82 FR 46671 - Income Taxes

DEPARTMENT OF THE TREASURY
Internal Revenue Service

Federal Register Volume 82, Issue 193 (October 6, 2017)

Page Range		46671-46671
FR Document		2017-21742

Federal Register, Volume 82 Issue 193 (Friday, October 6, 2017)

[Federal Register Volume 82, Number 193 (Friday, October 6, 2017)]
[Rules and Regulations]
[Page 46671]
From the Federal Register Online  [www.thefederalregister.org]
[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

Federal Register / Vol. 82, No. 193 / Friday, October 6, 2017 / Rules and Regulations 46671

rules on aviation safety. Subtitle I, the FAA amends 14 CFR part 39 as separation of pairs of major mating engine
section 106, describes the authority of follows: flanges.
the FAA Administrator. Subtitle VII: (i) Alternative Methods of Compliance
Aviation Programs, describes in more PART 39—AIRWORTHINESS (AMOCs)
detail the scope of the Agency’s DIRECTIVES
(1) The Manager, ECO Branch, FAA, has
authority. the authority to approve AMOCs for this AD,
We are issuing this rulemaking under ■ 1. The authority citation for part 39
continues to read as follows: if requested using the procedures found in 14
the authority described in Subtitle VII, CFR 39.19. In accordance with 14 CFR 39.19,
Part A, Subpart III, Section 44701: Authority: 49 U.S.C. 106(g), 40113, 44701. send your request to your principal inspector
‘‘General requirements.’’ Under that § 39.13 [Amended] or local Flight Standards District Office, as
section, Congress charges the FAA with appropriate. If sending information directly
promoting safe flight of civil aircraft in ■ 2. The FAA amends § 39.13 by adding to the manager of the certification office,
air commerce by prescribing regulations the following new airworthiness send it to the attention of the person
for practices, methods, and procedures directive (AD): identified in paragraph (j)(1) of this AD. You
the Administrator finds necessary for 2017–20–09 General Electric Company: may email your request to: ANE–AD–AMOC@
safety in air commerce. This regulation Amendment 39–19066; Docket No. faa.gov.
is within the scope of that authority FAA–2017–0254; Product Identifier (2) Before using any approved AMOC,
2017–NE–10–AD. notify your appropriate principal inspector,
because it addresses an unsafe condition
or lacking a principal inspector, the manager
that is likely to exist or develop on (a) Effective Date of the local flight standards district office/
products identified in this rulemaking This AD is effective November 13, 2017. certificate holding district office.
action.
This AD is issued in accordance with (b) Affected ADs (j) Related Information
authority delegated by the Executive None. (1) For more information about this AD,
Director, Aircraft Certification Service, (c) Applicability
contact David Bethka, Aerospace Engineer,
as authorized by FAA Order 8000.51C. ECO Branch, FAA, 1200 District Avenue,
In accordance with that order, issuance This AD applies to all General Electric Burlington, MA 01803; phone: 781–238–
Company (GE) CF34–8E2; CF34–8E2A1; 7129; fax: 781–238–7199; email:
of ADs is normally a function of the CF34–8E5; CF34–8E5A1; CF34–8E5A2;
Compliance and Airworthiness david.bethka@faa.gov.
CF34–8E6; and CF34–8E6A1 model turbofan (2) For General Electric service information
Division, but during this transition engines. identified in this AD, contact General Electric
period, the Executive Director has
(d) Subject Company, GE-Aviation, Room 285, 1
delegated the authority to issue ADs Neumann Way, Cincinnati, OH 45215,
applicable to engines, propellers, and Joint Aircraft System Component (JASC),
7270, Turbine Engine Bypass Section. phone: 513–552–3272; fax: 513–552–3329;
associated appliances to the Manager, email: geae.aoc@ge.com. You may view this
Engine and Propeller Standards Branch, (e) Unsafe Condition service information at the FAA, Engine and
Policy and Innovation Division. This AD was prompted by a report that Propeller Standards Branch, 1200 District
using a certain repair procedure for the fan Avenue, Burlington, MA. For information on
Regulatory Findings the availability of this material at the FAA,
outlet guide vane (OGV) frame could alter the
This AD will not have federalism strength capability of the fan OGV frame. We call 781–238–7125.
implications under Executive Order are issuing this AD to prevent failure of the (k) Material Incorporated by Reference
13132. This AD will not have a fan OGV frame, engine separation, and loss
substantial direct effect on the States, on of the airplane. None.
the relationship between the national (f) Compliance Issued in Burlington, Massachusetts, on
government and the States, or on the September 28, 2017.
Comply with this AD within the
distribution of power and compliance times specified, unless already Robert J. Ganley,
responsibilities among the various done. Manager, Engine and Propeller Standards
levels of government. Branch, Aircraft Certification Service.
For the reasons discussed above, I (g) Required Actions
[FR Doc. 2017–21345 Filed 10–5–17; 8:45 am]
certify that this AD: (1) For engines with a fan OGV frame BILLING CODE 4910–13–P
(1) Is not a ‘‘significant regulatory installed that was repaired using GE CF34–
action’’ under Executive Order 12866, 8E Engine Manual, GEK 112031, 72–00–23,
(2) Is not a ‘‘significant rule’’ under REPAIR 006:
DOT Regulatory Policies and Procedures (i) If the fan OGV frame has 24,900 cycles
since new (CSN) or more on the effective date DEPARTMENT OF THE TREASURY
(44 FR 11034, February 26, 1979), of this AD, remove the OGV frame from
(3) Will not affect intrastate aviation service within 100 cycles after the effective Internal Revenue Service
in Alaska, and date of this AD.
(4) Will not have a significant (ii) If the OGV frame has less than 24,900 26 CFR Part 1
economic impact, positive or negative, CSN on the effective date of this AD, remove
on a substantial number of small entities the fan OGV frame from service at the next Income Taxes
under the criteria of the Regulatory shop visit after the effective date of this AD,
Flexibility Act. or before exceeding 25,000 CSN, whichever CFR Correction
occurs earlier.
asabaliauskas on DSKBBXCHB2PROD with RULES

List of Subjects in 14 CFR Part 39 (2) After the effective date of this AD, do In Title 26 of the Code of Federal
not install a fan OGV frame that was repaired Regulations, Part 26, §§ 1.401 to 1.409,
Air transportation, Aircraft, Aviation
using GE CF34–8E Engine Manual, GEK revised as of April 1, 2017, on page 235,
safety, Incorporation by reference,
112031, 72–00–23, REPAIR 006. in § 1.401(a)(9)–6, at the end of
Safety.
(h) Definition paragraph (d)(3)(i), insert the words ‘‘as
Adoption of the Amendment of the date of purchase’’.
For the purpose of this AD, an ‘‘engine
Accordingly, under the authority shop visit’’ is the induction of an engine into [FR Doc. 2017–21742 Filed 10–5–17; 8:45 am]
delegated to me by the Administrator, the shop for maintenance involving the BILLING CODE 1301–00–D

VerDate Sep<11>2014 16:21 Oct 05, 2017 Jkt 244001 PO 00000 Frm 00017 Fmt 4700 Sfmt 9990 E:\FR\FM\06OCR1.SGM 06OCR1

Document Created: 2017-10-06 00:08:57
Document Modified: 2017-10-06 00:08:57

Category		Regulatory Information
Collection		Federal Register
sudoc Class		AE 2.7: GS 4.107: AE 2.106:
Publisher		Office of the Federal Register, National Archives and Records Administration
Section		Rules and Regulations
FR Citation		82 FR 46671

82 FR 46671 - Income Taxes

DEPARTMENT OF THE TREASURYInternal Revenue Service

Federal Register Volume 82, Issue 193 (October 6, 2017)

DEPARTMENT OF THE TREASURY
Internal Revenue Service