58628 Federal Register / Vol. 70, No. 194 / Friday, October 7, 2005 / Proposed Rules 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

2. The Federal Aviation 

Administration (FAA) amends § 39.13 

by adding the following new 

airworthiness directive (AD): 

EMBRAER: Docket No. FAA–2005–22631; 

Directorate Identifier 2005–NM–183–AD. 

Comments Due Date 

(a) The FAA must receive comments on 

this AD action by November 7, 2005. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to all EMBRAER Model 

EMB–120, –120ER, –120FC, –120QC, and 

–120RT airplanes, certificated in any 

category. 

Unsafe Condition 

(d) This AD results from fuel system 

reviews conducted by the manufacturer. We 

are issuing this AD to prevent chafed 

electrical harnesses, which could result in a 

potential source of ignition for fuel vapors 

near a fuel tank and consequent fire or fuel 

tank explosion. 

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. 

Corrective Action 

(f) Within 5,000 flight hours after the 

effective date of this AD, modify the 

electrical harnesses located at the left- and 

right-hand wing roots; and re-route and 

modify the harness of the right-hand 

outboard flap actuator; in accordance with 

the Accomplishment Instructions of 

EMBRAER Service Bulletin 120–24–0059, 

Revision 02, dated March 18, 2005. 

Previously Accomplished Actions 

(g) Actions done before the effective date 

of this AD in accordance with EMBRAER 

Service Bulletin 120–24–0059, dated April 6, 

2004; and Revision 01, dated November 9, 

2004; are acceptable for compliance with the 

requirements of paragraph (f) of this AD. 

Alternative Methods of Compliance 

(AMOCs) 

(h)(1) The Manager, International Branch, 

ANM–116, Transport Airplane Directorate, 

FAA, has the authority to approve AMOCs 

for this AD, if requested in accordance with 

the procedures found in 14 CFR 39.19. 

(2) Before using any AMOC approved in 

accordance with § 39.19 on any airplane to 

which the AMOC applies, notify the 

appropriate principal inspector in the FAA 

Flight Standards Certificate Holding District 

Office. 

Related Information 

(i) Brazilian airworthiness directive 2005–

06–01, dated June 29, 2005, also addresses 

the subject of this AD. 

Issued in Renton, Washington, on 

September 30, 2005. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 05–20269 Filed 10–6–05; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2005–22628; Directorate 

Identifier 2005–NM–056–AD] 

RIN 2120–AA64 

Airworthiness Directives; Boeing 

Model 737–300, –400, –500, –700, and 

–800 Series Airplanes; Model 747–400 

and –400F Series Airplanes; Model 

757–200 Series Airplanes; Model 767–

300 Series Airplanes; and Model 777–

300 Series Airplanes Equipped With 

Certain Driessen or Showa Galleys or 

Driessen Closets 

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 Boeing transport category 

airplanes. This proposed AD would 

require inspecting to determine if 

certain galleys and closets are installed, 

and replacing the spiral wire wrapping 

of the electrical cables of the galleys and 

closets with new spiral wire wrapping 

if necessary. This proposed AD results 

from testing and reports from the 

manufacturer indicating unacceptable 

flammability properties of wire 

wrapping installed in certain galleys 

and closets. We are proposing this AD 

to prevent fire propagation or smoke in 

the cabin area due to electrical arcing or 

sparking and ignition of the spiral wire 

wrapping. 

DATES: We must receive comments on 

this proposed AD by November 21, 

2005. 

ADDRESSES: Use one of the following 

addresses 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. 

• By 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. 

For service information identified in 

this proposed AD, contact Boeing 

Commercial Airplanes, P.O. Box 3707, 

Seattle, Washington 98124–2207. 

You can examine the contents of this 

AD docket on the Internet at http:// 

dms.dot.gov, or in person at the Docket 

Management Facility, U.S. Department 

of Transportation, 400 Seventh Street 

SW., Room PL–401, on the plaza level 

of the Nassif Building, Washington, DC. 

This docket number is FAA–2005–

22628; the directorate identifier for this 

docket is 2005–NM–056–AD. 

FOR FURTHER INFORMATION CONTACT: 

Susan Rosanske, Aerospace Engineer, 

Cabin Safety and Environmental 

Systems Branch, ANM–150S, FAA, 

Seattle Aircraft Certification Office, 

1601 Lind Avenue, SW., Renton, 

Washington 98055–4056; telephone 

(425) 917–6448; fax (425) 917–6590. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to submit any relevant 

written data, views, or arguments 

regarding this proposed AD. Send your 

comments to an address listed under 

ADDRESSES. Include ‘‘Docket No. FAA–

2005–22628; Directorate Identifier 

2005–NM–056–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 

submitted 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 that 

website, anyone can find and read the 

comments in 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.). You can 

review DOT’s complete Privacy Act 

Statement in the Federal Register 

published on April 11, 2000 (65 FR 

19477–78), or you can visit http:// 

dms.dot.gov. 

Federal Register / Vol. 70, No. 194 / Friday, October 7, 2005 / Proposed Rules 58629 

Examining the Docket 

You can examine the AD docket on 

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

person at the Docket Management 

Facility office between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. The Docket 

Management Facility office (telephone 

(800) 647–5227) is located on the plaza 

level of the Nassif Building at the DOT 

street address stated in the ADDRESSES

section. Comments will be available in 

the AD docket shortly after the Docket 

Management System (DMS) receives 

them. 

Discussion 

We received reports of testing by the 

manufacturer indicating unacceptable 

flammability properties of the spiral 

wire wrapping of the electrical cables in 

certain galleys and closets on various 

Boeing transport category airplanes. The 

existing spiral wire wrapping of certain 

galleys and closets was not tested for 

flammability standards and may not 

self-extinguish in the event of a fire. 

Electrical arcing or sparking and 

ignition of the spiral wire wrapping 

could result in fire propagation or 

smoke in the cabin area. 

Relevant Service Information 

We have reviewed the service 

information identified in the following 

table. 

SERVICE INFORMATION

Boeing Revision Dated 

Special Attention Service Bulletin 737–25–1438 ........................................................................................ 1 November 11, 2004. 

Service Bulletin 737–25–1439 ..................................................................................................................... 3 November 11, 2004. 

Special Attention Service Bulletin 747–25–3264 ........................................................................................ 1 November 11, 2004. 

Service Bulletin 747–25–3275 ..................................................................................................................... 1 April 4, 2002. 

Special Attention Service Bulletin 757–25–0238 ........................................................................................ 2 November 11, 2004. 

Special Attention Service Bulletin 767–25–0297 ........................................................................................ 1 November 11, 2004. 

Special Attention Service Bulletin 777–25–0180 ........................................................................................ 1 November 11, 2004. 

The service bulletins and special 

attention service bulletins describe 

procedures for replacing existing spiral 

wire wrapping of the electrical cables of 

the galleys and closets with new spiral 

protective wrapping that has been 

shown to meet certain flammability 

testing requirements. The procedures 

also describe installing a modification 

placard to indicate that new spiral 

protective wrapping has been installed. 

Each of the service bulletins reference 

Dreissen Aircraft Interior Systems 

Service Bulletin SB 25–442, Revision E, 

dated April 29, 2004, and Showa 

Aircraft Industry Co., Ltd., Service 

Bulletin SB 25–30–111, dated December 

11, 2000, as applicable, as additional 

sources of service information. 

Accomplishing the actions specified in 

the service information is intended to 

adequately address the unsafe 

condition. 

FAA’s Determination and Requirements 

of the Proposed AD 

We have evaluated all pertinent 

information and identified an unsafe 

condition that is likely to exist or 

develop on other airplanes of this same 

type design. Therefore, we are 

proposing this AD, which would require 

accomplishing the actions specified in 

the service information described 

previously, except as discussed under 

‘‘Differences Between the Proposed AD 

and the Service Information.’’

Differences Between the Proposed AD 

and the Service Information 

Each of the Boeing service bulletins 

referenced in this proposed AD specify 

certain Boeing series airplanes. 

However, this proposed AD is 

applicable to all the airplane models 

specified. Since galleys and closets may 

be removed from one airplane and 

installed in another airplane, this 

proposed AD would also require an 

inspection to determine if certain 

galleys or closets are installed, or a 

maintenance record check of the 

airplane to determine if certain galleys 

or closets are installed. 

Although the Boeing service bulletins 

refer to accomplishment of certain 

Driessen Aircraft Interior Systems and 

Showa service bulletins, or ‘‘the latest 

FAA-approved revision,’’ this proposed 

AD would require accomplishment of 

the Driessen Aircraft Interior Systems 

and Showa service bulletins specified in 

this proposed AD. Using the phrase, ‘‘or 

later FAA-approved revision,’’ violates 

Office of the Federal Register 

regulations for approving materials that 

are incorporated by reference. However, 

affected operators may request approval 

to use a later revision of the referenced 

service bulletin as an alternative method 

of compliance, under the provisions of 

paragraph (j) of the proposed AD. 

The Boeing service bulletins also 

specify an imprecise compliance time 

for replacing the spiral protective 

wrapping of the electrical cables of the 

galley, i.e., ‘‘at the next heavy 

maintenance check.’’ This proposed AD 

would require replacement within 72 

months after the effective date of the 

AD, and we have coordinated this 

compliance time with the manufacturer. 

Additionally, for clarification and for 

the purposes of this proposed AD, the 

use of the term ‘‘galley’’ includes the 

terms ‘‘buffet’’ and ‘‘closets’’ referenced 

in certain service information specified 

in this proposed AD. 

Costs of Compliance 

There are about 5,177 airplanes of the 

affected design in the worldwide fleet. 

This proposed AD would affect about 

2,621 airplanes of U.S. registry. The 

proposed inspection to determine part 

numbers of the galleys would take about 

1 work hour per galley, at an average 

labor rate of $65 per work hour. Some 

airplanes have only one galley and some 

have up to 11 galleys. With the 

exception of Boeing Model 777–300 

airplanes, we estimate the cost of the 

inspection proposed in this AD for U.S. 

operators to be between $65 and $715 

per airplane. 

If an operator is required to replace 

the spiral protective wrapping of the 

electrical cables of the galley, we 

estimate that cost to be as follows: 

1. For Dreissen galleys: About two 

work hours per galley, at an average 

labor rate of $65 per work hour, and the 

estimated cost for the new spiral 

protective wrapping to be about $1,450, 

per galley. The estimated total cost 

would be about $1,580, per galley. 

2. For Showa galleys: About 20 work 

hours per galley, at an average labor rate 

of $65 per work hour, and the estimated 

cost of the new spiral protective 

wrapping to be about $1,550, per galley. 

The estimated total cost would be about 

$2,850, per galley. 

Currently, there are no Boeing Model 

777–300 airplanes with the subject 

galleys on the U.S. Register. However, if 

a Model 777–300 is imported and 

placed on the U.S. Register in the future, 

the required actions would take about 1 

58630 Federal Register / Vol. 70, No. 194 / Friday, October 7, 2005 / Proposed Rules 

work hour per galley, at an average labor 

rate of $65 per work hour. 

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 

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. 

For the reasons discussed above, I 

certify that the proposed 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 a regulatory evaluation 

of the estimated costs to comply with 

this proposed AD. See the ADDRESSES

section for a location to examine the 

regulatory evaluation. 

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 FAA 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 adding 

the following new airworthiness 

directive (AD): 

Boeing: Docket No. FAA–2005–22628; 

Directorate Identifier 2005–NM–056–AD. 

Comments Due Date 

(a) The Federal Aviation Administration 

(FAA) must receive comments on this AD 

action by November 21, 2005. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Boeing transport 

category airplanes equipped with certain 

Driessen Aircraft Interior Systems or Showa 

galleys, certificated in any category; as 

identified in paragraphs (c)(1) through (c)(5) 

inclusive of this AD. 

(1) Model 737–300, –400, –500, –700, and 

–800 series airplanes; 

(2) Model 747–400 and 747–400F series 

airplanes; 

(3) Model 757–200 series airplanes; 

(4) Model 767–300 series airplanes; 

(5) Model 777–300 series airplanes. 

Unsafe Condition 

(d) This proposed AD results from testing 

and reports from the manufacturer indicating 

unacceptable flammability properties of wire 

wrapping installed in certain galleys and 

closets. We are proposing this AD to prevent 

fire propagation or smoke in the cabin area 

due to electrical arcing or sparking and 

ignition of the spiral wire wrapping. 

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. 

Note 1: For clarification and for the 

purposes of this AD, the use of the term 

‘‘galley’’ also includes the terms ‘‘buffet’’ and 

‘‘closets’’ that are referenced in certain 

service information specified in this AD. 

Determination of Part Installation 

(f) Within 72 months after the effective 

date of this AD, inspect the galleys to 

determine if any of the part numbers (P/Ns) 

installed are identified in the applicable 

service information specified in Table 1 of 

this AD. Instead of inspecting the galleys to 

determine if the P/Ns are installed, a review 

of airplane maintenance records is acceptable 

if the P/Ns can be positively determined from 

that review. 

TABLE 1.—SERVICE BULLETINS AND SPECIAL ATTENTION SERVICE BULLETINS

Model and service information Revision Dated 

Boeing Special Attention Service Bulletin 737–25–1438, for Model 737–300, –400, and –500 series airplanes.1 November 11, 2004. 

Boeing Service Bulletin 737–25–1439, for Model 737–700 and –800 series airplanes ............................. 3 November 11, 2004. 

Boeing Special Attention Service Bulletin 747–25–3264, for Model 747–400 series airplanes ................. 1 November 11, 2004. 

Boeing Service Bulletin 747–25–3275, for Model 747–400F series airplanes ........................................... 1 April 4, 2002. 

Boeing Special Attention 757–25–0238, for Model 757–200 series airplanes ........................................... 2 November 11, 2004. 

Boeing Special Attention Service Bulletin 767–25–0297, for Model 767–300 series airplanes ................. 1 November 11, 2004. 

Boeing Special Attention Service Bulletin 777–25–0180, for Model 777–300 series airplanes ................. 1 November 11, 2004. 

Note 2: The service bulletin and special 

attention service bulletins specified in Table 

1 of this AD reference Dreissen Aircraft 

Interior Systems Service Bulletin SB 25–442, 

Revision E, dated April 29, 2004; and Showa 

Aircraft Industry Co., Ltd., Service Bulletin 

SB 25–30–111, dated December 11, 2000; as 

applicable; as additional sources of service 

information. 

If Certain Galleys Are Not Installed 

(g) If no galley is installed having any P/ 

N identified in the service information 

specified in paragraph (f) of this AD, no 

further action is required by this AD. 

If Certain Galleys Are Installed 

(h) If any galley is installed having any P/ 

N identified in the service information 

specified in paragraph (f) of this AD: Within 

72 months after the effective date of this AD, 

replace the spiral protective wrapping of the 

electrical cables of the galley with new spiral 

protective wrapping that has been shown to 

meet certain flammability testing 

requirements, in accordance with the 

applicable service information specified in 

paragraph (f) of this AD. 

Credit for Previous Replacement 

(i) Replacement of the spiral protective 

wrapping of the electrical cables of any galley 

with new spiral protective wrapping that has 

been shown to meet certain flammability 

Federal Register / Vol. 70, No. 194 / Friday, October 7, 2005 / Proposed Rules 58631 

testing requirements, in accordance with the 

service information listed in the Table 2 of 

this AD, prior to the effective date of this AD, 

is acceptable for compliance with the 

requirements of paragraph (h) of this AD. 

TABLE 2.—PREVIOUS ACCOMPLISHMENT

Boeing service information Revision Dated 

Special Attention Service Bulletin 737–25–1438 ........................................................................................... Original ........ March 15, 2001. 

Special Attention Service Bulletin 737–25–1439 ........................................................................................... Original ........ March 15, 2001. 

Special Attention Service Bulletin 737–25–1439 ........................................................................................... 1 .................. August 2, 2001. 

Service Bulletin 737–25–1439 ....................................................................................................................... 2 .................. December 19, 2001. 

Special Attention Service Bulletin 747–25–3264 ........................................................................................... Original ........ March 15, 2001. 

Special Attention Service Bulletin 747–25–3275 ........................................................................................... Original ........ March 15, 2001. 

Special Attention Service Bulletin 757–25–0238 ........................................................................................... Original ........ March 15, 2001. 

Special Attention Service Bulletin 757–25–0238 ........................................................................................... 1 .................. November 15, 2001. 

Special Attention Service Bulletin 767–25–0297 ........................................................................................... Original ........ March 15, 2001. 

Special Attention Service Bulletin 777–25–0180 ........................................................................................... Original ........ March 15, 2001. 

Alternative Methods of Compliance 

(AMOCs) 

(j)(1) The Manager, Seattle Aircraft 

Certification Office (ACO), FAA, has the 

authority to approve AMOCs for this AD, if 

requested in accordance with the procedures 

found in 14 CFR 39.19. 

(2) An AMOC that provides an acceptable 

level of safety may be used for any 

replacement required by this AD, if it is 

approved by an Authorized Representative 

for the Boeing Commercial Airplanes 

Delegation Option Authorization 

Organization who has been authorized by the 

Manager, Seattle ACO, to make those 

findings. For a repair method to be approved, 

the repair must meet the certification basis of 

the airplane, and the approval must 

specifically refer to this AD. 

Issued in Renton, Washington, on 

September 28, 2005. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 05–20270 Filed 10–6–05; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2005–22632; Directorate 

Identifier 2005–NM–158–AD] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier 

Model CL–600–2C10 (Regional Jet 

Series 700, 701, & 702), CL–600–2D15 

(Regional Jet Series 705), and CL–600–

2D24 (Regional Jet Series 900) 

Airplanes 

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 Bombardier Model CL–600–

2C10 (Regional Jet Series 700, 701, & 

702), CL–600–2D15 (Regional Jet Series 

705), and CL–600–2D24 (Regional Jet 

Series 900) airplanes. This proposed AD 

would require repetitive inspections for 

cracking or fracturing of the output links 

of the power control unit (PCU) for the 

ailerons, and related investigative and 

corrective actions if necessary. This 

proposed AD results from reports of 

fractured output links of the aileron 

PCU. We are proposing this AD to 

prevent failure of an output link of the 

aileron PCU, which, if both links on one 

aileron fail, could result in reduced 

lateral control of the airplane. 

DATES: We must receive comments on 

this proposed AD by November 7, 2005. 

ADDRESSES: Use one of the following 

addresses 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. 

• 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. 

Contact Bombardier, Inc., Canadair, 

Aerospace Group, P.O. Box 6087, 

Station Centre-ville, Montreal, Quebec 

H3C 3G9, Canada, for service 

information identified in this proposed 

AD. 

FOR FURTHER INFORMATION CONTACT: 

Daniel Parrillo, Aerospace Engineer, 

Systems and Flight Test Branch, ANE–

172, FAA, New York Aircraft 

Certification Office, 1600 Stewart 

Avenue, suite 410, Westbury, New York 

11590; telephone (516) 228–7305; fax 

(516) 794–5531. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to submit any relevant 

written data, views, or arguments 

regarding this proposed AD. Send your 

comments to an address listed in the 

ADDRESSES section. Include the docket 

number ‘‘FAA–2005–22632; Directorate 

Identifier 2005–NM–158–AD’’ at the 

beginning 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 that 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 signed the 

comment on behalf of an association, 

business, labor union, etc.). 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.