21246 Federal Register / Vol. 74, No. 87 / Thursday, May 7, 2009 / Rules and Regulations 

change on which to seek public input, 

the Board has determined that the 

§ 553(b) notice and comment procedures 

are unnecessary. In addition, the 

underlying consolidation of Federal 

Reserve Bank check-processing offices 

involves a matter relating to agency 

management, which is exempt from 

notice and comment procedures. 

Paperwork Reduction Act 

In accordance with the Paperwork 

Reduction Act of 1995 (44 U.S.C. 3506; 

5 CFR 1320 Appendix A.1), the Board 

has reviewed the final rule under 

authority delegated to the Board by the 

Office of Management and Budget. The 

technical amendments to appendix A of 

Regulation CC will (i) delete the 

reference to the Seattle branch office of 

the Federal Reserve Bank of San 

Francisco and reassign the routing 

symbols listed under that office to the 

Los Angeles branch office of the Federal 

Reserve Bank of San Francisco, and (ii) 

delete the reference to the Denver 

branch office of the Federal Reserve 

Bank of Kansas City and reassign the 

routing symbols listed under that office 

to the Los Angeles branch office of the 

Federal Reserve Bank of San Francisco 

and to the head office of the Federal 

Reserve Bank of Dallas. The depository 

institutions that are located in the 

affected check-processing regions and 

that include the routing numbers in 

their disclosure statements would be 

required to notify customers of the 

resulting change in availability under 

§ 229.18(e). However, all paperwork 

collection procedures associated with 

Regulation CC already are in place, and 

the Board accordingly anticipates that 

no additional burden will be imposed as 

a result of this rulemaking. 

List of Subjects in 12 CFR Part 229 

Banks, Banking, Reporting and 

recordkeeping requirements. 

Authority and Issuance 

■ For the reasons set forth in the 

preamble, the Board is amending 12 

CFR part 229 to read as follows: 

PART 229—AVAILABILITY OF FUNDS 

AND COLLECTION OF CHECKS 

(REGULATION CC) 

■ 1. The authority citation for part 229 

continues to read as follows: 

Authority: 12 U.S.C. 4001–4010, 12 U.S.C. 

5001–5018. 

■ 2. Effective June 20, 2009, the Twelfth 

District routing symbol list in appendix 

A is revised to read as follows: 

Appendix A to Part 229—Routing 

Number Guide to Next-Day Availability 

Checks and Local Checks 

* * * * * 

Twelfth Federal Reserve District 

[Federal Reserve Bank of San Francisco] 

Los Angeles Branch 

1210 3210 

1211 3211 

1212 3212 

1213 3213 

1220 3220 

1221 3221 

1222 3222 

1223 3223 

1224 3224 

1230 3230 

1231 3231 

1232 3232 

1233 3233 

1250 3250 

1251 3251 

1252 3252 

* * * * * 

■ 3. Effective June 27, 2009, the Tenth, 

Eleventh, and Twelfth District routing 

symbol lists in appendix A are amended 

by removing the headings and listings 

for the Tenth Federal Reserve District 

and revising the listings for the Eleventh 

and Twelfth Federal Reserve Districts to 

read as follows: 

* * * * * 

Eleventh Federal Reserve District 

[Federal Reserve Bank of Dallas] 

Head Office 

0920 2920 

0921 2921 

0929 2929 

1010 3010 

1011 3011 

1012 3012 

1019 3019 

1020 3020 

1021 3021 

1022 3022 

1023 3023 

1030 3030 

1031 3031 

1039 3039 

1070 3070 

1110 3110 

1111 3111 

1113 3113 

1119 3119 

1120 3120 

1122 3122 

1123 3123 

1130 3130 

1131 3131 

1140 3140 

1149 3149 

1163 3163 

Twelfth Federal Reserve District 

[Federal Reserve Bank of San Francisco] 

Los Angeles Branch 

1210 3210 

1211 3211 

1212 3212 

1213 3213 

1220 3220 

1221 3221 

1222 3222 

1223 3223 

1224 3224 

1230 3230 

1231 3231 

1232 3232 

1233 3233 

1240 3240 

1241 3241 

1242 3242 

1243 3243 

1250 3250 

1251 3251 

1252 3252 

* * * * * 

By order of the Board of Governors of the 

Federal Reserve System, May 1, 2009. 

Jennifer J. Johnson, 

Secretary of the Board. 

[FR Doc. E9–10507 Filed 5–6–09; 8:45 am] 

BILLING CODE 6210–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2008–1214; Directorate 

Identifier 2007–NM–259–AD; Amendment 

39–15897; AD 2009–10–02] 

RIN 2120–AA64 

Airworthiness Directives; BAE 

Systems (Operations) Limited 

(Jetstream) Model 4101 Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: The FAA is superseding an 

existing airworthiness directive (AD), 

which applies to all BAE Systems 

(Operations) Limited (Jetstream) Model 

4101 airplanes. That AD currently 

requires operators to determine the 

number of flight cycles accumulated on 

each component of the main landing 

gear (MLG) and the nose landing gear 

(NLG), and to replace each component 

that reaches its life limit with a 

serviceable component. The existing AD 

also requires operators to revise the 

Airworthiness Limitations (AWL) 

section of the Instructions for Continued 

Airworthiness (ICA) in the aircraft 

maintenance manual to reflect the new 

life limits for structurally significant 

items. This new AD requires a new 

revision of the AWL section of the ICA 

to incorporate revised life limits for 

structurally significant items, 

Federal Register / Vol. 74, No. 87 / Thursday, May 7, 2009 / Rules and Regulations 21247 

operational and functional tests of 

certain systems, and instructions to 

retain critical ignition source prevention 

features during configuration changes. 

This AD results from mandatory 

continuing airworthiness information 

(MCAI) originated by an aviation 

authority of another country. We are 

issuing this AD to prevent failure of 

certain structurally significant items, 

including the MLG and the NLG, which 

could result in reduced structural 

integrity of the airplane; and to prevent 

fuel vapor ignition sources, which could 

result in fuel tank explosion and 

consequent loss of the airplane. 

DATES: This AD becomes effective June 

11, 2009. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of June 11, 2009. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain other publications as of 

October 26, 2005 (70 FR 55230, 

September 21, 2005). 

ADDRESSES: For service information 

identified in this AD, contact BAE 

Systems Regional Aircraft, 13850 

McLearen Road, Herndon, Virginia 

20171; telephone 703–736–1080; e-mail 

raebusiness@baesystems.com; Internet 

http://www.baesystems.com/Businesses/ 

RegionalAircraft/index.htm. 

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 (telephone 800–647–5527) 

is the 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: 

Todd Thompson, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue, SW., Renton, 

Washington 98057–3356; telephone 

(425) 227–1175; fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION:

Discussion 

The FAA issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an AD that 

supersedes AD 2005–19–15, amendment 

39–14280 (70 FR 55230, September 21, 

2005). The existing AD applies to all 

BAE Systems (Operations) Limited 

(Jetstream) Model 4101 airplanes. That 

NPRM was published in the Federal 

Register on November 17, 2008 (73 FR 

67817). That NPRM proposed to 

continue to require operators to 

determine the number of flight cycles 

accumulated on each component of the 

main landing gear and the nose landing 

gear, and to replace each component 

that reaches its life limit with a 

serviceable component. That NPRM also 

proposed to continue to require 

operators to revise the Airworthiness 

Limitations (AWL) section of the 

Instructions for Continued 

Airworthiness (ICA) in the aircraft 

maintenance manual to reflect the new 

life limits for structurally significant 

items. That NPRM also proposed to 

require a new revision of the AWL 

section of the ICA to incorporate revised 

life limits for structurally significant 

items, operational and functional tests 

of certain systems, and instructions to 

retain critical ignition source prevention 

features during configuration changes. 

Comments 

We provided the public the 

opportunity to participate in the 

development of this AD. No comments 

have been received on the NPRM or on 

the determination of the cost to the 

public. 

Conclusion 

We have carefully reviewed the 

available data and determined that air 

safety and the public interest require 

adopting the AD as proposed. 

Costs of Compliance 

The following table provides the 

estimated costs for U.S. operators to 

comply with this AD. 

ESTIMATED COSTS

Action Work hour Average labor 

rate per hour 

Cost per 

airplane 

Number of 

U.S.-registered 

airplanes 

Fleet cost 

AWL revision (required by AD 2005–19–15) ....................... 1 $80 $80 3 $240 

AWL revision (new action) ................................................... 1 80 80 3 240 

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 have 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 

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. 

See the ADDRESSES section for a location 

to examine the regulatory evaluation. 

21248 Federal Register / Vol. 74, No. 87 / Thursday, May 7, 2009 / Rules and Regulations 

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 Federal Aviation 

Administration (FAA) amends § 39.13 

by removing amendment 39–14280 (70 

FR 55230, September 21, 2005) and by 

adding the following new airworthiness 

directive (AD): 

2009–10–02 BAE Systems (Operations) 

Limited (Formerly British Aerospace 

Regional Aircraft): Amendment 39– 

15897. Docket No. FAA–2008–1214; 

Directorate Identifier 2007–NM–259–AD. 

Effective Date 

(a) This AD becomes effective June 11, 

2009. 

Affected ADs 

(b) This AD supersedes AD 2005–19–15. 

Applicability 

(c) This AD applies to all BAE Systems 

(Operations) Limited Model Jetstream 4101 

airplanes, certificated in any category. 

Unsafe Condition 

(d) This AD results from mandatory 

continuing airworthiness information (MCAI) 

originated by an aviation authority of another 

country. We are issuing this AD to prevent 

failure of certain structurally significant 

items, including the main landing gear and 

the nose landing gear, which could result in 

reduced structural integrity of the airplane; 

and to prevent fuel vapor ignition sources, 

which could result in fuel tank explosion and 

consequent loss of the airplane. 

Compliance 

(e) You are responsible for having the 

actions required by this AD performed within 

the compliance times specified, unless the 

actions have already been done. 

Certain Requirement of AD 2005–19–15: 

Revise Aircraft Maintenance Manual (AMM) 

(f) Within 30 days after October 26, 2005 

(the effective date of AD 2005–19–15): Revise 

the Airworthiness Limitations (AWL) section 

of the Instructions for Continued 

Airworthiness of the BAE Systems 

(Operations) Limited J41 AMM to include the 

life limits of the components listed in 

Chapter 05–10–10, Airworthiness 

Limitations—Description and Operation 

Section, Revision 23, dated February 15, 

2005, of the AMM. This may be 

accomplished by inserting a copy into the 

AWL section of the Instructions for 

Continued Airworthiness. Thereafter, except 

as provided in paragraph (i) of this AD, no 

alternative replacement times may be 

approved for any affected component. 

New Requirements of This AD: Revise AWL 

Section of Instructions for Continued 

Airworthiness 

(g) Within 90 days after the effective date 

of this AD: Revise the AWL section of the 

Instructions for Continued Airworthiness by 

incorporating the instructions of Subjects 05– 

10–10, ‘‘Airworthiness Limitations,’’ 05–10– 

20, ‘‘Certification Maintenance 

Requirements,’’ and 05–10–30, ‘‘Critical 

Design Configuration Control Limitations 

(CDCCL)—Fuel System’’ of the BAE Systems 

(Operations) Limited Jetstream Series 4100 

AMM, Revision 31, dated February 15, 2009. 

Thereafter, except as provided in paragraph 

(i) of this AD, no alternative replacement 

times or inspection intervals may be 

approved for any affected component. The 

revised Chapter 05–10–10 replaces the 

corresponding chapter specified in paragraph 

(f) of this AD. 

(h) Where paragraph 2.A.(2) of Subject 05– 

10–10 of the BAE Systems (Operations) 

Limited Jetstream Series 4100 AMM, 

Revision 31, dated February 15, 2009, 

specifies that certain landing gear units 

‘‘must be removed before 31st March 2008,’’ 

this AD requires compliance within 60 days 

after the effective date of this AD. 

Alternative Methods of Compliance 

(AMOCs) 

(i) 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. Send information to 

ATTN: Todd Thompson, Aerospace 

Engineer, International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 1601 

Lind Avenue, SW., Renton, Washington 

98057–3356; telephone (425) 227–1175; fax 

(425) 227–1149. Before using any approved 

AMOC on any airplane to which the AMOC 

applies, notify your appropriate principal 

inspector (PI) in the FAA Flight Standards 

District Office (FSDO), or lacking a PI, your 

local FSDO. 

Related Information 

(j) European Aviation Safety Agency 

airworthiness directive 2008–0094, dated 

May 16, 2008, also addresses the subject of 

this AD. 

Material Incorporated by Reference 

(k) You must use the service information 

contained in Table 1 of this AD to do the 

actions required by this AD, unless the AD 

specifies otherwise. 

TABLE 1—ALL MATERIAL INCORPORATED BY REFERENCE

Document Revision Date 

BAE Systems (Operations) Limited J41 (AMM) .............................................................................. 23 .............................. February 15, 2005. 

Subject 05–10–10 of the BAE Systems (Operations) Limited Jetstream Series 4100 AMM ......... 31 .............................. February 15, 2009. 

Subject 05–10–20 of the BAE Systems (Operations) Limited Jetstream Series 4100 AMM ......... 31 .............................. February 15, 2009. 

Subject 05–10–30 of the BAE Systems (Operations) Limited Jetstream Series 4100 AMM ......... 31 .............................. February 15, 2009. 

Chapter 05 of the BAE Systems 

(Operations) Limited Jetstream Series 4100 

AMM contains the following effective pages: 

TABLE 2—EFFECTIVE PAGES OF CHAPTER 05 

[List of effective pages] 

Page title/description Page number(s) Revision number Date shown 

on page(s) 

AMM Title Page ..................................................................... None shown ................................ Not shown on page* .. February 15, 2009 

AMM Publications Transmittal 

1 .................................................. 31 .............................. February 15, 2009. 

2–3 .............................................. Not shown on page* .. February 15, 2009. 

Federal Register / Vol. 74, No. 87 / Thursday, May 7, 2009 / Rules and Regulations 21249 

TABLE 2—EFFECTIVE PAGES OF CHAPTER 05—Continued 

[List of effective pages] 

Page title/description Page number(s) Revision number Date shown 

on page(s) 

Chapter 05 Airworthiness Limitations List of Effective Pages 1–2 .............................................. Not shown on page* .. February 15, 2009. 

Subject 05–10–10: Airworthiness Limitations 

1–4 .............................................. Not shown on page* .. September 15, 2004. 

5 .................................................. Not shown on page* .. February 15, 2006. 

6–10 ............................................ Not shown on page* .. February 15, 2005. 

12, 16, 18–40, 45 ........................ Not shown on page* .. February 15, 2009. 

11, 13–15, 17, 41-44, 46, 47 ...... Not shown on page* .. February 15, 2007. 

Subject 05–10–20: Certification Maintenance Requirements 

1, 5 .............................................. Not shown on page* .. December 1, 1997. 

2–3 .............................................. Not shown on page* .. September 15, 2004. 

4 .................................................. Not shown on page* .. October 15, 1999. 

Subject 05–10–30: Critical Design Configuration Control Limitations (CDCCL)—Fuel System 

1–2 .............................................. Not shown on page* .. February 15, 2008. 

*Page 1 of the Publications Transmittal of the BAE Systems (Operations) Limited Jetstream Series 4100 AMM is the only page that shows the 

revision level of this document. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

Subject 05–10–10, Subject 05–10–20, and 

Subject 05–10–30 of the BAE Systems 

(Operations) Limited Jetstream Series 4100 

AMM, Revision 31, dated February 15, 2009, 

under 5 U.S.C. 552(a) and 1 CFR part 51. 

(2) The Director of the Federal Register 

previously approved the incorporation by 

reference of the BAE Systems (Operations) 

Limited J41 AMM, Revision 23, dated 

February 15, 2005, on October 26, 2005 (70 

FR 55230, September 21, 2005). 

(3) For service information identified in 

this AD, contact BAE Systems Regional 

Aircraft, 13850 McLearen Road, Herndon, 

Virginia 20171; telephone 703–736–1080; email raebusiness@baesystems.com; Internet 

http://www.baesystems.com/Businesses/ 

RegionalAircraft/index.htm. 

(4) 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. 

(5) 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 April 27, 

2009. 

Stephen P. Boyd, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. E9–10425 Filed 5–6–09; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2008–1239; Directorate 

Identifier 2008–NM–131–AD; Amendment 

39–15894; AD 2009–09–08] 

RIN 2120–AA64 

Airworthiness Directives; Boeing 

Model 747 Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Boeing Model 747 airplanes. This AD 

requires repetitive external surface high 

frequency eddy current inspections to 

detect cracks in the radius detail of the 

upper lobe doubler on both sides of the 

airplane, and applicable corrective 

action. This AD results from reports of 

cracks in the radius detail of the upper 

lobe doublers. We are issuing this AD to 

detect and correct cracks in the upper 

lobe doublers. Such cracks could result 

in significant degradation of the fuselage 

structure and reduce its ability to carry 

flight loads from the vertical stabilizer, 

which could adversely affect the 

controllability of the airplane. 

DATES: This AD is effective June 11, 

2009. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of June 11, 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, Washington 98124– 

2207; telephone 206–544–5000, 

extension 1; fax 206–766–5680; e-mail 

me.boecom@boeing.com; Internet 

https://www.myboeingfleet.com. 

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 (telephone 800–647–5527) 

is the 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: Ivan 

Li, Aerospace Engineer, Airframe 

Branch, ANM–120S, FAA, Seattle 

Aircraft Certification Office, 1601 Lind 

Avenue, SW., Renton, Washington 

98057–3356; telephone (425) 917–6437; 

fax (425) 917–6590. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an airworthiness 

directive (AD) that would apply to 

certain Boeing Model 747 airplanes.