[Federal Register Volume 79, Number 119 (Friday, June 20, 2014)]
[Rules and Regulations]
[Page 35290]
[FR Doc No: 2014-14607]

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ENVIRONMENTAL PROTECTION AGENCY

40 CFR Part 261

Identification and Listing of Hazardous Waste

CFR Correction

0
In Title 40 of the Code of Federal Regulations, Parts 260 to 265,
revised as of July 1, 2013, on page 37, in Sec.  261.3, paragraphs
(a)(2)(v)(A) and (B) are reinstated to read as follows:

Sec.  261.3  Definition of hazardous waste.

    (a) * * *
    (2) * * *
    (v) * * *
    (A) The rebuttable presumption does not apply to metalworking oils/
fluids containing chlorinated paraffins, if they are processed, through
a tolling agreement, to reclaim metalworking oils/fluids. The
presumption does apply to metalworking oils/fluids if such oils/fluids
are recycled in any other manner, or disposed.
    (B) The rebuttable presumption does not apply to used oils
contaminated with chlorofluorocarbons (CFCs) removed from refrigeration
units where the CFCs are destined for reclamation. The rebuttable
presumption does apply to used oils contaminated with CFCs that have
been mixed with used oil from sources other than refrigeration units.
* * * * *
[FR Doc. 2014-14607 Filed 6-19-14; 8:45 am]
BILLING CODE 1505-01-D


[Federal Register Volume 83, Number 23 (Friday, February 2, 2018)]
[Notices]
[Pages 4941-4942]
[FR Doc No: 2018-02130]

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SECURITIES AND EXCHANGE COMMISSION

[Release No. 34-82602; File No. SR-NYSEArca-2017-139]

Self-Regulatory Organizations; NYSE Arca, Inc.; Notice of
Designation of a Longer Period for Commission Action on a Proposed Rule
Change To List and Trade the Shares of the ProShares Bitcoin ETF and
the ProShares Short Bitcoin ETF Under NYSE Arca Rule 8.200-E,
Commentary .02

January 30, 2018.
    On December 4, 2017, NYSE Arca, Inc. (``NYSE Arca'') filed with the
Securities and Exchange Commission (``Commission''), pursuant to
Section 19(b)(1) of the Securities Exchange Act of 1934 (``Act'') \1\
and Rule 19b-4 thereunder,\2\ a proposed rule change to list and trade
the shares of the ProShares Bitcoin ETF and the ProShares Short Bitcoin
ETF under NYSE Arca Rule 8.200-E, Commentary .02. The proposed rule
change was published for comment in the Federal Register on December
26, 2017.\3\ The

Commission has received one comment letter on the proposed rule
change.\4\
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    \1\ 15 U.S.C. 78s(b)(1).
    \2\ 17 CFR 240.19b-4.
    \3\ See Securities Exchange Act Release No. 82350 (Dec. 19,
2017), 82 FR 61100.
    \4\ See Letter from Abe Kohen, AK Financial Engineering
Consultants, LLC (Dec. 27, 2017). All comments on the proposed rule
change are available on the Commission's website at: https://www.sec.gov/comments/sr-nysearca-2017-139/nysearca2017139.htm.
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    Section 19(b)(2) of the Act \5\ provides that within 45 days of the
publication of notice of the filing of a proposed rule change, or
within such longer period up to 90 days as the Commission may designate
if it finds such longer period to be appropriate and publishes its
reasons for so finding or as to which the self-regulatory organization
consents, the Commission shall either approve the proposed rule change,
disapprove the proposed rule change, or institute proceedings to
determine whether the proposed rule change should be disapproved. The
Commission is extending this 45-day time period. The Commission finds
that it is appropriate to designate a longer period within which to
take action on the proposed rule change so that it has sufficient time
to consider the proposed rule change.
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    \5\ 15 U.S.C. 78s(b)(2).
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    Accordingly, the Commission, pursuant to Section 19(b)(2) of the
Act,\6\ designates March 26, 2018, as the date by which the Commission
shall either approve or disapprove, or institute proceedings to
determine whether to disapprove, the proposed rule change (File No. SR-
NYSEArca-2017-139).
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    \6\ Id.

    For the Commission, by the Division of Trading and Markets,
pursuant to delegated authority.\7\
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    \7\ 17 CFR 200.30-3(a)(31).
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Eduardo A. Aleman,
Assistant Secretary.
[FR Doc. 2018-02130 Filed 2-1-18; 8:45 am]
 BILLING CODE 8011-01-P


[Federal Register Volume 81, Number 60 (Tuesday, March 29, 2016)]
[Rules and Regulations]
[Pages 17369-17372]
[FR Doc No: 2016-06401]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2015-2966; Directorate Identifier 2015-NM-051-AD;
Amendment 39-18441; AD 2016-06-10]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
The Boeing Company Model 787-8 airplanes. This AD was prompted by a
report of fuel leaking onto the hot exhaust portion of an engine as a
result of an unintended leak path from the leading edge through the
pylon. This AD requires installing new seal dams in the inboard and
outboard corners of the aft pylon frame on the left and right engines,
including an inspection for damage of the outboard blade seal and
applicable corrective actions. We are issuing this AD to prevent fuel
leaking from an unintended drain path from the leading edge through
either the left or right pylon and onto the hot engine parts or brakes,
which could lead to a major ground fire.

DATES: This AD is effective May 3, 2016.
    The Director of the Federal Register approved the incorporation by
reference of certain publication listed in this AD as of May 3, 2016.

ADDRESSES: For service information identified in this final rule,
contact Boeing Commercial Airplanes, Attention: Data & Services
Management, P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone
206-544-5000, extension 1; fax<PHONE_NUMBER>; Internet https://www.myboeingfleet.com. You may view this referenced service information
at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW.,
Renton, WA. For information on the availability of this material at the
FAA, call<PHONE_NUMBER>. It is also available on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015-
2966.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015-
2966; or in person at the Docket Management Facility between 9 a.m.

and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this AD, the regulatory evaluation, any comments
received, and other information. The address for the Docket Office
(phone:<PHONE_NUMBER>) is Docket Management Facility, U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Sherry Vevea, Aerospace Engineer,
Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification Office
(ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-
6514; fax:<PHONE_NUMBER>; email<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain The Boeing Company
Model 787-8 airplanes. The NPRM published in the Federal Register on
July 30, 2015 (80 FR 45460) (``the NPRM''). The NPRM was prompted by a
report of fuel leaking onto the hot exhaust portion of an engine as a
result of an unintended leak path from the leading edge through the
pylon. The NPRM proposed to require installing new seal dams in the
inboard and outboard corners of the aft pylon frame on the left and
right engines, including an inspection for damage of the outboard blade
seal and applicable corrective actions. We are issuing this AD to
prevent fuel leaking from an unintended drain path from the leading
edge through either the left or right pylon and onto the hot engine
parts or brakes, which could lead to a major ground fire.

Comments

    We gave the public the opportunity to participate in developing
this AD. The following presents the comments received on the NPRM and
the FAA's response to each comment. United Airlines concurred with the
content of the NPRM.

Request To Add Revised Service Information

    Boeing and All Nippon Airways (ANA) asked that we reference Boeing
Alert Service Bulletin B787-81205-SB540004-00, Issue 002, dated
December 3, 2015, for accomplishing the actions in the NPRM. ANA stated
that there are several errors in the referenced service information.
Boeing stated that a revision would be issued to incorporate minor
clarifications, and to update the effectivity.
    We agree to reference Boeing Alert Service Bulletin B787-81205-
SB540004-00, Issue 002, dated December 3, 2015, in this AD. Since we
published the NPRM, Boeing issued Alert Service Bulletin B787-81205-
SB540004-00, Issue 002, dated December 3, 2015. That revision removes
three airplanes from the effectivity, and clarifies certain
instructions as a result of feedback reported by operators after
incorporation of Boeing Alert Service Bulletin B787-81205-SB540004-00,
Issue 001, dated October 24, 2014. Boeing Alert Service Bulletin B787-
81205-SB540004-00, Issue 001, dated October 24, 2014, was specified as
the appropriate source of service information for accomplishing the
actions in the NPRM.
    We have changed paragraphs (c) and (g) of this AD to specify Boeing
Alert Service Bulletin B787-81205-SB540004-00, Issue 002, dated
December 3, 2015. We have also added a new paragraph (h) of this AD to
give credit for actions done before the effective date of this AD using
Boeing Alert Service Bulletin B787-81205-SB540004-00, Issue 001, dated
October 24, 2014; and redesignated subsequent paragraphs accordingly.

Request To Reduce the Compliance Time

    The Air Line Pilots Association (ALPA) International asked that we
reduce the compliance time specified in the proposed AD (the proposed
compliance time is within 60 months after the effective date of this
AD). ALPA stated that the severity of a fuel leak from the leading edge
through the pylon and onto the hot exhaust part of the engines warrants
a shorter compliance time to correct this problem.
    We do not agree with the commenter's request to reduce the
compliance time. In developing an appropriate compliance time, we
considered the safety implications and normal maintenance schedules for
timely installation of inboard and outboard seal dams. In consideration
of all of these factors, we determined that the compliance time, as
proposed, represents an appropriate interval in which the inboard and
outboard seal dams can be installed in a timely manner within the
fleet, while still maintaining an adequate level of safety. Most ADs,
including this one, permit operators to accomplish the requirements of
an AD at a time earlier than the specified compliance time; therefore,
an operator may choose to install the inboard and outboard seal dams
before the 60-month compliance time specified in paragraph (g) of this
AD. If additional data are presented that would justify a shorter
compliance time, we may consider further rulemaking on this issue. We
have not changed this AD in this regard.

Conclusion

    We reviewed the relevant data, considered the comments received,
and determined that air safety and the public interest require adopting
this AD with the changes described previously and minor editorial
changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
     Do not add any additional burden upon the public than was
already proposed in the NPRM.
    We also determined that these changes will not increase the
economic burden on any operator or increase the scope of this AD.

Related Service Information Under 1 CFR Part 51

    We reviewed Boeing Alert Service Bulletin B787-81205-SB540004-00,
Issue 002, dated December 3, 2015. This service information describes
procedures for installing new seal dams in the inboard and outboard
corners of the aft pylon frame on the left and right engines, doing a
general visual inspection to detect damage of the outboard blade seal,
and doing corrective actions. This service information is reasonably
available because the interested parties have access to it through
their normal course of business or by the means identified in the
ADDRESSES section.

Costs of Compliance

    We estimate that this AD affects 17 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Cost on U.S.
             Action                   Labor cost          Parts cost       Cost per product        operators
----------------------------------------------------------------------------------------------------------------
Installation of seal dams.......  Up to 22 work-      Up to $14,611.....  Up to $16,481.....  Up to $280,177.
                                   hours x $85 per
                                   hour = $1,870.
----------------------------------------------------------------------------------------------------------------

    According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all costs in our cost
estimate.

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.
    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.

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, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness
directive (AD):

2016-06-10 The Boeing Company: Amendment 39-18441; Docket No. FAA-
2015-2966; Directorate Identifier 2015-NM-051-AD.

(a) Effective Date

    This AD is effective May 3, 2016.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to The Boeing Company Model 787-8 airplanes,
certificated in any category, as identified in Boeing Alert Service
Bulletin B787-81205-SB540004-00, Issue 002, dated December 3, 2015.

(d) Subject

    Air Transport Association (ATA) of America Code 54, Nacelles/
pylons.

(e) Unsafe Condition

    This AD was prompted by a report of fuel leaking onto the hot
exhaust portion of the engine as a result of an unintended leak path
from the leading edge through the pylon. We are issuing this AD to
prevent fuel leaking from an unintended drain path from the leading
edge through either the left or right pylon and onto the hot engine
parts or brakes, which could lead to a major ground fire.

(f) Compliance

    Comply with this AD within the compliance times specified,
unless already done.

(g) Installation of Inboard and Outboard Seal Dams

    Within 60 months after the effective date of this AD, install
new seal dams in the inboard and outboard corners of the aft pylon
frame on the left and right engines, including a general visual
inspection to detect damage of the outboard blade seal, and do all
applicable corrective actions, in accordance with the Accomplishment
Instructions of Boeing Alert Service Bulletin B787-81205-SB540004-
00, Issue 002, dated December 3, 2015. Do all applicable corrective
actions before further flight, in accordance with the Accomplishment
Instructions of Boeing Alert Service Bulletin B787-81205-SB540004-
00, Issue 002, dated December 3, 2015.

(h) Credit for Previous Actions

    This paragraph provides credit for actions required by paragraph
(g) of this AD, if those actions were performed before the effective
date of this AD using Boeing Alert Service Bulletin B787-81205-
SB540004-00, Issue 001, dated October 24, 2014; which is not
incorporated by reference in this AD.

(i) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Seattle Aircraft Certification Office (ACO),
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 ACO, send it to the
attention of the person identified in paragraph (j)(1) of this AD.
Information may be emailed to<EMAIL_ADDRESS>    (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.
    (3) An AMOC that provides an acceptable level of safety may be
used for any repair, modification, or alteration required by this AD
if it is approved by the Boeing Commercial Airplanes Organization
Designation Authorization (ODA) that has been authorized by the
Manager, Seattle ACO, to make those findings. To be approved, the
repair method, modification deviation, or alteration deviation must
meet the certification basis of the airplane, and the approval must
specifically refer to this AD.

(j) Related Information

    (1) For more information about this AD, contact Sherry Vevea,
Aerospace Engineer, Propulsion Branch, ANM-140S, FAA, Seattle ACO,
1601 Lind Avenue SW., Renton, WA 98057-3356; phone:<PHONE_NUMBER>;
fax:<PHONE_NUMBER>; email<EMAIL_ADDRESS>    (2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (k)(3) and (k)(4) of this AD.

(k) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
    (i) Boeing Alert Service Bulletin B787-81205-SB540004-00, Issue
002, dated December 3, 2015.
    (ii) Reserved.
    (3) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone 206-544-
5000, extension 1; fax<PHONE_NUMBER>; Internet https://www.myboeingfleet.com.
    (4) You may view this service information at FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
    (5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call<PHONE_NUMBER>, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on March 14, 2016.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-06401 Filed 3-28-16; 8:45 am]
BILLING CODE 4910-13-P