Investing in Qualified Opportunity Funds, 22987 [C1-2019-08075]

Download as PDF Federal Register / Vol. 84, No. 98 / Tuesday, May 21, 2019 / Proposed Rules 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. The FAA is 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. jbell on DSK3GLQ082PROD with PROPOSALS Regulatory Findings The FAA 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 this proposed regulation: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, (2) Will not affect intrastate aviation in Alaska, 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. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. VerDate Sep<11>2014 16:36 May 20, 2019 Jkt 247001 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): ■ GE Honda Aero Engines: Docket No. FAA– 2019–0352; Product Identifier 2019–NE– 09–AD. (a) Comments Due Date The FAA must receive comments by July 5, 2019. (b) Affected ADs None. (c) Applicability This AD applies to all GE Honda Aero Engines (GHAE) HF120 turbofan engines with fuel pump metering unit (FPMU) assembly, part number (P/N) 24100–Q0A– F000, installed. (d) Subject Joint Aircraft System Component (JASC) Code 7314, Engine Fuel Pump. (e) Unsafe Condition This AD was prompted by damage found on the permanent magnetic alternator (PMA) drive gear within the FPMU assembly. The FAA is issuing this AD to prevent failure of the FPMU assembly. The unsafe condition, if not addressed, could result in failure of one or more engines, loss of thrust control, and loss of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Within 20 engine hours after the effective date of this AD, or before accumulating 600 engine hours time since new, whichever occurs later, remove the affected FPMU assembly and replace it with a part eligible for installation. (h) Installation Prohibition After the effective date of this AD, do not install on any engine a FPMU assembly, P/N 24100–Q0A–F000. (i) Definition For the purposes of this AD, a ‘‘part eligible for installation’’ is: (1) A FPMU assembly, P/N 24100–Q0A– G000 or P/N 24100–Q0A–F100; or (2) a FPMU assembly, P/N 24100–Q0A– F000, that is rebuilt and marked as P/N 24100–Q0A–G000 or P/N 24100–Q0A–F100. PO 00000 Frm 00002 Fmt 4702 Sfmt 9990 22987 (j) Alternative Methods of Compliance (AMOCs) (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 (k)(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. (k) Related Information (1) For more information about this AD, contact Michael Richardson-Bach, Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone: 781– 238–7747; fax: 781–238–7199; email: michael.richardson-bach@faa.gov. (2) For service information identified in this AD, contact GE Honda Aero Engines, LLC, 9050 Centre Pointe Drive, Suite 200, West Chester, OH 45069; phone 513–552– 7820; email: info@honda-aero.com; internet: www.gehonda.com. You may view this referenced service information at the FAA, Engine and Propeller Standards Branch, 1200 District Avenue, Burlington, MA 01803. For information on the availability of this material at the FAA, call 781–238–7759. Issued in Burlington, Massachusetts, on May 15, 2019. Robert J. Ganley, Manager, Engine & Propeller Standards Branch, Aircraft Certification Service. [FR Doc. 2019–10525 Filed 5–20–19; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF THE TREASURY Internal Revenue Service 26 CFR Part 1 [REG–120186–18] RIN 1545–BP04 Investing in Qualified Opportunity Funds Correction In proposed rule document 2019– 08075 beginning on page 18652 in the issue of Wednesday, May 1, 2019 make the following correction: On pages 18652 through 18693 the date at the top of the page should read ‘‘Wednesday, May 1, 2019’’. [FR Doc. C1–2019–08075 Filed 5–20–19; 8:45 am] BILLING CODE 1301–00–D E:\FR\FM\21MYP1.SGM 21MYP1

Agencies

[Federal Register Volume 84, Number 98 (Tuesday, May 21, 2019)]
[Proposed Rules]
[Page 22987]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C1-2019-08075]


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DEPARTMENT OF THE TREASURY

Internal Revenue Service

26 CFR Part 1

[REG-120186-18]
RIN 1545-BP04


Investing in Qualified Opportunity Funds

Correction

    In proposed rule document 2019-08075 beginning on page 18652 in the 
issue of Wednesday, May 1, 2019 make the following correction:
    On pages 18652 through 18693 the date at the top of the page should 
read ``Wednesday, May 1, 2019''.

[FR Doc. C1-2019-08075 Filed 5-20-19; 8:45 am]
BILLING CODE 1301-00-D