### 8823 Federal Register / Vol. 81, No. 35 / Tuesday, February 23, 2016 / Rules and Regulations

Promotion and Economics Division, Specialty Crops Program, AMS, USDA, 1400 Independence Avenue SW., Room 1406–S, Stop 0244, Washington, DC 20250–0244, telephone: (202) 720–9915; facsimile: (202) 205–2800; or contact Maureen Pello at (503) 632–8848 or via electronic mail: Maureen.Pello@ ams.usda.gov.

**FOR FURTHER INFORMATION CONTACT :**  Maureen Pello, Marketing Specialist, PED, SC, AMS, USDA, 1400 Independence Avenue SW., Room 1406–S, Stop 0244, Washington, DC 20250–0244; telephone: (202) 720–9915, (503) 632–8848 (direct line); facsimile: (202) 205–2800; or electronic mail: Maureen.Pello@ams.usda.gov.

**SUPPLEMENTARY INFORMATION :**  Pursuant to the Commodity Promotion, Research and Information Act of 1996 (7 U.S.C. 7411–7425) (Act), it is hereby directed that a referendum be conducted to ascertain whether continuance of the Order (7 CFR part 1217) is favored by eligible domestic manufacturers and importers of softwood lumber. The Order is authorized under the Act.

The representative period for establishing voter eligibility for the referendum shall be the period from January 1 through December 31, 2015. Persons who domestically manufactured and shipped or imported 15 million board feet or more of softwood lumber during the representative period, paid assessments during that period, and are currently softwood lumber manufacturers or importers subject to assessment under the Order are eligible to vote. Persons who received an exemption from assessments for the entire representative period are ineligible to vote. The referendum will be conducted by mail ballot from August 1 through 25, 2016.

Section 518 of the Act authorizes continuance referenda. Under § 1217.81(b) of the Order, the U.S. Department of Agriculture (USDA) must conduct a referendum 5 years after the program has been in effect to determine whether persons subject to assessment favor continuance of the Order. The program became effective in 2011. USDA would continue the Order if continuance is favored by a majority of the domestic manufacturers and importers voting in the referendum, who also represent a majority of the volume of softwood lumber represented in the referendum.

In accordance with the Paperwork Reduction Act of 1995 (44 U.S.C. chapter 35), the referendum ballot has been approved by the Office of Management and Budget (OMB) and assigned OMB No. 0581–0093. It has been estimated that there are approximately 170 domestic manufacturers and 70 importers who will be eligible to vote in the referendum. It will take an average of 15 minutes for each voter to read the voting instructions and complete the referendum ballot.

Referendum Order

Maureen Pello, Marketing Specialist, and Heather Pichelman, Director, PED, SC, AMS, USDA, Stop 0244, Room 1406–S, 1400 Independence Avenue SW., Washington, DC 20250–0244, are designated as the referendum agents to conduct this referendum. The referendum procedures at 7 CFR 1217.100 through 1217.108, which were issued pursuant to the Act, shall be used to conduct the referendum.

The referendum agent will mail the ballots to be cast in the referendum and voting instructions to all known, eligible domestic manufacturers and importers prior to the first day of the voting period. Persons who domestically manufactured and shipped or imported 15 million board feet or more of softwood lumber during the representative period, paid assessments during that period, and are currently softwood lumber domestic manufacturers or importers subject to assessment under the Order are eligible to vote. Persons who received an exemption from assessments during the entire representative period are ineligible to vote. Any eligible domestic manufacturer or importer who does not receive a ballot should contact the referendum agent no later than one week before the end of the voting period. Ballots must be received by the referendum agent by 4:30 p.m. Eastern time, August 25, 2016, in order to be counted.
List of Subjects in 7 CFR Part 1217

Administrative practice and procedure, Advertising, Consumer information, Marketing agreements, Promotion, Reporting and recordkeeping requirements, Softwood lumber.

Authority: 7 U.S.C. 7411–7425; 7 U.S.C.

7401.

Dated: February 18, 2016. Elanor Starmer, Acting Administrator, Agricultural Marketing Service.
[FR Doc. 2016–03805 Filed 2–22–16; 8:45 am]

**BILLING CODE 3410–02–P DEPARTMENT OF TRANSPORTATION** 

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2016–3699; Directorate Identifier 2015–NM–109–AD; Amendment**  **39–18402; AD 2016–04–08]**

**RIN 2120–AA64**

**Airworthiness Directives; The Boeing Company Airplanes** 

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final rule; request for
comments.

**SUMMARY :**  We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787–8 airplanes. This AD requires revising the maintenance or inspection program, as applicable, to include an airworthiness limitation for repetitive inspections of the web fastener holes in the overwing flex-tees. This AD was prompted by a report that certain web fastener holes inthe overwing flex-tees at the wing-tobody interface might not have been deburred properly when manufactured. Fastener holes without the deburr chamfer applied can develop fatigue cracking. We are issuing this AD to detect and correct cracking in the web fastener holes in the overwing flex-tees, which can weaken the primary wing structure so it cannot sustain limit load.

**DATES :**  This AD is effective March 9,
2016.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 9, 2016.

We must receive comments on this AD by April 8, 2016.

**ADDRESSES :**  You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:

• Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.

• Fax: 202–493–2251.

• Mail: U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590.

• 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.

For service information identified in this final rule, contact Boeing


### 8824 Federal Register / Vol. 81, No. 35 / Tuesday, February 23, 2016 / Rules and Regulations

Commercial Airplanes, Attention: Data & Services Management, P. O. Box 3707, MC 2H–65, Seattle, WA 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. It is also available on the Internet at http:// www.regulations.gov by searching for and locating Docket No. FAA–2016–
3699. 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–2016– 3699; 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 street address for the Docket Office (phone: 800–647– 5527) is in the **ADDRESSES** section. Comments will be available in the AD docket shortly after receipt.

**FOR FURTHER INFORMATION CONTACT :**  Melanie Violette, Senior Aerospace Engineer, Airframe Branch, ANM–120S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057–3356; phone: 425– 917–6422; fax: 425–917–6590; email: Melanie.Violette@faa.gov.

Discussion

We received a report that certain web fastener holes in the overwing flex-tees at the wing-to-body interface might not have been deburred properly when manufactured. A deburr chamfer should have been applied to the fastener holes in the overwing flex-tees. Fastener holes without the deburr chamfer applied can develop fatigue cracking before the required supplemental structural fatigue inspections are scheduled to begin. Such fatigue cracking, if not corrected, could result in the primary wing structure being weakened so it cannot sustain limit load. We are issuing this AD to correct the unsafe condition on these products.

Related Service Information Under 1 CFR Part 51

We reviewed Boeing 787 Airworthiness Limitations—Line Number Specific, D011Z009–03–02, dated February 2015. The service information contains airworthiness limitation tasks pertaining to inspections for web fastener holes in the overwing flex-tees at the wing-to-body interface.

This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the **ADDRESSES** section.

FAA’s Determination

We are issuing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the same type design.
AD Requirements

This AD requires revising the maintenance or inspection program, as applicable, to include an airworthiness limitation for repetitive inspection of the web fastener holes in the overwing flex-tees.

This AD requires revisions to certain operator maintenance documents to include new actions ( e.g., inspections). Compliance with these actions is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by this AD, the operator may not be able to accomplish the actions described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance according to paragraph (h) of this AD. The request should include a description of changes to the required actions that will ensure the continued operational safety of the airplane.
FAA’s Justification and Determination of the Effective Date

There are no products of this type currently registered in the United States. However, this rule is necessary to ensure that the described unsafe condition is addressed if any of these products are placed on the U.S. Register in the future. Therefore, we find that notice and opportunity for prior public comment are unnecessary and that good cause exists for making this amendment effective in less than 30 days.

Comments Invited

This AD is a final rule that involves requirements affecting flight safety and was not preceded by notice and an opportunity for public comment. However, we invite you to send any written data, views, or arguments about this AD. Send your comments to an address listed under the **ADDRESSES** section. Include the docket number FAA–2016–3699 and Directorate Identifier 2015–NM–109–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 http:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD. Costs of Compliance

We estimate that this AD affects 0 airplanes of U.S. registry.

We estimate the following costs to comply with this AD:



### E STIMATED 

### COSTS

Action Labor cost Parts cost Cost per product Cost on U.S. operators

Maintenance/inspection program revision ...... 1 work-hour × $85 per hour = $85 ................. $0 $85 $0

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


### 8825 Federal Register / Vol. 81, No. 35 / Tuesday, February 23, 2016 / Rules and Regulations

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

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 adding the following new airworthiness directive (AD): 2016–04–08 The Boeing Company: Amendment 39–18402; Docket No. FAA–2016–3699; Directorate Identifier 2015–NM–109–AD.
(a) Effective Date

This AD is effective March 9, 2016.
(b) Affected ADs

None. (c) Applicability

The Boeing Company Model 787–8 airplanes, certificated in any category, having line numbers 78 and 82.
(d) Subject

Air Transport Association (ATA) of America Code 57, Wings. (e) Unsafe Condition This AD was prompted by a report that certain web fastener holes in the overwing flex-tees at the wing-to-body interface might not have been deburred properly when manufactured. We are issuing this AD to detect and correct cracking in the web fastener holes in the overwing flex-tees, which can weaken the primary wing structure so it cannot sustain limit load.
(f) Compliance

Comply with this AD within the compliance times specified, unless already done.
(g) Revision to Maintenance or Inspection Program

Within 30 days after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the applicable inspection requirement identified in paragraphs (g)(1) and (g)(2) of this AD, as specified in Boeing 787 Airworthiness Limitations—Line Number Specific, D011Z009–03–02, dated February 2015. The initial compliance time for the tasks is at the applicable time specified in Boeing 787 Airworthiness Limitations—Line Number Specific, D011Z009–03–02, dated February
2015.

(1) For the airplane having line number 78: Principal Structural Element 57–10–06a

_ MRB9, ‘‘Overwing Flex-Tee—Web Fastener Holes.’’

(2) For the airplane having line number 82: Principal Structural Element 57–10–06a

_ MRB10, ‘‘Overwing Flex-Tee—Web Fastener Holes.’’
(h) Alternative Methods of Compliance (AMOCs)

(1) The Manager, Settle 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 (i) of this AD. Information may be emailed to: 9-ANM-Seattle-ACO-AMOCRequests@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, modification, or alteration required by this AD if it is approved by the Boeing Commercial Airplanes Organization Designation Authorization (ODA) that has been authorized by the Manager, Seattle ACO, to make those findings. To be approved, the repair method, modification deviation, or alteration deviation must meet the certification basis of the airplane, and the approval must specifically refer to this AD.

(i) Related Information

For more information about this AD, contact Melanie Violette, Senior Aerospace Engineer, Airframe Branch, ANM–120S, FAA, Seattle ACO, 1601 Lind Avenue SW., Renton, WA 98057–3356; phone: 425–917– 6422; fax: 425–917–6590; email: Melanie.Violette@faa.gov.
(j) 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.

(i) Boeing 787 Airworthiness Limitations— Line Number Specific, D011Z009–03–02, dated February 2015.

(ii) Reserved. (3) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H–65, Seattle, WA 98124–2207; telephone 206– 544–5000, extension 1; fax 206–766–5680; Internet https://www.myboeingfleet.com.

(4) You may view this service information at 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.

(5) 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/ibrlocations.html.

Issued in Renton, Washington, on February 10, 2016. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2016–03562 Filed 2–22–16; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF COMMERCE**

**Bureau of Industry and Security**

**15 CFR Part 744**

**[Docket No. 151209999–5999–01]**

**RIN 0694—AG81**

**Addition of Certain Persons and Modification of Certain Entries to the**  **Entity List; and Removal of Certain Persons From the Entity List** 

**AGENCY :**  Bureau of Industry and Security, Commerce.

**ACTION :**  Final rule.

**SUMMARY :**  This rule amends the Export Administration Regulations (EAR) by adding eight persons under eight entries to the Entity List. The eight persons who are added to the Entity List have been determined by the U.S. Government to be acting contrary to the national