70812 Federal Register / Vol. 75, No. 223 / Friday, November 19, 2010 / Rules and Regulations 

removing a provision concerning CCC 

fee collection for administrative costs of 

implementing or modifying commodity 

assessment collections, as required by 

the 2008 Farm Bill, that are identified in 

this Final Rule is solely administrative. 

Therefore, FSA has determined that 

NEPA does not apply to this Final Rule 

and no environmental assessment or 

environmental impact statement will be 

prepared. 

Executive Order 12372 

This program is not subject to 

Executive Order 12372, which requires 

consultation with State and local 

officials. See the notice related to 7 CFR 

part 3015, subpart V, published in the 

Federal Register on June 24, 1983 (48 

FR 29115). 

Executive Order 12988 

This rule has been reviewed under 

Executive Order 12988. This final rule 

is not retroactive and it does not 

preempt State or local laws, regulations, 

or policies unless they present an 

irreconcilable conflict with this rule. 

Before any judicial action may be 

brought regarding the provisions of this 

rule the administrative appeal 

provisions of 7 CFR parts 11 and 780 

must be exhausted. 

Executive Order 13132 

The policies contained in this rule do 

not have any substantial direct effect on 

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. Nor does this rule 

impose substantial direct compliance 

costs on state and local governments. 

Therefore, consultation with the States 

is not required. 

Executive Order 13175 

The policies contained in this rule do 

not have tribal implications that 

preempt tribal law. 

Unfunded Mandates 

This rule contains no Federal 

mandates under the regulatory 

provisions of Title II of the Unfunded 

Mandates Reform Act of 1995 (UMRA) 

for State, local, or tribal governments, or 

the private sector. In addition, CCC was 

not required to publish a notice of 

proposed rulemaking for this rule. 

Therefore, this rule is not subject to the 

requirements of sections 202 and 205 of 

UMRA. 

Paperwork Reduction Act 

These regulations are exempt from the 

requirements of the Paperwork 

Reduction Act (44 U.S.C. Chapter 35), as 

specified in section 1601(c)(2)(a) of the 

2008 Farm Bill, which provides that 

these regulations, which are necessary 

to implement title I of the 2008 Farm 

Bill, be promulgated and administered 

without regard to the Paperwork 

Reduction Act. 

E-Government Act Compliance 

CCC is committed to complying with 

the E-Government Act, to promote the 

use of the Internet and other 

information technologies to provide 

increased opportunities for citizen 

access to Government information and 

services, and for other purposes. 

List of Subjects in 7 CFR part 1405 

Loan programs—agriculture, Price 

support programs. 

■ For the reasons set out above, CCC 

amends 7 CFR part 1405 as follows: 

PART 1405—LOANS, PURCHASES, 

AND OTHER OPERATIONS 

■ 1. The authority will continue to read 

as follows: 

Authority: 7 U.S.C. 1515; 7 U.S.C. 7416a; 

7 U.S.C. 7991(e); 15 U.S.C. 714b and 714c. 

§ 1405.9 [Amended] 

■ 2. Amend § 1405.9, in paragraph 

(c)(1), by removing the words ‘‘and for 

administrative costs’’, and adding, in 

their place, the words ‘‘but not for 

administrative costs’’. 

Signed in Washington, DC, on November 

15, 2010. 

Jonathan Coppess, 

Executive Vice President, Commodity Credit 

Corporation. 

[FR Doc. 2010–29249 Filed 11–18–10; 8:45 am] 

BILLING CODE 3410–05–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–1136; Directorate 

Identifier 2010–SW–069–AD; Amendment 

39–16522; AD 2010–24–04] 

RIN 2120–AA64 

Airworthiness Directives; Sikorsky 

Aircraft Corporation (Sikorsky) Model 

S–92A Helicopters 

AGENCY: Federal Aviation 

Administration, DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: This amendment supersedes 

an existing airworthiness directive (AD) 

for Sikorsky Model S–92A helicopters 

that currently requires cleaning and 

inspecting each main gearbox (MGB) 

assembly mounting foot pad and rib for 

a crack and corrosion. If you do not find 

a crack, the AD requires applying a 

corrosion preventive compound. If you 

find a crack, the AD requires replacing 

the MGB before further flight. If you 

find corrosion, bubbled paint, or paint 

discoloration, the AD requires you to 

repair the MGB before further flight. 

This amendment retains the current 

requirements and expands the 

applicability to include another partnumbered MGB assembly and MGB 

housing. This amendment is prompted 

by the need to expand the applicability 

to include another MGB assembly and 

MGB housing that is prone to the same 

cracks and corrosion as the MGB listed 

in the current AD. The actions specified 

by this AD are intended to prevent the 

loss of the MGB and subsequent loss of 

control of the helicopter. 

DATES: Effective December 6, 2010. 

The incorporation by reference of 

certain publications listed in the 

regulations was approved previously by 

the Director of the Federal Register as of 

February 19, 2010 (75 FR 5684, 

February 4, 2010). 

We must receive comments on this 

AD by January 18, 2011. 

ADDRESSES: Use one of the following 

addresses to comment on this AD. 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: (202) 493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue, SE., Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue, SE., Washington, DC 20590, 

between 9 a.m. and 5 p.m., Monday 

through Friday, except Federal holidays. 

You may get the service information 

identified in this AD from Sikorsky 

Aircraft Corporation, Attn: Manager, 

Commercial Technical Support, 

mailstop s581a, 6900 Main Street, 

Stratford, CT, telephone (203) 383–4866, 

e-mail address tsslibrary@sikorsky.com, 

or at http://www.sikorsky.com. 

Examining the Docket: You may 

examine the docket that contains the 

AD, any comments, and other 

information 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 Docket 

Operations office (telephone (800) 647– 


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Federal Register / Vol. 75, No. 223 / Friday, November 19, 2010 / Rules and Regulations 70813 

5527) is located in Room W12–140 on 

the ground floor of the West Building at 

the street address stated in the 

ADDRESSES section. Comments will be 

available in the AD docket shortly after 

receipt. 

FOR FURTHER INFORMATION CONTACT: 

Michael Schwetz, Aviation Safety 

Engineer, Boston Aircraft Certification 

Office, 12 New England Executive Park, 

Burlington, MA 01803, telephone (781) 

238–7761, fax (781) 238–7170. 

SUPPLEMENTARY INFORMATION: On 

December 18, 2009, we issued AD 2009– 

23–51, Amendment 39–16190 (75 FR 

5684, February 4, 2010), to require 

cleaning and inspecting each MGB 

assembly mounting foot pad and rib for 

a crack and corrosion. If you do not find 

a crack, the AD requires applying a 

corrosion preventive compound. If you 

find a crack, the AD requires replacing 

the MGB before further flight. If you 

find corrosion, bubbled paint, or paint 

discoloration, the AD requires you to 

repair the MGB before further flight. 

That action was prompted by reports of 

cracks in the MGB mounting foot pads 

and foot ribs. That condition, if not 

corrected, could result in loss of the 

MGB and subsequent loss of control of 

the helicopter. 

Since issuing that AD, we have 

determined the need to expand the 

applicability to include another MGB 

assembly and MBG housing, which 

introduced a six-stud attachment for the 

oil filter bowl and more edge distance 

on the right and left foot pads. This new 

housing configuration is added to the 

applicability of this AD because it is 

prone to the same cracks as the MGB 

listed in the current AD. The 

manufacturer is still investigating the 

root cause of these cracks. Contributing 

factors may include corrosion and the 

bushing press fit in the mounting foot 

bolt hole. The actions specified in this 

AD are interim actions until the root 

cause of the cracking is determined. 

After that determination, we anticipate 

further rulemaking. 

Since an unsafe condition has been 

identified that is likely to exist or 

develop on other Sikorsky S–92A 

helicopters of the same type design, this 

AD supersedes AD 2009–23–51 to retain 

the same requirements and to expand 

the applicability to include the MGB 

assembly, part number (P/N) 92351– 

15000–044, with a MGB housing, P/N 

92351–15110–046. This AD is being 

issued to prevent the loss of the MGB 

and subsequent loss of control of the 

helicopter. This AD requires an initial 

and at 10-hour time-in-service (TIS) 

intervals, cleaning and inspecting each 

MGB assembly mounting foot pad and 

rib for a crack and corrosion. If you do 

not find a crack, this AD requires 

applying a corrosion preventive 

compound. If you find a crack, this AD 

requires replacing the MGB before 

further flight. If you find corrosion, 

bubbled paint, or paint discoloration, 

this AD requires you to repair the MGB 

before further flight. 

The short compliance time is required 

because the previously described 

critical unsafe condition can adversely 

affect the structural integrity and 

controllability of the helicopter. 

Therefore, because of the short 

compliance time, this AD must be 

issued immediately. 

Since a situation exists that requires 

the immediate adoption of this 

regulation, it is found that notice and 

opportunity for prior public comment 

hereon are impracticable, and that good 

cause exists for making this amendment 

effective in less than 30 days. 

We estimate this AD will affect 44 

helicopters of U.S. registry, and 

inspecting the MGB assembly mounting 

foot pads and foot ribs for corrosion or 

a crack will take about: 

• 2 work hours to do the visual 

inspection, assuming 2200 (50 

inspections X 44 helicopters) 

inspections per year for commercial and 

part 91 operators; and 

• 24 work hours to remove and 

replace an MGB. 

The average labor rate is $85 per work 

hour and required parts will cost about 

$590,000 per helicopter. Based on these 

figures, we estimate the total cost 

impact of the AD on U.S. operators to 

be $26,423,760 assuming all 44 

helicopters will require an MGB 

replacement. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not precede it by notice and an 

opportunity for public comment. We 

invite you to send any written relevant 

data, views, or arguments regarding this 

AD. Send your comments to an address 

listed under the ADDRESSES section. 

Include ‘‘Docket No. FAA–2010–1136; 

Directorate Identifier 2010–SW–069– 

AD’’ at the beginning of your comments. 

We specifically invite comments on the 

overall regulatory, economic, 

environmental, and energy aspects of 

the AD. We will consider all comments 

received by the closing date and may 

amend the AD in light of those 

comments. 

We will post all comments we 

receive, without change, to http:// 

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

concerning this AD. Using the search 

function of the docket Web site, you can 

find and read the comments to any of 

our dockets, including the name of the 

individual who sent the comment. You 

may review the DOT’s complete Privacy 

Act Statement in the Federal Register 

published on April 11, 2000 (65 FR 

19477–78). 

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 the regulation: 

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); 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 an economic evaluation 

of the estimated costs to comply with 

this AD. See the AD docket to examine 

the economic evaluation. 

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. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 


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70814 Federal Register / Vol. 75, No. 223 / Friday, November 19, 2010 / Rules and Regulations 

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 

removing Airworthiness Directive (AD) 

2009–23–51, Amendment 39–16190 (75 

FR 5684, dated February 4, 2010), and 

by adding a new AD to read as follows: 

2010–24–04 Sikorsky Aircraft Corporation: 

Amendment 39–16522; Docket No. 

FAA–2010–1136; Directorate Identifier 

2010–SW–069–AD. Supersedes AD 

2009–23–51; Amendment 39–16190; 

Docket No. FAA–2010–0066; Directorate 

Identifier 2009–SW–52–AD. 

Applicability: Model S–92A helicopters, 

with main gearbox (MGB) assembly, part 

number (P/N) 92351–15000–042, –043, or 

–044, with MGB housing, P/N 92351–15110– 

042, –043, –044, –045, or –046, installed, 

certificated in any category. 

Compliance: Required as indicated. 

To prevent loss of an MGB and subsequent 

loss of control of the helicopter, do the 

following: 

(a) Within 10 hours time-in-service (TIS), 

unless accomplished previously, and 

thereafter at intervals not to exceed 10 hours 

TIS, clean and inspect each MGB assembly 

mounting foot pad and rib for a crack and 

corrosion in the area depicted in Figure 1 and 

as shown in the examples in Figures 2, 3, and 

4 of Sikorsky Alert Service Bulletin No. 92– 

63–020, dated September 11, 2009 (ASB). If 

no crack is found, apply the corrosion 

preventive compound to each foot pad and 

rib area. 

Note 1: When conducting a visual 

inspection, use a bright, non-LED light. 

(1) If you find a crack, replace the MGB 

before further flight. 

(2) If you find corrosion, bubbled paint, or 

paint discoloration, before further flight, 

repair the affected area. 

Note 2: Even though MGB assembly, P/N 

92351–15000–044, with MGB housing, P/N 

92351–15110–046, is not included in the 

ASB, following the Accomplishment 

Instructions in the ASB accomplishes the 

intent of this AD. 

(b) To request a different method of 

compliance or a different compliance time 

for this AD, follow the procedures in 14 CFR 

39.19. Contact the Manager, Boston Aircraft 

Certification Office, ATTN: Michael Schwetz, 

Aviation Safety Engineer, 12 New England 

Executive Park, Burlington, MA 01803, 

telephone (781) 238–7761, fax (781) 238– 

7170, for information about previously 

approved alternative methods of compliance. 

(c) The Joint Aircraft System/Component 

(JASC) Code is 6320: Main Rotor Gearbox. 

(d) Do the inspections by following the 

specified portions of Sikorsky Alert Service 

Bulletin No. 92–63–020, dated September 11, 

2009. The Director of the Federal Register 

approved this incorporation by reference 

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

of February 19, 2010 (75 FR 5684, February 

4, 2010). Copies may be obtained from 

Sikorsky Aircraft Corporation, Attn: Manager, 

Commercial Technical Support, mailstop 

s581a, 6900 Main Street, Stratford, CT, 

telephone (203) 383–4866, e-mail address 

tsslibrary@sikorsky.com, or at http:// 

www.sikorsky.com. Copies may be inspected 

at the FAA, Office of the Regional Counsel, 

Southwest Region, 2601 Meacham Blvd., 

Room 663, Fort Worth, Texas, or 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. 

(e) This amendment becomes effective on 

December 6, 2010. 

Issued in Fort Worth, Texas, on November 

9, 2010. 

Kim Smith, 

Manager, Rotorcraft Directorate, Aircraft 

Certification Service. 

[FR Doc. 2010–29201 Filed 11–18–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF THE INTERIOR 

Bureau of Ocean Energy Management, 

Regulation, and Enforcement 

30 CFR Parts 201, 202, 203, 204, 206, 

207, 208, 210, 212, 217, 218, 219, 220, 

227, 228, 229, 241, 243, and 290 

Office of Natural Resources Revenue 

30 CFR Parts 1201, 1202, 1203, 1204, 

1206, 1207, 1208, 1210, 1212, 1217, 

1218, 1219, 1220, 1227, 1228, 1229, 

1241, 1243, and 1290 

[Docket No. MMS–2010–MRM–0033] 

RIN 1010–AD70 

Reorganization of Title 30, Code of 

Federal Regulations 

Correction 

In rule document 2010–24721 

beginning on page 61051 in the issue of 

Monday, October 4, 2010, make the 

following corrections: 

PART 1206—PRODUCT VALUATION 

[CORRECTED] 

Amendment Table for Part 1206 

[Corrected] 

1. On page 61070, in the table, in the 

first column ‘‘Amend’’: 

a. In the fourth row, ‘‘§ 1206.52(c)(2)’’ 

should read ‘‘§ 1206.52(c)(2)(i)’’. 

b. In the 11th row, ‘‘§ 1206.53(e)(5) 

two times’’ should read ‘‘§ 1206.52(e)(5) 

two times’’. 

c. In both the 15th and 16th rows, 

‘‘§ 1206.52(c) introductory text’’ should 

read ‘‘§ 1206.53(c) introductory text’’. 

2. On page 61071, in the table, in the 

third column ‘‘And adding in its place:’’: 

a. In the 18th row from the bottom of 

the page, ‘‘part 207’’ should read ‘‘part 

1207.’’ 

b. In the seventh row from the bottom 

of the page, the blank entry should read 

‘‘ONRR.’’ 

3. On page 61072, in the table, in the 

third column ‘‘And adding in its place:’’, 

in the 22nd row, the blank entry should 

read ‘‘§ 1206.111’’. 

4. On page 61073, in the table, in the 

third column ‘‘And adding in its place:’’, 

in the 16th row, ‘‘Associate Director’’ 

should read ‘‘Director’’. 

PART 1208—SALE OF FEDERAL 

ROYALTY OIL [CORRECTED] 

Amendment Table for Part 1208 

[Corrected] 

5. On page 61081, in the table, in the 

third column ‘‘And adding in its place:’’: 

a. In the first row, ‘‘§ 208.8(a)’’ should 

read ‘‘§ 1208.8(a)’’. 

b. In the fifth row, ‘‘§ 208.7(g)’’ should 

read ‘‘§ 1208.7(g)’’. 

[FR Doc. C1–2010–24721 Filed 11–18–10; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF THE TREASURY 

Fiscal Service 

31 CFR Part 363 

Securities Held in Treasury Direct 

AGENCY: Bureau of the Public Debt, 

Fiscal Service, Treasury. 

ACTION: Final rule. 

SUMMARY: Treasury is enhancing 

TreasuryDirect to permit automatic 

purchases of savings bonds through a 

payroll savings plan. 

DATES: Effective date: November 19, 

2010. 

ADDRESSES: You can download this 

Final Rule at the following Internet 

addresses: 

http:\\www.publicdebt.treas.gov, 

http:\\www.gpo.gov, or 

http:\\www.regulations.gov. 

FOR FURTHER INFORMATION CONTACT: 

Elisha Whipkey, Director, Division of 

Program Administration, Office of Retail 

Securities, Bureau of the Public Debt, at 


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