64312 Federal Register / Vol. 80, No. 205 / Friday, October 23, 2015 / Rules and Regulations 

researchers, evaluators (including the 

independent evaluator for the program), 

practitioners, and other interested 

parties, including a plan for 

dissemination of results to stakeholders. 

(c) Other, non-eligibility 

considerations. Applicants are 

encouraged: 

(1) To propose projects that will 

provide employees with important job 

skills; and 

(2) To have experience the following 

areas: 

(i) Community food work, particularly 

concerning small and medium-size 

farms, including the provision of food to 

people in low-income communities and 

the development of new markets in lowincome communities for agricultural 

producers; and 

(ii) Job training and business 

development activities for food-related 

activities in low-income communities. 

(d) Partnerships. Applicants for a 

grant under this subpart are encouraged 

to seek and create partnerships with 

public or private, nonprofit or for-profit 

entities, including links with academic 

institutions (including minority-serving 

colleges and universities) or other 

appropriate professionals; communitybased organizations; local government 

entities; PromiseZone lead applicant/

organization or implementation 

partners; and StrikeForce area 

coordinators or partnering entities for 

the purposes of providing additional 

Federal resources and strengthening 

under-resourced communities. Only the 

applicant must meet the requirements 

specified in this section for grant 

eligibility. Project partners and 

collaborators need not meet the 

eligibility requirements. 

§ 3430.1104 Project types and priorities. 

(a) FINI Pilot Projects (FPP). FPPs are 

aimed at new entrants seeking funding 

for a project in the early stages of 

incentive program development. 

(b) FINI Projects (FP). FPs are aimed 

at mid-sized groups developing 

incentive programs at the local or State 

level. 

(c) FINI Large Scale Projects (FLSP). 

FLSPs are aimed at groups developing 

multi-county, State, and regional 

incentive programs with the largest 

target audience of all FINI projects. 

§ 3430.1105 Funding restrictions. 

(a) Construction. Funds made 

available for grants under this subpart 

shall not be used for the construction of 

a new building or facility or the 

acquisition, expansion, remodeling, or 

alteration of an existing building or 

facility (including site grading and 

improvement, and architect fees). 

(b) Indirect costs. Subject to § 3430.54, 

indirect costs are allowable. 

§ 3430.1106 Matching requirements. 

(a) In general. Recipients of a grant 

under this subpart must provide 

matching contributions on a dollar-fordollar basis for all Federal funds 

awarded. 

(b) Source and type. The non-Federal 

share of the cost of a project funded by 

a grant under this subpart may be 

provided by a State or local government 

or a private source. The matching 

requirement in this section may be met 

through cash or in-kind contributions, 

including third-party in-kind 

contributions fairly evaluated, including 

facilities, equipment, or services. 

(c) Limitation. If an applicant partners 

with a for-profit entity, the non-Federal 

share that is required to be provided by 

the applicant may not include the 

services of an employee of that for-profit 

entity, including salaries paid or 

expenses covered by that employer. 

(d) Indirect costs. Use of indirect costs 

as in-kind matching contributions is 

subject to § 3430.52(b). 

§ 3430.1107 Program requirements. 

The term of a grant under this subpart 

may not exceed 5 years. No-cost 

extensions of time beyond the 

maximum award terms will not be 

considered or granted. 

§ 3430.1108 Priorities. 

(a) In general. Except as provided in 

paragraph (b) of this section, in 

awarding grants under this subpart, 

NIFA will give priority to projects that: 

(1) Maximize the share of funds used 

for direct incentives to participants; 

(2) Use direct-to-consumer sales 

marketing; 

(3) Demonstrate a track record of 

designing and implementing successful 

nutrition incentive programs that 

connect low-income consumers and 

agricultural producers; 

(4) Provide locally or regionally 

produced fruits and vegetables; 

(5) Are located in underserved 

communities; or 

(6) Address other criteria as 

established by NIFA and included in the 

requests for applications. 

(b) Exception. The priorities in 

paragraph (a) of this section that are 

given by NIFA will depend on the 

project type identified in § 3430.1104. 

Applicants should refer to the requests 

for applications to determine which 

priorities will be given to which project 

types. 

Done at Washington, DC, this 16th day of 

October, 2015. 

Robert E. Holland, 

Associate Director for Operations, National 

Institute of Food and Agriculture. 

[FR Doc. 2015–26848 Filed 10–22–15; 8:45 am] 

BILLING CODE 3410–22–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–0913; Directorate 

Identifier 2012–NE–23–AD; Amendment 39– 

18261; AD 2015–18–03] 

RIN 2120–AA64 

Airworthiness Directives; Honeywell 

International Inc. Turboprop Engines 

(Type Certificate Previously Held by 

AlliedSignal Inc., Garrett Engine 

Division; Garrett Turbine Engine 

Company; and AiResearch 

Manufacturing Company of Arizona) 

Correction 

In rule document 2015–25606, 

appearing on pages 61091 through 

61093 in the issue of Friday, October 9, 

2015, make the following correction: 

On page 61093, at the top of the page, 

the image heading ‘‘Figure 2 to 

Paragraph (e)—Airplane Operating 

Procedures’’ should read ‘‘Figure 1 to 

Paragraph (e)—Airplane Operating 

Procedures’’. 

[FR Doc. C1–2015–25606 Filed 10–22–15; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0869; Directorate 

Identifier 2015–NE–11–AD; Amendment 39– 

18296; AD 2015–21–04] 

RIN 2120–AA64 

Airworthiness Directives; Pratt & 

Whitney Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Pratt & Whitney (PW) PW4164, PW4168, 

PW4168A, PW4164–1D, PW4168–1D, 

PW4168A–1D, and PW4170 turbofan 

engines. This AD was prompted by 

crack finds in the 6th stage low-pressure 

turbine (LPT) disk. This AD requires 

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Federal Register / Vol. 80, No. 205 / Friday, October 23, 2015 / Rules and Regulations 64313 

removal of the affected 6th stage LPT 

disks. We are issuing this AD to prevent 

failure of the 6th stage LPT disk, which 

could lead to an uncontained disk 

release, damage to the engine, and 

damage to the airplane. 

DATES: This AD is effective November 

27, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of November 27, 2015. 

ADDRESSES: For service information 

identified in this AD, contact Pratt & 

Whitney, 400 Main St., East Hartford, 

CT 06108; phone: 860–565–8770; fax: 

860–565–4503. You may view this 

service information at the FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA. For 

information on the availability of this 

material at the FAA, call 781–238–7125. 

It is also available on the Internet at 

http://www.regulations.gov by searching 

for and locating Docket No. FAA–2015– 

0869. 

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–2015– 

0869; or in person at the Docket 

Management Facility between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. The AD docket 

contains this AD, the regulatory 

evaluation, any comments received, and 

other information. The address for the 

Docket Office (phone: 800–647–5527) is 

Document Management Facility, U.S. 

Department of Transportation, Docket 

Operations, M–30, West Building 

Ground Floor, Room W12–140, 1200 

New Jersey Avenue SE., Washington, 

DC 20590. 

FOR FURTHER INFORMATION CONTACT: 

Besian Luga, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7750; fax: 781–238– 

7199; email: besian.luga@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 PW PW4164, PW4168, 

PW4168A, PW4164–1D, PW4168–1D, 

PW4168A–1D, and PW4170 turbofan 

engines. The NPRM published in the 

Federal Register on June 8, 2015 (80 FR 

32316). The NPRM was prompted by 

findings of cracks in the 6th stage LPT 

disk. The NPRM proposed to require 

removal of the affected 6th stage LPT 

disks. We are issuing this AD to correct 

the unsafe condition on these products. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. The 

following presents the comment 

received on the NPRM (80 FR 32316, 

June 8, 2015) and the FAA’s response to 

this comment. 

Request to Clarify Definition of LPT 

Shop Visit 

An individual commenter requested 

that we define ‘‘LPT shop visit’’ more 

precisely to prevent unnecessary 

discussions regarding its meaning. 

We agree. We revised the definition to 

read: ‘‘For the purpose of this AD, an 

‘‘LPT shop visit’’ is defined as the 

removal of the 6th stage disk from the 

LPT rotor and the removal of the blades 

from the disk.’’ 

Conclusion 

We reviewed the relevant data, 

considered the comment received, and 

determined that air safety and the 

public interest require adopting this AD 

with the change described previously. 

Related Service Information Under 1 

CFR Part 51 

We reviewed PW Service Bulletin 

(SB) No. PW4G–100–72–252, dated 

November 18, 2014. The SB provides a 

list of PW 6th stage LPT disks affected 

by this AD. This service information is 

reasonably available because the 

interested parties have access to it 

through their normal course of business 

or see ADDRESSES for other ways to 

access this service information. 

Costs of Compliance 

We estimate that this AD affects 18 

engines installed on airplanes of U.S. 

registry. We also estimate that no 

additional hours will be required per 

engine to comply with this AD because 

the engine is already disassembled in 

the shop when we require the part to be 

removed. The average labor rate is $85 

per hour. We estimate that 6 engines 

will require replacement parts during an 

LPT shop visit, and that the prorated 

replacement parts cost will be $108,800 

per engine. Based on these figures, we 

estimate the cost of this AD on U.S. 

operators to be $652,800. 

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 

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 to the extent that it justifies 

making a regulatory distinction, 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): 

2015–21–04 Pratt & Whitney: Amendment 

39–18296; Docket No. FAA–2015–0869; 

Directorate Identifier 2015–NE–11–AD. 

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64314 Federal Register / Vol. 80, No. 205 / Friday, October 23, 2015 / Rules and Regulations 

(a) Effective Date 

This AD is effective November 27, 2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all Pratt & Whitney 

(PW) PW4164, PW4168, PW4168A, PW4164– 

1D, PW4168–1D, PW4168A–1D, and PW4170 

turbofan engines with 6th stage low-pressure 

turbine (LPT) disks, part number 50N886, 

installed. 

(d) Unsafe Condition 

This AD was prompted by crack finds in 

the 6th stage LPT disk. We are issuing this 

AD to prevent failure of the 6th stage LPT 

disk, which could lead to an uncontained 

disk release, damage to the engine, and 

damage to the airplane. 

(e) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. At the next LPT shop visit after the 

effective date of this AD, remove from service 

6th stage LPT disks with serial numbers 

listed in the Accomplishment Instructions, 

Table 1, of PW Service Bulletin No. PW4G– 

100–72–252, dated November 18, 2014. 

(f) Definition 

For the purpose of this AD, an ‘‘LPT shop 

visit’’ is defined as the removal of the 6th 

stage disk from the LPT rotor and the 

removal of the blades from the disk. 

(g) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

FAA, may approve AMOCs for this AD. Use 

the procedures found in 14 CFR 39.19 to 

make your request. You may email your 

request to: ANE-AD-AMOC@faa.gov. 

(h) Related Information 

For more information about this AD, 

contact Besian Luga, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7750; fax: 781–238–7199; 

email: besian.luga@faa.gov. 

(i) 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 November 27, 2015. 

(i) Pratt & Whitney (PW) Service Bulletin 

No. PW4G–100–72–252, dated November 18, 

2014. 

(ii) Reserved. 

(4) For PW service information identified 

in this AD, contact Pratt & Whitney, 400 

Main St., East Hartford, CT 06108; phone: 

860–565–8770; fax: 860–565–4503. 

(5) You may view this service information 

at FAA, Engine & Propeller Directorate, 12 

New England Executive Park, Burlington, 

MA. For information on the availability of 

this material at the FAA, call 781–238–7125. 

(6) You may view this service information 

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 Burlington, Massachusetts, on 

October 9, 2015. 

Robert G. Mann, 

Acting Directorate Manager, Engine & 

Propeller Directorate, Aircraft Certification 

Service. 

[FR Doc. 2015–26346 Filed 10–22–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–1383; Directorate 

Identifier 2015–NE–15–AD; Amendment 39– 

18293; AD 2015–21–01] 

RIN 2120–AA64 

Airworthiness Directives; Technify 

Motors GmbH Reciprocating Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all 

Technify Motors GmbH TAE 125–02 

reciprocating engines with a dual mass 

flywheel installed. This AD requires 

installation of a start phase monitoring 

system and associated specified 

software. This AD was prompted by 

reports of a gearbox drive shaft breaking 

during starting or restarting of the 

engine. We are issuing this AD to 

prevent overload and failure of the 

gearbox drive shaft, which could result 

in failure of the engine, in-flight 

shutdown, and loss of control of the 

airplane. 

DATES: This AD becomes effective 

November 27, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of November 27, 2015. 

ADDRESSES: For service information 

identified in this AD, contact Technify 

Motors GmbH, Platanenstrasse 14, D– 

09356 Sankt Egidien, Germany; phone: 

+49 37204 696 0; fax: +49 37204 696 

29125; email: info@centurionengines.com; and Diamond Aircraft 

Industries GmbH, N. A. Otto-Strasse 5, 

2700 Wiener Neustadt, Austria; phone: 

+43 2622 26700; fax: +43 2622 26700 

1369; email: airworthiness@diamondair.at. You may view this service 

information at the FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA. For 

information on the availability of this 

material at the FAA, call 781–238–7125. 

It is also available on the Internet at 

http://www.regulations.gov by searching 

for and locating Docket No. FAA–2015– 

1383. 

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–2015– 

1383; 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 mandatory 

continuing airworthiness information 

(MCAI), the regulatory evaluation, any 

comments received, and other 

information. The address for the Docket 

Office (phone: 800–647–5527) is 

Document Management Facility, U.S. 

Department of Transportation, Docket 

Operations, M–30, West Building 

Ground Floor, Room W12–140, 1200 

New Jersey Avenue SE., Washington, 

DC 20590. 

FOR FURTHER INFORMATION CONTACT: 

Robert Green, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7754; fax: 781–238– 

7199; email: robert.green@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 the specified products. The 

NPRM was published in the Federal 

Register on July 8, 2015 (80 FR 38990). 

The NPRM proposed to correct an 

unsafe condition for the specified 

products. The MCAI states: 

Cases of a broken gearbox drive shaft have 

been reported on aeroplanes equipped with 

TAE 125–02 engines that have a Dual Mass 

Flywheel installed. 

Investigations results showed a possible 

overload of the gearbox drive shaft during 

starting of the engine or during restarting of 

the engine in-flight. 

This condition, if not corrected, could lead 

to engine power loss during flight, possibly 

resulting in loss of control of the aeroplane. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (80 

FR 38990, July 8, 2015). 

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