Income Taxes, 46671 [2017-21742]

Download as PDF Federal Register / Vol. 82, No. 193 / Friday, October 6, 2017 / Rules and Regulations 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. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to engines, propellers, and associated appliances to the Manager, Engine and Propeller Standards Branch, Policy and Innovation Division. asabaliauskas on DSKBBXCHB2PROD with RULES Regulatory Findings 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), (3) Will not affect intrastate aviation in Alaska, and (4) 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. 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, VerDate Sep<11>2014 16:21 Oct 05, 2017 Jkt 244001 the FAA amends 14 CFR part 39 as follows: 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD): ■ 2017–20–09 General Electric Company: Amendment 39–19066; Docket No. FAA–2017–0254; Product Identifier 2017–NE–10–AD. (a) Effective Date This AD is effective November 13, 2017. (b) Affected ADs None. (d) Subject Joint Aircraft System Component (JASC), 7270, Turbine Engine Bypass Section. (e) Unsafe Condition This AD was prompted by a report that using a certain repair procedure for the fan outlet guide vane (OGV) frame could alter the strength capability of the fan OGV frame. We are issuing this AD to prevent failure of the fan OGV frame, engine separation, and loss of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions (1) For engines with a fan OGV frame installed that was repaired using GE CF34– 8E Engine Manual, GEK 112031, 72–00–23, REPAIR 006: (i) If the fan OGV frame has 24,900 cycles since new (CSN) or more on the effective date of this AD, remove the OGV frame from service within 100 cycles after the effective date of this AD. (ii) If the OGV frame has less than 24,900 CSN on the effective date of this AD, remove the fan OGV frame from service at the next shop visit after the effective date of this AD, or before exceeding 25,000 CSN, whichever occurs earlier. (2) After the effective date of this AD, do not install a fan OGV frame that was repaired using GE CF34–8E Engine Manual, GEK 112031, 72–00–23, REPAIR 006. (h) Definition For the purpose of this AD, an ‘‘engine shop visit’’ is the induction of an engine into the shop for maintenance involving the Frm 00017 Fmt 4700 (1) The Manager, ECO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the certification office, send it to the attention of the person identified in paragraph (j)(1) of this AD. You may email your request to: ANE–AD–AMOC@ faa.gov. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/ certificate holding district office. (j) Related Information (c) Applicability This AD applies to all General Electric Company (GE) CF34–8E2; CF34–8E2A1; CF34–8E5; CF34–8E5A1; CF34–8E5A2; CF34–8E6; and CF34–8E6A1 model turbofan engines. PO 00000 separation of pairs of major mating engine flanges. (i) Alternative Methods of Compliance (AMOCs) PART 39—AIRWORTHINESS DIRECTIVES § 39.13 46671 Sfmt 9990 (1) For more information about this AD, contact David Bethka, Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone: 781–238– 7129; fax: 781–238–7199; email: david.bethka@faa.gov. (2) For General Electric service information identified in this AD, contact General Electric Company, GE-Aviation, Room 285, 1 Neumann Way, Cincinnati, OH 45215, phone: 513–552–3272; fax: 513–552–3329; email: geae.aoc@ge.com. You may view this service information at the FAA, Engine and Propeller Standards Branch, 1200 District Avenue, Burlington, MA. For information on the availability of this material at the FAA, call 781–238–7125. (k) Material Incorporated by Reference None. Issued in Burlington, Massachusetts, on September 28, 2017. Robert J. Ganley, Manager, Engine and Propeller Standards Branch, Aircraft Certification Service. [FR Doc. 2017–21345 Filed 10–5–17; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF THE TREASURY Internal Revenue Service 26 CFR Part 1 Income Taxes CFR Correction In Title 26 of the Code of Federal Regulations, Part 26, §§ 1.401 to 1.409, revised as of April 1, 2017, on page 235, in § 1.401(a)(9)–6, at the end of paragraph (d)(3)(i), insert the words ‘‘as of the date of purchase’’. [FR Doc. 2017–21742 Filed 10–5–17; 8:45 am] BILLING CODE 1301–00–D E:\FR\FM\06OCR1.SGM 06OCR1

Agencies

[Federal Register Volume 82, Number 193 (Friday, October 6, 2017)]
[Rules and Regulations]
[Page 46671]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-21742]


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DEPARTMENT OF THE TREASURY

Internal Revenue Service

26 CFR Part 1


Income Taxes

CFR Correction

    In Title 26 of the Code of Federal Regulations, Part 26, Sec. Sec.  
1.401 to 1.409, revised as of April 1, 2017, on page 235, in Sec.  
1.401(a)(9)-6, at the end of paragraph (d)(3)(i), insert the words ``as 
of the date of purchase''.

[FR Doc. 2017-21742 Filed 10-5-17; 8:45 am]
BILLING CODE 1301-00-D