Federal Register / Vol. 75, No. 156 / Friday, August 13, 2010 / Rules and Regulations 49365

VII. Small Business Regulatory published after January 1, 2000. The ■ For the reasons stated above, the Enforcement Fairness Act FDIC has sought to present the final rule Board of Directors of the Federal in a simple and straightforward manner. Deposit Insurance Corporation hereby The Office of Management and Budget amends parts 328, 330, and 347 of title has determined that the final rule is not List of Subjects 12 of the Code of Federal Regulations as a ‘‘major rule’’ within the meaning of the 12 CFR Part 328 follows: relevant sections of the Small Business Regulatory Enforcement Act of 1996 Advertising, Bank deposit insurance, Savings associations, Signs and PART 328—ADVERTISEMENT OF (‘‘SBREFA’’) (5 U.S.C. 801 et seq.). As MEMBERSHIP required by SBREFA, the FDIC will file symbols. the appropriate reports with Congress 12 CFR Part 330 ■ 1. The authority citation for part 328 and the General Accounting Office so Bank deposit insurance, Banks, continues to read as follows: that the final rule may be reviewed. Banking, Reporting and recordkeeping Authority: 12 U.S.C. 1818(a), 1813(m), VIII. Plain Language requirements, Savings and loan 1819 (Tenth), 1828(a). associations, Trusts and trustees. Section 722 of the Gramm-Leach- ■ 2. In § 328.1, paragraph (a) is amended Blilely Act (Pub. L. 106–102, 113 Stat. 12 CFR Part 347 by revising the graphic image of the 1338, 1471), requires the Federal Bank deposit insurance, Banks, banking agencies to use plain language Banking, International banking; Foreign official sign to appear as follows: in all proposed and final rules banks. (a) * * *

* * * * * Authority: 12 U.S.C. 1813, 1815, 1817, DEPARTMENT OF TRANSPORTATION 1819, 1820, 1828, 3103, 3104, 3105, 3108, PART 330—DEPOSIT INSURANCE 3109; Title IX, Pub. L. 98–181, 97 Stat. 1153. Federal Aviation Administration COVERAGE ■ 6. In § 347.202, paragraph (v) is 14 CFR Part 39 ■ 3. The authority citation for part 330 revised to read as follows: continues to read as follows: [Docket No. FAA–2010–0434; Directorate Authority: 12 U.S.C. 1813(1), 1813(m), § 347.202 Definitions. Identifier 2009–NM–221–AD; Amendment 1817(i), 1818(q), 1819 (Tenth), 1820(f), * * * * * 39–16386; AD 2010–16–09] 1821(a), 1822(c). (v) Standard maximum deposit RIN 2120–AA64 ■ 4. In § 330.1, paragraph (n) is revised insurance amount, referred to as the to read as follows: ‘‘SMDIA’’ hereafter, means $250,000 Airworthiness Directives; BAE Systems (Operations) Limited Model adjusted pursuant to subparagraph (F) of § 330.1 Definitions. BAe 146–100A and –200A Airplanes section 11(a)(1) of the FDI Act (12 U.S.C. * * * * * (n) Standard maximum deposit 1821(a)(1)(F)). AGENCY: Federal Aviation insurance amount, referred to as the * * * * * Administration (FAA), Department of Transportation (DOT). ‘‘SMDIA’’ hereafter, means $250,000 Dated at Washington DC, this 10th day of adjusted pursuant to subparagraph (F) of August 2010. ACTION: Final rule. section 11(a)(1) of the FDI Act (12 U.S.C. By order of the Board of Directors. 1821(a)(1)(F)). SUMMARY: We are adopting a new Federal Deposit Insurance Corporation. airworthiness directive (AD) for the * * * * * Robert E. Feldman, products listed above. This AD results PART 347—INTERNATIONAL Executive Secretary. from mandatory continuing airworthiness information (MCAI) BANKING [FR Doc. 2010–20008 Filed 8–12–10; 8:45 am] originated by an aviation authority of ■ 5. The authority citation for part 347 BILLING CODE P another country to identify and correct continues to read as follows: an unsafe condition on an aviation

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product. The MCAI describes the unsafe increasingly been exploited in recent years provided in the MCAI and related condition as: by a number of operators worldwide. service information. Frequently, these short field operations are The operation of the airbrake lever in the conducted from airports that are located in We might also have required different ‘‘airbrakes out’’ to ‘‘lift ’’ range has been mountainous terrain or in close proximity to actions in this AD from those in the the subject of two occurrence reports. The lift bodies of water, leaving fewer margins for MCAI in order to follow our FAA spoilers on the BAe 146 and 146–RJ error, e.g. long or at (too) high speed. policies. Any such differences are aeroplanes have been designed to deploy on The effects of deceleration and landing highlighted in a Note within the AD. landing to provide aerodynamic braking and inertia loads can cause uncommanded to dump lift to ensure that the wheel brakes movement of the airbrake selector lever from Costs of Compliance can provide the necessary speed reduction. ‘‘ ’’ ‘‘ the lift spoiler position to the airbrakes We estimate that this AD will affect * * * * * out’’ position, causing the lift spoilers to retract during the landing roll. This 1 product of U.S. registry. We also The effects of deceleration and landing estimate that it will take about 11 work- inertia loads can cause uncommanded condition, if not corrected, would increase the landing distance, possibly resulting in a hours per product to comply with the movement of the airbrake selector lever from basic requirements of this AD. The the ‘‘lift spoiler’’ position to the ‘‘airbrakes runway overrun and consequent injury to out’’ position, causing the lift spoilers to aeroplane occupants. average labor rate is $85 per work-hour. retract during the landing roll. This On certain BAe 146 aeroplanes, without Required parts will cost about $7,000 condition, if not corrected, would increase modifications HCM00889A and B or per product. Where the service the landing distance, possibly resulting in a modifications HCM00889A and C information lists required parts costs runway overrun and consequent injury to incorporated, negligible force is required to ‘‘ that are covered under warranty, we aeroplane occupants. move the airbrake lever back to the airbrakes out’’ position. From 1988 onwards, have assumed that there will be no * * * * * modifications were introduced on the charge for these parts. As we do not We are issuing this AD to require production line to incorporate a modified control warranty coverage for affected actions to correct the unsafe condition friction baulking device such that a force of parties, some parties may incur costs on these products. 12 lbs must be applied to move the airbrake higher than estimated here. Based on DATES: This AD becomes effective lever from the ‘‘lift spoiler’’ position to the these figures, we estimate the cost of ‘‘ ’’ September 17, 2010. airbrakes out position. These modifications this AD to the U.S. operator to be were also made available as an optional in- $7,935. The Director of the Federal Register service retrofit. approved the incorporation by reference For the reasons described above, this AD Authority for This Rulemaking of a certain publication listed in this AD requires the modification of the airbrake as of September 17, 2010. lever detent mechanism. Title 49 of the United States Code specifies the FAA’s authority to issue ADDRESSES: You may examine the AD You may obtain further information by rules on aviation safety. Subtitle I, docket on the Internet at http:// examining the MCAI in the AD docket. www.regulations.gov or in person at the section 106, describes the authority of U.S. Department of Transportation, Comments the FAA Administrator. ‘‘Subtitle VII: Docket Operations, M–30, West We gave the public the opportunity to Aviation Programs,’’ describes in more Building Ground Floor, Room W12–140, participate in developing this AD. We detail the scope of the Agency’s 1200 New Jersey Avenue, SE., received no comments on the NPRM or authority. Washington, DC. on the determination of the cost to the We are issuing this rulemaking under FOR FURTHER INFORMATION CONTACT: public. the authority described in ‘‘Subtitle VII, Part A, Subpart III, Section 44701: Todd Thompson, Aerospace Engineer, Explanation of Change to Applicability International Branch, ANM–116, General requirements.’’ Under that Transport Airplane Directorate, FAA, We have revised the applicability of section, Congress charges the FAA with 1601 Lind Avenue, SW., Renton, the existing AD to identify model promoting safe flight of civil aircraft in Washington 98057–3356; telephone designations as published in the most air commerce by prescribing regulations (425) 227–1175; fax (425) 227–1149. recent type certificate data sheet for the for practices, methods, and procedures affected models. SUPPLEMENTARY INFORMATION: the Administrator finds necessary for Conclusion safety in air commerce. This regulation Discussion is within the scope of that authority We reviewed the available data, and We issued a notice of proposed because it addresses an unsafe condition determined that air safety and the rulemaking (NPRM) to amend 14 CFR that is likely to exist or develop on public interest require adopting the AD part 39 to include an AD that would products identified in this rulemaking with the changes described previously. apply to the specified products. That action. We determined that these changes will NPRM was published in the Federal not increase the economic burden on Regulatory Findings Register on April 30, 2010 (75 FR any operator or increase the scope of the 22710). That NPRM proposed to correct We determined that this AD will not AD. an unsafe condition for the specified have federalism implications under products. The MCAI states: Differences Between This AD and the Executive Order 13132. This AD will The operation of the airbrake lever in the MCAI or Service Information not have a substantial direct effect on ‘‘airbrakes out’’ to ‘‘lift spoiler’’ range has been We have reviewed the MCAI and the States, on the relationship between the subject of two occurrence reports. The lift related service information and, in the national government and the States, spoilers on the BAe 146 and Avro 146–RJ general, agree with their substance. But or on the distribution of power and aeroplanes have been designed to deploy on we might have found it necessary to use responsibilities among the various landing to provide aerodynamic braking and different words from those in the MCAI levels of government. to dump lift to ensure that the wheel brakes For the reasons discussed above, I can provide the necessary speed reduction. to ensure the AD is clear for U.S. A review of the changing operational operators and is enforceable. In making certify this AD: profile of the aeroplane type concluded that these changes, we do not intend to differ 1. Is not a ‘‘significant regulatory its proven short field performance has substantively from the information action’’ under Executive Order 12866;

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2. Is not a ‘‘significant rule’’ under the Subject FAA AD Differences DOT Regulatory Policies and Procedures (d) Air Transport Association (ATA) of Note 1: This AD differs from the MCAI (44 FR 11034, February 26, 1979); and America Code 27: Flight Controls. and/or service information as follows: While 3. Will not have a significant Reason European Aviation Safety Agency (EASA) AD economic impact, positive or negative, (e) The mandatory continuing 2009–0206, dated September 30, 2009, on a substantial number of small entities airworthiness information (MCAI) states: considers Revision 0, 1, or 2 of 146 Modification Service Bulletin under the criteria of the Regulatory The operation of the airbrake lever in the 27–73–00889A&B as an acceptable method of Flexibility Act. ‘‘airbrakes out’’ to ‘‘lift spoiler’’ range has been compliance, this AD does not. However, We prepared a regulatory evaluation the subject of two occurrence reports. The lift spoilers on the BAe 146 and Avro 146–RJ operators may request approval of an of the estimated costs to comply with alternative method of compliance in this AD and placed it in the AD docket. aeroplanes have been designed to deploy on landing to provide aerodynamic braking and accordance with the procedures specified in Examining the AD Docket to dump lift to ensure that the wheel brakes paragraph (h)(1) of this AD. can provide the necessary speed reduction. You may examine the AD docket on A review of the changing operational Other FAA AD Provisions the Internet at http:// profile of the aeroplane type concluded that (h) The following provisions also apply to www.regulations.gov; or in person at the its proven short field performance has this AD: Docket Operations office between 9 a.m. increasingly been exploited in recent years (1) Alternative Methods of Compliance by a number of operators worldwide. and 5 p.m., Monday through Friday, (AMOCs): The Manager, International Frequently, these short field operations are Branch, ANM–116, Transport Airplane except Federal holidays. The AD docket conducted from airports that are located in contains the NPRM, the regulatory Directorate, FAA, has the authority to mountainous terrain or in close proximity to approve AMOCs for this AD, if requested evaluation, any comments received, and bodies of water, leaving fewer margins for using the procedures found in 14 CFR 39.19. error, e.g. landing long or at (too) high speed. other information. The street address for Send information to Attn: Todd Thompson, The effects of deceleration and landing the Docket Operations office (telephone Aerospace Engineer, International Branch, inertia loads can cause uncommanded (800) 647–5527) is in the ADDRESSES ANM–116, Transport Airplane Directorate, section. Comments will be available in movement of the airbrake selector lever from the ‘‘lift spoiler’’ position to the ‘‘airbrakes FAA, 1601 Lind Avenue, SW., Renton, the AD docket shortly after receipt. out’’ position, causing the lift spoilers to Washington 98057–3356; telephone (425) 227–1175; fax (425) 227–1149. Before using List of Subjects in 14 CFR Part 39 retract during the landing roll. This condition, if not corrected, would increase any approved AMOC on any airplane to Air transportation, Aircraft, Aviation the landing distance, possibly resulting in a which the AMOC applies, notify your safety, Incorporation by reference, runway overrun and consequent injury to principal maintenance inspector (PMI) or Safety. aeroplane occupants. principal avionics inspector (PAI), as On certain BAe 146 aeroplanes, without appropriate, or lacking a principal inspector, Adoption of the Amendment modifications HCM00889A and B or your local Flight Standards District Office. modifications HCM00889A and C The AMOC approval letter must specifically ■ Accordingly, under the authority incorporated, negligible force is required to reference this AD. delegated to me by the Administrator, move the airbrake lever back to the ‘‘airbrakes (2) Airworthy Product: For any requirement the FAA amends 14 CFR part 39 as out’’ position. From 1988 onwards, in this AD to obtain corrective actions from modifications were introduced on the a manufacturer or other source, use these follows: production line to incorporate a modified actions if they are FAA-approved. Corrective friction baulking device such that a force of actions are considered FAA-approved if they PART 39—AIRWORTHINESS 12 lbs must be applied to move the airbrake DIRECTIVES lever from the ‘‘lift spoiler’’ position to the are approved by the State of Design Authority ‘‘airbrakes out’’ position. These modifications (or their delegated agent). You are required ■ 1. The authority citation for part 39 were also made available as an optional in- to assure the product is airworthy before it continues to read as follows: service retrofit. is returned to service. For the reasons described above, this AD (3) Reporting Requirements: For any Authority: 49 U.S.C. 106(g), 40113, 44701. requires the modification of the airbrake reporting requirement in this AD, under the § 39.13 [Amended] lever detent mechanism. provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et seq.), the Office of Compliance ■ 2. The FAA amends § 39.13 by adding Management and Budget (OMB) has the following new AD: (f) You are responsible for having the approved the information collection actions required by this AD performed within requirements and has assigned OMB Control 2010–16–09 BAE Systems (Operations) the compliance times specified, unless the Number 2120–0056. Limited: Amendment 39–16386. Docket actions have already been done. No. FAA–2010–0434; Directorate Related Information Actions Identifier 2009–NM–221–AD. (i) Refer to MCAI EASA Airworthiness (g) Do the following actions. Directive 2009–0206, dated September 30, Effective Date (1) Within 12 months after the effective 2009; and (a) This airworthiness directive (AD) date of this AD, modify the airbrake lever becomes effective September 17, 2010. detent mechanism, in accordance with the Modification Service Bulletin 27–73– Accomplishment Instructions of British 00889A&B, Revision 4, dated June 15, 1990; Affected ADs Aerospace 146 Modification Service Bulletin for related information. (b) None. 27–73–00889A&B, Revision 4, dated June 15, Material Incorporated by Reference 1990. Applicability (2) Modifying the airbrake lever detent (j) You must use British Aerospace 146 (c) This AD applies to BAE Systems mechanism is also acceptable for compliance Modification Service Bulletin 27–73– (Operations) Limited Model BAe 146–100A with paragraph (g)(1) of this AD, if done 00889A&B, Revision 4, dated June 15, 1990, and –200A airplanes, certificated in any before the effective date of this AD, in to do the actions required by this AD, unless category, serial numbers as listed in British accordance with the Accomplishment the AD specifies otherwise. British Aerospace Aerospace 146 Modification Service Bulletin Instructions of British Aerospace 146 146 Modification Service Bulletin 27–73– 27–73–00889A&B, Revision 4, dated June 15, Modification Service Bulletin 27–73– 00889A&B, Revision 4, contains the 1990. 00889A&B, Revision 3, dated August 1, 1989. following effective pages:

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Revision level Date Page No. shown on page shown on page

1, 3–4, 7, 15–16, 19 ...... 4 June 15, 1990. 2 ...... 3 August 1, 1989. 5, 8–12, 17–18, 20 ...... 1 August 10, 1988. 6, 13–14 ...... 2 June 27, 1989.

(1) The Director of the Federal Register issued by an aviation authority of and 5 p.m., Monday through Friday, approved the incorporation by reference of another country to identify and correct except Federal holidays. The AD docket this service information under 5 U.S.C. an unsafe condition on an aviation contains this AD, the regulatory 552(a) and 1 CFR part 51. product. The MCAI describes the unsafe evaluation, any comments received, and (2) For service information identified in this AD, contact BAE Systems (Operations) condition as: other information. The street address for Limited, Customer Information Department, Wear, beyond Engine Manual limits, has the Docket Operations office (telephone Prestwick International Airport, Ayrshire, been identified on the abutment faces of the (800) 647–5527) is the same as the Mail KA9 2RW, Scotland, United Kingdom; splines on the Trent 900 Intermediate address provided in the ADDRESSES telephone +44 1292 675207; fax +44 1292 Pressure (IP) shaft rigid coupling on several section. Comments will be available in 675704; e-mail engines during strip. The shaft to coupling the AD docket shortly after receipt. [email protected]; Internet spline interface provides the means of http://www.baesystems.com/Businesses/ controlling the turbine axial setting and wear FOR FURTHER INFORMATION CONTACT: Ian RegionalAircraft/index.htm. through of the splines would permit the IP Dargin, Aerospace Engineer, Engine (3) You may review copies of the service turbine to move rearwards. Certification Office, FAA, Engine and information at the FAA, Transport Airplane Rearward movement of the IP turbine Directorate, 12 New England Directorate, 1601 Lind Avenue, SW., Renton, would enable contact with static turbine Executive Park; Burlington, MA 01803; Washington. For information on the components and would result in loss of e-mail: [email protected]; telephone availability of this material at the FAA, call engine performance with potential for in- (781) 238–7178; fax (781) 238–7199. 425–227–1221. flight shut down, oil migration and oil fire (4) You may also review copies of the below the LP turbine discs prior to sufficient SUPPLEMENTARY INFORMATION: service information that is incorporated by indication resulting in loss of LP turbine disc Discussion reference at the National Archives and integrity. Records Administration (NARA). For We are issuing this AD to detect The European Aviation Safety Agency information on the availability of this rearward movement of the IP turbine, (EASA), which is the Technical Agent material at NARA, call 202–741–6030, or go for the Member States of the European to: http://www.archives.gov/federal_register/ which could result in loss of disc _ _ _ integrity, an uncontained failure of the Community, has issued EASA code of federal regulations/ Airworthiness Directive 2010–0008, ibr_locations.html. engine, and damage to the airplane. DATES: This AD becomes effective dated January 15, 2010 (referred to after Issued in Renton, Washington, on July 28, this as ‘‘the MCAI’’), to correct an unsafe 2010. September 17, 2010. We must receive comments on this condition for the specified products. Ali Bahrami, AD by September 13, 2010. The MCAI states: Manager, Transport Airplane Directorate, The Director of the Federal Register Wear, beyond Engine Manual limits, has Aircraft Certification Service. approved the incorporation by reference been identified on the abutment faces of the [FR Doc. 2010–19329 Filed 8–12–10; 8:45 am] of Rolls-Royce Trent 900 Series splines on the Trent 900 Intermediate BILLING CODE 4910–13–P Propulsion Systems Alert Non- Pressure (IP) shaft rigid coupling on several Modification Service Bulletin (NMSB) engines during strip. The shaft to coupling RB.211–72–AG329, Revision 1, dated spline interface provides the means of DEPARTMENT OF TRANSPORTATION controlling the turbine axial setting and wear January 13, 2010, listed in the AD as of through of the splines would permit the IP Federal Aviation Administration September 17, 2010. turbine to move rearwards. ADDRESSES: You may send comments by Rearward movement of the IP turbine 14 CFR Part 39 any of the following methods: would enable contact with static turbine • Federal eRulemaking Portal: Go to components and would result in loss of [Docket No. FAA–2010–0748; Directorate http://www.regulations.gov and follow engine performance with potential for in- Identifier 2010–NE–13–AD; Amendment 39– the instructions for sending your flight shut down, oil migration and oil fire 16384; AD 2010–16–07] comments electronically. below the LP turbine discs prior to sufficient • indication resulting in loss of LP turbine disc RIN 2120–AA64 Mail: U.S. Department of Transportation, 1200 New Jersey integrity. This AD requires inspection of the IP shaft Airworthiness Directives; Rolls-Royce Avenue, SE., West Building Ground coupling splines and, depending on the plc (RR) RB211–Trent 900 Series Floor, Room W12–140, Washington, DC results, requires further repetitive inspections Engines 20590–0001. or corrective actions. • Hand Delivery: Deliver to Mail AGENCY: Federal Aviation address above between 9 a.m. and 5 You may obtain further information by Administration (FAA), DOT. p.m., Monday through Friday, except examining the MCAI in the AD docket. ACTION: Final rule; request for Federal holidays. Relevant Service Information comments. • Fax: (202) 493–2251. Rolls-Royce plc has issued RB211 SUMMARY: We are adopting a new Examining the AD Docket Trent 900 Series Propulsion Systems airworthiness directive (AD) for the You may examine the AD docket on Alert NMSB RB.211–72–AG329, products listed above. This AD results the Internet at http:// Revision 1, dated January 13, 2010. The from mandatory continuing www.regulations.gov; or in person at the actions described in this service airworthiness information (MCAI) Docket Operations office between 9 a.m. information are intended to correct the

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