Federal Register / Vol. 76, No. 208 / Thursday, October 27, 2011 / Rules and Regulations 66625 is within the scope of that authority (c) For helicopters with a tailboom specified portions of Agusta Alert Bollettino because it addresses an unsafe condition assembly, P/N 3G5350A00132, Tecnico No. 139–195, Revision B, dated that is likely to exist or develop on 3G5350A00133, or 3G5350A00134, and a February 2, 2010. The Director of the Federal serial number (S/N) with a prefix of ‘‘A’’ up Register approved this incorporation by products identified in this rulemaking to and including S/N 7/109 for the short nose reference in accordance with 5 U.S.C. 552(a) action. configuration and a S/N with a prefix of ‘‘A’’ and 1 CFR part 51. Copies may be obtained List of Subjects in 14 CFR Part 39 up to and including S/N 7/063 for the long- from Agusta, Via Giovanni Agusta, 520 21017 nose configuration, within 25 hours time-in- Cascina Costa di Samarate (VA), Italy, Air transportation, Aircraft, Aviation service (TIS) from the last inspection or telephone 39 0331–229111, fax 39 0331– safety, Incorporation by Reference, within 7 days, whichever occurs first, unless 229605/222595, or at http://customersupport. Safety. done previously, and thereafter at intervals agusta.com/technical_advice.php. Copies not to exceed 25 hours TIS, tap inspect each may be inspected at the FAA, Office of the Adoption of the Amendment tailboom panel on both sides of the tailboom Regional Counsel, Southwest Region, 2601 Accordingly, pursuant to the in AREAs 3 and 5 for debonding, using an Meacham Blvd., Room 663, Fort Worth, authority delegated to me by the aluminum hammer as depicted in Figure 2 of Texas, 76137, or at the National Archives and Agusta Alert Bollettino Tecnico No. 139–195, Records Administration (NARA). For Administrator, the Federal Aviation Revision B, dated February 2, 2010 (ABT). information on the availability of this Administration amends part 39 of the First, inspect AREA 5 then AREA 3. You do material at NARA, call 202–741–6030, or go Federal Aviation Regulations (14 CFR not need to tap inspect the longeron area to: http://www.archives.gov/federal_register/ part 39) as follows: contained in AREA 3. Pay particular code_of_federal_regulations/ibr_ attention to previously repaired areas. locations.html. PART 39—AIRWORTHINESS (d) For all affected helicopters, except (l) This amendment becomes effective on DIRECTIVES those with tailboom assembly part numbers November 14, 2011. and serial numbers described in paragraph Note: The subject of this AD is addressed ■ (c) of this AD, within 50 hours TIS, unless 1. The authority citation for part 39 in European Aviation Safety Agency AD No. continues to read as follows: done previously, and thereafter at intervals not to exceed 50 hours TIS, tap inspect each 2011–0019, dated February 3, 2011 Authority: 49 U.S.C. 106(g), 40113, 44701. tailboom panel on both sides of the tailboom Issued in Fort Worth, Texas, on September for debonding using an aluminum hammer. § 39.13 [Amended] 13, 2011. Pay particular attention to the previously Lance T. Gant, ■ 2. Section 39.13 is amended by repaired areas. removing Amendment 39–16129; (75 FR (e) If there is any debonding, mark the Acting Manager, Rotorcraft Directorate, 3615, January 22, 2010), and by adding debond area and measure the size of the Aircraft Certification Service. a new airworthiness directive (AD), marked area. [FR Doc. 2011–27690 Filed 10–26–11; 8:45 am] Amendment 39–16816, to read as (f) Before further flight, install tailboom BILLING CODE 4910–13–P follows: structural reinforcement per MOD, P/N 3G5309P01812; if: 2011–20–06 Agusta S.p.A.: Amendment 39– (1) The mathematical area of a single 16816. Docket No. FAA–2011–1034; debond is equal to or greater than 320 mm2 DEPARTMENT OF THE TREASURY Directorate Identifier 2011–SW–014–AD. and is wholly within AREA 3 as depicted in Supersedes AD 2009–19–51, Figure 2 of the ABT; Alcohol and Tobacco Tax and Trade Amendment 39–16129; Docket No. (2) The mathematical area of a single Bureau FAA–2009–1125, Directorate Identifier debond is equal to or exceeds 150 mm2 if the 2009–SW–50–AD. debond occurs in area 1, 2, 4, or 5 as depicted 27 CFR Part 4 Applicability: Model AB139 and AW139 in Figure 2 of the ABT; or helicopters, with a tail assembly, part (3) The distance between the edges of any [Docket No. TTB–2011–0002; T.D. TTB–95; number (P/N) 3G5350A00132, two debonded areas is less than 3 times the Re: Notice No. 116] 3G5350A00133, 3G5350A00134, or largest debond dimension of the two RIN 1513–AA42 3G5350A00135, except those with tailboom debonded areas measured on a line between reinforcement structural retro-modification the centers of the two debonded areas; or Approval of Grape Variety Names for (MOD), P/N 3G5309P01812, installed, (4) A debond is within 3 mm from any American Wines certificated in any category. bond joint edge. Compliance: Required as indicated. (g) If none of the criteria of paragraphs AGENCY: Alcohol and Tobacco Tax and To detect damage to the tailboom to (f)(1) through (f)(4) of this AD are met, before Trade Bureau, Treasury. prevent failure of a tailboom and subsequent further flight, repair the debonded area of the ACTION: loss of control of a helicopter, do the tailboom using FAA engineering approved Final rule; Treasury decision. following: data and procedures or replace the tailboom SUMMARY: This document adopts, as a (a) For all affected helicopters, before with an airworthy tailboom. further flight, visually check all tailboom (h) Modifying the tailboom per MOD, P/N final rule, a proposal to amend the panels on both sides of the tailboom for skin 3G5309P01812, is terminating action for the Alcohol and Tobacco Tax and Trade bulging or deformation. Pay particular requirements of this AD. Bureau regulations by adding a number attention to the previously repaired areas. (i) To request a different method of of new names to the list of grape variety This visual check may be performed by an compliance or a different compliance time names approved for use in designating owner/operator (pilot) holding at least a for this AD, follow the procedures in 14 CFR American wines, and to include in the private pilot certificate and must be entered 39.19. Contact the Manager, Safety list several separate entries for into the helicopter records showing Management Group, FAA Attn: Sharon synonyms of existing entries so that compliance with paragraph (a) of this AD in Miles, ASW–111, Aviation Safety Engineer, accordance with 14 CFR 43.9(a)(1)-(4) and Rotorcraft Directorate, Regulations and readers can more readily find them. 91.417(a)(2)(v). Guidance Group, 2601 Meacham Blvd, Fort These amendments will allow bottlers (b) If there is bulging or deformation of a Worth, Texas 76137, telephone (817) 222– of wine to use more grape variety names tailboom panel skin, before further flight, 5122, fax (817) 222–5961, for information on wine labels and in wine using an aluminum hammer (GF–06–00), P/ about previously approved alternative advertisements. N 109–3101–58–2 (aluminum hammer), tap methods of compliance. DATES: Effective Date: This final rule is inspect the area around the bulge or (j) The Joint Aircraft System/Component deformity for debonding. Mark the (JASC) Code is 5302: Rotorcraft Tailboom. effective November 28, 2011. boundaries of the debond area and measure (k) The inspections shall be done on both FOR FURTHER INFORMATION CONTACT: the size of the marked area. sides of the tailboom by following the Jennifer Berry, Alcohol and Tobacco VerDate Mar<15>2010 17:05 Oct 26, 2011 Jkt 226001 PO 00000 Frm 00025 Fmt 4700 Sfmt 4700 E:\FR\FM\27OCR1.SGM 27OCR1 mstockstill on DSK4VPTVN1PROD with RULES 66626 Federal Register / Vol. 76, No. 208 / Thursday, October 27, 2011 / Rules and Regulations Tax and Trade Bureau, Regulations and appears in § 4.91 (27 CFR 4.91). Notice of Proposed Rulemaking Rulings Division, P.O. Box 18152, Alternative grape variety names On January 20, 2011, TTB published Roanoke, VA 24014; telephone 202– temporarily authorized for use are listed Notice No. 116 in the Federal Register 453–1039, ext. 275. in § 4.92 (27 CFR 4.92). Finally, § 4.93 (76 FR 3573) proposing to add a number SUPPLEMENTARY INFORMATION: (27 CFR 4.93) sets forth rules for the of grape variety names to the list of approval of grape variety names. Background approved names in § 4.91, either as a Approval of Grape Variety Names grape variety not already listed or as a TTB Authority synonym for an existing listed name. Section 4.93 provides that any Section 105(e) of the Federal Alcohol Most of the name proposals were based interested person may petition the Administration Act (FAA Act), 27 on petitions that TTB had received and Administrator for the approval of a U.S.C. 205(e), authorizes the Secretary approved, and the evidence that had grape variety name and that the petition of the Treasury to prescribe regulations been submitted in support of each should provide evidence of the for the labeling of wine, distilled spirits, petitioned for name is summarized in following: and malt beverages. The FAA Act the preamble to Notice No. 116. These • That the new grape variety is requires that these regulations, among names, on which TTB solicited accepted; other things, prohibit consumer comments, are as follows: • That the name for identifying the deception and the use of misleading grape variety is valid; Auxerrois statements on labels, and ensure that • Biancolella labels provide the consumer with That the variety is used or will be used in winemaking; and Black Monukka adequate information as to the identity Blaufra¨nkish • That the variety is grown and used and quality of the product.