58100 Federal Register / Vol. 70, No. 192 / Wednesday, October 5, 2005 / Proposed Rules 

2. Paragraph (b)(2) of § 1260.172 is 

revised to read as follows: 

§ 1260.172 Assessments. 

* * * * * 

(b) * * * 

(2) The assessment rates for imported 

cattle, beef, and beef products are as 

follows: 

IMPORTED LIVE CATTLE

HTS No. Assessment rate 

0102.10.0010 ............ $1.00/head. 

0102.10.0020 ............ $1.00/head. 

0102.10.0030 ............ $1.00/head. 

0102.10.0050 ............ $1.00/head. 

0102.90.2011 ............ $1.00/head. 

0102.90.2012 ............ $1.00/head. 

0102.90.4024 ............ $1.00/head. 

0102.90.4028 ............ $1.00/head. 

0102.90.4034 ............ $1.00/head. 

0102.90.4038 ............ $1.00/head. 

0102.90.4054 ............ $1.00/head. 

0102.90.4058 ............ $1.00/head. 

0102.90.4062 ............ $1.00/head. 

0102.90.4064 ............ $1.00/head. 

0102.90.4066 ............ $1.00/head. 

0102.90.4068 ............ $1.00/head. 

0102.90.4072 ............ $1.00/head. 

0102.90.4074 ............ $1.00/head. 

0102.90.4082 ............ $1.00/head. 

0102.90.4084 ............ $1.00/head. 

IMPORTED BEEF AND BEEF PRODUCTS

HTS No. Assessment rate 

per kg 

0201.10.0510 ............ .01487175 

0201.10.0590 ............ .00386279 

0201.10.1010 ............ .01487175 

0201.10.1090 ............ .00386279 

0201.10.5010 ............ .01487175 

0201.10.5090 ............ .00521477 

0201.20.0200 ............ .00540791 

0201.20.0400 ............ .00521477 

0201.20.0600 ............ .00386279 

0201.20.1000 ............ .00540791 

0201.20.3000 ............ .00521477 

0201.20.5000 ............ .00386279 

0201.20.8090 ............ .00386279 

0201.30.0200 ............ .00540791 

0201.30.0400 ............ .00521477 

0201.30.0600 ............ .00386279 

0201.30.1000 ............ .00540791 

0201.30.3000 ............ .00521477 

0201.30.5000 ............ .00521477 

0201.30.8090 ............ .00521477 

0202.10.0510 ............ .01487175 

0202.10.0590 ............ .00386279 

0202.10.1010 ............ .01487175 

0202.10.1090 ............ .00386279 

0202.10.5010 ............ .01487175 

0202.10.5090 ............ .00386279 

0202.20.0200 ............ .00540791 

0202.20.0400 ............ .00521477 

0202.20.0600 ............ .00386279 

0202.20.1000 ............ .00540791 

0202.20.3000 ............ .00521477 

0202.20.5000 ............ .00386279 

0202.20.8000 ............ .00386279 

0202.30.0200 ............ .00540791 

IMPORTED BEEF AND BEEF

PRODUCTS—Continued 

HTS No. Assessment rate 

per kg 

0202.30.0400 ............ .00521477 

0202.30.0600 ............ .00527837 

0202.30.1000 ............ .00540791 

0202.30.3000 ............ .00521477 

0202.30.5000 ............ .00521477 

0202.30.8000 ............ .00386279 

0206.10.0000 ............ .00386279 

0206.21.0000 ............ .00386279 

0206.22.0000 ............ .00386279 

0206.29.0000 ............ .00386279 

0210.20.0000 ............ .00386279 

1601.00.4010 ............ .00482849 

1601.00.4090 ............ .00482849 

1601.00.6020 ............ .00482849 

1602.50.0900 ............ .00675989 

1602.50.1020 ............ .00675989 

1602.50.1040 ............ .00675989 

1602.50.2020 ............ .00714617 

1602.50.2040 ............ .00714617 

1602.50.6000 ............ .00733931 

* * * * * 

Dated: September 29, 2005. 

Kenneth C. Clayton, 

Acting Administrator, Agricultural Marketing 

Service. 

[FR Doc. 05–20016 Filed 10–4–05; 8:45 am] 

BILLING CODE 3410–02–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2005–20803; Directorate 

Identifier 2005–CE–19–AD] 

RIN 2120–AA64 

Airworthiness Directives; 

BURKHARDT GROB LUFT-UND 

RAUMFAHRT GmbH & CO KG Models 

G103 TWIN ASTIR, G103 TWIN II, 

G103A TWIN II ACRO, G103C TWIN III 

ACRO, and G103C Twin III SL 

Sailplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to 

supersede Airworthiness Directive (AD) 

2004–08–13, which applies to certain 

BURKHARDT GROB LUFT-UND 

RAUMFAHRT GmbH & CO KG (Grob) 

Models G103 TWIN ASTIR, G103 TWIN 

II, G103 TWIN III ACRO, and G103C 

Twin III SL sailplanes. AD 2004–08–13 

currently requires you to replace the 

center of gravity (CG) release hook 

attachment brackets with brackets of 

improved design. This proposed AD 

results from mandatory continuing 

airworthiness information (MCAI) 

issued by the airworthiness authority for 

Germany. This proposed AD would 

retain all the actions required in AD 

2004–08–13 and add Model G103A 

TWIN II ACRO sailplanes to the 

applicability. The actions specified by 

this proposed AD are to prevent 

abnormal or uncontrolled sailplane 

release due to cracked CG release hook 

attachment brackets. This condition 

could result in reduced or loss of 

sailplane control. 

DATES: We must receive any comments 

on this proposed AD by November 9, 

2005. 

ADDRESSES: Use one of the following to 

submit comments on this proposed AD: 

• DOT Docket Web site: Go to http:// 

dms.dot.gov and follow the instructions 

for sending your comments 

electronically. 

• Government-wide rulemaking Web 

site: Go to http://www.regulations.gov 

and follow the instructions for sending 

your comments electronically. 

• Mail: Docket Management Facility; 

U.S. Department of Transportation, 400 

Seventh Street, SW., Nassif Building, 

Room PL–401, Washington, DC 20590–

001. 

• Fax: 1–202–493–2251. 

• Hand Delivery: Room PL–401 on 

the plaza level of the Nassif Building, 

400 Seventh Street, SW., Washington, 

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

through Friday, except Federal holidays. 

To get the service information 

identified in this proposed AD, contact 

BURKHARDT GROB LUFT-UND 

RAUMFAHRT GmbH & CO KG, 

Letenbachstrasse 9, D–86874 

Tussenhausen-Mattsies, Germany; 

telephone: 011 49 8268 998139; 

facsimile: 011 49 8268 998200. 

To view the comments to this 

proposed AD, go to http://dms.dot.gov. 

The docket number is FAA–2005–

20803; Directorate Identifier 2005–CE–

19–AD. 

FOR FURTHER INFORMATION CONTACT: Greg 

Davison, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4130; facsimile: 

(816) 329–4090. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

How do I comment on this proposed 

AD? We invite you to submit any 

written relevant data, views, or 

arguments regarding this proposal. Send 

your comments to an address listed 

under ADDRESSES. Include the docket 

number, ‘‘FAA–2005–20803; Directorate 

Identifier 2005–CE–19–AD’’ at the 

Federal Register / Vol. 70, No. 192 / Wednesday, October 5, 2005 / Proposed Rules 58101 

beginning of your comments. We will 

post all comments we receive, without 

change, to http://dms.dot.gov, including 

any personal information you provide. 

We will also post a report summarizing 

each substantive verbal contact with 

FAA personnel concerning this 

proposed rulemaking. Using the search 

function of our docket Web site, anyone 

can find and read the comments 

received into any of our dockets, 

including the name of the individual 

who sent the comment (or signed the 

comment on behalf of an association, 

business, labor union, etc.). This is 

docket number FAA–2005–20803; 

Directorate Identifier 2005–CE–19–AD. 

You may review the DOT’s complete 

Privacy Act Statement in the Federal 

Register published on April 11, 2000 

(65 FR 19477–78) or you may visit 

http://dms.dot.gov. 

Are there any specific portions of this 

proposed AD I should pay attention to? 

We specifically invite comments on the 

overall regulatory, economic, 

environmental, and energy aspects of 

this proposed AD. If you contact us 

through a nonwritten communication 

and that contact relates to a substantive 

part of this proposed AD, we will 

summarize the contact and place the 

summary in the docket. We will 

consider all comments received by the 

closing date and may amend this 

proposed AD in light of those comments 

and contacts. 

Docket Information 

Where can I go to view the docket 

information? You may view the AD 

docket that contains this proposal, any 

comments received, and any final 

disposition in person at the DMS Docket 

Offices between 9 a.m. and 5 p.m. 

(eastern standard time), Monday 

through Friday, except Federal holidays. 

The Docket Office (telephone 1–800–

647–5227) is located on the plaza level 

of the Department of Transportation 

NASSIF Building at the street address 

stated in ADDRESSES. You may also view 

the AD docket on the Internet at http:// 

dms.dot.gov. The comments will be 

available in the AD docket shortly after 

the DMS receives them. 

Discussion 

Has FAA taken any action to this 

point? Reports of cracks found in the 

center of gravity (CG) release hook 

attachment brackets caused us to issue 

AD 2004–08–13, Amendment 39–13582 

(69 FR 21402, April 21, 2004). AD 2004–

08–13 applies to Grob Models G103 

TWIN ASTIR, G103 TWIN II, G103 

TWIN III ACRO, and G103C Twin III SL 

sailplanes. That AD currently requires 

you to replace the center of gravity (CG) 

release hook attachment brackets with 

brackets of improved design. 

What has happened since AD 2004– 

08–13 to initiate this proposed action? 

The Luftfahrt-Bundesamt (LBA), which 

is the airworthiness authority for 

Germany, notified FAA of the need to 

change AD 2004–08–13. The LBA 

reports that the actions required in AD 

2004–08–13 should also apply to Model 

G103A TWIN II ACRO sailplanes. 

What is the potential impact if FAA 

took no action? A cracked CG release 

hook attachment bracket, if not 

prevented, could lead to abnormal or 

uncontrolled sailplane release. This 

condition could result in reduced or 

loss of sailplane control. 

Is there new service information that 

applies to this subject? Grob has issued 

Service Bulletin No. MSB315–62/2, 

dated March 9, 2005. 

What are the provisions of this service 

information? The service bulletin 

includes procedures for inspecting and 

replacing the CG release hook 

attachment brackets for Models G103 

TWIN ASTIR, G103 TWIN II, G103A 

TWIN II ACRO, and G103C TWIN III 

ACRO sailplanes. 

What action did the LBA take? The 

LBA previously classified Grob Service 

Bulletin No. MSB315–62, dated January 

21, 2002, as mandatory and issued 

German AD No. 2002–067, effective 

date: March 21, 2002, to ensure the 

continued airworthiness of these 

sailplanes in Germany. 

Did the LBA inform the United States 

under the bilateral airworthiness 

agreement? These Grob Models G103 

TWIN ASTIR, G103 TWIN II, G103A 

TWIN II ACRO, G103C TWIN III ACRO, 

and G103C Twin III SL sailplanes are 

manufactured in Germany and are typecertificated for operation in the United 

States under the provisions of section 

21.29 of the Federal Aviation 

Regulations (14 CFR 21.29) and the 

applicable bilateral airworthiness 

agreement. 

Under this bilateral airworthiness 

agreement, the LBA has kept us 

informed of the situation described 

above. 

FAA’s Determination and Requirements 

of This Proposed AD 

What has FAA decided? We have 

examined the LBA’s findings, reviewed 

all available information, and 

determined that AD action is necessary 

for products of this type design that are 

certificated for operation in the United 

States. 

Since the unsafe condition described 

previously is likely to exist or develop 

on other Grob Models G103 TWIN 

ASTIR, G103 TWIN II, G103A TWIN II 

ACRO, G103C TWIN III ACRO, and 

G103C Twin III SL sailplanes of the 

same type design that are registered in 

the United States, we are proposing AD 

action to prevent abnormal or 

uncontrolled sailplane release due to 

cracked CG release hook attachment 

brackets. This condition could result in 

reduced or loss of sailplane control. 

What would this proposed AD 

require? This proposed AD would 

supersede AD 2004–08–13, Amendment 

39–13582 (69 FR 21402, April 21, 2004) 

with a new AD. This proposed AD 

would retain the actions exactly and 

currently required in AD 2008–08–13 

actions for Models G103 TWIN ASTIR, 

G103 TWIN II, G103C TWIN III ACRO, 

and G103C Twin III SL sailplanes and 

would add Model G103A TWIN II 

ACRO sailplanes to the applicability. 

How does the revision to 14 CFR part 

39 affect this proposed AD? On July 10, 

2002, we published a new version of 14 

CFR part 39 (67 FR 47997, July 22, 

2002), which governs FAA’s AD system. 

This regulation now includes material 

that relates to altered products, special 

flight permits, and alternative methods 

of compliance. This material previously 

was included in each individual AD. 

Since this material is included in 14 

CFR part 39, we will not include it in 

future AD actions. 

Costs of Compliance 

How many sailplanes would this 

proposed AD impact? We estimate that 

this proposed AD affects 136 sailplanes 

in the U.S. registry. 

What would be the cost impact of this 

proposed AD on owners/operators of the 

affected sailplanes? We estimate the 

following costs to do this proposed 

replacement: 

Labor cost Parts cost 

Total cost 

per sailplane 

Total cost on U.S. 

operators 

2 workhours × $65 per hour = $130. ..................................................................................... $67 $197 $197 × 136 = $26,792. 

58102 Federal Register / Vol. 70, No. 192 / Wednesday, October 5, 2005 / Proposed Rules 

What is the difference between the 

cost impact of this proposed AD and the 

cost impact of AD 2004–08–13? The 

only difference between the cost impact 

of AD 2004–08–13 and this proposed 

AD is the addition of Model G103A 

TWIN II ACRO sailplanes to the 

applicability. There is no difference in 

the cost to do the proposed required 

actions. 

Authority for This Rulemaking 

What authority does FAA have for 

issuing this rulemaking action? 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 AD. 

Regulatory Findings 

Would this proposed AD impact 

various entities? We have determined 

that this proposed AD would not have 

federalism implications under Executive 

Order 13132. This proposed AD would 

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. 

Would this proposed AD involve a 

significant rule or regulatory action? For 

the reasons discussed above, I certify 

that this proposed AD: 

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 a summary of the costs 

to comply with this proposed AD (and 

other information as included in the 

Regulatory Evaluation) and placed it in 

the AD Docket. You may get a copy of 

this summary by sending a request to us 

at the address listed under ADDRESSES. 

Include ‘‘AD Docket FAA–2005–20803; 

Directorate Identifier 2005–CE–19–AD’’

in your request. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Safety. 

The Proposed Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the Federal Aviation Administration 

proposes to amend 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) 

2004–08–13, Amendment 39–13582 (69 

FR 21402, April 21, 2004), and by 

adding a new AD to read as follows: 

Burkhardt Grob Luft-Und Raumfahrt GmBH 

& Co KG: Docket No. FAA–2005–20803; 

Directorate Identifier 2005–CE–19–AD; 

supersedes AD 2004–08–13, Amendment 

39–13582. 

When Is the Last Date I Can Submit 

Comments on This Proposed AD? 

(a) We must receive comments on this 

proposed airworthiness directive (AD) by 

November 9, 2005. 

What Other ADs Are Affected by This 

Action? 

(b) This AD supersedes AD 2004–08–13, 

Amendment 39–13582. 

What Sailplanes Are Affected by This AD? 

(c) This AD affects the following model 

sailplanes, all serial numbers, that are 

certificated in any category: 

MODELS

(1) G103 TWIN ASTIR 

(2) G103 TWIN II 

(3) G103A TWIN II ACRO 

(3) G103C TWIN III ACRO 

(4) G 103 C Twin III SL 

What Is the Unsafe Condition Presented in 

This AD? 

(d) This AD is the result of mandatory 

continuing airworthiness information (MCAI) 

issued by the airworthiness authority for 

Germany. The actions of this AD are 

intended to prevent abnormal or 

uncontrolled sailplane release due to cracked 

center of gravity (CG) release hook 

attachment brackets. This condition could 

result in reduced or loss of sailplane control. 

What Must I Do To Address This Problem? 

(e) To address this problem, you must do 

the following: 

Actions Compliance Procedures 

(1) Replace the CG release hook attachment 

brackets with improved design brackets, as 

follows: 

(i) For Models G103 TWIN ASTIR, G103 

TWIN II, G103A TWIN II ACRO, and 

G103C TWIN III ACRO sailplanes: install 

new part number (P/N) 103B–2360.01/1 

or 103B—2360.01/2 and P/N 103B–

2360.02/1 or 103B–2360–02/2; and 

(ii) For Model G103 TWIN ASTIR sailplanes: install an additional plate, P/N 

103–2360.02 below each attachment 

bracket; and 

Federal Register / Vol. 70, No. 192 / Wednesday, October 5, 2005 / Proposed Rules 58103 

Actions Compliance Procedures 

(iii) For Model G 103 C Twin III SL sailplanes: install new P/N 103B–2360.01/2 

and P/N 103B–2360.02/2.

For sailplanes previously affected by AD 

2004–08–13: Within the next 25 hours timein-service (TIS) after June 4, 2004 (the effective date of AD 2004–08–13), unless already done. For sailplanes not previously 

affected by AD 2004–08–13: Within the 

next 25 hours time-in-service (TIS) after the 

effective date of this AD, unless already 

done.

For Models G103 TWIN ASTIR, G103 TWIN 

II, G103A TWIN II ACRO, and G103C 

TWIN III ACRO sailplanes: Follow Grob 

Service Bulletin No. MSB315–62, dated 

January 21, 2002, or Grob Service Bulletin 

No. MSB315–62/2, dated March 9, 2005. 

For Model G 103 C Twin III SL sailplanes: 

Follow Grob Service Bulletin No. MSB869–

22, dated January 22, 2002. 

(2) Do not install any CG release hook attachment bracket that is not a part number referenced in paragraphs (e)(1)(i) and (e)(1)(iii) 

of this AD, as applicable.

As of the effective date of this AD ................... Not Applicable. 

May I Request an Alternative Method of 

Compliance? 

(f) You may request a different method of 

compliance or a different compliance time 

for this AD by following the procedures in 14 

CFR 39.19. Unless FAA authorizes otherwise, 

send your request to your principal 

inspector. The principal inspector may add 

comments and will send your request to the 

Manager, Standards Office, Small Airplane 

Directorate, FAA. For information on any 

already approved alternative methods of 

compliance, contact Greg Davison, Aerospace 

Engineer, FAA, Small Airplane Directorate, 

901 Locust, Room 301, Kansas City, Missouri 

64106; telephone: (816) 329–4130; facsimile: 

(816) 329–4090. 

Is There Other Information That Relates to 

This Subject? 

(g) German AD No. 2002–066, effective 

date: March 21, 2002; and German AD No. 

2002–067, effective date: March 21, 2002, 

also address the subject of this AD. 

May I Get Copies of the Documents 

Referenced in This AD? 

(h) To get copies of the documents 

referenced in this AD, contact BURKHARDT 

GROB LUFT-UND RAUMFAHRT GmbH & 

CO KG, Letenbachstrasse 9, D–86874 

Tussenhausen-Mattsies, Germany; telephone: 

011 49 8268 998139; facsimile: 011 49 8268 

998200. To view the AD docket, go to the 

Docket Management Facility; U.S. 

Department of Transportation, 400 Seventh 

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

Washington, DC, or on the Internet at http:// 

dms.dot.gov. This is docket number FAA–

2005–20803; Directorate ID 2005–CE–19–AD. 

Issued in Kansas City, Missouri, on 

September 28, 2005. 

David R. Showers, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 05–19942 Filed 10–4–05; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2005–21331; Directorate 

Identifier 2005–NE–07–AD] 

RIN 2120–AA64 

Airworthiness Directives; Engine 

Components Incorporated (ECi) 

Reciprocating Engine Connecting 

Rods 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to adopt a 

new airworthiness directive (AD) for 

certain Lycoming Engines (formerly 

Textron Lycoming) 360 and 540 series 

reciprocating engines with ECi 

connecting rods, part number (P/N) AEL 

11750, installed. This proposed AD 

would require replacing certain serialnumbered connecting rods, P/N AEL 

11750. This proposed AD would also 

prohibit installing certain ECi 

connecting rods, P/N AEL 11750 into 

any Lycoming 360 or 540 series 

reciprocating engines. This proposed 

AD results from reports of connecting 

rods with excessive variation in 

circularity of the journal bores. We are 

proposing this AD to prevent fatigue 

failure of the connecting rod and 

uncommanded shutdown of the engine. 

DATES: We must receive any comments 

on this proposed AD by December 5, 

2005. 

ADDRESSES: Use one of the following 

addresses to comment on this proposed 

AD. 

• DOT Docket Web site: Go to http:// 

dms.dot.gov and follow the instructions 

for sending your comments 

electronically. 

• Government-wide rulemaking Web 

site: Go to http://www.regulations.gov 

and follow the instructions for sending 

your comments electronically. 

• Mail: Docket Management Facility; 

U.S. Department of Transportation, 400 

Seventh Street, SW., Nassif Building, 

Room PL–401, Washington, DC 20590–

0001. 

• Fax: (202) 493–2251. 

• Hand Delivery: Room PL–401 on 

the plaza level of the Nassif Building, 

400 Seventh Street, SW., Washington, 

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

through Friday, except Federal holidays. 

You may examine the comments on 

this proposed AD in the AD docket on 

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

FOR FURTHER INFORMATION CONTACT: 

Peter Hakala, Aerospace Engineer, 

Special Certification Office, FAA, 

Rotorcraft Directorate, 2601 Meacham 

Blvd., Fort Worth, TX 76193; telephone 

(817) 222–5145; fax (817) 222–5785. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send us any written 

relevant data, views, or arguments 

regarding this proposal. Send your 

comments to an address listed under 

ADDRESSES. Include ‘‘Docket No. FAA–

2005–21331; Directorate Identifier 

2005–NE–07–AD’’ in the subject line of 

your comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of the proposed AD. We will 

consider all comments received by the 

closing date and may amend the 

proposed AD in light of those 

comments. 

We will post all comments we 

receive, without change, to http:// 

dms.dot.gov, including any personal 

information you provide. We will also 

post a report summarizing each 

substantive verbal contact with FAA 

personnel concerning this proposed AD. 

Using the search function of the DOT 

docket Web site, anyone can find and 

read the comments in any of our 

dockets, including the name of the 

individual who sent the comment (or