[Federal Register Volume 74, Number 124 (Tuesday, June 30, 2009)]
[Notices]
[Page 31270]
[FR Doc No: E9-15455]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. ER09-1323-000]

Lost Lakes Wind Farm LLC; Supplemental Notice That Initial
Market-Based Rate Filing Includes Request for Blanket Section 204
Authorization

June 24, 2009.
    This is a supplemental notice in the above-referenced proceeding of
Lost Lakes Wind Farm, LLC's application for market-based rate
authority, with an accompanying rate tariff, noting that such
application includes a request for blanket authorization, under 18 CFR
part 34, of future issuances of securities and assumptions of
liability.
    Any person desiring to intervene or to protest should file with the
Federal Energy Regulatory Commission, 888 First Street, NE.,
Washington, DC 20426, in accordance with Rules 211 and 214 of the
Commission's Rules of Practice and Procedure (18 CFR 385.211 and
385.214). Anyone filing a motion to intervene or protest must serve a
copy of that document on the Applicant.
    Notice is hereby given that the deadline for filing protests with
regard to the applicant's request for blanket authorization, under 18
CFR part 34, of future issuances of securities and assumptions of
liability, is July 14, 2009.
    The Commission encourages electronic submission of protests and
interventions in lieu of paper, using the FERC Online links at http://www.ferc.gov. To facilitate electronic service, persons with Internet
access who will eFile a document and/or be listed as a contact for an
intervenor must create and validate an eRegistration account using the
eRegistration link. Select the eFiling link to log on and submit the
intervention or protests.
    Persons unable to file electronically should submit an original and
14 copies of the intervention or protest to the Federal Energy
Regulatory Commission, 888 First St., NE., Washington, DC 20426.
    The filings in the above-referenced proceeding are accessible in
the Commission's eLibrary system by clicking on the appropriate link in
the above list. They are also 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 e-mail notification
when a document is added to a subscribed dockets(s). For assistance
with any FERC Online service, please e-mail<EMAIL_ADDRESS>
or call<PHONE_NUMBER> (toll free). For TTY, call<PHONE_NUMBER>.

Kimberly D. Bose,
Secretary.
[FR Doc. E9-15455 Filed 6-29-09; 8:45 am]
BILLING CODE P


[Federal Register Volume 79, Number 34 (Thursday, February 20, 2014)]
[Proposed Rules]
[Pages 9661-9663]
[FR Doc No: 2014-03606]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0092; Directorate Identifier 2014-CE-002-AD]
RIN 2120-AA64

Airworthiness Directives; GROB-WERKE Airplanes

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

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to adopt a new airworthiness directive (AD) for
certain GROB-WERKE Models G115EG and G120A airplanes. This proposed AD
results from mandatory continuing airworthiness information (MCAI)
originated by an aviation authority of another country to identify and
correct an unsafe condition on an aviation product. The MCAI describes
the unsafe condition as cracks in the left hand elevator flange. We are
issuing this proposed AD to require actions to address the unsafe
condition on these products.

DATES: We must receive comments on this proposed AD by April 7, 2014.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Fax:<PHONE_NUMBER>.
     Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
    For service information identified in this proposed AD, contact
Grob Aircraft AG, Customer Service, Lettenbachstrasse 9, 86874
Tussenhausen-Mattsies, Germany, telephone: + 49 (0) 8268-998-105; fax;
+ 49 (0) 8268-998-200; email<EMAIL_ADDRESS>
Internet: grob-aircraft.com. You may review this referenced service
information at the FAA, Small Airplane Directorate, 901 Locust, Kansas
City, Missouri 64106. For information on the availability of this
material at the FAA, call<PHONE_NUMBER>.

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-2014-
0092; 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 proposed AD, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Office (telephone<PHONE_NUMBER>) is in the ADDRESSES section. Comments
will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2014-0092;
Directorate Identifier 2014-CE-002-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of those comments.
    We will post all comments we receive, without change, to http://regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, has issued AD
No. 2014-0004, dated January 7, 2014 (referred to after this as ``the
MCAI''), to correct an unsafe condition for certain GROB-WERKE Models
G115EG and G120A airplanes. The MCAI states:

    An operator of a G 115E aeroplane reported finding a crack
during scheduled maintenance on the left hand (LH) elevator flange,
part number (P/N) 115E-3761.06. The design of the right hand (RH)
elevator flange, P/N 115E-3762.07, is identical. A similar design is
used for the elevator flanges installed on G 120A and G-120A-I
aeroplanes, P/N 120A-3561.20(A) and P/N 120A-3562.20(A). Therefore,
the reported deficiency may also exist on G 120 aeroplanes.
    This condition, if not detected and corrected, could lead to
elevator failure, resulting in reduced control of the aeroplane.
    To address this potential unsafe condition, GROB Aircraft AG
issued Service Bulletins (SB) MSB1078-194 and SB MSB1121-140 to
provide instruction for inspection and corrective action.
    For the reasons described above, this AD requires repetitive
inspections of both elevator flanges on an aeroplane to detect any
crack, and, depending on findings, replacement of the affected part.

You may examine the MCAI on the Internet at http://www.regulations.gov
by searching for and locating Docket No. FAA-2014-0092.

Relevant Service Information

    GROB Aircraft has issued Service Bulletin No. MSB1078-194/1 and
Service Bulletin No. MSB1121-140, both dated December 3, 2013. The
actions described in this service information are intended to correct
the unsafe condition identified in the MCAI.

FAA's Determination and Requirements of the Proposed AD

    This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with this State of Design Authority, they
have notified us of the unsafe condition described in the MCAI and
service information referenced above. We are proposing this AD because
we evaluated all information and determined the unsafe condition exists
and is likely to exist or develop on other products of the same type
design.

Costs of Compliance

    We estimate that this proposed AD will affect 6 products of U.S.
registry. We also estimate that it would take about 1 work-hour per
product to comply with the basic requirements of this proposed AD. The
average labor rate is $85 per work-hour.
    Based on these figures, we estimate the cost of the proposed AD on
U.S. operators to be $510, or $85 per product.
    In addition, we estimate that any necessary follow-on actions would
take about 8 work-hours and require parts costing approximately $306
for the left hand (LH) elevator flange and $365 for the right hand (RH)
elevator flange. We estimate a cost of $986 to replace the LH elevator
flange per product and $1,045 to replace the RH elevator flange per
product. We have no way of determining the number of products that may
need these actions.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
    We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.

Regulatory Findings

    We determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and

responsibilities among the various levels of government.
    For the reasons discussed above, I certify this proposed
regulation:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866,
    (2) 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.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

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 AD:

GROB-WERKE: Docket No. FAA-2014-0092; Directorate Identifier 2014-
CE-002-AD.

(a) Comments Due Date

    We must receive comments byApril 7, 2014.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to GROB-WERKE Model G115E airplanes, all serial
numbers, and Model G120A airplanes, serial numbers 85001 through
85007, 85026 through 85056, and 85058, certificated in any category.

(d) Subject

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

(e) Reason

    This AD was prompted by mandatory continuing airworthiness
information (MCAI) originated by an aviation authority of another
country to identify and correct an unsafe condition on an aviation
product. The MCAI describes the unsafe condition as cracks in the
left hand elevator flange. We are issuing this AD to detect and
correct cracks in the left hand and right hand elevator flanges,
which could cause the elevator to fail and could result in reduced
control.

(f) Actions and Compliance

    Unless already done, do the actions in paragraphs (f)(1) through
(f)(3) of this AD:
    (1) Within the next 30 days after the effective date of this AD
and repetitively thereafter at intervals not to exceed 100 hours
time-in-service (TIS), inspect the left hand (LH) and the right hand
(RH) elevator flanges, part number (P/N) 115E-3761.06 and P/N 115E-
3762.07, or P/N 120A-3561.20(A) and P/N 120A-3562.20(A), as
applicable, for cracks. Do the inspections following GROB Aircraft
Service Bulletin No. MSB1078- 194/1, dated December 3, 2013, or GROB
Aircraft Service Bulletin No. MSB1121-140, dated December 3, 2013,
as applicable.
    (2) If any crack is found during any inspection required in
paragraph (f)(1) of this AD, before further flight, replace the
affected elevator flange with a serviceable part. Do the replacement
following GROB Aircraft Service Bulletin No. MSB1078-194/1, dated
December 3, 2013, or GROB Aircraft Service Bulletin No. MSB1121-140,
dated December 3, 2013, as applicable.
    (3) As of the effective date of this AD, only install an
elevator flange P/N 115E-3761.06, P/N 115E-3762.07, P/N 120A-
3561.20(A), or P/N 120A-3562.20(A), if it has been inspected
following GROB Aircraft Service Bulletin No. MSB1078-194/1, dated
December 3, 2013, or GROB Aircraft Service Bulletin No. MSB1121-140,
dated December 3, 2013, as applicable, and is free of any cracks.

(g) Credit for Actions Accomplished in Accordance With Previous Service
Information for Model G115E Airplanes

    This paragraph provides credit for the initial inspection
required in paragraph (f)(1) of this AD and any replacement required
in paragraph (f)(2) based on the result of the initial inspection if
already done before the effective date of this AD following GROB
Aircraft Service Bulletin No. MSB1078-194, dated November 26, 2013.

(h) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Office, FAA, has the authority to approve AMOCs for this
AD, if requested using the procedures found in 14 CFR 39.19. Send
information to ATTN: Karl Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>;
email<EMAIL_ADDRESS>Before using any approved AMOC on
any airplane to which the AMOC applies, notify your appropriate
principal inspector (PI) in the FAA Flight Standards District Office
(FSDO), or lacking a PI, your local FSDO.
    (2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
    (3) Reporting Requirements: For any reporting requirement in
this AD, a federal agency may not conduct or sponsor, and a person
is not required to respond to, nor shall a person be subject to a
penalty for failure to comply with a collection of information
subject to the requirements of the Paperwork Reduction Act unless
that collection of information displays a current valid OMB Control
Number. The OMB Control Number for this information collection is
2120-0056. Public reporting for this collection of information is
estimated to be approximately 5 minutes per response, including the
time for reviewing instructions, completing and reviewing the
collection of information. All responses to this collection of
information are mandatory. Comments concerning the accuracy of this
burden and suggestions for reducing the burden should be directed to
the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn:
Information Collection Clearance Officer, AES-200.

 (i) Related Information

    Refer to MCAI European Aviation Safety Agency (EASA) AD No.
2014-0004, dated January 7, 2014; and GROB Aircraft Service Bulletin
No. MSB1078-194, dated November 26, 2013, for related information.
You may examine the MCAI on the Internet at  http://www.regulations.gov by searching for and locating Docket No. FAA-
2014-0092. For service information related to this AD, contact Grob
Aircraft AG, Customer Service, Lettenbachstrasse 9, 86874
Tussenhausen-Mattsies, Germany, telephone: + 49 (0) 8268-998-105;
fax; + 49 (0) 8268-998-200; email<EMAIL_ADDRESS>
Internet: grob-aircraft.com. You may review this referenced service
information at the FAA, Small Airplane Directorate, 901 Locust,
Kansas City, Missouri 64106. For information on the availability of
this material at the FAA, call<PHONE_NUMBER>.

    Issued in Kansas City, Missouri, on February 11, 2014.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2014-03606 Filed 2-19-14; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 82, Number 91 (Friday, May 12, 2017)]
[Notices]
[Page 22133]
[FR Doc No: 2017-09679]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

Combined Notice of Filings #1

    Take notice that the Commission received the following electric
corporate filings:

    Docket Numbers: EC17-112-000.
    Applicants: Playa Solar 1, LLC, Playa Solar 2, LLC, EDF Renewable
Energy, Inc.
    Description: Application for Authorization Under Section 203 of the
Federal Power Act and Request for Expedited Action, Confidential
Treatment, and Waivers of Playa Solar 1, LLC, et al.
    Filed Date: 5/5/17.
    Accession Number: 20170505-5227.
    Comments Due: 5 p.m. ET 5/26/17.

    Take notice that the Commission received the following electric
rate filings:

    Docket Numbers: ER11-4453-001.
    Applicants: Santanna Natural Gas Corporation.
    Description: Supplement to January 23, 2017 Notice of Material
Change in Status of Santanna Natural Gas Corporation.
    Filed Date: 5/3/17.
    Accession Number: 20170503-5176.
    Comments Due: 5 p.m. ET 5/24/17.

    Docket Numbers: ER15-1905-005.
    Applicants: Amazon Energy LLC.
    Description: Notice of Change in Status of Amazon Energy LLC.
    Filed Date: 5/3/17.
    Accession Number: 20170503-5179.
    Comments Due: 5 p.m. ET 5/24/17.

    Docket Numbers: ER16-1923-003.
    Applicants: LWP Lessee, LLC.
    Description: Compliance filing: LWP Lessee Filing of Reactive Power
Rate Schedule Approved in Settlement to be effective 8/14/2016.
    Filed Date: 5/5/17.
    Accession Number: 20170505-5193.
    Comments Due: 5 p.m. ET 5/26/17.

    Docket Numbers: ER17-1555-000.
    Applicants: Arizona Public Service Company.
    Description: Sec.  205(d) Rate Filing: Amendment No. 1 to Service
Agreement Nos. 338 and 339 to be effective 5/1/2017.
    Filed Date: 5/5/17.
    Accession Number: 20170505-5157.
    Comments Due: 5 p.m. ET 5/26/17.

    Docket Numbers: ER17-1556-000.
    Applicants: Midcontinent Independent System Operator, Inc.
    Description: Sec.  205(d) Rate Filing: 2017-05-05_Data Sharing with
Natural Gas Pipelines to be effective 7/5/2017.
    Filed Date: 5/5/17.
    Accession Number: 20170505-5177.
    Comments Due: 5 p.m. ET 5/26/17.

    Docket Numbers: ER17-1557-000.
    Applicants: Duke Energy Progress, LLC.
    Description: Sec.  205(d) Rate Filing: DEP-NCEMPA RS No. 200
Revised PPA to be effective 7/1/2017.
    Filed Date: 5/5/17.
    Accession Number: 20170505-5189.
    Comments Due: 5 p.m. ET 5/26/17.

    Docket Numbers: ER17-1559-000.
    Applicants: FirstEnergy Solutions Corp.
    Description: Request for Authorization to Make Wholesale Power
Sales to Affiliated Utility of FirstEnergy Solutions Corp.
    Filed Date: 5/3/17.
    Accession Number: 20170503-5175.
    Comments Due: 5 p.m. ET 5/24/17.

    The filings are accessible in the Commission's eLibrary system by
clicking on the links or querying the docket number.
    Any person desiring to intervene or protest in any of the above
proceedings must file in accordance with Rules 211 and 214 of the
Commission's Regulations (18 CFR 385.211 and 385.214) on or before 5:00
p.m. Eastern Time on the specified comment date. Protests may be
considered, but intervention is necessary to become a party to the
proceeding.
    eFiling is encouraged. More detailed information relating to filing
requirements, interventions, protests, service, and qualifying
facilities filings can be found at: http://www.ferc.gov/docs-filing/efiling/filing-req.pdf. For other information, call<PHONE_NUMBER>
(toll free). For TTY, call<PHONE_NUMBER>.

    Dated: May 8, 2017.
Kimberly D. Bose,
Secretary.
[FR Doc. 2017-09679 Filed 5-11-17; 8:45 am]
 BILLING CODE 6717-01-P