Federal Register / Vol. 74, No. 196 / Tuesday, October 13, 2009 / Rules and Regulations 52391 

Affairs, Office of Management and 

Budget. 

List of Subjects in 10 CFR Part 72 

Administrative practice and 

procedure, Hazardous waste, Nuclear 

materials, Occupational safety and 

health, 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: Secs. 51, 53, 57, 62, 63, 65, 69, 

81, 161, 182, 183, 184, 186, 187, 189, 68 Stat. 

929, 930, 932, 933, 934, 935, 948, 953, 954, 

955, as amended, sec. 234, 83 Stat. 444, as 

amended (42 U.S.C. 2071, 2073, 2077, 2092, 

2093, 2095, 2099, 2111, 2201, 2232, 2233, 

2234, 2236, 2237, 2238, 2282); sec. 274, Pub. 

L. 86–373, 73 Stat. 688, as amended (42 

U.S.C. 2021); sec. 201, as amended, 202, 206, 

88 Stat. 1242, as amended, 1244, 1246 (42 

U.S.C. 5841, 5842, 5846); Pub. L. 95–601, sec. 

10, 92 Stat. 2951 as amended by Pub. L. 102– 

486, sec. 7902, 106 Stat. 3123 (42 U.S.C. 

5851); sec. 102, Pub. L. 91–190, 83 Stat. 853 

(42 U.S.C. 4332); secs. 131, 132, 133, 135, 

137, 141, Pub. L. 97–425, 96 Stat. 2229, 2230, 

2232, 2241, sec. 148, Pub. L. 100–203, 101 

Stat. 1330–235 (42 U.S.C. 10151, 10152, 

10153, 10155, 10157, 10161, 10168); sec. 

1704, 112 Stat. 2750 (44 U.S.C. 3504 note); 

sec. 651(e), Pub. L. 109–58, 119 Stat. 806–10 

(42 U.S.C. 2014, 2021, 2021b, 2111). 

Section 72.44(g) also issued under secs. 

142(b) and 148(c), (d), Pub. L. 100–203, 101 

Stat. 1330–232, 1330–236 (42 U.S.C. 

10162(b), 10168(c),(d)). Section 72.46 also 

issued under sec. 189, 68 Stat. 955 (42 U.S.C. 

2239); sec. 134, Pub. L. 97–425, 96 Stat. 2230 

(42 U.S.C. 10154). Section 72.96(d) also 

issued under sec. 145(g), Pub. L. 100–203, 

101 Stat. 1330–235 (42 U.S.C. 10165(g)). 

Subpart J also issued under secs. 2(2), 2(15), 

2(19), 117(a), 141(h), Pub. L. 97–425, 96 Stat. 

2202, 2203, 2204, 2222, 2244 (42 U.S.C. 

10101, 10137(a), 10161(h)). Subparts K and L 

are also issued under sec. 133, 98 Stat. 2230 

(42 U.S.C. 10153) and sec. 218(a), 96 Stat. 

2252 (42 U.S.C. 10198). 

■ 2. In § 72.214, Certificate of 

Compliance 1014 is revised to read as 

follows: 

§ 72.214 List of approved spent fuel 

storage casks. 

* * * * * 

Certificate Number: 1014. 

Initial Certificate Effective Date: May 

31, 2000. 

Amendment Number 1 Effective Date: 

July 15, 2002. 

Amendment Number 2 Effective Date: 

June 7, 2005. 

Amendment Number 3 Effective Date: 

May 29, 2007. 

Amendment Number 4 Effective Date: 

January 8, 2008. 

Amendment Number 5 Effective Date: 

July 14, 2008. 

Amendment Number 6 Effective Date: 

August 17, 2009. 

Amendment Number 7 Effective Date: 

December 28, 2009. 

SAR Submitted by: Holtec 

International. 

SAR Title: Final Safety Analysis 

Report for the HI–STORM 100 Cask 

System. 

Docket Number: 72–1014. 

Certificate Expiration Date: May 31, 

2020. 

Model Number: HI–STORM 100 

Systems. 

* * * * * 

Dated at Rockville, MD, this 24th day of 

September 2009. 

For the Nuclear Regulatory Commission. 

R.W. Borchardt, 

Executive Director for Operations. 

[FR Doc. E9–24561 Filed 10–9–09; 8:45 am] 

BILLING CODE 7590–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2009–0611; Directorate 

Identifier 2008–NM–165–AD; Amendment 

39–16033; AD 2009–20–10] 

RIN 2120–AA64 

Airworthiness Directives; 

Construcciones Aeronauticas, S.A. 

(CASA), Model C–212–CB, C–212–CC, 

C–212–CD, and C–212–CE Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for the 

products listed above. This AD results 

from mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as: 

Honeywell International, the manufacturer 

of the SPZ200 autopilot system installed on 

the EADS–CASA C–212 series aircraft, has 

identified a series of servo-motors * * * 

designed for use in the SPZ200 autopilot 

system, whose failure can lead to a potential 

unsafe flight condition. * * * 

* * * * * 

The unsafe condition is failure of the 

servo-motors, which could result in roll 

oscillations or possible hard-over 

failures when the autopilot is engaged. 

We are issuing this AD to require 

actions to correct the unsafe condition 

on these products. 

DATES: This AD becomes effective 

November 17, 2009. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of November 17, 2009. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

www.regulations.gov or in person at the 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue, SE., 

Washington, DC. 

FOR FURTHER INFORMATION CONTACT: 

Shahram Daneshmandi, Aerospace 

Engineer, International Branch, ANM– 

116, Transport Airplane Directorate, 

FAA, 1601 Lind Avenue, SW., Renton, 

Washington 98057–3356; telephone 

(425) 227–1112; fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an AD that would 

apply to the specified products. That 

NPRM was published in the Federal 

Register on July 16, 2009 (74 FR 34520). 

That NPRM proposed to correct an 

unsafe condition for the specified 

products. The MCAI states: 

Honeywell International, the manufacturer 

of the SPZ200 autopilot system installed on 

the EADS–CASA C–212 series aircraft, has 

identified a series of servo-motors, P/N [part 

number] 4006719–904 and P/N 4006719–913, 

designed for use in the SPZ200 autopilot 

system, whose failure can lead to a potential 

unsafe flight condition. To address and 

correct this situation, Honeywell 

International has published Alert Service 

Bulletin (ASB) 4006719–22–A0016 (Revised) 

dated 1 November 2004, that identifies the 

affected servo-motors by serial number, 

recommending the removal of these units 

from the aircraft and including modification 

instructions to be accomplished prior to 

reinstallation. 

EADS–CASA has determined that the flight 

safety of the C–212 aircraft is at risk. 

Consequently, Boletin de Servicio (Service 


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52392 Federal Register / Vol. 74, No. 196 / Tuesday, October 13, 2009 / Rules and Regulations 

Bulletin) SB–212–22–16 has been published 

to advise C–212 operators of this condition 

and to recommend that the affected servomotors are modified or replaced with 

modified units. 

For the reasons described above, this EASA 

AD requires the identification of the affected 

servo-motors and modification or 

replacement with modified units. 

The unsafe condition is failure of the 

servo-motors, which could result in roll 

oscillations or possible hard-over 

failures when the autopilot is engaged. 

You may obtain further information by 

examining the MCAI in the AD docket. 

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 available data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed. 

Differences Between This AD and the 

MCAI or Service Information 

We have reviewed the MCAI and 

related service information and, in 

general, agree with their substance. But 

we might have found it necessary to use 

different words from those in the MCAI 

to ensure the AD is clear for U.S. 

operators and is enforceable. In making 

these changes, we do not intend to differ 

substantively from the information 

provided in the MCAI and related 

service information. 

We might also have required different 

actions in this AD from those in the 

MCAI in order to follow our FAA 

policies. Any such differences are 

highlighted in a NOTE within the AD. 

Costs of Compliance 

We estimate that this AD will affect 

26 products of U.S. registry. We also 

estimate that it will take about 5 workhours per product to comply with the 

basic requirements of this AD. The 

average labor rate is $80 per work-hour. 

Based on these figures, we estimate the 

cost of this AD to the U.S. operators to 

be $10,400, or $400 per product. 

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 AD will not 

have federalism implications under 

Executive Order 13132. This AD will 

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 AD: 

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); and 

3. 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. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this AD and placed it in the AD docket. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; 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 the NPRM, 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. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

■ Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 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 AD: 

2009–20–10 Construcciones Aeronauticas, 

S.A. (CASA): Amendment 39–16033. 

Docket No. FAA–2009–0611; Directorate 

Identifier 2008–NM–165–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective November 17, 2009. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to CASA Model C– 

212–CB, C–212–CC, C–212–CD and C–212– 

CE airplanes, all serial numbers; certificated 

in any category; on which autopilot servodrive actuators (servo-motors) having part 

number (P/N) 4006719–904 or 4006719–913 

are installed. 

Subject 

(d) Air Transport Association (ATA) of 

America Code 22: Auto flight. 

Reason 

(e) The mandatory continuing 

airworthiness information (MCAI) states: 

Honeywell International, the manufacturer 

of the SPZ200 autopilot system installed on 

the EADS–CASA C–212 series aircraft, has 

identified a series of servo-motors, P/N [part 

number] 4006719–904 and P/N 4006719–913, 

designed for use in the SPZ200 autopilot 

system, whose failure can lead to a potential 

unsafe flight condition. To address and 

correct this situation, Honeywell 

International has published Alert Service 

Bulletin (ASB) 4006719–22–A0016 (Revised) 

dated 1 November 2004, that identifies the 

affected servo-motors by serial number, 

recommending the removal of these units 

from the aircraft and including modification 

instructions to be accomplished prior to 

reinstallation. 

EADS–CASA has determined that the flight 

safety of the C–212 aircraft is at risk. 

Consequently, Boletin de Servicio (Service 

Bulletin) SB–212–22–16 has been published 

to advise C–212 operators of this condition 

and to recommend that the affected servomotors are modified or replaced with 

modified units. 

For the reasons described above, this EASA 

AD requires the identification of the affected 

servo-motors and modification or 

replacement with modified units. 

The unsafe condition is failure of the servomotors, which could result in roll 

oscillations or possible hard-over failures 

when the autopilot is engaged. 

Actions and Compliance 

(f) Unless already done, do the following 

actions. 


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Federal Register / Vol. 74, No. 196 / Tuesday, October 13, 2009 / Rules and Regulations 52393 

(1) Within 2 months after the effective date 

of this AD: Identify affected servo-motors 

having P/N 4006719–904 and P/N 4006719– 

913 and modify each unit or replace with a 

modified unit, in accordance with the 

instructions of EADS–CASA Service Bulletin 

SB–212–22–16, dated March 13, 2006. 

(2) As of the effective date of this AD, no 

person may install, on any airplane, a servomotor having P/N 4006719–904 or 4006719– 

913, and any affected serial number 

identified in Honeywell Alert Service 

Bulletin 4006719–22–A0016, Revision 001, 

dated November 1, 2004 (referenced in 

EADS–CASA Service Bulletin SB–212–22– 

16, dated March 13, 2006, as the source of 

service information for accomplishing the 

modification), unless it has been modified in 

accordance with paragraph (f)(1) of this AD. 

Note 1: The 8 digit serial number specified 

in Honeywell Alert Service Bulletin 

4006719–22–A0016, Revision 001, dated 

November 1, 2004, is a combination date 

code and serial number. The format is as 

follows: YYMMXXXX—YY is the year; MM 

is the month, and XXXX is a sequential 

manufacturing serial number (e.g., a unit 

with number 0111XXXX was manufactured 

in November 2001). 

FAA AD Differences 

Note 2: This AD differs from the MCAI 

and/or service information as follows: No 

differences. 

Other FAA AD Provisions 

(g) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, FAA, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

Send information to ATTN: Shahram 

Daneshmandi, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue, SW., Renton, Washington 98057– 

3356; telephone (425) 227–1112; fax (425) 

227–1149. Before using any approved AMOC 

on any airplane to which the AMOC applies, 

notify your principal maintenance inspector 

(PMI) or principal avionics inspector (PAI), 

as appropriate, or lacking a principal 

inspector, your local Flight Standards District 

Office. 

(2) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, under the 

provisions of the Paperwork Reduction Act, 

the Office of Management and Budget (OMB) 

has approved the information collection 

requirements and has assigned OMB Control 

Number 2120–0056. 

Related Information 

(h) Refer to MCAI European Aviation 

Safety Agency Airworthiness Directive 2008– 

0144, dated August 1, 2008; EADS–CASA 

Service Bulletin SB–212–22–16, dated March 

13, 2006; and Honeywell Alert Service 

Bulletin 4006719–22–A0016, Revision 001, 

dated November 1, 2004; for related 

information. 

Material Incorporated by Reference 

(i) You must use EADS–CASA Service 

Bulletin SB–212–22–16, dated March 13, 

2006; and Honeywell Alert Service Bulletin 

4006719–22–A0016, Revision 001, dated 

November 1, 2004; as applicable; to do the 

actions required by this AD, unless the AD 

specifies otherwise. (The revision level of 

Honeywell Alert Service Bulletin 4006719– 

22–A0016, Revision 001, dated November 1, 

2004, is indicated only on pages 1 and 2 of 

the document.) 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

this service information under 5 U.S.C. 

552(a) and 1 CFR part 51. 

(2) For service information identified in 

this AD, contact EADS–CASA, Military 

Transport Aircraft Division (MTAD), 

Integrated Customer Services (ICS), 

Technical Services, Avenida de Arago ́n 404, 

28022 Madrid, Spain; telephone +34 91 585 

55 84; fax +34 91 585 55 05; e-mail 

MTA.TechnicalService@casa.eads.net; 

Internet http://www.eads.net. 

(3) You may review copies of the service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue, SW., Renton, 

Washington. For information on the 

availability of this material at the FAA, call 

425–227–1221 or 425–227–1152. 

(4) You may also review copies of the 

service information that is incorporated by 

reference at the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at NARA, call 202–741–6030, or go 

to: http://www.archives.gov/federal_register/ 

code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Renton, Washington, on 

September 18, 2009. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. E9–23507 Filed 10–9–09; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2009–0057; Directorate 

Identifier 85–ANE–25–AD; Amendment 39– 

16037; AD 2009–20–14] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

plc (RR) RB211–535E4 Series Turbofan 

Engines 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: The FAA is superseding an 

existing airworthiness directive (AD) for 

RR RB211–535E4 series turbofan 

engines. That AD currently requires 

initial and repetitive inspections of the 

outer combustion case for cracks and 

possible removal if cracks are found. 

This AD requires the same inspections, 

but requires using RR Mandatory 

Service Bulletin (MSB) RB.211–72– 

7775, Revision 3, dated April 9, 1999. 

This AD results from the FAA 

approving Revision 3 to the MSB, which 

adds an alternative eddy current 

inspection (ECI) method. We are issuing 

this AD to prevent an uncontained outer 

combustion case burst, which could 

result in damage to the airplane. 

DATES: This AD becomes effective 

November 17, 2009. The Director of the 

Federal Register approved the 

incorporation by reference of certain 

publications listed in the regulations as 

of November 17, 2009. 

ADDRESSES: You can get the service 

information identified in this AD from 

Rolls-Royce plc, P.O. Box 31, Derby, 

DE24 8BJ, United Kingdom; telephone: 

44 (0) 1332–242424; fax: 44 (0) 1332– 

249936. 

The Docket Operations office is 

located at Docket Management Facility, 

U.S. Department of Transportation, 1200 

New Jersey Avenue, SE., West Building 

Ground Floor, Room W12–140, 

Washington, DC 20590–0001. 

FOR FURTHER INFORMATION CONTACT: Ian 

Dargin, Aerospace Engineer, Engine 

Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

e-mail: ian.dargin@faa.gov; telephone 

(781) 238–7178; fax (781) 238–7199. 

SUPPLEMENTARY INFORMATION: The FAA 

proposed to amend 14 CFR part 39 by 

superseding AD 86–07–01, Amendment 

39–5273 (51 FR 12511, April 11, 1986), 

with a proposed AD. The proposed AD 

applies to RR RB211–535E4 series 

turbofan engines. We published the 

proposed AD in the Federal Register on 

February 12, 2009, (74 FR 7002). 

Airworthiness directive 86–07–01 

requires initial and repetitive 

inspections of the combustor case welds 

using RR MSB RB.211–72–7775, dated 

June 28, 1985. The NPRM to supersede 

AD 86–07–01 proposed to require the 

same inspections, but proposed to 

require using RR Mandatory Service 

Bulletin (MSB) RB.211–72–7775, 

Revision 3, dated April 9, 1999. 


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