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economic development and community development plans are encouraged to review and consider 7 CFR part 1980, subpart K, which contains provisions for providing priority to projects that support the implementation of strategic economic development and communitydevelopment plans on a Multijurisdictional basis.
**Chapter XVIII—Rural Housing Service, Rural Business-Cooperative Service, Rural**  **Utilities Service, and Farm Service Agency, Department of Agriculture** 

**PART 1942—ASSOCIATIONS**

■ 5. The authority citation for part 1942 continues to read as follows:

Authority: 5 U.S.C. 301; 7 U.S.C. 1989.

**Subpart A—Community Facility Loan**

■ 6. Add § 1942.10 to read as follows:

**§ 1942.10 Strategic economic and community development.** 

Applicants with projects that support the implementation of strategic economic development and community development plans are encouraged to review and consider 7 CFR part 1980, subpart K, which contains provisions for providing priority to projects that support the implementation of strategic economic development and communitydevelopment plans on a Multijurisdictional basis.

**Subpart C—Fire and Rescue and Other Small Community Facilities Projects** 

■ 7. Add § 1942.110 to read as follows:

**§ 1942.110 Strategic economic and community development.** 

Applicants with projects that support the implementation of strategic economic development and community development plans are encouraged to review and consider 7 CFR part 1980, subpart K, which contains provisions for providing priority to projects that support the implementation of strategic economic development and communitydevelopment plans on a Multijurisdictional basis.

**Chapter XXXV—Rural Housing Service, Department of Agriculture** 

**PART 3570—COMMUNITY PROGRAMS**

■ 8. The authority citation for part 3570 continues to read as follows:

Authority: 5 U.S.C. 301; 7 U.S.C. 1989.

■ 9. Add § 3570.71 to read as follows:

**§ 3570.71 Strategic economic and community development.** 

Applicants with projects that support the implementation of strategic economic development and community development plans are encouraged to review and consider 7 CFR part 1980, subpart K, which contains provisions for providing priority to projects that support the implementation of strategic economic development and communitydevelopment plans on a Multijurisdictional basis.

**PART 3575—GENERAL**

■ 10. The authority citation for part 3575 continues to read as follows:

Authority: 5 U.S.C. 301, 7 U.S.C. 1989.

**Subpart A—Community Programs Guaranteed Loans** 

■ 11. Add § 3575.51 to read as follows:

**§ 3575.51 Strategic economic and community development.** 

Applicants with projects that support the implementation of strategic economic development and community development plans are encouraged to review and consider 7 CFR part 1980, subpart K, which contains provisions for providing priority to projects that support the implementation of strategic economic development and communitydevelopment plans on a Multijurisdictional basis.

**Chapter XLII—Rural Business-Cooperative Service and Rural Utilities Service,**  **Department of Agriculture**

**PART 4279—GUARANTEED LOANMAKING** 

■ 12. The authority citation for part 4279 continues to read as follows:

Authority: 5 U.S.C. 301; and 7 U.S.C. 1989.

**Subpart B—Business and Industry Loans** 

■ 13. Add § 4279.162 to read as follows:

**§ 4279.162 Strategic economic and community development.** 

Applicants with projects that support the implementation of strategic economic development and community development plans are encouraged to review and consider 7 CFR part 1980, subpart K, which contains provisions for providing priority to projects that support the implementation of strategic economic development and communitydevelopment plans on a Multijurisdictional basis.

**PART 4280—LOANS AND GRANTS**

■ 14. The authority citation for part 4280 continues to read as follows:

Authority: 5 U.S.C. 301; 7 U.S.C. 904c and 7 U.S.C. 1932(c). **Subpart E—Rural Business Development Grants** 

■ 15. Add § 4280.428 to read as follows:

**§ 4280.428 Strategic economic and community development.** 

Applicants with projects that support the implementation of strategic economic development and community development plans are encouraged to review and consider 7 CFR part 1980, subpart K, which contains provisions for providing priority to projects that support the implementation of strategic economic development and communitydevelopment plans on a Multijurisdictional basis.

Dated: February 19, 2016. Lisa Mensah, Under Secretary, Rural Development.

Dated: February 19, 2016. Michael Scuse, Under Secretary, Farm and Foreign Agricultural Services.
[FR Doc. 2016–04309 Filed 2–29–16; 8:45 am]

**BILLING CODE 3410–XY–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2015–3144; Directorate Identifier 2014–NM–110–AD; Amendment**  **39–18403; AD 2016–04–09]**

**RIN 2120–AA64**

**Airworthiness Directives; Dassault Aviation Airplanes** 

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

**ACTION :**  Final rule.

**SUMMARY :**  We are adopting a new airworthiness directive (AD) for certain Dassault Aviation Model FALCON 900EX and FALCON 2000EX airplanes. This AD was prompted by a report of significant fuel leakage at the middle position of the left outboard slat. This AD would require modifying the assembly of the slat extension mechanical stop. We are issuing this AD to prevent failure of the assembly of the slat extension mechanical stop, which if not corrected, could lead to a significant fuel leak and result in an uncontained fire.

**DATES :**  This AD becomes effective April 5, 2016.

The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of April 5, 2016.


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**ADDRESSES :**  You may examine the AD docket on the Internet at http:// www.regulations.gov/ #!docketDetail;D=FAA-2015-3144; or in person at the 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.

For service information identified in this final rule, contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201–440–6700; Internet http://www.dassaultfalcon.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–2015–
3144.

**FOR FURTHER INFORMATION CONTACT :**  Tom Rodriguez, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1137; fax 425–227–1149.

**SUPPLEMENTARY INFORMATION :** 

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Dassault Aviation Model FALCON 900EX and FALCON 2000EX airplanes. The NPRM published in the Federal Register on August 21, 2015 (80 FR 50810). The NPRM was prompted by a report of significant fuel leakage at the middle position of the left outboard slat. The NPRM proposed to require modifying the assembly of the slat extension mechanical stop. We are issuing this AD to prevent failure of the assembly of the slat extension mechanical stop, which if not corrected, could lead to a significant fuel leak and result in an uncontained fire.

The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2014–0115, dated May 13, 2014 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for certain Dassault Aviation Model FALCON 900EX and FALCON 2000EX airplanes. The MCAI
states:

After landing, an airplane experienced a significant fuel leakage at the middle position of the left outboard slat. Investigations showed that the fuel spillage originated in a structural cap, which had been punctured by a broken locking pin of the slat extension mechanical stop.

A design review revealed that the locking pin could become loose due to an incorrectinstallation combined with a non-faulttolerant design.

This condition, if not corrected, may lead to a significant fuel leak, possibly resulting in an uncontained fire.

To address this potential unsafe condition, Dassault Aviation developed a modification of the slat extension mechanical stop assembly (Mod M3678 for [Model] F2000EX aeroplanes and Mod M5870 for [Model] F900EX aeroplanes) with the purpose to increase its robustness with regards to possible mishandling on production or during maintenance. Dassault Aviation also published Service Bulletin (SB) F2000EX– 344 and SB F900EX–450, for embodiment in service of that modification.

For the reasons described above, this [EASA AD] requires modification of the slat extension mechanical stop assembly.

You may examine the MCAI in the AD docket on the Internet at http:// www.regulations.gov/ #!documentDetail;D=FAA-2015-3144-
0002.

Comments

We gave the public the opportunity to participate in developing this AD. The following presents the comment received on the NPRM (80 FR 50810, August 21, 2015) and the FAA’s response to that comment. Request To Refer to the Latest Service Information

Dassault Aviation requested that we refer to the latest service information: Erratum Service Bulletin F900EX–450, dated July 16, 2014; and Erratum Service Bulletin F2000EX–344, dated July 16, 2014. Dassault Aviation stated that it issued changes to Dassault Service Bulletin F900EX–450, dated March 10, 2014; and Dassault Service Bulletin F2000EX–344, dated March 10, 2014 (which we referred to as the appropriate sources of service information for accomplishing the actions specified in the proposed AD (80 FR 50810, August 21, 2015)).

We agree with the commenter. Dassault Erratum Service Bulletin F900EX–450, dated July 16, 2014; and Erratum Service Bulletin F2000EX–344, dated July 16, 2014; include among other minor changes, additional illustrations. We have revised paragraph (g) of this AD to refer to Dassault Erratum Service Bulletin F900EX–450, dated July 16, 2014; and Dassault Erratum Service Bulletin F2000EX–344, dated July 16, 2014. We have also added a new paragraph (h) to this AD to provide credit for the actions specified in paragraph (g) of this AD, if those actions are done before the effective date of this AD using Dassault Service Bulletin F900EX–450, dated March 10, 2014; or Dassault Service Bulletin F2000EX–344, dated March 10, 2014; as applicable. We have redesignated the subsequent paragraphs accordingly.

Conclusion

We reviewed the relevant data 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 (80 FR 50810, August 21, 2015) for correcting the unsafe condition; and

• Do not add any additional burden upon the public than was already proposed in the NPRM (80 FR 50810, August 21, 2015).

Related Service Information Under 1 CFR Part 51

Dassault Aviation has issued Erratum Service Bulletin F900EX–450, dated July 16, 2014; and Erratum Service Bulletin F2000EX–344, dated July 16, 2014. This service information describes procedures for modifying the assembly of the slat extension mechanical stop. 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. Costs of Compliance

We estimate that this AD affects 67 airplanes of U.S. registry.

We also estimate that it will take about 8 work-hours per product to comply with the basic requirements of this AD. The average labor rate is $85 per work-hour. Required parts will cost about $3,510 per product. Based on these figures, we estimate the cost of this AD on U.S. operators to be $280,730, or $4,190 per product. 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


### 10459 Federal Register / Vol. 81, No. 40 / Tuesday, March 1, 2016 / Rules and Regulations

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 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 the 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. Examining the AD Docket

You may examine the AD docket on the Internet at http:// www.regulations.gov/ #!docketDetail;D=FAA-2015-3144 ; 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 Operations office (telephone 800–647–5527) is in the **ADDRESSES** section. 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):

2016–04–09 Dassault Aviation: Amendment 39–18403. Docket No. FAA–2015–3144; Directorate Identifier 2014–NM–110–AD.
(a) Effective Date

This AD becomes effective April 5, 2016.
(b) Affected ADs

None. (c) Applicability

This AD applies to Dassault Aviation airplanes specified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.

(1) Dassault Aviation Model FALCON 900EX airplanes, all serial numbers on which Dassault Aviation Modification M5281 has been embodied, except those on which Dassault Aviation Modification M5870 has been embodied in production.

(2) Dassault Aviation Model FALCON 2000EX airplanes, all serial numbers on which Dassault Aviation Modification M2846 has been embodied, except those on which Dassault Aviation Modification M3678 has been embodied in production.
(d) Subject

Air Transport Association (ATA) of America Code 57, Wings.
(e) Reason

This AD was prompted by a report of significant fuel leakage at the middle position of the left outboard slat. We are issuing this AD to prevent failure of the assembly of the slat extension mechanical stop, which if not corrected, could lead to a significant fuel leak and result in an uncontained fire.
(f) Compliance

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

Within 9 months or 440 flight hours, whichever occurs first after the effective date of this AD: Modify the assembly of the slat extension mechanical stop, in accordance with Accomplishment Instructions of Dassault Erratum Service Bulletin F900EX– 450, dated July 16, 2014; or Dassault Erratum Service Bulletin F2000EX–344, dated July 16, 2014; as applicable.
(h) Credit for Previous Actions

This paragraph provides credit for actions required by paragraph (g) of this AD, if those actions were performed before the effective date of this AD using the applicable service information identified in paragraphs (h)(1) and (h)(2) of this AD, which are not incorporated by reference in this AD.

(1) Dassault Service Bulletin F900EX–450, dated March 10, 2014; and

(2) Dassault Service Bulletin F2000EX–344, dated March 20, 2014.
(i) Other FAA AD Provisions

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 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 International Branch, send it to ATTN: Tom Rodriguez, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1137; fax 425–227–1149. Information may be emailed to: 9-ANM-116- AMOC-REQUESTS@faa.gov. 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. The AMOC approval letter must specifically reference this AD.

(2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Branch, ANM– 116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Dassault Aviation’s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.
(j) Related Information

(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2014–0115, dated May 13, 2014, for related information. This MCAI may be found in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA–
2015–3144.

(2) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (k)(3) and (k)(4) of this AD.
(k) 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 this AD specifies otherwise.

(i) Dassault Erratum Service Bulletin F900EX–450, dated July 16, 2014. (All pages of this revised service bulletin are marked ‘‘Initial issuance’’ and dated July 16, 2014.)

(ii) Dassault Erratum Service Bulletin F2000EX–344, dated July 16, 2014. (All pages of this revised service bulletin are marked ‘‘Initial issuance’’ and dated July 16, 2014.)

(3) For service information identified in this AD, contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201–440–6700; Internet http:// www.dassaultfalcon.com.

(4) You may view this service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For


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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 15, 2016. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2016–03694 Filed 2–29–16; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2014–0755; Directorate Identifier 2014–NM–080–AD; Amendment**  **39–18414; AD 2016–04–20]**

**RIN 2120–AA64**

**Airworthiness Directives; The Boeing Company Airplanes** 

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

**ACTION :**  Final rule.

**SUMMARY :**  We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 737–600, –700, –700C, –800, –900, and –900ER series airplanes, Model 757 airplanes, Model 767 airplanes, and Model 777 airplanes. This AD results from fuel system reviews conducted by the manufacturer. This AD requires an inspection to determine if certain motor-operated valve (MOV) actuators for the fuel valves are installed, and replacement of any affected actuators. Previous ADs addressed this Special Federal Aviation Regulation No. 88 (SFAR 88) issue for the majority of the airplanes delivered with these actuators. Since those ADs did not cover all of the airplanes, and for some airplanes delivered with improved actuators, there was no restriction on installation of replacement actuators with the unsafe condition, this additional rulemaking action is required. As with the related ADs, we are issuing this AD to prevent electrical energy from lightning, hot shorts, or fault current from entering the fuel tank through the fuel valve actuator shaft, which could result in fuel tank explosions and consequent loss of the airplane.

**DATES :**  This AD is effective April 5,
2016. **ADDRESSES :**  For service information identified in this final rule, 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. 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– 0755; 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 :**  Rebel Nichols, Aerospace Engineer, Propulsion Branch, ANM–140S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057–3356; phone: 425–917–6509; fax: 425–917–6590; email: rebel.nichols@ faa.gov.

**SUPPLEMENTARY INFORMATION :** 

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all The Boeing Company Model 737–600, –700, –700C, –800, –900, and –900ER series airplanes, Model 757 airplanes, Model 767 airplanes, and Model 777 airplanes. The NPRM published in the Federal Register on November 7, 2014 (79 FR 66343) (‘‘the NPRM’’). The NPRM results from fuel system reviews conducted by the manufacturer. The NPRM proposed to require an inspection to determine if certain actuators for the fuel valves are installed, and replacement of any affected actuators. Previous ADs addressed this SFAR 88 (66 FR 23086, May 7, 2001) issue for the majority of the airplanes delivered with these actuators. Since those ADs did not cover all of the airplanes, and for some airplanes delivered with improved actuators, there was no restriction on installation of replacement actuators with the unsafe condition, this additional rulemaking action is required. As with the related ADs, we are issuing this AD to prevent electrical energy from lightning, hot shorts, or fault current from entering the fuel tank through the fuel valve actuator shaft, which could result in fuel tank explosions and consequent loss of the airplane.

Comments

We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the NPRM and the FAA’s response to each comment. Requests To Revise the Proposed Applicability

Boeing, All Nippon Airways (ANA), American Airlines (AAL), Southwest Airlines (SWA), and United Airlines (UAL), requested that we delete Model 737–600, –700, 700C, –800, –900, and –900ER series airplanes from the applicability of the NPRM. The commenters stated that AD 2008–06–03, Amendment 39–15415 (73 FR 13081, March 12, 2008) (‘‘AD 2008–06–03’’), mandated replacement of all fuel system MOV actuators having Part Number (P/N) MA20A1001–1 (S343T003–39) on Model 737 airplanes, and that the compliance time for AD 2008–06–03 ended April 16, 2013. Boeing stated that first production delivery of the SFAR88 compliant actuator having P/N MA20A2027 (S343T003–56) occurred on line number 1877, and that the illustrated parts catalog (IPC) for that airplane and subsequent airplanes prohibited installation of MOV actuators having P/N MA20A1001–1 (S343T003– 39).

We partially agree with the commenters’ requests. We agree there is little risk that MOV actuators having P/ N MA20A1001–1 (S343T003–39) are currently installed on Model 737–600, –700, 700C, –800, –900, and –900ER series airplanes for the reasons provided by the commenter. However, we want to ensure that MOV actuators having P/N MA20A1001–1 (S343T003–39) are not installed on these airplanes in the future. Therefore, we have removed Model 737 airplanes from the actions required by paragraph (g) of this AD but not from the applicability of the AD. We have retained Model 737 airplanes in paragraph (i) of this AD, which states that no person may install an MOV actuator having P/N MA20A1001–1 (S343T003–39) on any airplane. Paragraph (i) of this AD ensures that installation of MOV actuators having P/