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prevent providers from determining, at the time the required disclosures must be provided, the exact exchange rate on the date of availability for a transfer involving a currency exchange.

The Final Rule explains that a remittance transfer provider may rely on this list, unless the provider has information that a country’s laws or the method by which transactions are conducted in that country permits a determination of the exact disclosure
amount. See 12 CFR 1005.32(b)(1)(ii) and comment 32(b)(1)–2 (containing examples of when this exception does and does not apply). For example, for transfers to Aruba and Brazil, the Bureau believes that a remittance transfer provider can only rely on the list when the sender funds a transfer in
a currency other than the local currency (i.e., not the Aruban florin and the Brazilian real, respectively), and the transfer is exchanged into the local currency in the foreign country as opposed to being exchanged in the United States. The Bureau believes that exception is limited to such scenarios because under Brazil’s and Aruba’s laws the exchange rate is set when a transfer is picked up only where the transfer is funded in a foreign currency and is then exchanged into the local currency in Brazil or Aruba, respectively. In addition to the Bureau’s list, the Final Rule permits providers to make their own determinations that the laws of other recipient countries or the method of sending transfers to recipient countries, which are not on the list, do not permit a determination of exact
amounts. See 12 CFR 1005.32(b)(1)(i).

This list is subject to change. As applicable, the Bureau will publish revisions to the list on its Web site and in the Federal Register . To facilitate compliance when the Final Rule goes into effect, the Bureau will not remove any countries on this version of the list before July 1, 2014. Furthermore, if the Bureau believes that it may be appropriate to remove a country or area from the list, the Bureau will provide 90-days advance notice.

The Bureau will next review the list in spring 2014. To have your suggestions or input considered for the Bureau’s next review, please send your feedback on whether the Bureau should make changes to the list and any supporting materials (in English) on or before March 17, 2014 to:

— CFPB

_ CountriesList@CFPB.gov or —Office of the Executive Secretary,

Bureau of Consumer Financial Protection, 1700 G Street NW., Washington, DC 20552. To receive an alert when the Bureau releases a revised countries list, please sign up for email updates at http://www.consumerfinance.gov/remittancestransfer-rule-amendment-toregulation-e/

.

Dated: October 24, 2013. Christopher D’Angelo, Chief of Staff, Bureau of Consumer Financial Protection.
[FR Doc. 2013–25754 Filed 11–4–13; 8:45 am]

**BILLING CODE 4810–AM–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2013–0488; Directorate Identifier 2008–SW–002–AD; Amendment**  **39–17619; AD 2013–20–13]**

**RIN 2120–AA64**

**Airworthiness Directives; Bell Helicopter Textron Canada Limited**  **(Bell) Helicopters**

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

**ACTION :**  Final rule.

**SUMMARY :**  We are adopting a new airworthiness directive (AD) for certain Bell Model 206B and 206L helicopters. This AD requires installing a placard beneath the engine power dual tachometer and revising the operating limitations section of the rotorcraft flight manual (RFM). This AD was prompted by several incidents of third stage engine turbine wheel failures, which were caused by excessive vibrations at certain engine speeds during steady-state operations. These actions are intended to alert pilots to avoid certain engine speeds during steady-state operations, prevent failure of the third stage engine turbine, engine power loss, and subsequent loss of control of the helicopter.

**DATES :**  This AD is effective December 10, 2013.

The Director of the Federal Register approved the incorporation by reference of a certain document listed in this AD as of December 10, 2013.

**ADDRESSES :**  For service information identified in this AD, contact Bell Helicopter Textron Canada Limited, 12,800 Rue de l’Avenir, Mirabel, Quebec J7J1R4; telephone (450) 437–2862 or (800) 363–8023; fax (450) 433–0272; or
at http://www.bellcustomer.com/files/. You may review the referenced service information at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137. 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 this AD, the foreignauthority’s AD, any incorporated-byreference service information, the economic evaluation, any comments received, and other information. The street address for the Docket Operations Office (phone: 800–647–5527) is U.S. Department of Transportation, Docket Operations Office, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590.

**FOR FURTHER INFORMATION CONTACT :**  Chinh Vuong, Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222–5110; email chinh.vuong@ faa.gov.

**SUPPLEMENTARY INFORMATION :** 

Discussion

On June 7, 2013, at 78 FR 34280, the Federal Register published our notice of proposed rulemaking (NPRM), which proposed to amend 14 CFR part 39 by adding an AD that would apply to Bell Model 206B helicopters, serial number (S/N) 004 through 4675, including helicopters converted from Model 206A and Model 206L helicopters, S/N 45001 through 45153, and 46601 through 46617. The NPRM proposed to require installing a placard on the instrument panel below the NR/N2 dual tachometer and revising the Operating Limitations section of the Model 206B RFM and 206L RFM to limit steady-state operation between speeds of 75% and 88%. The proposed requirements were intended to alert pilots to avoid certain engine speeds during steady-state operations, prevent failure of the third stage engine turbine, engine power loss, and subsequent loss of control of the helicopter.

The NPRM was prompted by AD No. CF–2007–13R2, dated November 10, 2009, issued by Transport Canada Civil Aviation (TCCA), which is the aviation authority for Canada. TCCA issued AD No. CF–2007–13R2 to correct an unsafe condition for certain Model 206B (including those converted from Model 206A) and 206L helicopters. TCCA advises of several failures of third stage turbine wheels used in Rolls Royce 250– C20. According to TCCA, Rolls Royce


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has determined that detrimental vibrations can occur within a particular range of turbine speeds, and may be a contributing factor to these failures. Bell has revised the RFM and has provided a corresponding decal to inform pilots to avoid steady-state operations between 75% and 88% turbine speeds.

The TCCA AD requires amending the RFMs, advising pilots of the change, and installing a decal as described in Bell Alert Service Bulletin (ASB) No. 206– 07–115, Revision C, dated February 4, 2009, for Model 206B helicopters (ASB 206–07–115) and Bell ASB No. 206L– 07–146, Revision B, dated March 3, 2009, for Model 206L helicopters (ASB 206L–07–146).

Comments

After our NPRM (78 FR 34280, June 7, 2013) was published, we received comments from one commenter.
Request

Rolls-Royce Corporation requested that in addition to requiring the placard on the instrument panel, we allow operators the option to temporarily mark the N
r/Np gauge with colored tape, to provide a more visual aide to the pilot for the speed avoidance zone.

We disagree. Marking the glass surface of the gauge can create parallax issues when viewing the avoidance ranges on the gauge, resulting in erroneous readings.

FAA’s Determination

These helicopters have been approved by the aviation authority of Canada and are approved for operation in the United States. Pursuant to our bilateral agreement with Canada, TCCA, its technical representative, has notified us of the unsafe condition described in the TCCA AD. We are issuing this AD because we evaluated all information provided by TCCA, reviewed the relevant information, considered the comment received, and determined the unsafe condition exists and is likely to exist or develop on other helicopters of the same type design and that air safety and the public interest require adopting the AD requirements as proposed.

Differences Between This AD and the TCCA AD

The TCCA AD requires compliance within 10 calendar days, while this AD requires compliance within 30 days.

Related Service Information

Bell has issued ASB 206–07–115 and ASB 206L–07–146, which contain procedures for installing a placard on the instrument panel below the main rotor RPM (Nr)/power turbine RPM (N2) dual tachometer and for inserting the RFM changes into the flight manual. Costs of Compliance

We estimate that this AD will affect 970 helicopters of U.S. Registry. Based on an average labor rate of $85 per hour, we estimate that operators will incur the following costs in order to comply with this AD. Amending the RFM will require about 0.5 work-hour, for a cost per helicopter of about $43 and a cost to U.S. operators of $41,710. Installingthe decal will require about 0.2 workhour and required parts will cost $20, for a cost per helicopter of $37 and a cost to U.S. operators of $35,890. Based on these estimates, the total cost of this AD is $80 per helicopter and $77,600 for the U.S. operator fleet. 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 helicopters identified in this rulemaking action. Regulatory Findings

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 DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979);

(3) Will not affect intrastate aviation in Alaska to the extent that it justifies making a regulatory distinction; 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 an economic evaluation of the estimated costs to comply with this AD and placed it in the AD docket. 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 airworthiness directive (AD):
2013–20–13 Bell Helicopter Textron Canada Limited (Bell): Amendment 39– 17619; Docket No. FAA–2013–0488; Directorate Identifier 2008–SW–002–AD.
(a) Applicability

This AD applies to the following helicopters, certificated in any category:

(1) Bell Model 206B, serial number (S/N) 004 through 4675, including helicopters converted from Model 206A; and

(2) Bell Model 206L, S/N 45001 through 45153, and 46601 through 46617.
(b) Unsafe Condition

This AD defines the unsafe condition as a third stage turbine vibration, which could result in turbine failure, engine power loss, and subsequent loss of control of the helicopter.
(c) Effective Date

This AD becomes effective December 10,
2013. (d) Compliance

You are responsible for performing each action required by this AD within the specified compliance time unless it has already been accomplished prior to that time.
(e) Required Actions

Within 30 days: (1) For Model 206B helicopters: (i) Revise the Operating Limitations section of the Model 206B Rotorcraft Flight Manual (RFM) by inserting Section 1, Operating Limitations, page 1–2A, of Bell BHT–206B– FM–1, revision B–50, dated December 8,
2008.

(ii) Remove placard part number (P/N) 230–075–213–121, if installed.

(iii) Install placard P/N 230–075–213–125, or equivalent, on the instrument panel directly below the dual tachometer.

(2) For Model 206L helicopters:


### 66254 Federal Register / Vol. 78, No. 214 / Tuesday, November 5, 2013 / Rules and Regulations

(i) Revise the Operating Limitations section of the Model 206L RFM by inserting Section 1, Operating Limitations, page 1–4B, of Bell BHT–206L–FM–1, revision 28, dated December 8, 2008.

(ii) Remove placard P/N 230–075–213–123, if installed.

(ii) Install placard P/N 230–075–213–127, or equivalent, on the instrument panel below the dual tachometer.
(f) Alternative Methods of Compliance (AMOCs)

(1) The Manager, Safety Management Group, FAA, may approve AMOCs for this AD. Send your proposal to: Chinh Vuong, Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222–5110; email chinh.vuong@faa.gov.

(2) For operations conducted under a 14 CFR part 119 operating certificate or under 14 CFR part 91, subpart K, we suggest that you notify your principal inspector, or lacking a principal inspector, the manager of the local flight standards district office or certificate holding district office, before operating any aircraft complying with this AD through an AMOC.
(g) Additional Information

(1) Bell Alert Service Bulletin (ASB) No. 206–07–115, Revision C, dated February 4, 2009, and Bell ASB No. 206L–07–146, Revision B, dated March 3, 2009, which are not incorporated by reference, contain additional information about the subject of this AD. For service information identified in this AD, contact Bell Helicopter Textron Canada Limited, 12,800 Rue de l’Avenir, Mirabel, Quebec J7J1R4; telephone (450) 437–2862 or (800) 363–8023; fax (450) 433– 0272; or at http://www.bellcustomer.com/ files/. You may review a copy of the service information at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137.

(2) The subject of this AD is addressed in Transport Canada Civil Aviation (TCCA) AD No. CF–2007–13R2, dated December 9, 2009. You may view the TCCA AD on the internet in the AD Docket at http:// www.regulations.gov.
(h) Subject

Joint Aircraft Service Component (JASC) Code: 7250: Turbine Section.
(i) Material Incorporated by Reference

(1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.

(i) Page 1–2A of Section 1, Operating Limitations, of Bell Rotorcraft Flight Manual BHT–206B–FM–1, Revision B–50, dated December 8, 2008.

(ii) Page 1–4B of Section 1, Operating Limitations, of Bell Rotorcraft Flight Manual BHT–206L–FM–1, Revision 28, dated December 8, 2008. (3) For Bell service information identified in this AD, contact Bell Helicopter Textron Canada Limited, 12,800 Rue de l’Avenir, Mirabel, Quebec J7J1R4; telephone (450) 437–2862 or (800) 363–8023; fax (450) 433– 0272; or at http://www.bellcustomer.com/ files/.

(4) You may view this service information at FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137. For information on the availability of this material at the FAA, call (817) 222–5110.

(5) You may view this 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/cfr/ibrlocations.html.

Issued in Fort Worth, Texas, on September 25, 2013. Lance T. Gant, Acting Directorate Manager, Rotorcraft Directorate, Aircraft Certification Service.

[FR Doc. 2013–24037 Filed 11–4–13; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2013–0328; Directorate Identifier 2012–NM–184–AD; Amendment**  **39–17643; AD 2013–22–11]**

**RIN 2120–AA64**

**Airworthiness Directives; The Boeing Company Airplanes** 

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

**ACTION :**  Final rule.

**SUMMARY :**  We are superseding Airworthiness Directive (AD) 2009–10– 06 for certain The Boeing Company Model 747–400 and –400D series airplanes. AD 2009–10–06 required repetitive inspections to detect cracks in the floor panel attachment fastener holes of the Section 41 upper deck floor beam upper chords, and correctiveactions if necessary; and repetitive postrepair and post-modification inspections, and corrective actions if necessary. This new AD adds repetitive inspections of Section 44 upper deck floor beam upper chords, and correctiveactions if necessary; repetitive postrepair and post-modification inspections, and corrective actions if necessary; and replacement of the upper deck floor beam upper chords. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that certain upper chords of the upper deck floor beam are subject to widespread fatigue damage (WFD). We are issuing this AD to detect and correct fatigue cracking in certain upper chords of the upper deck floor beam, which could become large and cause the floor beams to become severed and result in rapid decompression or reduced controllability of the airplane.

**DATES :**  This AD is effective December 10, 2013.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of December 10, 2013.

The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of June 17, 2009 (74 FR 22424, May 13, 2009).

**ADDRESSES :**  For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H–65, Seattle, WA 98124–2207; telephone 206–544–5000, extension 1; fax 206–766–5680; Internet https:// www.myboeingfleet.com. You may view this referenced service information at the FAA, 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; 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 :**  Bill Ashforth, Aerospace Engineer, Airframe Branch, ANM–120S, FAA, Seattle ACO, 1601 Lind Avenue SW., Renton, WA 98057–3356; phone: 425–917–6432; fax: 425–917–6590; email: bill.ashforth@ faa.gov.

**SUPPLEMENTARY INFORMATION :** 

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2009–10–06, Amendment 39–15901 (74 FR 22424, May 13, 2009). AD 2009–10–06 applied to the specified products. The NPRM published in the Federal Register on