### 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.

2 Full 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,


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

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.


### 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