, a “change in product” alternative method of compliance

(AMOC)approval request is not necessary to comply with the requirements of 14 CFR 39.17.

(d)Subject Air Transport Association

(ATA)of America Code 57: Wings.

(e)Unsafe Condition This AD was prompted by a report of failure of both flap carriages. We are issuing this AD to detect and correct cracked, corroded, or fractured carriage spindles, which could lead to severe flap asymmetry, and could result in reduced control or loss of controllability of the airplane.

(f)Compliance Comply with this AD within the compliance times specified, unless already done.

(g)Compliance Times for Paragraphs

(h)and

(j)of This AD This paragraph restates the requirements of paragraph

(g)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010), with revised service information that shortens the compliance times for certain inspections. The tables in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003; and Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012; specify the compliance times for paragraphs

(g)through

(k)of this AD. For carriage spindles that have accumulated the number of flight cycles or years in service specified in the “Threshold” column of the tables in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003, accomplish the gap check, nondestructive test

(NDT)inspection, and general visual inspection specified in paragraphs

(h)and

(j)of this AD within the corresponding interval after December 4, 2003 (the effective date AD 2003-24-08, Amendment 39-13337 (68 FR 67027, December 1, 2003)), as specified in the “Interval” column of the tables in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003, except as specified in paragraph (g)(1) or (g)(2) of this AD. Repeat the gap check, NDT, and general visual inspections at the intervals specified in the “Interval” column of the tables in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003, except as specified in paragraph (g)(1) and (g)(2) of this AD. As of the effective date of this AD, accomplish the gap check, NDT inspection, and general visual inspections specified in paragraphs

(h)and

(j)of this AD within the corresponding interval as specified in the “Interval” column of the tables in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003, and thereafter at the intervals specified in Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012, except as specified in paragraphs (g)(1) and (g)(2) of this AD. Repeat the gap check, NDT, and general visual inspections thereafter at the intervals specified in the “Interval” column of the tables in paragraph 1.E., “Compliance,” of Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012, except as specified in paragraphs (g)(1) and (g)(2) of this AD.

(1)The gap check does not have to be done at the same time as an NDT inspection; after doing an NDT inspection, the interval for doing the next gap check may be measured from the NDT inspection.

(2)As carriage spindles gain flight cycles or years in service and move from one category in the “Threshold” column to another, they are subject to the repetitive inspection intervals corresponding to the new threshold category.

(h)Retained Work Package 2: Gap Check This paragraph restates the requirements of paragraph

(h)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010), with revised service information. Perform a gap check of the inboard and outboard carriage of the left and right outboard mid-flaps to determine if there is a positive indication of a severed carriage spindle, in accordance with Work Package 2 of paragraph 3.B., “Work Instructions,” of Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003; or Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012. As of the effective date of this AD, only Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012, may be used to perform the actions specified in this paragraph.

(i)Retained Work Package 2: Corrective Actions with New Optional Actions and Exception This paragraph restates the requirements of paragraph

(i)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010), with revised service information and new optional actions and exception. If there is a positive indication of a severed carriage spindle during the gap check required by paragraph

(h)of this AD, before further flight, do the actions specified in paragraph (i)(1) or (i)(2) of this AD, except for carriage spindles on which an ultrasonic inspection has been done in accordance with the “Work Instructions” of Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012; and the spindle has been confirmed not to be severed, no further actions are required by this paragraph for that carriage spindle.

(1)Remove the carriage spindle and install a new or serviceable carriage spindle, in accordance with the “Work Instructions” of any service bulletin specified in paragraph (i)(1)(i), (i)(1)(ii), (i)(1)(iii), or (i)(1)(iv) of this AD. As of the effective date of this AD, only Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012, may be used to perform the actions specified in this paragraph.

(i)Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003.

(ii)Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012.

(iii)Boeing Alert Service Bulletin 737-57A1218, Revision 5, dated February 9, 2009.

(iv)Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011.

(2)Do a detailed inspection of the spindle to determine if there is corrosion, cracking, or a severed spindle, and, before further flight, do all related investigative and corrective actions, in accordance with the “Work Instructions” of Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003; or Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012. If, during the detailed inspection described in paragraph 4.b. of Work Package 2 of Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003; or Boeing Alert Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012; a carriage spindle is found not to be severed, and no corrosion and no cracking is present, it can be reinstalled on the outboard mid-flap, in accordance with any service bulletin specified in paragraph (i)(2)(i), (i)(2)(ii), (i)(2)(iii), or (i)(2)(iv) of this AD. As of the effective date of this AD, only Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012, may be used to perform the actions specified in this paragraph.

(i)Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003.

(ii)Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012.

(iii)Boeing Alert Service Bulletin 737-57A1218, Revision 5, dated February 9, 2009.

(iv)Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011.

(j)Retained Work Package 1: NDT (Ultrasonic) and General Visual Inspections This paragraph restates the requirements of paragraph

(j)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010), with revised service information. Perform an NDT (ultrasonic) inspection and general visual inspection for each carriage spindle of the left and right outboard mid-flaps to detect cracks, corrosion, or severed carriage spindles, in accordance with “Work Package 1” of the “Work Instructions” of Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003; or Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012. As of the effective date of this AD, only Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012, may be used to perform the actions specified in this paragraph.

(k)Retained Work Package 1: Corrective Actions and New Optional Action This paragraph restates the requirements of paragraph

(k)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010), with revised service information and new optional action. If any corroded, cracked, or severed carriage spindle is found during any inspection required by paragraph

(j)of this AD: Before further flight, do the actions specified in paragraph (k)(1) or (k)(2) of this AD.

(1)Remove the carriage spindle and install a new or serviceable carriage spindle, in accordance with any service bulletin identified in paragraph (k)(1)(i), (k)(1)(ii), (k)(1)(iii), or (k)(1)(iv) of this AD. As of the effective date of this AD, only Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012, may be used to perform the actions specified in this paragraph.

(i)Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003.

(ii)Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012.

(iii)Boeing Alert Service Bulletin 737-57A1218, Revision 5, dated February 9, 2009.

(iv)Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011.

(2)Do a detailed inspection of the spindle to determine if there is corrosion, cracking, or a severed spindle, in accordance with the “Work Instructions” of Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003; or Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012. If any corrosion, cracking, or a severed spindle is found, before further flight, install a new or serviceable carriage spindle, in accordance with any service bulletin identified in paragraph (k)(1)(i), (k)(1)(ii), (k)(1)(iii), or (k)(1)(iv) of this AD. As of the effective date of this AD, only Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012, may be used to perform the actions specified in this paragraph.

(l)Retained Parts Installation Limitation This paragraph restates the requirements of paragraph

(l)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010). Except as provided by paragraph

(i)of this AD: As of December 4, 2003 (the effective date AD 2003-24-08, Amendment 39-13337 (68 FR 67027, December 1, 2003)), no person may install on any airplane a carriage spindle that has been removed as required by paragraph

(i)or

(k)of this AD, unless it has been overhauled in accordance with the “Work Instructions” of the applicable service bulletin identified in paragraph (l)(1), (l)(2), (l)(3), or (l)(4) of this AD. As of the effective date of this AD, only Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012; or Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011; may be used to perform the actions specified in this paragraph. To be eligible for installation under this paragraph, the carriage spindle must have been overhauled in accordance with the requirements of paragraph

(m)of this AD.

(1)Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003.

(2)Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012.

(3)Boeing Alert Service Bulletin 737-57A1218, Revision 5, dated February 9, 2009.

(4)Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011.

(m)Retained Electrodeposited Nickel Plating With New Plating Restrictions This paragraph restates the requirements of paragraph

(m)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010) with revised plating application procedures. As of the effective date of this AD, during accomplishment of any overhaul specified in paragraph

(l)or

(o)of this AD, follow the requirements specified in paragraphs (m)(1), (m)(2), and (m)(3) of this AD during application of the plating to the carriage spindle, in accordance with a method approved by the Manager, Seattle, Aircraft Certification Office (ACO), FAA. For a repair method to be approved, the repair must meet the certification basis of the airplane, and the approval must specifically refer to this AD.

(1)The maximum deposition rate of the nickel plating in any one plating/baking cycle must not exceed 0.002-inch-per-hour.

(2)Begin the hydrogen embrittlement relief bake within 10 hours after application of the nickel plating, or less than 24 hours after the current was first applied to the part, whichever is first.

(3)The carriage must not be plated using any high velocity oxygen fuel

(HVOF)thermal spray process. Note 1 to paragraph

(m)of this AD: Guidance on the application of nickel plating can be found in Chapter 20-42-09, Electrodeposited Nickel Plating, of the Boeing

(737)Standard Overhaul Practices Manual, Revision 25, dated July 1, 2009.

(n)Retained Exception to Reporting Recommendations This paragraph restates the provisions of paragraph

(n)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010), with revised service information. Although Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003; and Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012; recommend that operators report inspection findings to the manufacturer, this AD does not require reporting.

(o)Retained Inspections, Measurements, and Overhauls of the Carriage Spindle With Clarification of Overhaul Restrictions This paragraph restates the requirements of paragraph

(o)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010) with clarification of overhaul restrictions. At the applicable times specified in paragraphs (o)(1) and (o)(2) of this AD: Do the detailed inspection for corrosion, pitting, and cracking of the carriage spindle; magnetic particle inspection for cracking of the carriage spindle; measurements of the spindle to determine if it meets the allowable minimum diameter; overhauls of the carriage spindle; and applicable corrective actions; in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 737-57A1218, Revision 5, dated February 9, 2009; or Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011. As of the effective date of this AD, only Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011, may be used to perform the actions specified in this paragraph. The applicable corrective actions must be done before further flight. Repeat these actions thereafter at intervals not to exceed every 12,000 flight cycles on the carriage spindle or every 8 years since first installation of the carriage spindle on the airplane, whichever comes first. As of the effective date of this AD: For any overhaul required by this paragraph, the carriage spindle must be overhauled in accordance with the requirements of paragraph

(m)of this AD.

(1)For Model 737-100, -200, -200C series airplanes: At the later of the times specified in paragraphs (o)(1)(i) and (o)(1)(ii) of this AD.

(i)Before the accumulation of 12,000 total flight cycles on the carriage spindle since new or overhauled, or within 8 years after the installation of the new or overhauled part, whichever comes first.

(ii)Within 1 year after August 31, 2010 (the effective date of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010)).

(2)For Model -300, -400, and -500 series airplanes: At the later of the times specified in paragraphs (o)(2)(i) and (o)(2)(ii) of this AD.

(ii)Within 2 years after August 31, 2010 (the effective date of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010)).

(p)Retained Carriage Spindle Replacement for Model 737-100, -200, and -200C Series Airplanes This paragraph restates the requirements of paragraph

(p)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010), with revised service information and a shortened compliance time. For Model 737-100, -200, -200C series airplanes: Replace the carriage spindle with a new or documented (for which the service life, in total flight cycles, is known) carriage spindle, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 737-57A1218, Revision 5, dated February 9, 2009; or Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011; at the earlier of the times specified in paragraphs (p)(1) and (p)(2) of this AD, except as required by paragraph

(r)of this AD. As of the effective date of this AD, only Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011, may be used to perform the replacement. Overhauling the carriage spindles does not zero-out the flight cycles. Total flight cycles accumulate since new.

(1)At the later of the times specified in paragraphs (p)(1)(i) and (p)(1)(ii) of this AD.

(i)Before the accumulation of 48,000 total flight cycles on the new or overhauled carriage.

(ii)Within 3 years or 7,500 flight cycles after August 31, 2010 (the effective date of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010)), whichever occurs first.

(2)Before the accumulation of 40,000 total flight cycles on the new or overhauled carriage or 6 months after the effective date of this AD, whichever occurs later.

(q)Retained Carriage Spindle Replacement for Model 737-300, -400, and -500 Series Airplanes This paragraph restates the requirements of paragraph

(q)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010), with revised service information and a shortened compliance time. For Model 737-300, -400, and -500 series airplanes: Replace the carriage spindle with a new or documented (for which the service life, in flight cycles, is known) carriage spindle, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 737-57A1218, Revision 5, dated February 9, 2009; or Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011; at the later of the times specified in paragraphs (q)(1) and (q)(2) of this AD, except as required by paragraph

(r)of this AD. As of the effective date of this AD, only Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011, may be used to perform the replacement required by this paragraph. Overhauling the carriage spindles does not zero-out the flight cycles. Total flight cycles accumulate since new.

(1)Before the accumulation of 40,000 total flight cycles on the new or overhauled carriage.

(2)Within 6 years or 15,000 flight cycles after August 31, 2010 (the effective date of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010)), whichever occurs first.

(r)Retained Carriage Spindle Replacement for Airplanes With an Undocumented Carriage This paragraph restates the requirements of paragraph

(r)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010). For airplanes with an undocumented carriage: Do the applicable actions specified in paragraph

(p)or

(q)of this AD at the applicable time specified in paragraph (r)(1) or (r)(2) of this AD.

(1)For Model 737-100, -200, -200C series airplanes: Do the actions specified in paragraph

(p)of this AD at the time specified in paragraph (p)(1)(ii) of this AD.

(2)For Model -300, -400, and -500 series airplanes: Do the actions specified in paragraph

(q)of this AD at the time specified in paragraph (q)(2) of this AD.

(s)Retained Repetitive Replacements of Carriage Spindle This paragraph restates the requirements of paragraph

(s)of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010), with revised compliance times.

(1)For airplanes on which the actions required by paragraph

(p)or

(q)of this AD, as applicable, have been done as of the effective date of this AD: Repeat the replacement of the carriage spindle specified by paragraph

(p)or

(q)of this AD, as applicable, one time at the later of the times specified in paragraphs (s)(1)(i) and (s)(1)(ii) of this AD, and thereafter at intervals not to exceed 40,000 total flight cycles on the new or overhauled carriage spindle.

(i)Before the accumulation of 40,000 total flight cycles on the new or overhauled carriage.

(ii)Within 6 years or 15,000 flight cycles after August 31, 2010 (the effective date of AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010)), whichever occurs first.

(2)For airplanes on which the actions required by paragraph

(p)or

(q)of this AD, as applicable, have not been done as of the effective date of this AD: Repeat the replacement of the carriage spindle specified by paragraph

(p)or

(q)of this AD, as applicable, thereafter at intervals not to exceed 40,000 total flight cycles on the new or overhauled carriage spindle.

(t)Exception to Compliance Time Where Boeing Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012, and Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011, specify a compliance time after the dates of those service bulletins, this AD requires compliance within the specified compliance time after the effective date of this AD.

(u)Credit for Previous Actions This paragraph provides credit for actions required by paragraphs

(g)through

(s)of this AD, if those actions were performed before the effective date of this AD using Boeing Alert Service Bulletin 737-57A1277, Revision 2, dated June 9, 2011, which is not incorporated by reference in this AD.

(v)Alternative Methods of Compliance (AMOCs)

(1)The Manager, Seattle Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the ACO, send it to the attention of the person identified in paragraph

(w)of this AD. Information may be emailed to: *9-ANM-Seattle-ACO-AMOC-Requests@faa.gov* .

(2)Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office.

(3)An AMOC that provides an acceptable level of safety may be used for any repair required by this AD if it is approved by the Boeing Commercial Airplanes Organization Designation Authorization

(ODA)that has been authorized by the Manager, ACO, to make those findings. For a repair method to be approved, the repair must meet the certification basis of the airplane, and the approval must specifically refer to this AD.

(4)AMOCs previously approved in accordance with AD 2003-24-08, Amendment 39-13377 (68 FR 67027, December 1, 2003), or AD 2010-15-08, Amendment 39-16374 (75 FR 43803, July 27, 2010), are approved as AMOCs for individual repairs are acceptable for compliance with the corresponding provisions of this AD. All other existing AMOCs are not acceptable.

(w)Related Information

(1)For more information about this AD, contact Nancy Marsh, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone:

(425)917-6440; fax:

(425)917-6590; email: *nancy.marsh@faa.gov* .

(2)Service information identified in this AD that is not incorporated by reference may be obtained at the addresses specified in paragraphs (x)(5) and (x)(6) of this AD.

(x)Material Incorporated by Reference

(1)The Director of the Federal Register approved the incorporation by reference

(IBR)of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.

(2)You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.

(3)The following service information was approved for IBR on April 22, 2014.

(i)Boeing Alert Service Bulletin 737-57A1218, Revision 6, dated June 9, 2011.

(ii)Boeing Alert Service Bulletin 737-57A1277, Revision 3, dated May 16, 2012.

(4)The following service information was approved for IBR on August 31, 2010 (75 FR 43803, July 27, 2010).

(i)Boeing Alert Service Bulletin 737-57A1218, Revision 5, dated February 9, 2009.

(ii)Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003.

(5)For Boeing service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P. O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206-544-5000, extension 1; fax 206-766-5680; Internet *https://www.myboeingfleet.com* .

(6)You may view this service information at FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221.

(7)You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: *http://www.archives.gov/federal-register/cfr/ibr-locations.html* . Issued in Renton, Washington, on February 18, 2014. Ross Landes, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2014-04819 Filed 3-17-14; 8:45 am]

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