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

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 other 

control 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). 


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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 other 

control 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 ‘‘PL = PL–1g ± UsA ̄ ’’, the 

equation should be ‘‘PL = PL–1g ± UsA ̄ ’’. 

In two cases, the three Greek letters 

‘‘rej’’ after sigma ‘‘s’’ in the subscript 

of ‘‘U’’ are changed to ‘‘ref’’. In these 

cases, ‘‘Usrej’’ should be ‘‘Usref’’. 

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 ‘‘PL = PL–1g ± UsA ̄ ’’ 

is corrected to read ‘‘PL = PL–1g ± UsA ̄ ’’. 

3. On page 73467, second column, 

fifth line from the bottom, the equation 

‘‘Us = UsrejFg’’ is corrected to read 

‘‘Us = Usref Fg’’. 

4. On page 73467, second column, 

third line from the bottom, the text 

‘‘Usrej’’ is corrected to read ‘‘Usref’’. 

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 


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