### 4761 Federal Register / Vol. 80, No. 19 / Thursday, January 29, 2015 / Rules and Regulations

TABLE 

### 1—Continued

Document title ADAMS Accession No.

‘‘Submission of a Supplement to NAC’s Request to Amend the U.S. Nuclear Regulatory Commission Certificate of Compliance No. 1031 for the NAC International MAGNASTOR Cask System,’’ June 17, 2014. ML14170A022

‘‘Submission of a Supplement to NAC’s Request to Amend the U.S. Nuclear Regulatory Commission Certificate of Compliance No. 1031 for the NAC International MAGNASTOR Cask System,’’ July 17, 2014. ML14199A501

List of Subjects in 10 CFR Part 72

Administrative practice and procedure, Criminal penalties, Manpower training programs, Nuclear materials, Occupational safety and health, Penalties, Radiation protection, Reporting and recordkeeping requirements, Security measures, Spent fuel, Whistleblowing.

For the reasons set out in the preamble and under the authority of the Atomic Energy Act of 1954, as amended; the Energy Reorganization Act of 1974, as amended; the Nuclear Waste Policy Act of 1982, as amended; and 5 U.S.C. 552 and 553; the NRC is adopting the following amendments to 10 CFR part
72.

**PART 72—LICENSING REQUIREMENTS FOR THE**  **INDEPENDENT STORAGE OF SPENT NUCLEAR FUEL, HIGH-LEVEL**  **RADIOACTIVE WASTE AND REACTOR-RELATED GREATER THAN**  **CLASS C WASTE**

■ 1. The authority citation for part 72 continues to read as follows:

Authority: Atomic Energy Act secs. 51, 53, 57, 62, 63, 65, 69, 81, 161, 182, 183, 184, 186, 187, 189, 223, 234, 274 (42 U.S.C. 2071, 2073, 2077, 2092, 2093, 2095, 2099, 2111, 2201, 2232, 2233, 2234, 2236, 2237, 2239, 2273, 2282, 2021); Energy Reorganization Act secs. 201, 202, 206, 211 (42 U.S.C. 5841, 5842, 5846, 5851); National Environmental Policy Act sec. 102 (42 U.S.C. 4332); Nuclear Waste Policy Act secs. 131, 132, 133, 135, 137, 141, 148 (42 U.S.C. 10151, 10152, 10153, 10155, 10157, 10161, 10168); Government Paperwork Elimination Act sec. 1704 (44 U.S.C. 3504 note); Energy Policy Act of 2005, Pub. L. 109–58, 119 Stat. 549 (2005).

Section 72.44(g) also issued under Nuclear Waste Policy Act secs. 142(b) and 148(c), (d) (42 U.S.C. 10162(b), 10168(c), (d)). Section 72.46 also issued under Atomic Energy Act sec. 189 (42 U.S.C. 2239); Nuclear Waste Policy Act sec. 134 (42 U.S.C. 10154). Section 72.96(d) also issued under Nuclear Waste Policy Act sec. 145(g) (42 U.S.C. 10165(g)). Subpart J also issued under Nuclear Waste Policy Act secs. 117(a), 141(h) (42 U.S.C. 10137(a), 10161(h)). Subpart K also issued under Nuclear Waste Policy Act sec. 218(a) (42 U.S.C. 10198).

■ 2. In § 72.214, Certificate of Compliance No. 1031 is revised to read as follows: **§ 72.214 List of approved spent fuel storage casks.** 
* * * * *

Certificate Number: 1031. Initial Certificate Effective Date: February 4, 2009.

Amendment Number 1 Effective Date: August 30, 2010.

Amendment Number 2 Effective Date: January 30, 2012.

Amendment Number 3 Effective date: July 25, 2013.

Amendment Number 4 Effective Date: April 14, 2015.

SAR Submitted by: NAC International, Inc.

SAR Title: Final Safety Analysis Report for the MAGNASTOR ® System.

Docket Number: 72–1031. Certificate Expiration Date: February 4, 2029. Model Number: MAGNASTOR ®

.

Dated at Rockville, Maryland, this 15th day of January 2015.

For the Nuclear Regulatory Commission. Mark A. Satorius, Executive Director for Operations.
[FR Doc. 2015–01693 Filed 1–28–15; 8:45 am]

**BILLING CODE 7590–01–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Parts 25**

**[Docket No. FAA–2013–0142; Amdt. No. 25– 141]** 

**RIN 2120–AK12**

**Harmonization of Airworthiness Standards—Gust and Maneuver Load**  **Requirements; Correction**

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

**ACTION :**  Final rule; correction.

**SUMMARY :**  The FAA is correcting the final rule, ‘‘Harmonization of Airworthiness Standards—Gust and Maneuver Load Requirements’’ (79 FR 73462), published December 11, 2014. In the rule, the FAA amended certain airworthiness regulations for transport category airplanes to eliminate regulatory differences between the airworthiness standards of the FAA and European Aviation Safety Agency (EASA). It does not add new requirements beyond what manufacturers currently meet for EASA certification and does not affect current industry design practices. This final rule revises the pitch maneuver design loads criteria; revises the gust and turbulence design loads criteria; revises the application of gust loads to engine mounts, high lift devices, and othercontrol surfaces; adds a ‘‘round-theclock’’ discrete gust criterion and a multi-axis discrete gust criterion for airplanes equipped with wing-mounted engines; revises the engine torque loads criteria; adds an engine failure dynamic load condition; revises the ground gust design loads criteria; revises the criteria used to establish the rough air design speed; and requires the establishment of a rough air Mach number. This document corrects errors in the rule by ensuring that certain letters in the included equations have the right formatting and therefore the correct meaning.

**DATES :**  This correction is effective February 9, 2015.

**FOR FURTHER INFORMATION CONTACT :**  For technical questions concerning this action, contact Todd Martin, Airframe and Cabin Safety Branch, ANM–115, Transport Airplane Directorate, Aircraft Certification Service, Federal Aviation Administration, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone (425) 227–1178; facsimile (425) 227– 1232; email Todd.Martin@faa.gov.

For legal questions concerning this action, contact Sean Howe, Office of the Regional Counsel, ANM–7, Federal Aviation Administration, 1601 Lind Avenue SW., Renton, Washington 98057–3356; telephone (425) 227–2591; facsimile (425) 227–1007; email Sean.Howe@faa.gov.

**SUPPLEMENTARY INFORMATION :**  Background

On December 11, 2014, the FAA published the final rule entitled, ‘‘Harmonization of Airworthiness Standards—Gust and Maneuver Load Requirements’’ (79 FR 73462).


### 4762 Federal Register / Vol. 80, No. 19 / Thursday, January 29, 2015 / Rules and Regulations

In the rule, the FAA amended certain airworthiness regulations for transport category airplanes to eliminate regulatory differences between the airworthiness standards of the FAA and European Aviation Safety Agency (EASA). It does not add new requirements beyond what manufacturers currently meet for EASA certification and does not affect current industry design practices. This final rule revises the pitch maneuver design loads criteria; revises the gust and turbulence design loads criteria; revises the application of gust loads to engine mounts, high lift devices, and othercontrol surfaces; adds a ‘‘round-theclock’’ discrete gust criterion and a multi-axis discrete gust criterion for airplanes equipped with wing-mounted engines; revises the engine torque loads criteria; adds an engine failure dynamic load condition; revises the ground gust design loads criteria; revises the criteria used to establish the rough air design speed; and requires the establishment of a rough air Mach number.

This document corrects three errors in the Greek letters and subscripts contained in various equations in the regulatory text. In one case, the ‘‘U’’ in the equation is changed from subscript to regular, uppercase text. In another case, instead of ‘‘P L = P L–1 g ± UsA  ̄ ’’, the equation should be ‘‘P L = P L–1 g ± U sA  ̄ ’’. In two cases, the three Greek letters

‘‘ rej ’’ after sigma ‘‘ s ’’ in the subscript of ‘‘U’’ are changed to ‘‘ref’’. In these cases, ‘‘U srej ’’ should be ‘‘U sref ’’.

This correction also corrects the statement in the rule’s preamble that the FAA received 33 comments to the Advisory Circulars, rather than none.

Corrections

In FR Doc. 2014–28938, beginning on page 73464, in the Federal Register of December 11, 2014, make the following corrections:

1. On Page 73464, second column, under the heading ‘‘C. Advisory Material’’, the sentence, ‘‘The FAA did not receive any comments on the proposed ACs’’ is corrected to read ‘‘The FAA received 33 comments on the proposed ACs. These comments did not have an impact on the regulatory requirements’’.

2. On page 73467, second column, line 11, the equation ‘‘P L = P L–1g ± UsA  ̄ ’’ is corrected to read ‘‘P L = P L–1g ± U sA  ̄ ’’. 3. On page 73467, second column, fifth line from the bottom, the equation ‘‘U s = U srej F g ’’ is corrected to read ‘‘U s = U sref F g ’’.

4. On page 73467, second column, third line from the bottom, the text ‘‘U srej ’’ is corrected to read ‘‘U sref ’’. Issued in Washington, DC, on January 16,
2015. Lirio Liu, Director, Office of Rulemaking.
[FR Doc. 2015–01205 Filed 1–28–15; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2015–0078; Directorate Identifier 2014–NM–235–AD; Amendment**  **39–18084; AD 2015–02–17]**

**RIN 2120–AA64**

**Airworthiness Directives; Airbus Airplanes** 

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

**ACTION :**  Final rule; request for
comments.

**SUMMARY :**  We are adopting a new airworthiness directive (AD) for all Airbus Model A330–200, A330–200 Freighter, and A330–300 series airplanes. This AD requires revising the electrical emergency configuration procedure in the Emergency Procedures section of the airplane flight manual (AFM) to include procedures for deploying the ram air turbine manually to provide sufficient hydraulic power and avoid constant speed motor/ generator (CSM/G) shedding. This AD was prompted by an electrical load analysis that revealed that hydraulic power might not be sufficient to supply the CSM/G during slat/flap extension when only one engine is running. We are issuing this AD to prevent such a condition which, in conjunction with the loss of the main electrical system, could lead to the scenario where the flightcrew is not clearly warned that the electrical system has switched on the battery and thus has a limited duration that would allow a safe landing.

**DATES :**  This AD becomes effective February 13, 2015.

The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of February 13, 2015.

We must receive comments on this AD by March 16, 2015.

**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: 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 AD, contact Airbus SAS, Airworthiness Office—EAL, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 45 80; email airworthiness.A330–A340@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–2015– 0078; 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 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 :**  Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1138; fax 425–227–1149.

**SUPPLEMENTARY INFORMATION :** 

Discussion

The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2014–0281, dated December 22, 2014 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition on all Airbus Model A330–200, A330–200 Freighter, and A330–300 series airplanes. The MCAI
states:

The Constant Speed Motor/Generator (CSM/G), as installed on Airbus A330