Income Taxes, 46671 [2017-21742]
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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.
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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
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]]>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
