61982 Federal Register / Vol. 81, No. 174 / Thursday, September 8, 2016 / Rules and Regulations 
1532, requires that covered agencies 
prepare a budgetary impact statement before promulgating a rule that includes any Federal mandate that may result in the expenditure by State, local, and tribal governments, in the aggregate, or by the private sector, of $100 million or more in any one year. If a budgetary impact statement is required, section 205 of the Unfunded Mandates Act, 2 U.S.C. 1535, also requires covered agencies to identify and consider a reasonable number of regulatory alternatives before promulgating a rule. OMB determined that the joint interim- final rule would not result in expenditures by State, local, and tribal governments, or by the private sector, of $100 million or more in any one year. See 79 FR 75877. Thus, a budgetary impact statement was not required for the interim final rule, and is not required here. 
Executive Order 13132 Determination 
The Department determined, as 
required by Executive Order 13132, 
‘‘Federalism’’, that the joint interim final rule did not have any federalism implications. This final rule similarly has no federalism implications. 
List of Subjects 
2 CFR Part 2800 
Accounting, Colleges and universities, 
Grant programs, Hospitals, Indians, 
Intergovernmental relations, Nonprofit organizations, Reporting and recordkeeping requirements. 
28 CFR Part 66 
Accounting, Administrative practice 
and procedure, Reporting and 
recordkeeping requirements. 
28 CFR Part 70 
Accounting, Administrative practice 
and procedure, Reporting and 
recordkeeping requirements. 
Accordingly, the interim final rule 
published by the Department of Justice on December 19, 2014, adding 2 CFR part 2800, and removing 28 CFR parts 66 and 70, is adopted as a final rule with the following changes: 
Title 2—Grants and Agreements 
CHAPTER XXVIII—DEPARTMENT OF 
JUSTICE 
PART 2800—UNIFORM 
ADMINISTRATIVE REQUIREMENTS, COST PRINCIPLES, AND AUDIT REQUIREMENTS FOR FEDERAL AWARDS BY THE DEPARTMENT OF JUSTICE 
■1. The authority citation for part 2800 
continues to read as follows: Authority: 5 U.S.C. 301; 28 U.S.C. 509; 28 
U.S.C. 530C(a)(4); 42 U.S.C. 3789; 2 CFR part 
200. 
■2. Section 2800.101 is revised to read 
as follows: 
§ 2800.101 Adoption of 2 CFR part 200. 
Under the authority listed above, the 
Department of Justice adopts the Office 
of Management and Budget (OMB) Guidance in 2 CFR part 200, except as otherwise may be provided by this Part. Unless expressly provided otherwise, any reference in this part to any provision of law not in this part shall be understood to constitute a general reference and thus to include any subsequent changes to the provision. 
Dated: August 31, 2016. 
Loretta E. Lynch, 
Attorney General. 
[FR Doc. 2016–21452 Filed 9–7–16; 8:45 am] 
BILLING CODE 4410–18–P 
DEPARTMENT OF ENERGY 
10 CFR Part 430 
[Docket No. EERE–2011–BT–TP–0071] 
RIN 1904–AC67 
Energy Conservation Program: Test 
Procedures for Integrated Light- Emitting Diode Lamps; Correction 
AGENCY : Office of Energy Efficiency and 
Renewable Energy, Department of Energy. 
ACTION : Final rule; correction. 
SUMMARY : On July 1, 2016, the U.S. 
Department of Energy (DOE) published a final rule adopting a test procedure for integrated light-emitting diode (LED) lamps (hereafter referred to as ‘‘LED lamps’’) to support the implementation of labeling provisions by the Federal Trade Commission, as well as the ongoing general service lamps rulemaking, which includes LED lamps (hereafter the ‘‘July 2016 final rule’’). This correction addresses an error in the July 2016 final rule to add appendix BB to 10 CFR 430.3(p)(5). Neither the error nor the correction in this document affect the substance of the test procedure rulemaking or any of the conclusions reached in support of the final rule. 
DATES : Effective Date: September 8, 
2016. 
FOR FURTHER INFORMATION CONTACT : 
Ms. Lucy deButts, U.S. Department of 
Energy, Office of Energy Efficiency and Renewable Energy, Building Technologies Program, EE–2J, 1000 Independence Avenue SW., Washington, DC 20585–0121. Telephone: (202) 287–1604. Email: light_ emitting_ diodes@ee.doe.gov. 
Ms. Celia Sher, U.S. Department of 
Energy, Office of the General Counsel, GC–33, 1000 Independence Avenue SW., Washington, DC 20585–0121. Telephone: (202) 287–6122. Email: Celia.Sher@hq.doe.gov. 
SUPPLEMENTARY INFORMATION : DOE 
published the July 2016 final rule in the Federal Register on July 1, 2016, which adopted the test procedures for LED lamps in Appendix BB to support the implementation of labeling provisions by the Federal Trade Commission, as well as the ongoing general service lamps rulemaking, which includes LED lamps. 81 FR 43403. The test procedure for standby power adopted in the July 2016 final rule references the test standard published by the International Electrotechnical Commission (IEC), titled ‘‘Household electrical appliances—Measurement of standby power,’’ IEC 62301 (Edition 2.0, 2011– 01). Therefore, to incorporate by reference IEC 62301 for appendix BB, DOE attempted to amend § 430.3 to add appendix BB to the list of approved appendices in existing paragraph (p)(5). However, the amendatory instruction was incorrectly written and appendix BB was not added. This final rule corrects § 430.3(p)(5) to include appendix BB. 
Procedural Issues and Regulatory 
Review 
The regulatory reviews conducted for 
this rulemaking are those set forth in the July 2016 final rule that originally codified DOE’s adopted test procedures for integrated LED lamps. The test procedures in the July 2016 final rule became effective August 1, 2016. 
Pursuant to the Administrative 
Procedure Act, 5 U.S.C. 553(b), DOE has determined that notice and prior opportunity for comment on this rule are unnecessary and contrary to the public interest. Neither the error nor the correction in this document affect the substance of the rulemaking or any of the conclusions reached in support of the final rule. For these reasons, DOE has also determined that there is good cause to waive the 30-day delay in effective date. 
List of Subjects in 10 CFR Part 430 
Administrative practice and 
procedure, Confidential business 
information, Energy conservation, Household appliances, Imports, Incorporation by reference, Intergovernmental relations, Small businesses. 
VerDate Sep<11>2014 15:15 Sep 07, 2016 Jkt 238001 PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 E:\FR\FM\08SER1.SGM 08SER1Lhorne on DSK30JT082PROD with RULES61983 Federal Register / Vol. 81, No. 174 / Thursday, September 8, 2016 / Rules and Regulations 
Issued in Washington, DC, on August 31, 
2016. 
Kathleen B. Hogan, Deputy Assistant Secretary, Energy Efficiency 
and Renewable Energy. 
For the reasons stated in the 
preamble, DOE amends part 430 of title 
10 of the Code of Federal Regulations by making the following correcting amendment: 
PART 430—ENERGY CONSERVATION 
PROGRAM FOR CONSUMER PRODUCTS 
■1. The authority citation for part 430 
continues to read as follows: 
Authority: 42 U.S.C. 6291–6309; 28 U.S.C. 
2461 note. 
§ 430.3 [Corrected] 
■2. Section 430.3(p)(5) is corrected by 
removing the text ‘‘Z and CC’’ and 
adding in its place, the text ‘‘Z, BB, and CC’’. 
[FR Doc. 2016–21577 Filed 9–7–16; 8:45 am] 
BILLING CODE 6450–01–P 
DEPARTMENT OF TRANSPORTATION 
Federal Aviation Administration 
14 CFR Part 39 
[Docket No. FAA–2016–6665; Directorate 
Identifier 2015–NM–070–AD; Amendment 39–18644; AD 2016–18–13] 
RIN 2120–AA64 
Airworthiness Directives; Fokker 
Services B.V. Airplanes 
AGENCY : Federal Aviation 
Administration (FAA), Department of Transportation (DOT). 
ACTION : Final rule. 
SUMMARY : We are adopting a new 
airworthiness directive (AD) for all Fokker Services B.V. Model F28 Mark 0070 and 0100 airplanes. This AD was prompted by an aileron-wing flutter analysis finding that, when a hydraulic aileron actuator is not powered while at least one aileron flutter damper is inoperative (latent failure), the maximum speed currently defined in the airplane flight manual (AFM) is insufficient to meet the required safety margin. This AD requires revising the AFM to include procedures to follow in the event of a hydraulic system failure and abnormal flight control behavior. We are issuing this AD to ensure that the flightcrew has procedures to follow in the event of a hydraulic system failure and abnormal flight control behavior. If not corrected, this condition could lead to aileron flutter and possible reduced control of the airplane. 
DATES : This AD is effective October 13, 
2016. 
The Director of the Federal Register 
approved the incorporation by reference of a certain publication listed in this AD as of October 13, 2016. 
ADDRESSES : For service information 
identified in this final rule, contact Fokker Services B.V., Technical Services Dept., P.O. Box 1357, 2130 EL Hoofddorp, the Netherlands; telephone +31 (0)88–6280–350; fax +31 (0)88– 6280–111; email technicalservices@fokker.com; Internet http://
www.myfokkerfleet.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– 6665. 
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– 6665; 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 (telephone 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 : Tom 
Rodriguez, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 253–227–1137; fax 253–227–1149. 
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 all Fokker Services B.V. Model F28 Mark 0070 and 0100 airplanes. The NPRM published in the Federal Register on May 13, 2016 (81 FR 29800) 
(‘‘the NPRM’’). The NPRM was prompted by an aileron-wing flutter analysis finding that, when a hydraulic aileron actuator is not powered while at least one aileron flutter damper is inoperative (latent failure), the maximum speed currently defined in the AFM is insufficient to meet the required safety margin. The NPRM proposed to require revising the AFM to include procedures to follow in the event of a hydraulic system failure and abnormal flight control behavior. We are issuing this AD to ensure that the flightcrew has procedures to follow in the event of a hydraulic system failure and abnormal flight control behavior. If not corrected, this condition could lead to aileron flutter and possible reduced control of the airplane. 
The European Aviation Safety Agency 
(EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2015–0078, dated May 6, 2015 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for all Fokker Services B.V. Model F28 Mark 0070 and 0100 airplanes. The MCAI states: 
In the frame of a complementary aileron- 
wing flutter analysis performed by Fokker 
Services, it has been found that in case a hydraulic aileron actuator is not powered, while at least one aileron flutter damper is inoperative (latent failure), the maximum speed currently defined in the Airplane Flight Manual (AFM) is insufficient to meet the required safety margin. 
This condition, if not corrected, could lead 
to aileron flutter, possibly resulting in 
reduced control of the aeroplane. 
To address this potential unsafe condition, 
Fokker Services published an AFM change through Manual Change Notification— Operational (MCNO) F100–066 which introduces an additional step in the Abnormal Procedures for [a] hydraulic [system] failure and for abnormal flight control behaviour. This new step consists in a speed reduction to Vra (IAS 250kt/M 0.65) to restore a sufficient margin to the flutter speed. 
For the reasons described above, this 
[EASA] AD requires incorporation of the amended abnormal procedures into the applicable AFM. 
You may examine the MCAI in the AD 
docket on the Internet at http://www.regulations.gov by searching for 
and locating Docket No. FAA–2016– 6665. 
Comments 
We gave the public the opportunity to 
participate in developing this AD. We 
received no comments on the NPRM or on the determination of the cost to the public. 
Conclusion 
We reviewed the relevant data and 
determined that air safety and the 
public interest require adopting this AD 
VerDate Sep<11>2014 15:15 Sep 07, 2016 Jkt 238001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\08SER1.SGM 08SER1Lhorne on DSK30JT082PROD with RULES