26154 Federal Register / Vol. 77, No. 86 / Thursday, May 3, 2012 / Rules and Regulations 

The NRC application fee for an access authorization of 

type . . . 

Is the sum of the current OPM investigation billing rate 

charged for an investigation of type . . . 

Plus the NRC’s processing 

fee (rounded to the nearest 

dollar), which is equal to the 

OPM investigation billing rate 

for the type of investigation 

referenced multiplied by . . . 

Initial ‘‘L’’ access authorization 1 ..................................... ANACI—Access National Agency Check with Inquiries 

(Standard Service, Code C).

55.8% 

Reinstatement of ‘‘L’’ access authorization 2 .................. No fee assessed for most applications .......................... ................................................

Renewal of ‘‘L’’ access authorization 1 ........................... NACLC—Access National Agency Check with Law and 

Credit (Standard Service, Code C).

55.8% 

Initial ‘‘Q’’ access authorization ...................................... SSBI—Single Scope Background Investigation (Standard Service, Code C).55.8% 

Initial ‘‘Q’’ access authorization (expedited processing) SSBI—Single Scope Background Investigation (Priority 

Handling, Code A).

55.8% 

Reinstatement of ‘‘Q’’ access authorization 2 ................. No fee assessed for most applications .......................... ................................................

Renewal of ‘‘Q’’ access authorization 1 .......................... SSBI–PR—Periodic Reinvestigation for SSBI (Standard Service, Code C).55.8% 

1 If the NRC determines, based on its review of available data, that a single scope investigation is necessary, the appropriate fee for an Initial 

‘‘Q’’ access authorization will be assessed before the conduct of investigation. 2Full fee will only be charged if an investigation is required. 

Dated at Rockville, Maryland, this 19th day 

of April 2012. 

For the Nuclear Regulatory Commission. 

R.W. Borchardt, 

Executive Director for Operations. 

[FR Doc. 2012–10711 Filed 5–2–12; 8:45 am] 

BILLING CODE 7590–01–P 

BUREAU OF CONSUMER FINANCIAL 

PROTECTION 

12 CFR Part 1012 

[Docket No. CFPB–2011–0025] 

RIN 3170–AA06 

Interstate Land Sales Registration 

Program, Special Rules of Practice; 

Correction 

AGENCY: Bureau of Consumer Financial 

Protection. 

ACTION: Correcting amendments. 

SUMMARY: The Bureau of Consumer 

Financial Protection published an 

interim final rule on December 21, 2011 

(76 FR 79486), republishing 

implementing regulations under the 

Interstate Land Sales Full Disclosure 

Act (ILSA). The interim final rule 

contained a typographical error, which 

this document corrects. 

DATES: This correcting amendment is 

effective on May 3, 2012. 

FOR FURTHER INFORMATION CONTACT: 

Whitney Patross, Office of Regulations, 

at (202) 435–7700. 

SUPPLEMENTARY INFORMATION: The 

Bureau of Consumer Financial 

Protection (Bureau) published an 

interim final rule republishing and 

making technical and conforming 

amendments to regulations of the 

Department of Housing and Urban 

Development (HUD) in connection with 

the transfer of rulemaking authority for 

ILSA from HUD to the Bureau. The 

interim final rule contained a 

typographical error, which this 

document corrects. The heading of Part 

1012—Special Rules of Practice is 

incorrectly labeled as ‘‘Regulation J’’ 

and should be labeled ‘‘Regulation L.’’ 

List of Subjects in 12 CFR Part 1012 

Advertising disclaimers, Adjudicatory 

proceedings, Certification of 

substantially equivalent state law, Filing 

assistance, Purchasers’ revocation 

rights, Land registration, Reporting 

requirements, Unlawful sales practices. 

Accordingly, 12 CFR Part 1012 is 

amended by making the following 

correcting amendments: 

PART 1012—SPECIAL RULES OF 

PRACTICE (REGULATION L) 

■ 1. The authority citation for part 1012 

continues to read as follows: 

Authority: 12 U.S.C. 5512, 5581; 15 U.S.C. 

1718. 

■ 2. The heading of part 1012 is revised 

to read as set forth above. 

Dated: April 25, 2012. 

Richard Cordray, 

Director, Bureau of Consumer Financial 

Protection. 

[FR Doc. 2012–10602 Filed 5–2–12; 8:45 am] 

BILLING CODE 4810–AM–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–0041; Directorate 

Identifier 2011–NM–167–AD; Amendment 

39–17037; AD 2012–09–02] 

RIN 2120–AA64 

Airworthiness Directives; Airbus 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all 

Airbus Model A300 B2–1C, B2K–3C, 

B2–203, B4–2C, B4–103, and B4–203 

airplanes. This AD was prompted by 

analysis that in a specific failure case of 

the upper primary attachment of the 

trimmable horizontal stabilizer actuator 

(THSA), the THSA upper secondary 

attachment engaged because it could 

only withstand the loads for a limited 

period of time. This AD requires 

installing three secondary retention 

plates for the gimbal bearings on the 

THSA upper primary attachment. We 

are issuing this AD to prevent failure of 

the secondary load path, which could 

result in loss of control of the airplane. 

DATES: This AD becomes effective June 

7, 2012. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of June 7, 2012. 

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, 


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Federal Register / Vol. 77, No. 86 / Thursday, May 3, 2012 / Rules and Regulations 26155 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue SE., 

Washington, DC. 

FOR FURTHER INFORMATION CONTACT: Dan 

Rodina, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue SW., Renton, 

Washington 98057–3356; telephone 

(425) 227–2125; 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 February 6, 2012 (77 FR 

5726). That NPRM proposed to correct 

an unsafe condition for the specified 

products. The MCAI states: 

A specific failure case of the THSA 

[trimmable horizontal stabilizer actuator] 

upper primary attachment, which may result 

in a loading of the upper secondary 

attachment, has been identified by analysis. 

Primary load path failure can be caused by 

bearing migration from the upper attachment 

gimbal by failure or loss of a retention bolt. 

In case of failure of the THSA upper 

primary attachment, the THSA upper 

secondary attachment would engage. Because 

the upper attachment secondary load path 

can only withstand the loads for a limited 

period of time, the condition where it would 

be engaged could lead, if not detected and 

corrected, to the failure of the secondary load 

path, which would likely result in loss of 

control of the aeroplane. 

For the reasons explained above, this 

[EASA] AD requires installation of three 

secondary retention plates for the gimbal 

bearings on the THSA upper primary 

attachment. 

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 (77 

FR 5726, February 6, 2012) 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, except for minor editorial 

changes. We have determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (77 FR 5726, 

February 6, 2012) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (77 FR 5726, 

February 6, 2012). 

Costs of Compliance 

We estimate that this AD will affect 

about 15 products of U.S. registry. We 

also estimate that it will take about 2 

work-hours per product to comply with 

the basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Required parts will cost about $6,541 

per product. Where the service 

information lists required parts costs 

that are covered under warranty, we 

have assumed that there will be no 

charge for these parts. As we do not 

control warranty coverage for affected 

parties, some parties may incur costs 

higher than estimated here. Based on 

these figures, we estimate the cost of 

this AD to the U.S. operators to be 

$100,665, or $6,711 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 that 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); 

3. Will not affect intrastate aviation in 

Alaska; 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. 

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 77 FR 5726, 

February 6, 2012), 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: 

2012–09–02 Airbus: Amendment 39–17037. 

Docket No. FAA–2012–0041; Directorate 

Identifier 2011–NM–167–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective June 7, 2012. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all Airbus Model A300 

B2–1C, B2K–3C, B2–203, B4–2C, B4–103, 

and B4–203 airplanes, certificated in any 

category. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 27: Flight controls. 

(e) Reason 

This AD was prompted by analysis that in 

a specific failure case of the upper primary 

attachment of the trimmable horizontal 

stabilizer actuator (THSA), the THSA upper 

secondary attachment engaged because it 

could only withstand the loads for a limited 

period of time. We are issuing this AD to 

prevent failure of the secondary load path, 

which could result in loss of control of the 

airplane. 


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26156 Federal Register / Vol. 77, No. 86 / Thursday, May 3, 2012 / Rules and Regulations 

(f) Compliance 

You are responsible for having the actions 

required by this AD performed within the 

compliance times specified, unless the 

actions have already been done. 

(g) Actions 

Within 30 months after the effective date 

of this AD, install 3 retention plates for the 

gimbal bearings on the THSA upper primary 

attachment, in accordance with the 

Accomplishment Instructions of Airbus 

Mandatory Service Bulletin A300–27–0204, 

dated March 11, 2011. 

(h) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, FAA, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

In accordance with 14 CFR 39.19, send your 

request to your principal inspector or local 

Flight Standards District Office, as 

appropriate. If sending information directly 

to the International Branch, send it to Attn: 

Dan Rodina, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, Washington 98057– 

3356; telephone (425) 227–2125; fax (425) 

227–1149. Information may be emailed to: 

9-ANM-116-AMOC-REQUESTS@faa.gov. 

Before using any approved AMOC, notify 

your appropriate principal inspector, or 

lacking a principal inspector, the manager of 

the local flight standards district office/ 

certificate holding district office. The AMOC 

approval letter must specifically reference 

this AD. 

(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. 

(i) Related Information 

Refer to MCAI European Aviation Safety 

Agency (EASA) Airworthiness Directive 

2011–0112, dated June 15, 2011; and Airbus 

Mandatory Service Bulletin A300–27–0204, 

dated March 11, 2011; for related 

information. 

(j) Material Incorporated by Reference 

(1) You must use the following service 

information to do the actions required by this 

AD, unless the AD specifies otherwise. The 

Director of the Federal Register approved the 

incorporation by reference (IBR) of the 

following service information under 5 U.S.C. 

552(a) and 1 CFR part 51: 

(i) Airbus Mandatory Service Bulletin 

A300–27–0204, dated March 11, 2011. 

(2) For service information identified in 

this AD, contact Airbus SAS—EAW 

(Airworthiness Office), 1 Rond Point Maurice 

Bellonte, 31707 Blagnac Cedex, France; 

telephone +33 5 61 93 36 96; fax +33 5 61 

93 44 51; email account.airwortheas@airbus.com; Internet http:// 

www.airbus.com. 

(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. 

(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 an NARA facility, 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 April 23, 

2012. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2012–10471 Filed 5–2–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2011–1413; Directorate 

Identifier 2011–NM–062–AD; Amendment 

39–17036; AD 2012–09–01] 

RIN 2120–AA64 

Airworthiness Directives; Cessna 

Aircraft Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Cessna Aircraft Company Model 560XL 

airplanes. This AD was prompted by 

reports of wheel inserts becoming loose 

and damaging brake assemblies on 

Model 560XL airplanes. This AD 

requires an inspection of the torque lug 

and surrounding components (wheel 

base, side rim, lock ring) for damage 

(such as corrosion, cracks, dents, bent 

areas, damaged or missing paint or 

primer, or wear on the metal), and of the 

bearing cup for corrosion, turned cup, or 

clearance that exceeds limits, and repair 

as applicable; measuring the torque lugs 

for width and replacing screws and 

inserts with new, improved screws and 

inserts; and re-identifying the wheel 

assemblies. We are issuing this AD to 

prevent brake failure, which could 

result in an airplane not being able to 

stop on the runway. 

DATES: This AD is effective June 7, 2012. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of June 7, 2012. 

ADDRESSES: For Cessna service 

information identified in this AD, 

contact Cessna Aircraft Co., P.O. Box 

7706, Wichita, Kansas 67277–7706; 

telephone 316–517–6215; fax 316–517– 

5802; email 

citationpubs@cessna.textron.com; 

Internet https:// 

www.cessnasupport.com/newlogin.html. 

For Goodrich service information 

identified in this AD, contact Goodrich 

Corporation, Aircraft Wheels & Brakes, 

P.O. Box 340, Troy, Ohio 45373–3872; 

telephone 937–440–2130; fax 937–440– 

2055; email WBPubsAdmin@goodrich.com; Internet http:// 

www.goodrich.com/TechPubs. You may 

review copies of the referenced 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. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; 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 address for the 

Docket Office (phone: 800–647–5527) is 

Document 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: 

David Fairback, Aerospace Engineer, 

Mechanical Systems and Propulsion 

Branch, ACE–116W, FAA, Wichita 

Aircraft Certification Office, 1801 

Airport Road, Room 100, Mid-Continent 

Airport, Wichita, KS 67209; phone: 

316–946–4154; fax: 316–946–4107; 

email: david.fairback@faa.gov. 

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 published in the Federal 

Register on January 19, 2012 (77 FR 

2659). That NPRM proposed to require 

an inspection of the torque lug and 

surrounding components (wheel base, 

side rim, lock ring) for damage (such as 

corrosion, cracks, dents, bent areas, 

damaged or missing paint or primer, or 

wear on the metal), and of the bearing 


wreier-aviles on DSK7SPTVN1PROD with RULES