Federal Register / Vol. 70, No. 180 / Monday, September 19, 2005 / Rules and Regulations 54835 

After consideration of all relevant 

material presented, including the 

information and recommendation 

submitted by the Committee and other 

available information, it is hereby found 

that this rule, as hereinafter set forth, 

will tend to effectuate the declared 

policy of the Act. 

List of Subjects in 7 CFR Part 922 

Apricots, Marketing agreements, 

Reporting and recordkeeping 

requirements. 

PART 922—APRICOTS GROWN IN 

DESIGNATED COUNTIES IN 

WASHINGTON 

■ Accordingly, the interim final rule 

amending 7 CFR part 922 which was 

published at 70 FR 36812 on June 27, 

2005, is adopted as a final rule without 

change. 

Dated: September 14, 2005. 

Lloyd C. Day, 

Administrator, Agricultural Marketing 

Service. 

[FR Doc. 05–18584 Filed 9–16–05; 8:45 am] 

BILLING CODE 3410–02–P 

DEPARTMENT OF ENERGY 

10 CFR Part 300 

RIN 1901–AB11 

Guidelines for Voluntary Greenhouse 

Gas Reporting 

AGENCY: Office of Policy and 

International Affairs, U.S. Department of 

Energy. 

ACTION: Final rule; delay of effective 

date. 

SUMMARY: The Department of Energy 

(DOE) published interim final General 

Guidelines for its Voluntary Reporting 

of Greenhouse Gases Program on March 

24, 2005 (70 FR 15169), and published 

in the same issue of the Federal Register 

a notice of availability inviting public 

comment on draft Technical Guidelines 

needed to fully implement the revised 

Voluntary Reporting of Greenhouse 

Gases Program (70 FR 15164). DOE 

today is delaying the effective date of 

the guidelines to address the comments 

received by DOE in response to the 

March 24, 2005 Federal Register notice 

and to align the effective date with the 

likely availability of final reporting 

forms being developed by the Energy 

Information Administration. 

DATES: The effective date of the rule 

establishing 10 CFR part 300 published 

in the Federal Register at 70 FR 15169 

on March 24, 2005, is delayed until June 

1, 2006. 

FOR FURTHER INFORMATION CONTACT: 

Mark Friedrichs, PI–40, Office of Policy 

and International Affairs, U.S. 

Department of Energy, 1000 

Independence Ave., SW., Washington, 

DC 20585, or e-mail: 

1605bguidelines.comments@hq.doe.gov. 

SUPPLEMENTARY INFORMATION: As DOE 

explained in the notice of interim final 

rulemaking, the Technical Guidelines 

that supplement the General Guidelines 

will provide the specificity necessary 

for DOE to fully implement the 

greenhouse gas emissions inventory and 

emissions reduction elements of the 

voluntary reporting guidelines (70 FR 

15171). DOE received a substantial 

number of written comments on the 

Interim Final General Guidelines and 

draft Technical Guidelines, and DOE 

expects to issue final General and 

Technical Guidelines by the end of 

2005. At that time, the Energy 

Information Administration (EIA) will 

prepare reporting forms that conform to 

the Final General Guidelines and Final 

Technical Guidelines and begin 

developing the electronic reporting 

software necessary to implement the 

revised Program. 

Because DOE does not expect to issue 

final guidelines until the end of the 

calendar year, and because the Office of 

Management and Budget (OMB) 

clearance process under the Paperwork 

Reduction Act for EIA’s revised 

reporting forms will take at least 120 

days following the issuance of the final 

guidelines, DOE is delaying the 

September 20, 2005 effective date of the 

rule published on March 24, 2005 until 

June 1, 2006. This delay in the effective 

date will allow EIA time to complete the 

development of revised reporting forms, 

including an opportunity for public 

review, after the final General and 

Technical Guidelines are issued at the 

end of 2005. Once EIA has completed 

the development of its planned 

electronic reporting system, 

approximately 9 to 12 months after the 

guidelines are finalized, reporting 

entities would be able to use it to report 

under the revised guidelines. Since it is 

unlikely that entities will be able to 

report under the revised guidelines by 

July 1, 2006, DOE will revise the 

General Guidelines to provide that 

entities may use DOE’s October 1994 

guidelines for reporting in calendar year 

2006. Entities that wish to report their 

emissions and reductions for 2005, or 

prior years, using the revised guidelines 

will be able to do so during the normal 

2007 reporting cycle. 

Issued in Washington, DC, on September 

13, 2005. 

Karen A. Harbert, 

Assistant Secretary, Policy and International 

Affairs. 

[FR Doc. 05–18628 Filed 9–15–05; 9:21 am] 

BILLING CODE 6450–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2005–20944; Directorate 

Identifier 2003–NE–64–AD; Amendment 39–

14247; AD 2005–18–01] 

RIN 2120–AA64 

Airworthiness Directives; General 

Electric Company CT7–5, –7, and –9 

Series Turboprop Engines 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for General 

Electric Company (GE) CT7–5A2, –5A3, 

–7A, –7A1, –9B, –9B1, and –9B2 

turboprop engines, with stage 2 turbine 

aft cooling plate, part number (P/N) 

6064T07P01, 6064T07P02, 6064T07P05, 

or 6068T36P01 installed. This AD 

requires a onetime eddy current 

inspection (ECI) of certain P/N stage 2 

turbine aft cooling plate boltholes. This 

AD results from reports of six stage 2 

turbine aft cooling plates found cracked 

during inspection. We are issuing this 

AD to prevent stage 2 aft cooling plate 

separation, resulting in uncontained 

engine failure and damage to the 

airplane. 

DATES: This AD becomes effective 

October 24, 2005. The Director of the 

Federal Register approved the 

incorporation by reference of certain 

publications listed in the regulations as 

of October 24, 2005. 

ADDRESSES: You can get the service 

information identified in this AD from 

General Electric Aircraft Engines CT7 

Series Turboprop Engines, 1000 

Western Ave., Lynn, MA 01910; 

telephone (781) 594–3140, fax (781) 

594–4805. 

You may examine the AD docket on 

the Internet at http://dms.dot.gov or in 

Room PL–401 on the plaza level of the 

Nassif Building, 400 Seventh Street, 

SW., Washington, DC. 

FOR FURTHER INFORMATION CONTACT: 

Eugene Triozzi, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

54836 Federal Register / Vol. 70, No. 180 / Monday, September 19, 2005 / Rules and Regulations 

and Propeller Directorate, 12 New 

England Executive Park, Burlington, MA 

01803–5299; telephone (781) 238–7148; 

fax (781) 238–7199. 

SUPPLEMENTARY INFORMATION: The FAA 

proposed to amend 14 CFR part 39 with 

a proposed AD. The proposed AD 

applies to GE CT7–5A2, –5A3, –7A, 

–7A1, –9B, –9B1, and –9B2 turboprop 

engines, with stage 2 turbine aft cooling 

plate, P/N 6064T07P01, 6064T07P02, 

6064T07P05, or 6068T36P01 installed. 

We published the proposed AD in the 

Federal Register on April 15, 2005 (70 

FR 19893). That action proposed to 

require a onetime ECI of certain P/N 

stage 2 turbine aft cooling plate 

boltholes. 

Examining the AD Docket 

You may examine the docket that 

contains the AD, any comments 

received, and any final disposition in 

person at the Docket Management 

Facility Docket Offices between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. The Docket 

Office (telephone (800) 647–5227) is 

located on the plaza level of the 

Department of Transportation Nassif 

Building at the street address stated in 

ADDRESSES. Comments will be available 

in the AD docket shortly after the 

Document Management Facility receives 

them. 

Comments 

We provided the public the 

opportunity to participate in the 

development of this AD. We received no 

comments on the proposal 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 

There are about 1,240 GE CT7–5, –7, 

and –9 series turboprop engines of the 

affected design in the worldwide fleet. 

We estimate that 550 engines installed 

on airplanes of U.S. registry will be 

affected by this AD. We also estimate 

that it would take about one work hour 

per engine to perform the actions, and 

that the average labor rate is $65 per 

work hour. We estimate that 2.5% (or 

14) of the 550 engines will require stage 

2 turbine aft cooling plates being 

rejected by the onetime ECI. Required 

parts will cost about $17,000 per engine. 

Based on these figures, we estimate the 

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

be $270,700. 

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, Incorporation by reference, 

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: 

2005–18–01 General Electric Company: 

Amendment 39–14241. Docket No. 

FAA–2005–20944; Directorate Identifier. 

2003–NE–64–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective October 24, 2005. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to General Electric 

Company (GE) CT7–5A2, –5A3, –7A, –7A1, 

–9B, –9B1, and –9B2 turboprop engines, with 

stage 2 turbine aft cooling plate, part number 

(P/N) 6064T07P01, 6064T07P02, 

6064T07P05, or 6068T36P01 installed. These 

engines are installed on, but not limited to, 

Construcciones Aeronauticas, SA CN–235 

series and SAAB Aircraft AB SF340 series 

airplanes. 

Unsafe Condition 

(d) This AD results from reports of six stage 

2 turbine aft cooling plates found cracked 

during inspection. The actions specified in 

this AD are intended to prevent stage 2 aft 

cooling plate separation, resulting in 

uncontained engine failure and damage to 

the airplane. 

Compliance 

(e) You are responsible for having the 

actions required by this AD performed at the 

next engine or hot section module shop visit, 

but before accumulating an additional 6,000 

cycles-in-service after the effective date of the 

AD, unless already done. 

Onetime Eddy Current Inspection (ECI) 

(f) Perform a onetime ECI of the stage 2 

turbine aft cooling plate boltholes, using 

paragraph 3.B. of GE Alert Service Bulletin 

(ASB) No. CT7–TP S/B 72–A0464, Revision 

2, dated May 9, 2003. 

(g) Remove from service any stage 2 turbine 

aft cooling plate that does not pass the return 

to service criteria specified in paragraph 

3.B.(2) of GE Alert Service Bulletin (ASB) No. 

CT7–TP S/B 72–A0464, Revision 2, dated 

May 9, 2003. 

Previous Credit 

(h) Previous credit is allowed for onetime 

ECIs of the stage 2 turbine aft cooling plate 

boltholes that were done using GE ASB No. 

CT7–TP S/B 72–A0464, dated February 25, 

2003, or GE ASB No. CT7–TP S/B 72–A0464, 

Revision 1, dated March 12, 2003, before the 

effective date of this AD. 

Definition of Engine or Hot Section Module 

Shop Visit 

(i) For the purposes of this AD, an engine 

or hot section module shop visit is defined 

as the introduction of the engine or hot 

section module into a shop that includes 

separation of CT7 turboprop engine major 

case flanges. 

Federal Register / Vol. 70, No. 180 / Monday, September 19, 2005 / Rules and Regulations 54837 

Alternative Methods of Compliance 

(j) 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 

(k) None. 

Issued in Burlington, Massachusetts, on 

August 19, 2005. 

Material Incorporated by Reference 

(l) You must use GE Alert Service Bulletin 

(ASB) No. CT7–TP S/B 72–A0464, Revision 

2, dated May 9, 2003, to perform the 

inspection required by this AD. The Director 

of the Federal Register approved the 

incorporation by reference of this service 

bulletin in accordance with 5 U.S.C. 552(a) 

and 1 CFR part 51. Contact General Electric 

Aircraft Engines CT7 Series Turboprop 

Engines, 1000 Western Ave., Lynn, MA 

01910; telephone (781) 594–3140, fax (781) 

594–4805, for a copy of this service 

information. You may review copies at the 

Docket Management Facility; U.S. 

Department of Transportation, 400 Seventh 

Street, SW., Nassif Building, Room PL–401, 

Washington, DC 20590–0001, on the Internet 

at http://dms.dot.gov, 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/federalregister/cfr/ibr-locations.html. 

Issued in Burlington, Massachusetts, on 

August 19, 2005. 

Richard Noll, 

Acting Manager, Engine and Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 05–17493 Filed 9–16–05; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA 2003–16091; Airspace 

Docket No. 03–AGL–12] 

RIN 2120–AA66 

Establishment of Domestic VOR 

Federal Airway V–19; OH 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action establishes 

Domestic Very High Frequency Omnidirectional Range (VOR) Federal Airway 

V–19 northeast of the Cincinnati, OH, 

VOR/Tactical Air Navigation 

(VORTAC). The FAA is taking this 

action to reduce congestion on VOR 

Federal Airway V–5 between Columbus, 

OH, and Cincinnati, OH, and to enhance 

the management of aircraft operations 

over the Cincinnati, OH area. 

EFFECTIVE DATE: 0901 UTC, December 

22, 2005. 

FOR FURTHER INFORMATION CONTACT: 

Steve Rohring, Airspace and Rules, 

Office of System Operations Airspace 

and AIM, Federal Aviation 

Administration, 800 Independence 

Avenue, SW., Washington, DC 20591; 

telephone: (202) 267–8783. 

SUPPLEMENTARY INFORMATION: 

Background 

On December 9, 2003, the FAA 

published in the Federal Register a 

notice of proposed rulemaking to 

establish V–19 northeast of the 

Cincinnati, OH, VORTAC to reduce 

congestion on V–5 between Columbus, 

OH, and Cincinnati, OH, and to enhance 

the management of aircraft operations 

over the Cincinnati, OH, area (68 FR 

68576). Interested parties were invited 

to participate in this rulemaking effort 

by submitting written comments on this 

proposal to the FAA. No comments 

were received in response to the 

proposal. With the exception of editorial 

changes, this amendment is the same as 

that proposed in the notice. 

Domestic VOR Federal airways are 

published in paragraph 6010(a) of FAA 

Order 7400.9N dated September 1, 2005, 

and effective September 16, 2005, which 

is incorporated by reference in 14 CFR 

71.1. The Federal airway listed in this 

document will be published 

subsequently in the order. 

The Rule 

This action amends Title 14 Code of 

Federal Regulations (14 CFR part 71) by 

establishing V–19 in the Cincinnati, OH, 

area. Specifically, this action establishes 

V–19 between Columbus, OH, and 

Cincinnati, OH, to the south of V–5 and 

to the north of the Buckeye Military 

Operations Area. The FAA is taking this 

action to reduce congestion on V–5 and 

to enhance the management of aircraft 

operations over the Cincinnati, OH, 

area. 

The FAA has determined that this 

regulation only involves an established 

body of technical regulations for which 

frequent and routine amendments are 

necessary to keep them operationally 

current. Therefore, this regulation: (1) Is 

not a ‘‘significant regulatory action’’

under Executive Order 12866; (2) is not 

a ‘‘significant rule’’ under Department of 

Transportation (DOT) Regulatory 

Policies and Procedures (44 FR 11034; 

February 26, 1979); and (3) does not 

warrant preparation of a regulatory 

evaluation as the anticipated impact is 

so minimal. Since this is a routine 

matter that will only affect air traffic 

procedures and air navigation, it is 

certified that this rule, when 

promulgated, will not have a significant 

economic impact on a substantial 

number of small entities under the 

criteria of the Regulatory Flexibility Act. 

List of Subjects in 14 CFR Part 71 

Airspace, Incorporation by reference, 

Navigation (air). 

Adoption of the Amendment 

■ In consideration of the foregoing, the 

Federal Aviation Administration 

amends 14 CFR part 71 as follows: 

PART 71—DESIGNATION OF CLASS A, 

B, C, D, AND E AIRSPACE AREAS; AIR 

TRAFFIC SERVICE ROUTES; AND 

REPORTING POINTS 

■ 1. The authority citation for part 71 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40103, 40113, 

40120; E.O. 10854, 24 FR 9565, 3 CFR, 1959–

1963 Comp., p. 389. 

§ 71.1 [Amended] 

■ 2. The incorporation by reference in 

14 CFR 71.1 of FAA Order 7400.9N, 

Airspace Designations and Reporting 

Points, dated September 1, 2005, and 

effective September 16, 2005, is 

amended as follows: 

Paragraph 6010(a) Domestic VOR Federal 

Airways. 

* * * * * 

V–19 (New) 

From Cincinnati, OH; INT Cincinnati 063° 

and Appleton, OH, 229° radials; Appleton. 

* * * * * 

Issued in Washington, DC, on September 

12, 2005. 

Edith V. Parish, 

Acting Manager, Airspace and Rules. 

[FR Doc. 05–18502 Filed 9–16–05; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 73 

[Docket No. FAA–2005–22400; Airspace 

Docket No. 05–AWP–10] 

RIN 2120–AA66 

Amendment to Using Agency for 

Restricted Areas R–2510 A & B; El 

Centro, CA 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action changes the using 

agency of Restricted Areas R–2510A &