19844 Federal Register / Vol. 79, No. 69 / Thursday, April 10, 2014 / Proposed Rules 

Done in Washington, DC, this 4th day of 

April 2014. 

Kevin Shea, 

Administrator, Animal and Plant Health 

Inspection Service. 

[FR Doc. 2014–08019 Filed 4–9–14; 8:45 am] 

BILLING CODE 3410–34–P 

DEPARTMENT OF ENERGY 

10 CFR Parts 429 and 431 

[Docket Number EERE–2011–BT–TP–0024] 

RIN 1904–AC46 

Energy Conservation for Certain 

Industrial Equipment: Alternative 

Efficiency Determination Methods and 

Test Procedures for Walk-In Coolers 

and Walk-In Freezers; Extension of 

Public Comment Period 

AGENCY: Office of Energy Efficiency and 

Renewable Energy, Department of 

Energy. 

ACTION: Extension of public comment 

period. 

SUMMARY: The U.S. Department of 

Energy (DOE) is reopening of the 

comment period for interested parties to 

submit comments on the February 20, 

2014 supplemental notice of proposed 

rulemaking for walk-in cooler and walkin freezer alternative efficiency 

determination methods and test 

procedures. The comment period is 

extended to April 25, 2014. 

DATES: Comments: DOE will accept 

comments, data, and information 

regarding the supplemental notice of 

proposed rulemaking (SNOPR) for walkin cooler and walk-in freezer alternative 

efficiency determination methods and 

test procedures no later than April 25, 

2014. 

ADDRESSES: Interested persons are 

encouraged to submit comments using 

the Federal eRulemaking Portal at 

www.regulations.gov. Alternatively, 

interested persons may submit 

comments, identified by docket number 

EERE–2011–BT–TP–0024 and/or RIN 

1904–AC46, by any of the following 

methods: 

• Email: AED-ARM-2011-TP-0024@

ee.doe.gov. Include EERE–2011–BT– 

TP–0024 and/or RIN 1904–AC46in the 

subject line of the message. Submit 

electronic comments in WordPerfect, 

Microsoft Word, PDF, or ASCII file 

format, and avoid the use of special 

characters or any form of encryption. 

• Postal Mail: Ms. Brenda Edwards, 

U.S. Department of Energy, Building 

Technologies Office, Mailstop EE–5B, 

1000 Independence Avenue SW., 

Washington, DC 20585–0121. If 

possible, please submit all items on a 

compact disc (CD), in which case it is 

not necessary to include printed copies. 

• Hand Delivery/Courier: Ms. Brenda 

Edwards, U.S. Department of Energy, 

Building Technologies Office, 950 

L’Enfant Plaza SW., 6th Floor, 

Washington, DC 20024. Telephone: 

(202) 586–2945. If possible, please 

submit all items on a CD, in which case 

it is not necessary to include printed 

copies. 

Docket: The docket is available for 

review at www.regulations.gov, 

including Federal Register notices, 

public meeting attendee lists and 

transcripts, comments, and other 

supporting documents/materials. All 

documents in the docket are listed in 

the www.regulations.gov index. 

However, not all documents listed in 

the index may be publicly available, 

such as information that is exempt from 

public disclosure. 

A link to the docket Web page can be 

found at: http://www.regulations.gov/

#!docketDetail;D=EERE-2011-BT-TP0024. This Web page contains a link to 

the docket for this notice on the 

www.regulations.gov site. The 

www.regulations.gov Web page contains 

simple instructions on how to access all 

documents, including public comments, 

in the docket. 

For information on how to submit a 

comment or review other public 

comments and the docket, contact Ms. 

Brenda Edwards at (202) 586–2945 or by 

email: Brenda.Edwards@ee.doe.gov. 

FOR FURTHER INFORMATION CONTACT: Ms. 

Ashley Armstrong, U.S. Department of 

Energy, Office of Energy Efficiency and 

Renewable Energy, Building 

Technologies Office, EE–5B, 1000 

Independence Avenue SW., 

Washington, DC 20585–0121. 

Telephone: (202) 586–6590. Email: 

Ashley.Armstrong@ee.doe.gov. 

Mr. Michael Kido, U.S. Department of 

Energy, Office of the General Counsel, 

GC–71, 1000 Independence Avenue 

SW., Washington, DC 20585–0121. 

Telephone: (202) 586–8145. Email: 

Michael.Kido@hq.doe.gov. 

SUPPLEMENTARY INFORMATION: On 

February 20, 2014 DOE issued a 

supplemental notice of proposed 

rulemaking (SNOPR) that proposed to 

revise its existing regulations for walkin coolers and walk-in freezers 

regarding the use of methods other than 

testing for certifying compliance and 

reporting ratings in accordance with 

energy conservation standards. DOE 

also proposed clarifications to its test 

procedures for this equipment. 79 FR 

9817. In today’s notice, the Department 

is reopening the comment period for the 

February 20, 2014 SNOPR to allow 

interested parties additional time to 

provide the Department with comments, 

data, and information. The Department 

will accept comments regarding the 

February 20, 2014 SNOPR received no 

later than April 25, 2014. 

Issued in Washington, DC, on April 4, 

2014. 

Kathleen B. Hogan, 

Deputy Assistant Secretary for Energy 

Efficiency, Energy Efficiency and Renewable 

Energy. 

[FR Doc. 2014–08070 Filed 4–9–14; 8:45 am] 

BILLING CODE 6450–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0159; Directorate 

Identifier 2014–NE–01–AD] 

RIN 2120–AA64 

Airworthiness Directives; Pratt & 

Whitney Canada Corporation 

Turboprop Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for certain 

serial number Pratt & Whitney Canada 

Corporation (P&WC) model PW150A 

turboprop engines. This proposed AD 

was prompted by reports of damage to 

a high-pressure fuel line, which could 

result in a high-pressure fuel leak into 

the engine nacelle. This proposed AD 

would require rerouting of the igniter 

cables and installation of new support 

brackets. We are proposing this AD to 

prevent high-pressure fuel leaks, which 

could cause engine fire and damage to 

the engine and the airplane. 

DATES: We must receive comments on 

this proposed AD by June 9, 2014. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov and follow 

the instructions for sending your 

comments electronically. 

• Mail: Docket Management Facility, 

U.S. Department of Transportation, 1200 

New Jersey Avenue SE., West Building 

Ground Floor, Room W12–140, 

Washington, DC 20590–0001. 

• Hand Delivery: Deliver to Mail 

address above between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 


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Federal Register / Vol. 79, No. 69 / Thursday, April 10, 2014 / Proposed Rules 19845 

• Fax: 202–493–2251. 

For service information identified in 

this proposed AD, contact Pratt & 

Whitney Canada Corp., 1000 MarieVictorin, Longueuil, Quebec, Canada, 

J4G 1A1; phone: 800–268–8000; fax: 

450–647–2888; Internet: www.pwc.ca. 

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. 

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– 

0159; or in person at the Docket 

Operations office between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. The AD docket 

contains this proposed AD, the 

mandatory continuing airworthiness 

information (MCAI), the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Operations office (phone: 

800–647–5527) is the same as the Mail 

address provided in the ADDRESSES

section. Comments will be available in 

the AD docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Wego Wang, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7134; fax: 781–238– 

7199; email: wego.wang@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 

this proposed AD. Send your comments 

to an address listed under the 

ADDRESSES section. Include ‘‘Docket No. 

FAA–2014–0159; Directorate Identifier 

2014–NE–01–AD’’ at the beginning of 

your comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this proposed AD. We will 

consider all comments received by the 

closing date and may amend this 

proposed AD based on 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 with FAA 

personnel concerning this proposed AD. 

Discussion 

Transport Canada Civil Aviation, 

which is the aviation authority for 

Canada, has issued Transport Canada 

AD CF–2014–09, dated February 12, 

2014, (referred to hereinafter as ‘‘the 

MCAI’’), to correct an unsafe condition 

for the specified products. The MCAI 

states: 

There have been reports of damage in 

excess of acceptable criteria to the high 

pressure fuel line from the P&WC PW150A 

engine flowmeter to the flow divider. Damage 

has included fretting wear through contact 

with the engine igniter cables. The contact is 

the result of incorrectly routed igniter cables. 

While there has been no report of associated 

fuel leakage, the fretting wear, if undetected, 

could progress to a point where high pressure 

fuel would leak into the engine nacelle. 

You may examine the MCAI in the AD 

docket on the Internet at http://

www.regulations.gov by searching for 

and locating it in Docket No. FAA– 

2014–0159. 

Relevant Service Information 

P&WC has issued Service Bulletin 

(SB) No. PW150–72–35274, Revision 1, 

dated May 3, 2012. The SB describes 

procedures for rerouting the igniter 

cables and installing new support 

brackets. 

FAA’s Determination and Requirements 

of This Proposed AD 

This product has been approved by 

the aviation authority of Canada, and is 

approved for operation in the United 

States. Pursuant to our bilateral 

agreement with Canada, they have 

notified us of the unsafe condition 

described in the MCAI and service 

information referenced above. We are 

proposing this AD because we evaluated 

all information provided by Transport 

Canada Civil Aviation and determined 

the unsafe condition exists and is likely 

to exist or develop on other products of 

the same type design. This proposed AD 

would require rerouting of the igniter 

cables and installation of new support 

brackets. 

Costs of Compliance 

We estimate that this proposed AD 

affects 180 engines installed on 

airplanes of U.S. registry. We also 

estimate that it would take about 1 hour 

per engine to comply with this proposed 

AD. The average labor rate is $85 per 

hour. Required parts cost about $682 per 

engine. Based on these figures, we 

estimate the cost of this proposed AD on 

U.S. operators to be $138,060. 

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 proposed 

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 proposed AD 

would not have federalism implications 

under Executive Order 13132. This 

proposed AD would not have a 

substantial direct effect on the States, on 

the relationship between the national 

Government and the States, or on the 

distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify this proposed regulation: 

(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 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. 

The Proposed Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA proposes to amend 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): 


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19846 Federal Register / Vol. 79, No. 69 / Thursday, April 10, 2014 / Proposed Rules 

Pratt & Whitney Canada Corporation: Docket 

No. FAA–2014–0159; Directorate 

Identifier 2014–NE–01–AD. 

(a) Comments Due Date 

We must receive comments by June 9, 

2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Pratt & Whitney Canada 

Corporation (P&WC) model PW150A 

turboprop engines, serial number PCE– 

FA0916 and earlier. 

(d) Reason 

This AD was prompted by reports of 

damage to a high-pressure fuel line, which 

could result in a high-pressure fuel leak into 

the engine nacelle. We are issuing this AD to 

prevent high-pressure fuel leaks, which 

could cause engine fire and damage to the 

engine and the airplane. 

(e) Actions and Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(1) At the next shop visit, but before 36 

months from the effective date of this AD, 

reroute the igniter cables and install new 

support brackets in accordance with 

Accomplishment Instructions, paragraph 

3.B., of P&WC Service Bulletin (SB) No. 

PW150–72–35274, Revision 1, dated May 3, 

2012. 

(2) Reserved. 

(f) Definition 

For the purpose of this AD, a shop visit is 

when the engine is disassembled to the 

extent necessary to gain access to the igniter 

cables. 

(g) Credit for Previous Action 

If you performed the actions of paragraph 

(e) of this AD before the effective date of this 

AD using P&WC SB No. PW150–72–35274, 

Initial Issue, dated March 23, 2012, you met 

the requirements of this AD. 

(h) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

FAA, may approve AMOCs to this AD. Use 

the procedures found in 14 CFR 39.19 to 

make your request. 

(i) Related Information 

(1) For more information about this AD, 

contact Wego Wang, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7134; fax: 781–238–7199; 

email: wego.wang@faa.gov. 

(2) Refer to MCAI Transport Canada AD 

CF–2014–09, dated February 12, 2014, for 

more information. You may examine the 

MCAI in the AD docket on the Internet at 

http://www.regulations.gov by searching for 

and locating it in Docket No. FAA–2014– 

0159. 

(3) P&WC SB No. PW150–72–35274, 

Revision 1, dated May 3, 2012, pertains to the 

subject of this AD and can be obtained from 

P&WC using the contact information in 

paragraph (i)(4) of this AD. 

(4) For service information identified in 

this AD, contact Pratt & Whitney Canada 

Corp., 1000 Marie-Victorin, Longueuil, 

Quebec, Canada, J4G 1A1; phone: 800–268– 

8000; fax: 450–647–2888; Internet: 

www.pwc.ca. 

(5) 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. 

Issued in Burlington, Massachusetts, on 

April 3, 2014. 

Colleen M. D’Alessandro, 

Assistant Directorate Manager, Engine & 

Propeller Directorate, Aircraft Certification 

Service. 

[FR Doc. 2014–08009 Filed 4–9–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0193; Directorate 

Identifier 2013–NM–234–AD] 

RIN 2120–AA64 

Airworthiness Directives; Airbus 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for certain 

Airbus Model A318, A319, A320, and 

A321 series airplanes. This proposed 

AD was prompted by a report of a crack 

found in the fuselage during a fatigue 

test campaign. This proposed AD would 

require repetitive rototest inspections 

for cracking; corrective actions if 

necessary; and modification of the 

torsion box, which would terminate the 

repetitive inspections. We are proposing 

this AD to prevent cracking in the side 

box beam flange of the fuselage, which 

could affect the structural integrity of 

the airplane. 

DATES: We must receive comments on 

this proposed AD by May 27, 2014. 

ADDRESSES: You may send comments 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, between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

For service information identified in 

this proposed AD, contact Airbus, 

Airworthiness Office—EAS, 1 Rond 

Point Maurice Bellonte, 31707 Blagnac 

Cedex, France; telephone +33 5 61 93 36 

96; fax +33 5 61 93 44 51; email 

account.airworth-eas@airbus.com; 

Internet http://www.airbus.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– 

0193; 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 proposed 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. Comments will 

be available in the AD docket shortly 

after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Sanjay Ralhan, Aerospace Engineer, 

International Branch, ANM 116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue SW., Renton, WA 

98057–3356; telephone (425) 227–1405; 

fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 

this proposed AD. Send your comments 

to an address listed under the 

ADDRESSES section. Include ‘‘Docket No. 

FAA–2014–0193; Directorate Identifier 

2013–NM–234–AD’’ at the beginning of 

your comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this proposed AD. We will 

consider all comments received by the 

closing date and may amend this 

proposed AD based on 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 


ehiers on DSK2VPTVN1PROD with PROPOSALS-1