72730 Federal Register / Vol. 70, No. 234 / Wednesday, December 7, 2005 / Proposed Rules 

‘‘Material—Cost and Availability’’ of 

EMBRAER Service Bulletin 145–27–0062, 

Revision 03, dated December 11, 2002, or 

Revision 04, dated March 8, 2004. Do the 

replacement in accordance with the 

Accomplishment Instructions of the service 

bulletin. Where the service bulletin specifies 

to send parts to the parts manufacturer, that 

action is not required by this AD. 

Corrective Actions for Cracked or Failed PCA 

Connecting Fittings 

(k) If any cracked or failed PCA connecting 

fitting at the wing or aileron side is found 

during any inspection required by paragraph 

(h) of this AD: Before further flight, replace 

the PCA connecting fitting with a new, 

reinforced fitting, in accordance with Part I 

of the Accomplishment Instructions of 

EMBRAER Service Bulletin 145–57–0019, 

Change 02, dated May 3, 2001, or Change 03, 

dated February 11, 2004; and EMBRAER 

Service Bulletin 145–27–0061, Change 02, 

dated September 12, 2000, Change 03, dated 

March 14, 2001, or Revision 04, dated August 

11, 2004. 

PCA Connecting Fitting Replacement 

(l) For airplanes with aileron PCAs with 

P/N 394900–1003, 394900–1005, 394900–

1007, 418800–1001, 418800–1003, 418800–

9003, 418800–1005, 418800–9005, 418800–

1007, or 418800–9007: Except as required by 

paragraph (k) of this AD, at the applicable 

time in paragraphs (l)(1) and (l)(2) of this AD, 

replace the aileron PCA connecting fittings 

with new, reinforced fittings, in accordance 

with Part I of the Accomplishment 

Instructions of EMBRAER Service Bulletin 

145–57–0019, Change 02, dated May 3, 2001, 

or Change 03, dated February 11, 2004; and 

Part I of the Accomplishment Instructions of 

EMBRAER Service Bulletin 145–27–0061, 

Change 02, dated September 12, 2000, 

Change 03, dated March 14, 2001, or 

Revision 04, dated August 11, 2004. 

(1) For airplanes with PCAs with 

P/N 394900–1003, 394900–1005, or 394900–

1007: At the later of the times in paragraphs 

(l)(1)(i) and (l)(1)(ii) of this AD. 

(i) Before the airplane accumulates 6,000 

total flight hours. 

(ii) Within 3 days or 25 flight hours after 

the effective date of this AD, whichever 

occurs later. 

(2) For airplanes with PCAs with P/N 

418800–1001, 418800–1003, 418800–9003, 

418800–1005, 418800–9005, 418800–1007, or 

418800–9007: Before the airplane 

accumulates 6,000 total flight hours, or 

within 600 flight hours after the effective 

date of this AD, whichever occurs later. 

(m) For airplanes with PCAs with P/N 

418800–1001, 418800–1003, 418800–9003, 

418800–1005, 418800–9005, 418800–1007, or 

418800–9007: At the applicable time 

specified in Table 1 of this AD following the 

replacement specified in paragraph (l) of this 

AD, do a general visual inspection of the 

replaced part using a method approved by 

either the Manager, International Branch, 

ANM–116, Transport Airplane Directorate, 

FAA; or the Departmento de Aviacao Civil 

(or its delegated agent). Doing the inspections 

in accordance with EMBRAER EMB–145 

Aircraft Maintenance Manual Task 27–12–

01–212–002–A00, ‘‘Inspect (Visual 

Inspection) Aileron PCA Rod Ends/Fitting 

Lugs for Integrity and General Condition’’, is 

one approved method. Thereafter, repeat the 

inspection at the applicable time specified in 

Table 1 of this AD. 

Optional Terminating Action 

(n) Airplanes that meet all conditions in 

paragraphs (n)(1), (n)(2), (n)(3), and (n)(4) of 

this AD are not subject to the requirements 

of paragraphs (f), (h), (i), (j), (k), (l), and (m) 

of this AD. 

(1) The airplane is equipped with new 

aileron PCAs with P/N 418800–1001, 

418800–1003, 418800–9003, 418800–1005, 

418800–9005, 418800–1007, or 418800–9007. 

(2) The airplane is equipped with new, 

reinforced PCA fittings installed in 

production or in accordance with the 

Accomplishment Instructions of EMBRAER 

Service Bulletin 145–57–0019, Change 02, 

dated May 3, 2001, or Change 03, dated 

February 11, 2004; and EMBRAER Service 

Bulletin 145–27–0061, Change 02, dated 

September 12, 2000, Change 03, dated March 

14, 2001, or Revision 04, dated August 11, 

2004; as applicable. 

(3) The airplane is equipped with an 

aileron damper with P/N 41012130–103 or 

41012130–104 that was installed in 

production or in accordance with the 

Accomplishment Instructions of any service 

bulletin listed in Table 2 of this AD. 

TABLE 2.—AILERON DAMPER INSTALLATION SERVICE BULLETINS

EMBRAER service bulletin Revision level Date 

145–27–0063 ................................................................................................................................... Original ...................... March 30, 2000. 

145–27–0063 ................................................................................................................................... Change 01 ................. October 2, 2000. 

145–27–0063 ................................................................................................................................... Change 02 ................. March 22, 2002. 

145–27–0063 ................................................................................................................................... Change 03 ................. May 27, 2004. 

145–27–0063 ................................................................................................................................... Revision 04 ............... October 13, 2004. 

145–27–0063 ................................................................................................................................... Revision 05 ............... March 16, 2005. 

(4) The general visual inspections for 

structural integrity of the aileron PCA and 

the aileron damper terminals and fittings at 

the wing and aileron sides at intervals not 

exceeding 1,000 flight hours, established in 

the EMBRAER Model EMB–145 Maintenance 

Review Board document, are implemented. 

Alternative Methods of Compliance (AMOCs) 

(o)(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. 

(3) Alternative methods of compliance 

approved previously in accordance with AD 

99–05–04 are approved as alternative 

methods of compliance with this AD. 

Related Information 

(p) Brazilian airworthiness directive 1999–

02–01R6, dated June 21, 2004, also addresses 

the subject of this AD. 

Issued in Renton, Washington, on 

November 1, 2005. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 05–23702 Filed 12–6–05; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF ENERGY 

Federal Energy Regulatory 

Commission 

18 CFR Parts 41, 158, 286 and 349 

[Docket No. RM06–2–000] 

Procedures for Disposition of 

Contested Audit Matters 

November 30, 2005. 

AGENCY: Federal Energy Regulatory 

Commission, DOE. 

ACTION: Notice of proposed rulemaking: 

Extension of comment period. 

SUMMARY: On October 20, 2005, the 

Federal Energy Regulatory Commission 

issued a Notice of Proposed Rulemaking 

regarding procedures for the disposition 

of contested audit matters (70 FR 65866, 

November 1, 2005). The Commission is 

Federal Register / Vol. 70, No. 234 / Wednesday, December 7, 2005 / Proposed Rules 72731 

extending the date for filing reply 

comments at the request of the Interstate 

Natural Gas Association. 

DATES: Reply comments are due on or 

before December 9, 2005. 

ADDRESSES: Reply comments may be 

filed electronically via the eFiling link 

on the Commission’s Web site at 

http://www.ferc.gov. Commenters 

unable to file comments electronically 

must send an original and 14 copies of 

their comments to: Federal Energy 

Regulatory Commission, Office of the 

Secretary, 888 First Street, NE., 

Washington, DC 20426. Refer to the 

Comment Procedures section of the 

preamble for additional information on 

how to file comments. 

FOR FURTHER INFORMATION CONTACT: John 

R. Kroeger, Office of Market Oversight 

and Investigations, Federal Energy 

Regulatory Commission, 888 First 

Street, NE., Washington, DC 20426. 

(202) 502–8177. 

SUPPLEMENTARY INFORMATION: 

Notice of Extension of Time 

On November 29, 2005, the Interstate 

Natural Gas Association of America 

(INGAA) filed a motion for an extension 

of time to file reply comments in 

response to the Commission’s Notice of 

Proposed Rulemaking issued October 

20, 2005, in the above-docketed 

proceeding. Procedures for Disposition 

of Contested Audit Matters, 113 FERC 

¶ 61,069 (2005). The motion states that 

because of the extensive and substantial 

initial comments that were filed in this 

proceeding, the intervening 

Thanksgiving holiday and the press of 

the significant Commission proceedings 

in which INGAA is participating, 

INGAA requires additional time to 

consult with its members and prepare 

well-developed and responsive reply 

comments. 

Upon consideration, notice is hereby 

given that an extension of time for filing 

reply comments in this proceeding is 

granted to and including December 9, 

2005, as requested by INGAA. 

Magalie R. Salas, 

Secretary. 

[FR Doc. 05–23728 Filed 12–6–05; 8:45 am] 

BILLING CODE 6717–01–M 

DEPARTMENT OF THE TREASURY 

Alcohol and Tobacco Tax and Trade 

Bureau 

27 CFR Parts 4, 5, and 7 

[Notice No. 53] 

RIN 1513—AB16 

Use of the Word ‘‘Pure’’ or Its Variants 

on Labels or in Advertisements of 

Alcohol Beverage Products; Request 

for Public Comment 

AGENCY: Alcohol and Tobacco Tax and 

Trade Bureau, Treasury. 

ACTION: Advance notice of proposed 

rulemaking. 

SUMMARY: The Alcohol and Tobacco Tax 

and Trade Bureau is considering 

amending the regulations concerning 

the use of the word ‘‘pure’’ on labels or 

in advertisements of alcohol beverage 

products. We wish to gather information 

by inviting comments from the public 

and industry as to whether the existing 

regulations should be revised. 

DATES: We must receive written 

comments on or before February 6, 

2006. 

ADDRESSES: You may send comments to 

any one of the following addresses: 

• Director, Regulations and Rulings 

Division, Alcohol and Tobacco Tax and 

Trade Bureau, Attn: Notice No. 53, P.O. 

Box 14412, Washington, DC 20044–

4412. 

• 202–927–8525 (facsimile). 

• nprm@ttb.gov (e-mail). 

• http://www.ttb.gov/alcohol/rules/ 

index.htm (an online comment form is 

posted with this notice on our Web site). 

• http://www.regulations.gov (Federal 

e-rulemaking portal; follow instructions 

for submitting comments). 

You may view copies of this advance 

notice and any comments we receive on 

this notice by appointment at the TTB 

Library, 1310 G Street, NW., 

Washington, DC 20220. To make an 

appointment, call 202–927–2400. You 

may also access copies of the advance 

notice and comments online at http:// 

www.ttb.gov/alcohol/rules/index.htm. 

See Section VI of this notice for 

specific instructions and requirements 

for submitting comments and for 

information on how to request a public 

hearing. 

FOR FURTHER INFORMATION CONTACT: Lisa 

M. Gesser, Regulations and Rulings 

Division, Alcohol and Tobacco Tax and 

Trade Bureau, P.O. Box 128, Morganza, 

MD 20660; (301) 290–1460. 

SUPPLEMENTARY INFORMATION: 

I. Authority to Prescribe Alcohol 

Beverage Labeling and Advertising 

Regulations 

Sections 105(e) and 105(f) of the 

Federal Alcohol Administration Act 

(FAA Act), codified in the United States 

Code at 27 U.S.C. 205(e) and 205(f), set 

forth standards for the regulation of the 

labeling and advertising of distilled 

spirits, wine (at least 7 percent alcohol 

by volume), and malt beverages, 

generally referred to as ‘‘alcohol 

beverage products’’ throughout this 

document. These sections give the 

Secretary of the Treasury the authority 

to issue regulations to prevent deception 

of the consumer, to provide the 

consumer with ‘‘adequate information’’

as to the identity and quality of the 

product, and to prohibit false or 

misleading statements on product labels 

and in advertisements. Additionally, 

these FAA Act provisions give the 

Secretary the authority to prohibit, 

irrespective of falsity, statements 

relating to age, manufacturing processes, 

analyses, guarantees, and scientific or 

irrelevant matters which are likely to 

mislead the consumer. In the case of 

malt beverages, the labeling and 

advertising provisions of the FAA Act 

apply only if the laws of the State into 

which the malt beverages are to be 

shipped impose similar requirements. 

The Alcohol and Tobacco Tax and 

Trade Bureau (TTB) is responsible for 

the administration of the FAA Act and 

the regulations promulgated under it. 

The labeling and adverting regulations 

for wine, distilled spirits, and malt 

beverages are codified in title 27 of the 

Code of Federal Regulations (CFR), parts 

4, 5, and 7, respectively. 

II. Current Regulatory Standards 

Sections 5.42(b)(5) and 5.65(a)(8) of 

the TTB regulations (27 CFR 5.42(b)(5) 

and 5.65(a)(8)), hereinafter referred to 

collectively as the ‘‘pure regulations,’’

currently state that the word ‘‘pure’’

may not be used on distilled spirits 

labels or in advertisements unless: 

• It refers to a particular ingredient 

used in the production of the distilled 

spirits, and is a truthful representation 

about the ingredient; or 

• It is part of the bona fide name of 

a permittee or retailer for whom the 

distilled spirits are bottled; or 

• It is part of the bona fide name of 

the permittee who bottled the distilled 

spirits. 

TTB considers variants of the word 

‘‘pure’’ such as ‘‘purest,’’ ‘‘purity,’’ and 

‘‘pureness’’ to fall within the purview of 

these regulations. These prohibitions 

apply only to distilled spirits. There are 

no similar prohibitions on the use of the