34924 Federal Register / Vol. 75, No. 118 / Monday, June 21, 2010 / Rules and Regulations 

York-Newark-Bridgeport, NY–NJ–CT– 

PA CSA, plus Monroe County, PA, 

Warren County, NJ, and all of Joint Base 

McGuire-Dix-Lakehurst; 

(21) Philadelphia-Camden-Vineland, 

PA–NJ–DE–MD—consisting of the 

Philadelphia-Camden-Vineland, PA– 

NJ–DE–MD CSA excluding Joint Base 

McGuire-Dix-Lakehurst, plus Kent 

County, DE, Atlantic County, NJ, and 

Cape May County, NJ; 

* * * * * 

(24) Portland-Vancouver-Hillsboro, 

OR–WA—consisting of the PortlandVancouver-Hillsboro, OR–WA MSA, 

plus Marion County, OR, and Polk 

County, OR; 

* * * * * 

[FR Doc. 2010–14981 Filed 6–18–10; 8:45 am] 

BILLING CODE 6325–39–P 

DEPARTMENT OF AGRICULTURE 

Commodity Credit Corporation 

7 CFR Part 1470 

RIN 0578–AA43 

Conservation Stewardship Program 

AGENCY: Commodity Credit Corporation, 

Natural Resources Conservation Service, 

United States Department of 

Agriculture. 

ACTION: Final rule; correction. 

SUMMARY: The Natural Resources 

Conservation Service is correcting a 

final rule that appeared in the Federal 

Register of June 3, 2010 (75 FR 31653). 

The document 2010–12699, concerning 

the Conservation Stewardship Program, 

contained an error in the words of 

‘‘issuance’’ at the end of the preamble. 

DATES: Effective Date: The rule is 

effective June 3, 2010. 

FOR FURTHER INFORMATION CONTACT: 

Dwayne Howard, Branch Chief, 

Financial Assistance Programs Division, 

Department of Agriculture, Natural 

Resources Conservation Service, 1400 

Independence Avenue, SW., Room 5237 

South Building, Washington, DC. 20250; 

Telephone: (202) 720–1845; Fax: (202) 

720–4265; or e-mail: 

Dwayne.howard@wdc.usda.gov. 

SUPPLEMENTARY INFORMATION: In FR Doc. 

2010–12699 appearing on page 31653 in 

the Federal Register of Thursday, June 

3, 2010, the following correction is 

made: 

Words of Issuance [Corrected] 

(1) On page 31653, in the second 

column, the Words of Issuance that read 

‘‘For the reasons stated above, the CCC 

adds part 1470 of the CFR to read as 

follows:’’ is corrected to read: ’’For the 

reasons stated above, the CCC revises 

part 1470 of Title 7 of the CFR to read 

as follows:’’ 

Signed June 15, 2010, in Washington, DC. 

Teressa Davis, 

Rulemaking Manager, Natural Resources 

Conservation Service. 

[FR Doc. 2010–14847 Filed 6–18–10; 8:45 am] 

BILLING CODE 3410–16–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–0026; Directorate 

Identifier 2010–NE–03–AD; Amendment 39– 

16340; AD 2010–13–09] 

RIN 2120–AA64 

Airworthiness Directives; CFM 

International, S.A. CFM56–5, –5B, and 

–7B Series Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for CFM 

International, S.A. CFM56–5, –5B, and 

–7B series turbofan engines. This AD 

requires removing from service, nine 

stage 3 low-pressure turbine (LPT) 

disks, identified by serial number (S/N). 

This AD results from the discovery of a 

material nonconformity requiring 

removal of the disk before the certified 

disk life of certain stage 3 LPT disks. We 

are issuing this AD to prevent 

uncontained failure of the stage 3 LPT 

disk and damage to the airplane. 

DATES: This AD becomes effective July 

26, 2010. 

ADDRESSES: The Docket Operations 

office is located at Docket Management 

Facility, U.S. Department of 

Transportation, 1200 New Jersey 

Avenue, SE., West Building Ground 

Floor, Room W12–140, Washington, DC 

20590–0001. 

FOR FURTHER INFORMATION CONTACT: 

Antonio Cancelliere, Aerospace 

Engineer, Engine Certification Office, 

FAA, Engine & Propeller Directorate, 12 

New England Executive Park, 

Burlington, MA 01803; e-mail: 

antonio.cancelliere@faa.gov; telephone 

(781) 238–7751; fax (781) 238–7199. 

SUPPLEMENTARY INFORMATION: The FAA 

proposed to amend 14 CFR part 39 with 

a proposed AD. The proposed AD 

applies to CFM International, S.A. 

CFM56–5, –5B, and –7B series turbofan 

engines. We published the proposed AD 

in the Federal Register on March 18, 

2010 (75 FR 13045). That action 

proposed to require removing from 

service, nine stage 3 LPT disks, 

identified by S/N. 

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 regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Operations office (telephone 

(800) 647–5527) is provided in the 

ADDRESSES section. Comments will be 

available in the AD docket shortly after 

receipt. 

Comments 

We provided the public the 

opportunity to participate in the 

development of this AD. We have 

considered the comments received. Two 

commenters support the proposal as 

written. 

Remove the Airbus A340 Reference 

One commenter, CFM International, 

S.A., requests that we remove the 

reference to the Airbus A340 airplane 

from the applicability paragraph, as the 

engines used on that airplane are 

CFM56–5C engines, and use a different 

disk P/N not affected by this AD. 

We agree. We removed the A340 

reference from the AD. 

Request To Reference the Disk Part 

Number 

CFM International, S.A., requests that 

we reference the disk part number of 

336–002–006–0, along with the affected 

disk serial numbers, in the applicability 

paragraph to help identify the parts to 

be removed. 

We agree. We added the disk part 

number to the applicability paragraph. 

Request To Clarify the Applicability 

Paragraph 

CFM International, S.A., requests 

clarification of the applicability 

paragraph that none of these affected 

disk S/Ns were originally installed on 

any CFM56–5 turbofan engines, 

however, that disk P/N is certified for 

use on CFM56–5 engines. 

We agree and changed the 

applicability paragraph. 

Request To Reference European 

Aviation Safety Agency (EASA) Related 

AD 

CFM International, S.A., requests that 

we reference the EASA related AD in 

our AD. 

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Federal Register / Vol. 75, No. 118 / Monday, June 21, 2010 / Rules and Regulations 34925 

We agree and added a reference to 

EASA AD 2009–0270 in the AD. 

Conclusion 

We have carefully reviewed the 

available data, including the comments 

received, and determined that air safety 

and the public interest require adopting 

the AD with the changes described 

previously. We have determined that 

these changes will neither increase the 

economic burden on any operator nor 

increase the scope of the AD. 

Costs of Compliance 

We estimate that this AD will affect 

two engines installed on airplanes of 

U.S. registry. The pro-rated cost of the 

replacement parts is $40,375 per engine. 

We estimate that no additional labor 

costs will be incurred to perform the 

required disk removals, because the 

removals will be done at time of engine 

shop visit. Based on these figures, we 

estimate the total cost of the AD to U.S. 

operators to be $80,750. 

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 summary of the costs 

to comply with this AD and placed it in 

the AD Docket. You may get a copy of 

this summary at the address listed 

under ADDRESSES. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Safety. 

Adoption of the Amendment 

■ Accordingly, under the authority 

delegated to me by the Administrator, 

the Federal Aviation Administration 

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: 

2010–13–09 CFM International, S.A.: 

Amendment 39–16340. Docket No. 

FAA–2010–0026; Directorate Identifier 

2010–NE–03–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective July 26, 2010. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to: 

(1) CFM International CFM56–5, –5B, and 

–7B series turbofan engines with stage 3 lowpressure turbine (LPT) disks part number 

(P/N) 336–002–006–0, installed with the 

following serial numbers (S/Ns), DE255844, 

DE256388, DE256622, DE256623, DE256625, 

DE256627, DE256628, DE256631, and 

DE256637. 

(2) CFM International, S.A. has stated that 

none of these affected disk S/Ns were 

originally installed on any CFM56–5 turbofan 

engine, however, that disk P/N is certified for 

use on CFM56–5 engines. 

(3) The –5 and –5B series engines are 

installed on, but not limited to, Airbus A318, 

A319, A320, and A321 airplanes, and the –7B 

series engines are installed on, but not 

limited to, Boeing 737 series airplanes. 

Unsafe Condition 

(d) This AD results from the discovery of 

a material nonconformity requiring removal 

of the disk before the certified disk life of 

certain stage 3 LPT disks. We are issuing this 

AD to prevent uncontained failure of the 

stage 3 LPT disk and damage to the airplane. 

Compliance 

(e) You are responsible for having the 

actions required by this AD performed within 

the compliance time specified unless the 

actions have already been done. 

Removal of Affected Stage 3 LPT Disks From 

Service 

(f) Before accumulating 9,500 cycles-sincenew, remove stage 3 LPT disks from service. 

(g) After the effective date of this AD, do 

not reinstall any stage 3 LPT disk removed 

from service per paragraph (f) of this AD into 

any engine. 

Alternative Methods of Compliance 

(h) The Manager, Engine Certification 

Office, has the authority to approve 

alternative methods of compliance for this 

AD if requested using the procedures found 

in 14 CFR 39.19. 

Related Information 

(i) Contact Antonio Cancelliere, Aerospace 

Engineer, Engine Certification Office, FAA, 

Engine & Propeller Directorate, 12 New 

England Executive Park, Burlington, MA 

01803; e-mail: antonio.cancelliere@faa.gov; 

telephone (781) 238–7751; fax (781) 238– 

7199, for more information about this AD. 

(j) European Aviation Safety Agency AD 

2009–0270, dated December 17, 2009, also 

addresses the subject of this AD. 

(k) CFM International, S.A. Service 

Bulletin (SB) No. CFM56–5B S/B 72–0733, 

dated October 26, 2009, and SB No. CFM56– 

7B S/B 72–0743, dated October 26, 2009, 

pertain to the subject of this AD. Contact 

CFM International, Technical Publications 

Department, 1 Neumann Way, Cincinnati, 

OH 45215; telephone (513) 552–2800; fax 

(513) 552–2816, for a copy of this service 

information. 

Material Incorporated by Reference 

(l) None. 

Issued in Burlington, Massachusetts, on 

June 15, 2010. 

Peter A. White, 

Assistant Manager, Engine and Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 2010–14819 Filed 6–18–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Office of the Secretary 

14 CFR Part 234 

[Docket No. DOT–OST–2007–0022] 

RIN No. 2105–AE02 

Posting of Flight Delay Data on Web 

Sites 

AGENCY: Office of the Secretary (OST), 

Department of Transportation (DOT). 

ACTION: Direct Final Rule, request for 

comments. 

SUMMARY: This direct final rule amends 

the time period for uploading flight 

mstockstill on DSKH9S0YB1PROD with RULES