### 13764 Federal Register / Vol. 81, No. 50 / Tuesday, March 15, 2016 / Proposed Rules

contains instructions on how to access all documents in the docket, including public comments.

**FOR FURTHER INFORMATION CONTACT :**  Ms. Lucy deButts, U.S. Department of

Energy, Office of Energy Efficiency and Renewable Energy, Building Technologies, EE–5B, 1000 Independence Avenue SW., Washington, DC 20585–0121. Telephone: (202)-287–1604. Email: ceiling

_ fans@ee.doe.gov. In the Office of the General Counsel,

contact Ms. Elizabeth Kohl, U.S. Department of Energy, Office of the General Counsel, GC–33, 1000 Independence Avenue SW., Washington, DC 20585–0121. Telephone: (202) 586–7796. Email: Elizabeth.Kohl@hq.doe.gov.

**SUPPLEMENTARY INFORMATION :**  On January 13, 2016, the U.S. Department of Energy (DOE) published a notice of proposed rulemaking (NOPR) for ceiling fans energy conservation standards in the Federal Register to make available and invite comments on the analysis for ceiling fans energy conservation standards. 81 FR 1687. The notice provided for the written submission of comments by March 14, 2016, and oral comments were also accepted at a public meeting held on February 3, 2016. At the public meeting, various stakeholders have requested an extension of the comment period to consider the NOPR, technical support documents and public meeting presentation, and to prepare and submit comments accordingly. On March 2, American Lighting Association sent a written request for 30-day comment period extension due additional testing manufacturers have to conduct to review their existing products against the ceiling fan test procedures SNOPR, published in the Federal Register on June 3, 2015, and the conservation standards NOPR.

DOE has determined that an extension of the public comment period is appropriate based on the foregoing reason. DOE will consider any comments received by midnight of April 14, 2016, and deems any comments received by that time to be timely submitted.

Issued in Washington, DC, on March 10,

2016. Kathleen B. Hogan, Deputy Assistant Secretary for Energy Efficiency, Energy Efficiency and Renewable Energy.
[FR Doc. 2016–05824 Filed 3–14–16; 8:45 am]

**BILLING CODE 6450–01–P DEPARTMENT OF TRANSPORTATION** 

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2015–4866; Directorate Identifier 2015–NE–33–AD]** 

**RIN 2120–AA64**

**Airworthiness Directives; Honeywell International Inc. Turboprop and**  **Turboshaft 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 Honeywell International Inc. (Honeywell) TPE331 model turboprop engines and TSE331–3U model turboshaft engines. This proposed AD was prompted by the discovery of cracks in a 2nd stage compressor impeller during a routine shop visit. This proposed AD would require removal of the 2nd stage compressor impeller. We are proposing this AD to prevent failure of the compressor impeller, uncontained part release, damage to the engine, and damage to the airplane.

**DATES :**  We must receive comments on this proposed AD by May 16, 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: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. 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– 4866; 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 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 :**  Joseph Costa, Aerospace Engineer, Los Angeles Aircraft Certification Office, FAA, Transport Airplane Directorate, 3960 Paramount Blvd., Lakewood, CA 90712–4137; phone: 562–627–5246; fax: 562–627–5210; email: joseph.costa@faa.gov.

**SUPPLEMENTARY INFORMATION :** 
Comments Invited

We invite you to send any written relevant data, views, or arguments about this NPRM. Send your comments to an address listed under the **ADDRESSES** section. Include ‘‘Docket No. FAA– 2015–4866; Directorate Identifier 2015– NE–33–AD’’ at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this NPRM. We will consider all comments received by the closing date and may amend this NPRM 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 NPRM.

Discussion

Several 2nd stage compressor impellers were found cracked in the aft curvic root radius when inspected during a routine shop visit. This condition, if not corrected, could result in failure of the compressor impeller, uncontained part release, damage to the engine, and damage to the airplane.

FAA’s Determination

We are proposing this NPRM 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. Proposed AD Requirements

This NPRM would require accomplishing the actions specified in the service information described previously. Costs of Compliance

We estimate that this proposed AD would affect 4,000 engines installed on airplanes of U.S. registry. We estimate that it would take 0 hours per engine to comply with this proposed AD. The average labor rate is $85 per hour. We also estimate that required parts would cost about $1,513.25 per engine. Based


### 13765 Federal Register / Vol. 81, No. 50 / Tuesday, March 15, 2016 / Proposed Rules

on these figures, we estimate the total cost of this proposed AD on U.S. operators to be $6,053,000. 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 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):
Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc., Garrett Engine Division; Garrett Turbine Engine Company; and AiResearch Manufacturing Company of Arizona): Docket No. FAA–2015–4866; Directorate Identifier 2015–NE–33–AD.

(a) Comments Due Date

We must receive comments by May 16,
2016.
(b) Affected ADs

None. (c) Applicability

This AD applies to Honeywell International Inc. (Honeywell) TPE331–3U, –3UW, –5, –5A, –5AB, –5B, –6, –6A, –8, –10, –10AV, –10GP, –10GT, –10N, –10P, –10R, –10T, –10U, –10UA, –10UF, –10UG, –10UGR, –10UR, and –11U model turboprop engines, and TSE331–3U model turboshaft engines, with a 2nd stage compressor impeller, part number (P/N) 893482–1 through –5, inclusive, or P/N 3107056–1 or P/N 3107056–2, installed.

(d) Unsafe Condition

This AD was prompted by the discovery of cracks in a 2nd stage compressor impeller during a routine shop visit. We are issuing this AD to prevent failure of the compressor impeller, uncontained part release, damage to the engine, and damage to the airplane.
(e) Compliance

Comply with this AD within the compliance times specified, unless already done.

(1) Remove from service the 2nd stagecompressor impeller within 200 cycles-inservice after the effective date of the AD, or before exceeding 7,000 cycles since last overhaul, whichever occurs later.

(f) Installation Prohibition

After the effective date of this AD, do not install a 2nd stage compressor impeller, part number (P/N) 893482–1 through –5, inclusive, or P/N 3107056–1 or P/N 3107056–2 into any engine.
(g) Alternative Methods of Compliance (AMOCs)

The Manager, Los Angeles Aircraft Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request.

(h) Related Information

(1) For more information about this AD, contact Joseph Costa, Aerospace Engineer, Los Angeles Aircraft Certification Office, FAA, Transport Airplane Directorate, 3960 Paramount Blvd., Lakewood, CA 90712– 4137; phone: 562–627–5246; fax: 562–627– 5210; email: joseph.costa@faa.gov.

Issued in Burlington, Massachusetts, on March 4, 2016. Colleen M. D’Alessandro, Manager, Engine & Propeller Directorate, Aircraft Certification Service.
[FR Doc. 2016–05704 Filed 3–14–16; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF DEFENSE**

**Office of the Secretary**

**32 CFR Part 69**

**[Docket ID: DOD–2014–OS–0006]**

**RIN 0790–AJ18**

**School Boards for DoD Domestic Dependent Elementary and Secondary**  **Schools (DDESS)**

**AGENCY :**  Under Secretary of Defense for Personnel and Readiness, DoD.

**ACTION :**  Proposed rule.

**SUMMARY :**  This proposed rule establishes policy, assigns responsibilities, and provides procedures for the establishment and operation of elected school boards for elementary, middle and high schools operated by the DoD Education Activity in the Continental United States and the Territories, Possessions and Commonwealths. Specific direction is given to facilitate compliance with 10 U.S.C. 2164(d), as implemented by DoD Instruction 1342.25, regarding the election of board members, composition, roles and responsibilities, operating procedures and resolution of conflicts.

**DATES :**  Comments must be received by May 16, 2016.

**ADDRESSES :**  You may submit comments, identified by docket number or Regulatory Information Number (RIN) number and title, by any of the following methods:

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

• Mail: Department of Defense, Office of the Deputy Chief Management Officer, Directorate of Oversight and Compliance, Regulatory and Audit Matters Office, 9010 Defense Pentagon, Washington, DC 20301–9010.

Instructions: All submissions received must include the agency name and docket number or RIN for this Federal Register document. The general policy