[Federal Register Volume 85, Number 96 (Monday, May 18, 2020)]
[Notices]
[Page 29777]
[FR Doc No: 2020-10623]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

[Summary Notice No. 2020-16]

Petition for Exemption; Summary of Petition Received; Patrick
Tohill

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Notice.

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SUMMARY: This notice contains a summary of a petition seeking relief
from specified requirements of Federal Aviation Regulations. The
purpose of this notice is to improve the public's awareness of, and
participation in, the FAA's exemption process. Neither publication of
this notice nor the inclusion or omission of information in the summary
is intended to affect the legal status of the petition or its final
disposition.

DATES: Comments on this petition must identify the petition docket
number and must be received on or before June 8, 2020.

ADDRESSES: Send comments identified by docket number FAA-2020-0226
using any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov and follow the online instructions for sending your
comments electronically.
     Mail: Send comments to Docket Operations, M-30; U.S.
Department of Transportation, 1200 New Jersey Avenue SE, Room W12-140,
West Building Ground Floor, Washington, DC 20590-0001.
     Hand Delivery or Courier: Take comments to Docket
Operations in Room W12-140 of the West Building Ground Floor at 1200
New Jersey Avenue SE, Washington, DC 20590-0001, between 9 a.m. and 5
p.m., Monday through Friday, except Federal holidays.
     Fax: Fax comments to Docket Operations at<PHONE_NUMBER>.
    Privacy: In accordance with 5 U.S.C. 553(c), DOT solicits comments
from the public to better inform its rulemaking process. DOT posts
these comments, without edit, including any personal information the
commenter provides, to http://www.regulations.gov, as described in the
system of records notice (DOT/ALL-14 FDMS), which can be reviewed at
http://www.dot.gov/privacy.
    Docket: Background documents or comments received may be read at
http://www.regulations.gov at any time. Follow the online instructions
for accessing the docket or go to the Docket Operations in Room W12-140
of the West Building Ground Floor at 1200 New Jersey Avenue SE,
Washington, DC 20590-0001, between 9 a.m. and 5 p.m., Monday through
Friday, except Federal holidays.

FOR FURTHER INFORMATION CONTACT: Jake Troutman<PHONE_NUMBER>, Office
of Rulemaking, Federal Aviation Administration, 800 Independence Avenue
SW, Washington, DC 20591.
    This notice is published pursuant to 14 CFR 11.85.

    Issued in Washington, DC, on May 13, 2020.
Brandon Roberts,
Deputy Executive Director, Office of Rulemaking.

Petition for Exemption

    Docket No.: FAA-2020-0226
    Petitioner: Patrick Tohill
    Section(s) of 14 CFR Affected: Sec. Sec.  61.3(a)(1)(i); 91.119(c);
91.121; 91.151(b); 91.405(a); 91.407(a)(1); 91.409(a)(1) & (2); &
91.417(a) & (b).
    Description of Relief Sought: The proposed exemption, if granted,
would allow the petitioner to operate the Freefly Systems, Inc. Alta X
unmanned aircraft system, over 55 pounds (lbs.) but no more than 70
lbs., for controlled, low-risk, closed-set aerial cinematography
operations for the television and motion picture industry.

[FR Doc. 2020-10623 Filed 5-15-20; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register: March 1, 2006 (Volume 71, Number 40)]
[Notices]
[Page 10491]
[DOCID:fr01mr06-42]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. RP06-222-000]

Viking Gas Transmission Company; Notice of Tariff Filing

February 22, 2006.
    Take notice that on February 15, 2006, Viking Gas Transmission
Company (Viking) tendered for filing to be part of its FERC Gas Tariff,
First Revised Volume No. 1, Sixteenth Revised Sheet No. 5B, to become
effective April 1, 2006.
    Any person desiring to intervene or to protest this filing must
file in accordance with Rules 211 and 214 of the Commission's Rules of
Practice and Procedure (18 CFR 385.211 and 385.214). Protests will be
considered by the Commission in determining the appropriate action to
be taken, but will not serve to make protestants parties to the
proceeding. Any person wishing to become a party must file a notice of
intervention or motion to intervene, as appropriate. Such notices,
motions, or protests must be filed in accordance with the provisions of
Section 154.210 of the Commission's regulations (18 CFR 154.210).
Anyone filing an intervention or protest must serve a copy of that
document on the Applicant. Anyone filing an intervention or protest on
or before the intervention or protest date need not serve motions to
intervene or protests on persons other than the Applicant.
    The Commission encourages electronic submission of protests and
interventions in lieu of paper using the ``eFiling'' link at http://www.ferc.gov.
 Persons unable to file electronically should submit an

original and 14 copies of the protest or intervention to the Federal
Energy Regulatory Commission, 888 First Street, NE., Washington, DC
20426.
    This filing is accessible on-line at http://www.ferc.gov, using the

``eLibrary'' link and is available for review in the Commission's
Public Reference Room in Washington, DC. There is an ``eSubscription''
link on the Web site that enables subscribers to receive email
notification when a document is added to a subscribed docket(s). For
assistance with any FERC Online service, please email
<EMAIL_ADDRESS>or call<PHONE_NUMBER> (toll free). For

TTY, call<PHONE_NUMBER>.

Magalie R. Salas,
Secretary.
[FR Doc. E6-2869 Filed 2-28-06; 8:45 am]

BILLING CODE 6717-01-P


[Federal Register Volume 76, Number 250 (Thursday, December 29, 2011)]
[Notices]
[Page 81923]
[FR Doc No: 2011-33317]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. EL12-14-000]

Trans-Allegheny Interstate Line Company; Notice of Amendment To
Petition for Declaratory Order

    Take notice that on December 20, 2011, Trans-Allegheny Interstate
Line Company (TrAILCo) filed an amendment to its December 14, 2011
filing of Petition for Declaratory Order, in response to the Federal
Energy Regulatory Commission Staff's informal request.
    Any person desiring to intervene or to protest this filing must
file in accordance with Rules 211 and 214 of the Commission's Rules of
Practice and Procedure (18 CFR 385.211, 385.214). Protests will be
considered by the Commission in determining the appropriate action to
be taken, but will not serve to make protestants parties to the
proceeding. Any person wishing to become a party must file a notice of
intervention or motion to intervene, as appropriate. Such notices,
motions, or protests must be filed on or before the comment date. On or
before the comment date, it is not necessary to serve motions to
intervene or protests on persons other than the Applicant.
    The Commission encourages electronic submission of protests and
interventions in lieu of paper using the ``eFiling'' link at http://www.ferc.gov. Persons unable to file electronically should submit an
original and 14 copies of the protest or intervention to the Federal
Energy Regulatory Commission, 888 First Street NE., Washington, DC
20426.
    This filing is accessible on-line at http://www.ferc.gov, using the
``eLibrary'' link and is available for review in the Commission's
Public Reference Room in Washington, DC. There is an ``eSubscription''
link on the Web site that enables subscribers to receive email
notification when a document is added to a subscribed docket(s). For
assistance with any FERC Online service, please email
<EMAIL_ADDRESS>or call<PHONE_NUMBER> (toll free). For
TTY, call<PHONE_NUMBER>.
    Comment Date: 5 p.m. Eastern Time on December 27, 2011.

    Dated: December 21, 2011.
Kimberly D. Bose,
Secretary.
[FR Doc. 2011-33317 Filed 12-28-11; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register Volume 78, Number 248 (Thursday, December 26, 2013)]
[Notices]
[Page 78349]
[FR Doc No: 2013-30782]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket Nos. EL14-15-000; ER13-2412-000 (Not consolidated)]

Cities of Anaheim, Azusa, Banning, Colton, Pasadena, Riverside,
CA v. Trans Bay Cable LLC; Notice of Complaint

    Take notice that on December 17, 2013, pursuant to sections 206 and
306 of the Federal Power Act (FPA); 16 U.S.C. 824e and 825e (2013), and
Rule 206 and 212 of the Federal Energy Regulatory Commission's
(Commission) Rules of Practice and Procedure, 18 CFR 385.206 and 18 CFR
385.212 (2013), the Cities of Anaheim, Azusa, Banning, Colton,
Pasadena, and Riverside, CA (collectively, Six Cities or Complainants)
filed a formal complaint against Trans Bay Cable LLC (Trans Bay or
Respondent), alleging that Trans Bay's transmission revenue requirement
(TRR) is unjust and unreasonable and should be reduced below the
currently-effective level. Six Cities request to consolidate this
complaint with Trans Bay's TRR proceeding in Docket No. ER13-2412-000,
as more fully described in this complaint.
    The Complainants certify that copies of the complaint were served
on the contacts for the Respondents as listed on the Commission's list
of Corporate Officials.
    Any person desiring to intervene or to protest this filing must
file in accordance with Rules 211 and 214 of the Commission's Rules of
Practice and Procedure (18 CFR 385.211, 385.214). Protests will be
considered by the Commission in determining the appropriate action to
be taken, but will not serve to make protestants parties to the
proceeding. Any person wishing to become a party must file a notice of
intervention or motion to intervene, as appropriate. The Respondent's
answer and all interventions, or protests must be filed on or before
the comment date. The Respondent's answer, motions to intervene, and
protests must be served on the Complainants.
    The Commission encourages electronic submission of protests and
interventions in lieu of paper using the ``eFiling'' link at http://www.ferc.gov. Persons unable to file electronically should submit an
original and 5 copies of the protest or intervention to the Federal
Energy Regulatory Commission, 888 First Street NE., Washington, DC
20426.
    This filing is accessible on-line at http://www.ferc.gov, using the
``eLibrary'' link and is available for review in the Commission's
Public Reference Room in Washington, DC. There is an ``eSubscription''
link on the Web site that enables subscribers to receive email
notification when a document is added to a subscribed docket(s). For
assistance with any FERC Online service, please email
<EMAIL_ADDRESS>or call<PHONE_NUMBER> (toll free). For
TTY, call<PHONE_NUMBER>.
    Comment Date: 5:00 p.m. Eastern Time on January 6, 2014.

    Dated: December 18, 2013.
Kimberly D. Bose,
Secretary.
[FR Doc. 2013-30782 Filed 12-24-13; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register Volume 88, Number 118 (Wednesday, June 21, 2023)]
[Notices]
[Pages 40256-40257]
[FR Doc No: 2023-13188]

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ENVIRONMENTAL PROTECTION AGENCY

[EPA-HQ-ORD-2015-0765; FRL-10950-01-ORD]

Value of Information (VOI) Under the Board of Scientific
Counselors (BOSC)--July 2023

AGENCY: Environmental Protection Agency (EPA).

ACTION: Notice of public meeting.

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SUMMARY: The U.S. Environmental Protection Agency (EPA) has selected
technical experts to serve as Special Government Employees (SGEs) on a
review panel under the authority of the Board of Scientific Counselors
(BOSC), a federal advisory committee to the Office of Research and
Development (ORD). Selected experts will participate in the review of
the Office of Research and Development (ORD)'s draft report on a case
study that uses value of information (VOI) analysis to weigh the public
health and economic trade-offs associated with the timeliness,
uncertainty, and costs of the draft EPA Transcriptomic Assessment
Product (ETAP). The ETAP is a proposed ORD assessment product that
utilizes a standardized short-term in vivo study design and data
analysis procedures to develop a transcriptomic-based reference values
for data poor chemicals.

DATES: The meeting will be held on Tuesday, July 25, 2023, from 11 a.m.
to 5 p.m., and Wednesday, July 26, 2023, from 11 a.m. to 5 p.m. All
times noted are Eastern Time and approximate. The meeting may adjourn
early if all business is finished. Attendees should register by July
18, 2023, at https://EPA-VOI_July_meeting.eventbrite.com. Requests for
making oral presentations at the meeting will be accepted up to one
business day before the meeting. Comments may be submitted through
Friday, July 21, 2023.

ADDRESSES: Instructions on how to connect to the videoconference via
Zoom will be provided upon registration at: https://EPA-VOI_July_meeting.eventbrite.com. Please note that no Zoom information
for the meeting will be provided without registration.
     www.regulations.gov: Follow the on-line instructions for
submitting comments.
     Email: Send comments by electronic mail (email) to:
[email protected], Attention Docket ID No. EPA-HQ-ORD-2015-0765.
     Fax: Fax comments to:<PHONE_NUMBER>, Attention Docket ID
No. EPA-HQ-ORD-2015-0765.
     Mail: Send comments by mail to: Board of Scientific
Counselors (BOSC) Executive Committee Docket, Mail Code: 2822T, 1301
Constitution Ave. NW, Washington, DC 20004, Attention Docket ID No.
EPA-HQ-ORD-2015-0765.
     Hand Delivery or Courier: Deliver comments to: EPA Docket
Center (EPA/DC), Room 3334, William Jefferson Clinton West Building,
1301 Constitution Ave. NW, Washington, DC, Attention Docket ID No. EPA-
HQ-ORD-2015-0765. Note: This is not a mailing address. Deliveries are
only accepted during the docket's normal

hours of operation, and special arrangements should be made for
deliveries of boxed information.
    Instructions: The EPA's policy is that all comments received will
be included in the public docket without change and may be made
available online at www.regulations.gov including any personal
information provided unless the comment includes information claimed to
be Confidential Business Information (CBI) or other information whose
disclosure is restricted by statute. Do not submit information that you
consider to be CBI or otherwise protected through www.regulations.gov
or email. The www.regulations.gov website is an ``anonymous access''
system, which means the EPA will not know your identity or contact
information unless you provide it in the body of your comment. If you
send an email comment directly to the EPA without going through
www.regulations.gov your email address will be automatically captured
and included as part of the comment that is placed in the public docket
and made available on the internet. If you submit an electronic
comment, the EPA recommends that you include your name and other
contact information in the body of your comment and with any disk or
CD-ROM you submit. If the EPA cannot read your comment due to technical
difficulties and cannot contact you for clarification, the EPA may not
be able to consider your comment. Electronic files should avoid the use
of special characters, any form of encryption, and be free of any
defects or viruses. For additional information about the EPA's public
docket visit the EPA Docket Center homepage at http://www.epa.gov/dockets/.

FOR FURTHER INFORMATION CONTACT: The Designated Federal Officer (DFO),
Tom Tracy, via phone/voicemail at:<PHONE_NUMBER>; or via email at:
[email protected].

SUPPLEMENTARY INFORMATION:
    General Information: The meeting is open to the public. Any member
of the public interested in receiving a draft agenda, attending the
meeting, or making a presentation at the meeting may contact Tom Tracy,
the Designated Federal (DFO), via any of the contact methods listed in
the FOR FURTHER INFORMATION CONTACT section above. Individuals making
an oral presentation will be limited to a total of three minutes.
    For security purposes, all attendees must provide their names to
the DFO by registering online at https://EPA-VOI_July_meeting.eventbrite.com by July 21, 2023, and must go through a
metal detector, sign in with the security desk, and show REAL ID Act-
compliant government-issued photo identification to enter the building.
Attendees are encouraged to arrive at least 15 minutes prior to the
start of the meeting to allow enough time for security screening.
Proposed agenda items for the meeting include but are not limited to
the following: Review of charge questions, overview of the report
outlining the case study that uses VOI analysis to weigh the public
health and economic trade-offs associated with the timeliness,
uncertainty, and costs of the draft EPA Transcriptomic Assessment
Product (ETAP), and subcommittee deliberations.
    Information on Services for Individuals with Disabilities: For
information on access or services for individuals with disabilities,
please contact Tom Tracy<PHONE_NUMBER> or [email protected]. To
request accommodation of a disability, please contact Tom Tracy,
preferably at least ten days prior to the meeting, to give the EPA as
much time as possible to process your request.

Mary Ross,
Director, Office of Science Advisor, Policy, and Engagement.
[FR Doc. 2023-13188 Filed 6-20-23; 8:45 am]
BILLING CODE 6560-50-P


[Federal Register Volume 76, Number 213 (Thursday, November 3, 2011)]
[Notices]
[Pages 68237-68238]
[FR Doc No: 2011-28460]

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SECURITIES AND EXCHANGE COMMISSION

[Release No. 34-65653; File No. SR-NASDAQ-2011-122]

Self-Regulatory Organizations; The NASDAQ Stock Market LLC;
Notice of Designation of a Longer Period for Commission Action on
Proposed Rule Change To Describe Complimentary Services That Are
Offered to Certain New Listings on NASDAQ's Global and Global Select
Markets

October 28, 2011.
    On August 30, 2011, The NASDAQ Stock Market LLC (``NASDAQ'' or
``Exchange'') 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 add rule text explaining services offered by
NASDAQ to certain newly listing companies and the retail value of such
services. The proposed rule change was published for comment in the
Federal

Register on September 16, 2011.\3\ The Commission received four comment
letters on the proposal.\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. 65324 (September 12,
2011), 76 FR 57781 (September 16, 2011).
    \4\ See Letters to Elizabeth M. Murphy, Secretary, Commission,
from Neil Hershberg, Senior Vice President, Business Wire Inc.,
dated September 28, 2011; John Viglotti, Vice President, PR Newswire
Association LLC, dated October 7, 2011; Jesse W. Markham, Jr., Roger
Myers, and Michael R. MacPhail, Holme Roberts & Owen LLP (writing on
behalf of Business Wire, Inc.), dated October 7, 2011; and Patrick
Healy, CEO, Issuer Advisory Group LLC, dated October 22, 2011.
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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
45th day for this filing is October 31, 2011.
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    \5\ 15 U.S.C. 78s(b)(2).
---------------------------------------------------------------------------

    The Commission is extending the 45-day time period for Commission
action on the proposed rule change. 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
Exchange's proposal, as described above, and to consider the comment
letters that have been submitted in connection with the proposed rule
change.
    Accordingly, pursuant to Section 19(b)(2) of the Act,\6\ the
Commission designates December 15, 2011 as the date by which the
Commission should either approve or disapprove, or institute
proceedings to determine whether to disapprove, the proposed rule
change (File Number SR-NASDAQ-2011-122).
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    \6\ 15 U.S.C. 78s(b)(2).

    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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Kevin M. O'Neill,
Deputy Secretary.
[FR Doc. 2011-28460 Filed 11-2-11; 8:45 am]
BILLING CODE 8011-01-P


[Federal Register: March 5, 2008 (Volume 73, Number 44)]
[Notices]
[Page 11970-11971]
[DOCID:fr05mr08-115]

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SECURITIES AND EXCHANGE COMMISSION

[Release No. 34-57385; File No. SR-NSCC-2007-17]

Self-Regulatory Organizations; the National Securities Clearing
Corporation; Notice of Filing and Immediate Effectiveness of a Proposed
Rule Change Relating to the Fee Schedule

February 27, 2008.
    Pursuant to section 19(b)(1) of the Securities Exchange Act of 1934
(``Act''),\1\ notice is hereby given that on December 31, 2007, the
National Securities Clearing Corporation (``NSCC'') filed with the
Securities and Exchange Commission (``Commission'') the proposed rule
change as described in Items I, II, and III below, which items have
been prepared primarily by NSCC. The Commission is publishing this
notice to solicit comments on the proposed rule change from interested
persons.
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    \1\ 15 U.S.C. 78s(b)(1).
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I. Self-Regulatory Organization's Statement of the Terms of Substance
of the Proposed Rule Change

    The proposed rule change modifies NSCC's fee schedule.

II. Self-Regulatory Organization's Statement of the Purpose of, and
Statutory Basis for, the Proposed Rule Change

    In its filing with the Commission, NSCC included statements
concerning the purpose of and basis for the proposed rule change and
discussed any comments it received on the proposed rule change. The
text of these statements may be examined at the places specified in
Item IV below. NSCC has prepared summaries, set forth in sections (A),
(B), and (C) below, of the most significant aspects of such
statements.\2\
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    \2\ The Commission has modified parts of these statements.
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(A) Self-Regulatory Organization's Statement of the Purpose of, and
Statutory Basis for, the Proposed Rule Change

    The purpose of the proposed rule change is to revise fees for
certain services provided by NSCC. These revisions include the
following fee changes to align fees with costs of delivering services:
    1. Implementation of a restructured clearing fee model, changing
from the current solely transaction-based pricing structure to a
methodology that combines the number of transactions processed with the
value of those transactions;
    2. reductions in Automated Customer Account Transfer Services
(ACATS) fee;
    3. reductions in Fund/SERV and Networking fees;
    4. elimination of Insurance and Retirement Processing Services file
fees; and
    5. introduction of new fees for a new Funds Transfers service to be
introduced in 2008 under NSCC's Insurance and Retirement Processing
Services product line.
    NSCC's fee schedule as it is being modified by this proposed rule
change is attached as Exhibit 5 to NSCC's filing.\3\ Unless otherwise
noted in Exhibit 5, the proposed fee changes became effective on
January 2, 2008.
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    \3\ File No. SR-NSCC-2007-17, including Exhibit 5, can be viewed
at http://www.dtcc.com/downloads/legal/rule_filings/2007/nscc/2007-
17.pdf.
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    The proposed rule change is consistent with the requirements of
Section 17A of the Act and the rules and regulations thereunder,
because it provides for the equitable allocation of fees among its
participants.

(B) Self-Regulatory Organization's Statement on Burden on Competition

    NSCC does not believe that the proposed rule change will have any
impact, or impose any burden, on competition.

(C) Self-Regulatory Organization's Statement on Comments on the
Proposed Rule Change Received From Members, Participants, or Others

    Written comments relating to the proposed rule change have not yet
been solicited or received. NSCC will notify the Commission of any
written comments received by NSCC.

III. Date of Effectiveness of the Proposed Rule Change and Timing for
Commission Action

    Because the foregoing rule change changes fees charged by NSCC, it
has become effective pursuant to section 19(b)(3)(A)(ii) of the Act \4\
and Rule 19b-4(f)(2) \5\ thereunder. At any time within sixty days of
the filing of the proposed rule change, the Commission may summarily
abrogate such rule change if it appears to the Commission that such
action is necessary or appropriate in the public interest, for the
protection of investors, or otherwise in furtherance of the purposes of
the Act.
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    \4\ 15 U.S.C. 78s(b)(3)(A)(ii).
    \5\ 17 CFR 240.19b-4(f)(2).

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IV. Solicitation of Comments

    Interested persons are invited to submit written data, views, and
arguments concerning the foregoing, including whether the proposed rule
change is consistent with the Act. Comments may be submitted by any of
the following methods:

Electronic Comments

     Use the Commission's Internet comment form (http://
www.sec.gov/rules/sro.shtml); or
     Send an e-mail to<EMAIL_ADDRESS>Please include
File Number SR-NSCC-2007-17 on the subject line.

Paper Comments

     Send paper comments in triplicate to Nancy M. Morris,
Secretary, Securities and Exchange Commission, 100 F Street, NE.,
Washington, DC 20549-1090.

All submissions should refer to File Number SR-NSCC-2007-17. This file
number should be included on the subject line if e-mail is used. To
help the Commission process and review your comments more efficiently,
please use only one method. The Commission will post all comments on
the Commission's Internet Web site (http://www.sec.gov/rules/
sro.shtml). Copies of the submission, all subsequent amendments, all
written statements with respect to the proposed rule change that are
filed with the Commission, and all written communications relating to
the proposed rule change between the Commission and any person, other
than those that may be withheld from the public in accordance with the
provisions of 5 U.S.C. 552, will be available for inspection and
copying in the Commission's Public Reference Room, 100 F Street, NE.,
Washington, DC 20549, on official business days between the hours of 10
a.m. and 3 p.m. Copies of such filing also will be available for
inspection and copying at the principal office of NSCC. All comments
received will be posted without change; the Commission does not edit
personal identifying information from submissions. You should submit
only information that you wish to make available publicly. All
submissions should refer to File Number SR-NSCC-2007-17 and should be
submitted on or before March 26, 2008.

    For the Commission by the Division of Trading and Markets,
pursuant to delegated authority.\6\
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    \6\ 17 CFR 200.30-3(a)(12).
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Florence E. Harmon,
Deputy Secretary.
 [FR Doc. E8-4171 Filed 3-4-08; 8:45 am]

BILLING CODE 8011-01-P


[Federal Register Volume 78, Number 159 (Friday, August 16, 2013)]
[Notices]
[Pages 50134-50135]
[FR Doc No: 2013-20102]

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SECURITIES AND EXCHANGE COMMISSION

[File No. 500-1]

Altus Pharmaceuticals, Inc., Blackhawk Capital Group BDC, Inc.,
Cargo Connection Logistics Holding, Inc., Diapulse Corporation of
America, Globus International Resources Corp., Kingston Systems, Inc.,
and Mega Media Group, Inc.; Order of Suspension of Trading

August 14, 2013.
    It appears to the Securities and Exchange Commission that there is
a lack of current and accurate information concerning the securities of
Altus Pharmaceuticals, Inc. because it has not filed any periodic
reports since the period ended June 30, 2009.
    It appears to the Securities and Exchange Commission that there is
a lack of current and accurate information concerning the securities of
Blackhawk Capital Group BDC, Inc. because it has

not filed any periodic reports since the period ended September 30,
2010.
    It appears to the Securities and Exchange Commission that there is
a lack of current and accurate information concerning the securities of
Cargo Connection Logistics Holding, Inc. because it has not filed any
periodic reports since the period ended December 31, 2009.
    It appears to the Securities and Exchange Commission that there is
a lack of current and accurate information concerning the securities of
Diapulse Corporation of America because it has not filed any periodic
reports since the period ended September 30, 2008.
    It appears to the Securities and Exchange Commission that there is
a lack of current and accurate information concerning the securities of
Globus International Resources Corp. because it has not filed any
periodic reports since the period ended December 31, 2004.
    It appears to the Securities and Exchange Commission that there is
a lack of current and accurate information concerning the securities of
Kingston Systems, Inc. because it has not filed any periodic reports
since the period ended December 27, 2008.
    It appears to the Securities and Exchange Commission that there is
a lack of current and accurate information concerning the securities of
Mega Media Group, Inc. because it has not filed any periodic reports
since the period ended July 31, 2009.
    The Commission is of the opinion that the public interest and the
protection of investors require a suspension of trading in the
securities of the above-listed companies. Therefore, it is ordered,
pursuant to Section 12(k) of the Securities Exchange Act of 1934, that
trading in the securities of the above-listed companies is suspended
for the period from 9:30 a.m. EDT on August 14, 2013, through 11:59
p.m. EDT on August 27, 2013.

    By the Commission.
Jill M. Peterson,
Assistant Secretary.
[FR Doc. 2013-20102 Filed 8-14-13; 11:15 am]
BILLING CODE 8011-01-P


[Federal Register Volume 82, Number 170 (Tuesday, September 5, 2017)]
[Rules and Regulations]
[Pages 41878-41883]
[FR Doc No: 2017-18396]

-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-9521; Product Identifier 2016-NM-061-AD; Amendment
39-19018; AD 2017-18-09]
RIN 2120-AA64

Airworthiness Directives; Airbus Defense and Space S.A. (Formerly
Known as Construcciones Aeronauticas, S.A.) Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for all
Airbus Defense and Space S.A. Model CN-235, CN-235-100, CN-235-200, CN-
235-300, and C-295 airplanes. This AD was prompted by reports of
excessive play between bushings and their respective fitting housings
at certain elevator fittings. This AD requires a one-time detailed
inspection and repetitive eddy current inspections of the elevator
hinge fitting and bracket assembly, and corrective actions if
necessary. We are issuing this AD to address the unsafe condition on
these products.

DATES: This AD is effective October 10, 2017.
    The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of October 10,
2017.

ADDRESSES: For service information identified in this final rule,
contact Airbus Defense and Space, Services/Engineering Support, Avenida
de Arag[oacute]n 404, 28022 Madrid, Spain; fax +34 91 585 31 27; email
<EMAIL_ADDRESS>You may view this referenced service
information at the FAA, Transport Standards Branch, 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-2016-9521.

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-2016-
9521; 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 street address for the Docket Office (telephone
800-647-5527) 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: Shahram Daneshmandi, Aerospace
Engineer, International Section, Transport Standards Branch, FAA, 1601
Lind Avenue SW., Renton, WA 98057-3356; telephone:<PHONE_NUMBER>; fax:
425-227-1149.

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 all Airbus Defense and
Space S.A. Model CN-235, CN-235-100, CN-235-200, CN-235-300, and C-295
airplanes. The NPRM published in the Federal Register on January 5,
2017 (82 FR 1269) (``the NPRM''). The NPRM was prompted by reports of
excessive play between bushings and their respective fitting housings
at certain elevator fittings. The NPRM proposed to require a one-time
detailed inspection and repetitive eddy current inspections of the
elevator hinge fitting and bracket assembly, and corrective actions if
necessary. We are issuing this AD to prevent excessive play between
bushings and their respective fitting housings, which could lead to
failure or detachment of any of the affected structural parts, with a
possible result of reduced control of the airplane.
    The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA AD
2016-0075, dated April 19, 2016 (referred to after this as the
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to
correct an unsafe condition for all Airbus Defense and Space S.A. Model
CN-235, CN-235-100, CN-235-200, CN-235-300, and C-295 airplanes. The
MCAI states:

    Excessive play between bushings and their respective fitting
housing was reported at Stabilizer Station (STA) 4850, affecting the
outboard and inboard elevator hinge fittings and attachment
fittings; and the horizontal stabilizer elevator linkage.
Additionally, excessive misalignment was detected between the
elevator hinge fittings and the elevator brackets during further
analysis of the reported cases. Furthermore, an occurrence of an
elevator hinge fitting crack was reported.
    This condition, if not detected and corrected, could lead to
failure or detachment of any of the affected structural parts,
possibly resulting in reduced control of the aeroplane.
    To address this potentially unsafe condition, Airbus Defence &
Space (D&S) issued Alert Operator Transmissions (AOT) AOT-CN235-55-
0001 Revision 2 and AOT-C295-55-0001 Revision 2 to provide
inspection instructions to detect misalignment between the elevator
hinge fittings and the elevator brackets. Additionally, Airbus D&S
issued AOT-CN235-55-0003 and AOT-C295-55-0003 to provide inspection
instructions to detect cracking of elevator hinge fitting and
attachment fitting.
    For the reasons described above, this [EASA] AD requires a one-
time [detailed] inspection of the elevator hinge fittings and the
elevator brackets, repetitive [eddy current] inspections of elevator
hinge fittings and attachment fittings, and depending on findings,
accomplishment of applicable corrective action(s) [e.g. repair(s)].

    You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
9521.

Comments

    We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.

Conclusion

    We reviewed the relevant data and determined that air safety and
the public interest require adopting this AD as proposed, except for
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.

Related Service Information Under 1 CFR Part 51

    Airbus Defense and Space S.A. has issued the following Alert
Operators Transmissions (AOT).
     Airbus Defense and Space S.A. AOT AOT-CN235-55-0001,
Revision 2, dated March 10, 2015. The service information describes
procedures for a detailed visual inspection of the elevator hinge
fitting and bracket assembly to detect excessive play between bushings
and their respective fitting housings, and to detect cracks; and
corrective actions if necessary.
     Airbus Defense and Space S.A. AOT AOT-CN235-55-0003, dated
December 22, 2015. The service

information describes procedures for repetitive eddy current
inspections to detect cracks in the elevator hinge fitting and bracket
assembly, and corrective actions if necessary.
     Airbus Defense and Space S.A. AOT AOT-C295-55-0001,
Revision 2, dated April 9, 2015. The service information describes
procedures for a detailed visual inspection of the elevator hinge
fitting and bracket assembly to detect excessive play between bushings
and their respective fitting housings, and to detect cracks; and
corrective actions if necessary.
     Airbus Defense and Space S.A. AOT AOT-C295-55-0003, dated
December 22, 2015. The service information describes procedures for
repetitive eddy current inspections to detect cracks in the elevator
hinge fitting and bracket assembly, and corrective actions if
necessary.
    These documents are distinct since they apply to different airplane
models in different configurations. 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 14 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
----------------------------------------------------------------------------------------------------------------
Inspection........................  2 work-hours x $85           $0   $170 per inspection   $2,380 per
                                     per hour = $170 per               cycle.                inspection cycle.
                                     inspection cycle.
----------------------------------------------------------------------------------------------------------------

    We estimate the following costs to do any necessary repairs that
will be required based on the results of the inspection. We have no way
of determining the number of airplanes that might need this repair:

                                               On-Condition Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Cost per
                    Action                                Labor cost               Parts cost        product
----------------------------------------------------------------------------------------------------------------
Repair.......................................  45 work-hours x $85 per hour =          $10,000          $13,825
                                                $3,825.
----------------------------------------------------------------------------------------------------------------

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.
    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 transport category airplanes to
the Director of the System Oversight Division.

Regulatory Findings

    We determined that 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 the 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):

2017-18-09 Airbus Defense and Space S.A. (Formerly Known as
Construcciones Aeronauticas, S.A.): Amendment 39-19018; Docket No.
FAA-2016-9521; Product Identifier 2016-NM-061-AD.

(a) Effective Date

    This AD is effective October 10, 2017.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Airbus Defense and Space S.A. (formerly known
as Construcciones Aeronauticas, S.A.) Model CN-235, CN-235-100, CN-
235-200, CN-235-300, and C-295 airplanes, certificated in any
category, all manufacturer serial numbers.

(d) Subject

    Air Transport Association (ATA) of America Code 55, Stabilizers.

(e) Reason

    This AD was prompted by reports of excessive play between
bushings and their respective fitting housings at certain elevator
fittings. We are issuing this AD to prevent excessive play between
bushings and their respective fitting housings, which could lead to
failure or detachment of any of the affected structural parts, with
a possible result of reduced control of the airplane.

(f) Compliance

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

(g) One-Time Detailed Visual Inspection

    Before exceeding 600 flight hours since first flight of the
airplane, or within 300 flight hours after the effective date of
this AD, whichever occurs later, but not before exceeding 300 flight
hours since first flight of the airplane: Do a detailed visual
inspection of the elevator hinge fitting and bracket assembly to
detect excessive play between bushings and their respective fitting
housings, and to detect cracks, in accordance with the instructions
of Airbus Defense and Space S.A. Alert Operators Transmission (AOT)
AOT-CN235-55-0001, Revision 2, dated March 10, 2015; or AOT AOT-
C295-55-0001, Revision 2, dated April 9, 2015; as applicable.

(h) Corrective Action for Discrepancies Found During Detailed Visual
Inspection

    If, during the inspection required by paragraph (g) of this AD,
any discrepancy is detected, as defined in the instructions of
Airbus Defense and Space S.A. AOT AOT-CN235-55-0001, Revision 2,
dated March 10, 2015; or AOT AOT-C295-55-0001 Revision 2, dated
April 9, 2015; as applicable: Before further flight, accomplish
applicable corrective actions, in accordance with the instructions
of Airbus Defense and Space S.A. AOT AOT-CN235-55-0001, Revision 2,
dated March 10, 2015; or AOT AOT-C295-55-0001, Revision 2, dated
April 9, 2015; as applicable. Where Airbus Defense and Space S.A.
AOT AOT-CN235-55-0001, Revision 2, dated March 10, 2015; or AOT AOT-
C295-55-0001 Revision 2, dated April 9, 2015; specifies to contact
Airbus Defense and Space S.A. for corrective actions, before further
flight, accomplish corrective actions in accordance with the
procedures specified in paragraph (n)(2) of this AD.

(i) Repetitive Eddy Current Inspections--Model CN-235, CN-235-100, CN-
235-200, and CN-235-300 Airplanes

    For Model CN-235, CN-235-100, CN-235-200, and CN-235-300
airplanes: Do the actions required by paragraphs (i)(1) and (i)(2)
of this AD.
    (1) Within the applicable compliance time specified in table 1
to paragraph (i)(1) of this AD: Do an eddy current inspection to
detect cracks in the elevator hinge fitting and bracket assembly, in
accordance with the instructions of Airbus Defense and Space S.A.
AOT AOT-CN235-55-0003, dated December 22, 2015.

 Table 1 to Paragraph (i)(1) of This AD--Initial Compliance Times for Model CN-235, CN-235-100, CN-235-200, and
                                              CN-235-300 Airplanes
----------------------------------------------------------------------------------------------------------------

----------------------------------------------------------------------------------------------------------------
Manufacturer's Serial No.             Elevator hinge fitting       Compliance time for initial eddy current
                                                                                inspection
(MSN)                                             (part No.)               (whichever occurs later)
----------------------------------------------------------------------------------------------------------------
MSN001 through MSN154 inclusive....            35-31193-0201  Before exceeding 8,800       Within 300 flight
                                               35-31193-0202   flight cycles since first    cycles after the
                                                               flight of the airplane; or   effective date of
                                                               before exceeding the         this AD.
                                                               applicable flight hours
                                                               since first flight of the
                                                               airplane as calculated in
                                                               table 2 to paragraph
                                                               (i)(1) of this AD;
                                                               whichever occurs first.
MSN155 through MSN241 inclusive....            35-31193-0501  Before exceeding 3,600       Within 300 flight
                                               35-31193-0502   flight cycles since first    cycles after the
                                                               flight of the airplane; or   effective date of
                                                               before exceeding the         this AD.
                                                               applicable flight hours
                                                               since first flight of the
                                                               airplane as calculated in
                                                               table 2 to paragraph
                                                               (i)(1) of this AD;
                                                               whichever occurs first.
MSN242 through MSN999 inclusive....            35-31193-0503  Before exceeding 1,000       Within 50 flight
                                               35-31193-0504   flight cycles since first    cycles after the
                                                               flight of the airplane; or   effective date of
                                                               before exceeding the         this AD.
                                                               applicable flight hours
                                                               since first flight of the
                                                               airplane as calculated in
                                                               table 2 to paragraph
                                                               (i)(1) of this AD;
                                                               whichever occurs first.
----------------------------------------------------------------------------------------------------------------

  Table 2 to Paragraph (i)(1) of This AD--Flight Cycles to Flight Hours
              Conversion Since First Flight of the Airplane
------------------------------------------------------------------------
                                   Civilian or        Flight cycles to
     CN-235 Model/version         military type         flight hours
                                   certificate           conversion
------------------------------------------------------------------------
CN-235 (Commercial              Civilian.........  Flight hours since
 Identification S10).                               first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 0.861.
CN-235-100....................  Civilian.........  Flight hours since
                                                    first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 0.861.
CN-235-200....................  Civilian.........  Flight hours since
                                                    first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 0.806.
CN-235-300....................  Civilian.........  Flight hours since
                                                    first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 0.861.
CN-235 (Commercial              Military.........  Flight hours since
 Identification S10M).                              first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 0.861.
CN-235-100M...................  Military.........  Flight hours since
                                                    first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 2.222.
CN-235-200M...................  Military.........  Flight hours since
                                                    first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 2.222.
CN-235-300M...................  Military.........  Flight hours since
                                                    first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 2.167.
CN-235-100M/IR01..............  Military.........  Flight hours since
                                                    first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 1.389.
CN-235-100M/EA02V.............  Military.........  Flight hours since
                                                    first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 1.389.

CN-235-200M/CL02..............  Military.........  Flight hours since
                                                    first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 1.389.
CN-235/EA01F (Commercial        Military.........  Flight hours since
 Identification S10M).                              first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 0.861.
CN-235-300/SM01...............  Civilian.........  Flight hours since
                                                    first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 3.125.
CN-235 -300M/CG01, -300M/GC01,  Military.........  Flight hours since
 -300/MM01, -300/CL04.                              first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 1
                                                    to paragraph (i)(1)
                                                    of this AD x 3.125.
------------------------------------------------------------------------

    (2) Repeat the eddy current inspection specified in paragraph
(i)(1) of this AD thereafter within the applicable interval
specified in table 3 to paragraph (i)(2) of this AD.

 Table 3 to Paragraph (i)(2) of This AD--Repetitive Inspection Intervals
------------------------------------------------------------------------
                                     Elevator       Compliance time for
   Manufacturer's serial No.        attachment        repetitive eddy
                                  fitting  (P/N)    current inspections
------------------------------------------------------------------------
MSN001 through MSN154               35-31193-0201  Before exceeding
 inclusive.                         35-31193-0202   1,300 flight cycles
                                                    since the most
                                                    recent inspection;
                                                    or before exceeding
                                                    the applicable
                                                    flight hours since
                                                    the most recent
                                                    inspection as
                                                    calculated in table
                                                    4 to paragraph
                                                    (i)(2) of this AD;
                                                    whichever occurs
                                                    first.
MSN155 through MSN241               35-31193-0501  Before exceeding
 inclusive.                         35-31193-0502   1,000 flight cycles
                                                    since the most
                                                    recent inspection;
                                                    or before exceeding
                                                    the applicable
                                                    flight hours since
                                                    the most recent
                                                    inspection as
                                                    calculated in table
                                                    4 to paragraph
                                                    (i)(2) of this AD;
                                                    whichever occurs
                                                    first.
MSN242 through MSN999               35-31193-0503  Before exceeding
 inclusive.                         35-31193-0504   1,000 flight cycles
                                                    since the most
                                                    recent inspection;
                                                    or before exceeding
                                                    the applicable
                                                    flight hours since
                                                    the most recent
                                                    inspection as
                                                    calculated in table
                                                    4 to paragraph
                                                    (i)(2) of this AD;
                                                    whichever occurs
                                                    first.
------------------------------------------------------------------------

  Table 4 to Paragraph (i)(2) of This AD--Flight Cycles to Flight Hours
                  Conversion for Repetitive Inspections
------------------------------------------------------------------------
                                   Civilian or        Flight cycles to
     CN-235 Model/version         military type         flight hours
                                   certificate           conversion
------------------------------------------------------------------------
CN-235 (Commercial              Civilian.........  Flight hours since
 Identification S10).                               most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 0.861.
CN-235-100....................  Civilian.........  Flight hours since
                                                    most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 0.861.
CN-235-200....................  Civilian.........  Flight hours since
                                                    most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 0.806.
CN-235-300....................  Civilian.........  Flight hours since
                                                    first flight of the
                                                    airplane = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 0.861.
CN-235 (Commercial              Military.........  Flight hours since
 Identification S10M).                              most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 0.861.
CN-235-100M...................  Military.........  Flight hours since
                                                    most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 2.222.
CN-235-200M...................  Military.........  Flight hours since
                                                    most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 2.222.
CN-235-300M...................  Military.........  Flight hours since
                                                    most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 2.167.
CN-235-100M/IR01..............  Military.........  Flight hours since
                                                    most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 1.389.
CN-235-100M/EA02V.............  Military.........  Flight hours since
                                                    most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 1.389.
CN-235-200M/CL02..............  Military.........  Flight hours since
                                                    most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 1.389.
CN-235/EA01F (Commercial        Military.........  Flight hours since
 Identification S10M).                              most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 0.861.
CN-235-300/SM01...............  Civilian.........  Flight hours since
                                                    most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 3.125.
CN-235 -300M/CG01, -300M/GC01,  Military.........  Flight hours since
 -300/MM01, -300/CL04.                              most recent
                                                    inspection = the
                                                    applicable flight
                                                    cycles from table 3
                                                    to paragraph (i)(2)
                                                    of this AD x 3.125.
------------------------------------------------------------------------

(j) Repetitive Eddy Current Inspections--Model C-295 Airplanes

    For Model C-295 airplanes: Do the actions required by paragraphs
(j)(1) and (j)(2) of this AD.
    (1) At the later of the times specified in table 5 to paragraph
(j)(1) of this AD: Do an eddy current inspection of the elevator
hinge fitting and attachment fitting to detect cracks, in accordance
with the instructions of Airbus Defense and Space S.A. AOT AOT-C295-
55-0003, dated December 22, 2015.

           Table 5 to Paragraph (j)(1) of This AD--Initial Compliance Times for Model C-295 Airplanes
----------------------------------------------------------------------------------------------------------------

----------------------------------------------------------------------------------------------------------------
C-295 Model/Version              Manufacturer's        Elevator Hinge   Compliance time for initial eddy current
                                  Serial Number.              Fitting                  inspection
                                 (MSN)............      (Part Number)           (whichever occurs later)
----------------------------------------------------------------------------------------------------------------
C-295M/ EA03(01-10), RJ01 (01-   MSN001 through         95-31193-0501  Since first flight of   Within 300 flight
 02), PO01(01-08), AG01(01-06),   MSN030 inclusive.     95-31193-0502   the airplane: Before    cycles after the
 BR01(01-03).                                                           exceeding 3,600         effective date
                                                                        flight cycles; or       of this AD.
                                                                        before exceeding
                                                                        5,040 flight hours;
                                                                        whichever occurs
                                                                        first.
C-295M (from MSN 031)..........  MSN031 through         95-31193-0503  Since first flight of   Within 50 flight
                                  MSN999 inclusive.     95-31193-0504   the airplane: Before    cycles after the
                                                                        exceeding 1,000         effective date
                                                                        flight cycles; or       of this AD.
                                                                        before exceeding
                                                                        1,400 flight hours;
                                                                        whichever occurs
                                                                        first.
C-295M/FI01, FI02..............  MSN031 through         95-31193-0503  Since first flight of   Within 50 flight
                                  MSN999 inclusive.     95-31193-0504   the airplane: Before    cycles after the
                                                                        exceeding 1,000         effective date
                                                                        flight cycles; or       of this AD.
                                                                        before exceeding
                                                                        1,000 flight hours;
                                                                        whichever occurs
                                                                        first.
C-295M/PG01....................  MSN031 through         95-31193-0503  Since first flight of   Within 50 flight
                                  MSN999 inclusive.     95-31193-0504   the airplane: Before    cycles after the
                                                                        exceeding 1,000         effective date
                                                                        flight cycles; or       of this AD.
                                                                        before exceeding
                                                                        1,400 flight hours;
                                                                        whichever occurs
                                                                        first.
C-295M/PG02, PG03..............  MSN031 through         95-31193-0503  Since first flight of   Within 50 flight
                                  MSN999 inclusive.     95-31193-0504   the airplane: Before    cycles after the
                                                                        exceeding 1,000         effective date
                                                                        flight cycles; or       of this AD.
                                                                        before exceeding
                                                                        1,900 flight hours;
                                                                        whichever occurs
                                                                        first.
C-295M/CH01....................  MSN031 through         95-31193-0503  Since first flight of   Within 50 flight
                                  MSN999 inclusive.     95-31193-0504   the airplane: Before    cycles after the
                                                                        exceeding 1,000         effective date
                                                                        flight cycles; or       of this AD.
                                                                        before exceeding
                                                                        1,200 flight hours;
                                                                        whichever occurs
                                                                        first.
C-295M/CH02, OM03..............  MSN031 through         95-31193-0503  Since first flight of   Within 50 flight
                                  MSN999 inclusive.     95-31193-0504   the airplane: Before    cycles after the
                                                                        exceeding 1,000         effective date
                                                                        flight cycles; or       of this AD.
                                                                        before exceeding
                                                                        1,500 flight hours;
                                                                        whichever occurs
                                                                        first.
C-295MW........................  MSN031 through         95-31193-0503  Since first flight of   Within 50 flight
                                  MSN999 inclusive.     95-31193-0504   the airplane: Before    cycles after the
                                                                        exceeding 1,000         effective date
                                                                        flight cycles; or       of this AD.
                                                                        before exceeding
                                                                        1,400 flight hours;
                                                                        whichever occurs
                                                                        first.
----------------------------------------------------------------------------------------------------------------

    (2) Repeat the eddy current inspection specified in paragraph
(j)(1) of this AD thereafter within the applicable interval
specified in table 6 to paragraph (j)(2) of this AD.

        Table 6 to Paragraph (j)(2) of This AD--Repetitive Inspection Intervals for Model C-295 Airplanes
----------------------------------------------------------------------------------------------------------------
                                                                   Elevator hinge        Compliance time for
         C-295 Model/version             Manufacturer's serial     fitting  (part      repetitive eddy current
                                              No.  (MSN)              number)                inspections
----------------------------------------------------------------------------------------------------------------
C-295M/ EA03(01-10), RJ01 (01-02),     MSN001 through MSN030         95-31193-0501  Before exceeding 1,000
 PO01(01-08), AG01(01-06), BR01(01-     inclusive.                   95-31193-0502   flight cycles since the
 03).                                                                                most recent inspection; or
                                                                                before exceeding 1,400
                                                                                flight hours since the most
                                                                                recent inspection;
                                                                                whichever occurs first.
C-295M (from MSN 031)................  MSN031 through MSN999         95-31193-0503  Before exceeding 1,000
                                        inclusive.                   95-31193-0504   flight cycles since the
                                                                                most recent inspection; or
                                                                                before exceeding 1,400
                                                                                flight hours since the most
                                                                                recent inspection;
                                                                                whichever occurs first.
C-295M/FI01, FI02....................  MSN031 through MSN999         95-31193-0503  Before exceeding 1,000
                                        inclusive.                   95-31193-0504   flight cycles since the
                                                                                most recent inspection; or
                                                                                before exceeding 1,000
                                                                                flight hours since the most
                                                                                recent inspection;
                                                                                whichever occurs first.
C-295M/PG01..........................  MSN031 through MSN999         95-31193-0503  Before exceeding 1,000
                                        inclusive.                   95-31193-0504   flight cycles since the
                                                                                most recent inspection; or
                                                                                before exceeding 1,400
                                                                                flight hours since the most
                                                                                recent inspection;
                                                                                whichever occurs first.
C-295M/PG02, PG03....................  MSN031 through MSN999         95-31193-0503  Before exceeding 1,000
                                        inclusive.                   95-31193-0504   flight cycles since the
                                                                                most recent inspection; or
                                                                                before exceeding 1,900
                                                                                flight hours since the most
                                                                                recent inspection;
                                                                                whichever occurs first.

C-295M/CH01..........................  MSN031 through MSN999         95-31193-0503  Before exceeding 1,000
                                        inclusive.                   95-31193-0504   flight cycles since the
                                                                                most recent inspection; or
                                                                                before exceeding 1,200
                                                                                flight hours since the most
                                                                                recent inspection;
                                                                                whichever occurs first.
C-295M/CH02, OM03....................  MSN031 through MSN999         95-31193-0503  Before exceeding 1,000
                                        inclusive.                   95-31193-0504   flight cycles since the
                                                                                most recent inspection; or
                                                                                before exceeding 1,500
                                                                                flight hours since the most
                                                                                recent inspection;
                                                                                whichever occurs first.
C-295MW..............................  MSN031 through MSN999         95-31193-0503  Before exceeding 1,000
                                        inclusive.                   95-31193-0504   flight cycles since the
                                                                                most recent inspection; or
                                                                                before exceeding 1,400
                                                                                flight hours since the most
                                                                                recent inspection;
                                                                                whichever occurs first.
----------------------------------------------------------------------------------------------------------------

(k) Corrective Action for Discrepancies Found During Eddy Current
Inspection

    If, during any inspection required by paragraph (i)(1), (i)(2),
(j)(1), or (j)(2) of this AD, any crack is detected, as defined in
Airbus Defense and Space S.A. AOT AOT-CN235-55-0003, dated December
22, 2015; or AOT AOT-C295-55-0003, dated December 22, 2015; as
applicable: Before further flight, accomplish applicable corrective
actions in accordance with the instructions of Airbus Defense and
Space S.A. AOT AOT-CN235-55-0003, dated December 22, 2015; or AOT
AOT-C295-55-0003, dated December 22, 2015; as applicable. Where
Airbus Defense and Space S.A. AOT AOT-CN235-55-0003, dated December
22, 2015; or AOT AOT-C295-55-0003, dated December 22, 2015;
specifies to contact Airbus Defense and Space S.A. for corrective
actions, before further flight, accomplish corrective actions in
accordance with the procedures specified in paragraph (n)(2) of this
AD.

(l) Provision Regarding Terminating Action

    Accomplishing corrective actions, as required by paragraph (k)
of this AD, does not constitute terminating action for the
repetitive inspections required by paragraphs (i)(2) and (j)(2) of
this AD, unless explicitly stated in the approved method of
compliance for the corrective action.

(m) Credit for Previous Actions

    This paragraph provides credit for the actions required by
paragraph (g) of this AD, if those actions were performed before the
effective date of this AD using Airbus Defense and Space S.A. AOT
AOT-CN235-55-0001, Revision 1, dated March 6, 2015; or AOT AOT-C295-
55-0001, Revision 1, dated May 29, 2014.

(n) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
International Section, Transport Standards 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. 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.
    (2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, International
Section, Transport Standards Branch, FAA; or the European Aviation
Safety Agency (EASA); or Airbus Defense and Space S.A.'s EASA DOA.
If approved by the DOA, the approval must include the DOA-authorized
signature.

(o) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2016-0075, dated April 19, 2016, for related
information. This MCAI may be found in the AD docket on the Internet
at http://www.regulations.gov by searching for and locating Docket
No. FAA-2016-9521.
    (2) For more information about this AD, contact Shahram
Daneshmandi, Aerospace Engineer, International Section, Transport
Standards Branch, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356;
telephone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>.
    (3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (p)(3) and (p)(4) of this AD.

(p) 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 this AD specifies otherwise.
    (i) Airbus Defense and Space S.A. Alert Operators Transmission
(AOT) AOT-CN235-55-0001, Revision 2, dated March 10, 2015.
    (ii) Airbus Defense and Space S.A. AOT AOT-CN235-55-0003, dated
December 22, 2015.
    (iii) Airbus Defense and Space S.A. AOT AOT-C295-55-0001,
Revision 2, dated April 9, 2015.
    (iv) Airbus Defense and Space S.A. AOT AOT-C295-55-0003, dated
December 22, 2015.
    (3) For service information identified in this AD, contact
Airbus Defense and Space, Services/Engineering Support, Avenida de
Arag[oacute]n 404, 28022 Madrid, Spain; fax +34 91 585 31 27; email
<EMAIL_ADDRESS>    (4) You may view this service information at the FAA, Transport
Standards Branch, 1601 Lind Avenue SW., Renton, WA. For information
on the availability of this material at the FAA, call<PHONE_NUMBER>.
    (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 August 22, 2017.
Dionne Palermo,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2017-18396 Filed 9-1-17; 8:45 am]
 BILLING CODE 4910-13-P


[Federal Register: March 20, 2008 (Volume 73, Number 55)]
[Notices]
[Page 14978-14979]
[DOCID:fr20mr08-37]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. CP08-88-000]

Texas Eastern Transmission, LP; Notice of Request Under Blanket
Authorization

March 13, 2008
    Take notice that on March 7, 2008, Texas Eastern Transmission, LP
(Texas Eastern), Post Office Box 1642, Houston, Texas 77251-1642, filed
in Docket No. CP08-88-000, an application pursuant to sections 157.205,
157.208, and 157.212 of the Commission's

Regulations under the Natural Gas Act (NGA) as amended, to construct,
own, and operate a new receipt point to receive revaporized liquefied
natural gas near Eunice, Evangeline Parish, Louisiana, under Texas
Eastern's blanket certificate issued in Docket No. CP82-535-000,\1\ all
as more fully set forth in the application which is on file with the
Commission and open to the public for inspection.
---------------------------------------------------------------------------

    \1\ 21 FERC ] 62,199 (1982).
---------------------------------------------------------------------------

    Texas Eastern states that it proposes to construct, own, and
operate a new receipt point on Texas Eastern's 30-inch diameter Lines
Nos. 14 and 18 to receive revaporized liquefied natural gas from the
Sabine Pass LNG, L.P. LNG import terminal located in Cameron Parish,
Louisiana, via Kinder Morgan Louisiana Pipeline (Kinder Morgan). The
taps into Texas Eastern's mainline would be located in Evangeline
Parish, Louisiana. This new receipt point would provide Texas Eastern
with the ability to receive up to 500 MMcf of natural gas per day from
Kinder Morgan into Texas Eastern's pipeline system. Texas Eastern also
states that the addition of the receipt point would have no significant
impact on Texas Eastern's peak day or annual deliveries and is not
prohibited by Texas Eastern's FERC Gas Tariff. Texas Eastern further
states that it would be reimbursed by Kinder Morgan for the estimated
$2,109,396 total cost to construct and operate the proposed receipt
point facilities.
    Any questions concerning this application may be directed to Garth
Johnson, General Manager, Certificates & Reporting, Texas Eastern
Transmission, LP, P.O. Box 1642, Houston, Texas 77251-1642, via
telephone at<PHONE_NUMBER>, or facsimile<PHONE_NUMBER>.
    This filing is available for review at the Commission or may be
viewed on the Commission's Web site at http://www.ferc.gov, using the
``eLibrary'' link. Enter the docket number excluding the last three
digits in the docket number filed to access the document. For
assistance, please contact FERC Online Support at FERC
<EMAIL_ADDRESS>or call toll-free at<PHONE_NUMBER>, or, for
TTY, contact<PHONE_NUMBER>. Comments, protests and interventions may
be filed electronically via the Internet in lieu of paper. See, 18 CFR
385.2001(a)(1)(iii) and the instructions on the Commission's Web site
under the ``e-Filing'' link. The Commission strongly encourages
intervenors to file electronically.
    Any person or the Commission's staff may, within 60 days after
issuance of the instant notice by the Commission, file pursuant to Rule
214 of the Commission's Procedural Rules (18 CFR 385.214) a motion to
intervene or notice of intervention and pursuant to section 157.205 of
the regulations under the NGA (18 CFR 157.205), a protest to the
request. If no protest is filed within the time allowed therefore, the
proposed activity shall be deemed to be authorized effective the day
after the time allowed for filing a protest. If a protest is filed and
not withdrawn within 30 days after the allowed time for filing a
protest, the instant request shall be treated as an application for
authorization pursuant to section 7 of the NGA.

Kimberly D. Bose,
Secretary.
 [FR Doc. E8-5593 Filed 3-19-08; 8:45 am]

BILLING CODE 6717-01-P


[Federal Register Volume 78, Number 220 (Thursday, November 14, 2013)]
[Notices]
[Page 68432]
[FR Doc No: 2013-27164]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[ Docket No. EL13-90-000]

Pacific Gas and Electric Company; Notice of Initiation of
Proceeding and Refund Effective Date

    On September 24, 2013, the Commission issued an order that
initiated a proceeding in Docket No. EL13-90-000, pursuant to section
206 of the Federal Power Act (FPA), 16 U.S.C. 824e (2006), to determine
the justness and reasonableness of the rate increase proposed by
Pacific Gas and Electric Company. Pacific Gas and Electric Company, 144
FERC ] 61,277 (2013).
    The refund effective date in Docket No. EL13-90-000, established
pursuant to section 206(b) of the FPA, will be the date of publication
of this notice in the Federal Register.

    Dated: November 7, 2013.
Nathaniel J. Davis, Sr.,
Deputy Secretary.
[FR Doc. 2013-27164 Filed 11-13-13; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register Volume 88, Number 84 (Tuesday, May 2, 2023)]
[Notices]
[Pages 27542-27543]
[FR Doc No: 2023-09205]

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SECURITIES AND EXCHANGE COMMISSION

[Investment Company Act Release No. 34901; 812-15425]

Total Fund Solution and Cromwell Investment Advisors, LLC

April 26, 2023.
AGENCY: Securities and Exchange Commission (``Commission'' or ``SEC'').

ACTION: Notice.

-----------------------------------------------------------------------

    Notice of an application under section 6(c) of the Investment
Company Act of 1940 (``Act'') for an exemption from section 15(a) of
the Act, as well as from certain disclosure requirements in rule 20a-1
under the Act, Item 19(a)(3) of Form N-1A, Items 22(c)(1)(ii),
22(c)(1)(iii), 22(c)(8) and 22(c)(9) of Schedule 14A under the
Securities Exchange Act of 1934, and sections 6- 07(2)(a), (b), and (c)
of Regulation S-X (``Disclosure Requirements'').

Summary of Application:  The requested exemption would permit
Applicants (as defined below) to enter into and materially amend
subadvisory agreements with subadvisers without shareholder approval
and would grant relief from the Disclosure Requirements as they relate
to fees paid to the subadvisers.

Applicants: Total Fund Solution and Cromwell Investment Advisors, LLC.

Filing Dates: The application was filed on January 20, 2023, and
amended on March 30, 2023 and April 17, 2023.

Hearing or Notification of Hearing: An order granting the requested
relief will be issued unless the Commission orders a hearing.
Interested persons may request a hearing on any application by emailing
the SEC's Secretary at [email protected] and serving the
Applicants with a copy of the request by email, if an email address is
listed for the relevant Applicant below, or personally or by mail, if a
physical address is listed for the relevant Applicant below. Hearing
requests should be received by the Commission by 5:30 p.m. on May 22,
2023, and

should be accompanied by proof of service on the Applicants, in the
form of an affidavit, or, for lawyers, a certificate of service.
Pursuant to rule 0-5 under the Act, hearing requests should state the
nature of the writer's interest, any facts bearing upon the
desirability of a hearing on the matter, the reason for the request,
and the issues contested. Persons who wish to be notified of a hearing
may request notification by emailing the Commission's Secretary.

ADDRESSES: The Commission: [email protected]. Applicants: Fabio
Battaglia, III, [email protected] and Elaine E. Richards,
[email protected].

FOR FURTHER INFORMATION CONTACT: Trace W. Rakestraw, Senior Special
Counsel, at<PHONE_NUMBER> (Division of Investment Management, Chief
Counsel's Office).

SUPPLEMENTARY INFORMATION: For Applicants' representations, legal
analysis, and conditions, please refer to Applicants' amended and
restated application, dated April 17, 2023, which may be obtained via
the Commission's website by searching for the file number at the top of
this document, or for an Applicant using the Company name search field
on the SEC's EDGAR system. The SEC's EDGAR system may be searched at
https://www.sec.gov/edgar/searchedgar/legacy/companysearch.html. You
may also call the SEC's Public Reference Room at<PHONE_NUMBER>.

    For the Commission, by the Division of Investment Management,
under delegated authority.
Sherry R. Haywood,
Assistant Secretary.
[FR Doc. 2023-09205 Filed 5-1-23; 8:45 am]
BILLING CODE 8011-01-P