[Federal Register Volume 77, Number 182 (Wednesday, September 19, 2012)]
[Notices]
[Pages 58207-58208]
[FR Doc No: 2012-22994]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

Agency Information Collection Activities: Requests for Comments;
Clearance of Renewed Approval of Information Collection: Changes in
Permissible Stage 2 Airplane Operations

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice and request for comments.

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SUMMARY: In accordance with the Paperwork Reduction Act of 1995, FAA
invites public comments about our intention to request the Office of
Management and Budget (OMB) approval to renew an information
collection. The Federal Register Notice with a 60-day comment period
soliciting comments on the following collection of information was
published on July 9, 2012, vol. 77, no. 131, page 40405. This
information is used to issue special flight authorizations for non-
revenue transports and non-transport jet operations of Stage 2
airplanes at U.S. airports. A minimal amount of data is requested to
identify the affected parties and determine whether the purpose for the
flight is one enumerated by law.

DATES: Written comments should be submitted by October 19, 2012.

FOR FURTHER INFORMATION CONTACT: Kathy DePaepe at<PHONE_NUMBER>, or by
email at<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:
    OMB Control Number: 2120-0652.
    Title: Changes in Permissible Stage 2 Airplane Operations.
    Form Numbers: There are no FAA forms associated with this
collection.
    Type of Review: Renewal of an information collection.
    Background: This collection is required under the Airport Noise and
Capacity Act of 1990 (as amended by Pub. L. 106-113) and the FAA
Modernization and Reform Act of 2012. The information is used by the
FAA to issue special flight authorizations for nonrevenue operations of
transports and non-transport jet Stage 2 airplanes at U.S. airports. A
minimal amount of data is requested to identify the affected

parties and determine whether the purpose for the flight is enumerated
in the law.
    Respondents: 50 applicants.
    Frequency: Information is collected on occasion.
    Estimated Average Burden per Response: 15 minutes.
    Estimated Total Annual Burden: 12.5 hours.

ADDRESSES: Interested persons are invited to submit written comments on
the proposed information collection to the Office of Information and
Regulatory Affairs, Office of Management and Budget. Comments should be
addressed to the attention of the Desk Officer, Department of
Transportation/FAA, and sent via electronic mail to<EMAIL_ADDRESS>or faxed to<PHONE_NUMBER>, or mailed to the
Office of Information and Regulatory Affairs, Office of Management and
Budget, Docket Library, Room 10102, 725 17th Street NW., Washington, DC
20503.
    Public Comments Invited: You are asked to comment on any aspect of
this information collection, including (a) Whether the proposed
collection of information is necessary for FAA's performance; (b) the
accuracy of the estimated burden; (c) ways for FAA to enhance the
quality, utility and clarity of the information collection; and (d)
ways that the burden could be minimized without reducing the quality of
the collected information. The agency will summarize and/or include
your comments in the request for OMB's clearance of this information
collection.

    Issued in Washington, DC on September 13, 2012.
Albert R. Spence,
FAA Assistant Information Collection Clearance Officer, IT Enterprises
Business Services Division, AES-200.
[FR Doc. 2012-22994 Filed 9-18-12; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 80, Number 119 (Monday, June 22, 2015)]
[Notices]
[Pages 35696-35697]
[FR Doc No: 2015-15273]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

Notice of Availability of the Final Environmental Assessment (EA)
and Finding of No Significant Impact/Record of Decision (FONSI/ROD) for
the Obstruction Removal Project for the Duluth-Sky Harbor Airport (DYT)
in Duluth, MN

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice.

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SUMMARY: The FAA is issuing this notice to advise the public that the
FAA has prepared and approved (May 8, 2015) a FONSI/ROD based on the
Final EA for the DYT Obstruction Removal Project. The Final EA was
prepared in accordance with the National Environmental Policy Act
(NEPA) of 1969, as amended, FAA Orders 1050.1E, ``Environmental
Impacts: Policies and Procedures'' and 5050.4B, ``NEPA Implementing
Instructions for Airport Actions''.

DATES: This notice is effective June 22, 2015.

FOR FURTHER INFORMATION CONTACT: Mr. Josh Fitzpatrick, Environmental
Protection Specialist, FAA Dakota-Minnesota Airports District Office
(ADO), 6020 28th Avenue South, Suite 102, Minneapolis, Minnesota,
55450. Telephone number is<PHONE_NUMBER>. Copies of the FONSI/ROD and/
or Final EA are available upon written request by contacting Mr. Josh
Fitzpatrick through the contact information above.

SUPPLEMENTARY INFORMATION: The Final EA evaluated the DYT Obstruction
Removal Project. The purpose of the project is to provide a safe
airport facility that will meet FAA and MnDOT aeronautics design and
operation requirements and safely maintain adequate runways with clear
approach surfaces for local, regional, and interregional aviation
users.
    The FAA and the Duluth Airport Authority (DAA) jointly prepared the
Final EA, pursuant to the requirements of the NEPA and the Minnesota
Environmental Policy Act, respectively. A joint Federal-State EA was
prepared.
    Chapter 2 of the Final EA identified and evaluated all reasonable
alternatives. Numerous alternatives were considered but eventually
discarded for not meeting the purpose and need. Three alternatives (No
Action, Alternative 5a Short, and Alternative 13) were examined in
detail. After careful analysis and consultation with various resource
agencies, the DAA selected Alternative 5a Short as the preferred
alternative. Alternative 5a Short satisfies the purpose and need while
minimizing impacts.
    Alternative 5a Short includes the construction of a rotated and
shortened runway. Compared to the existing runway, the new runway would
be shortened by 450 feet and rotated five degrees (Runway 32 end) into
Superior Bay. The primary surface would be graded and the parallel
taxiway reconstructed at a separation of 150 feet. The existing Medium
Intensity Runway Lights (MIRLs), Runway End Identifier Lights (REILs),
Precision Approach Path Indicators (PAPIs) and Medium Intensity Taxiway
Lights (MITLs) would be relocated or replaced. Existing pavements would
be removed and previously paved areas would be restored with native
vegetation.
    Alternative 5a Short includes placing approximately 69,800 cubic
yards of soil for runway construction (combined in water and on land),
50,000 cubic yards of surcharge (fill to be placed in order to compact
soft soils, and then removed) and 25,000 tons of riprap over a total
project area of 29.47 acres. The project will not impact the Scientific
Natural Area.
    Based on the analysis in the Final EA, the FAA has determined that
Alternative 5a Short will not result in significant impacts to
resources identified in accordance with FAA Orders 1050.1E and 5054.4B.
Therefore, an environmental impact statement will not be prepared.

    Issued in Minneapolis, Minnesota, on May 8, 2015.
Christopher Hugunin,
Manager, Dakota-Minnesota Airports District Office, FAA, Great Lakes
Region.
[FR Doc. 2015-15273 Filed 6-19-15; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 83, Number 228 (Tuesday, November 27, 2018)]
[Rules and Regulations]
[Pages 60756-60759]
[FR Doc No: 2018-25663]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0639; Product Identifier 2018-NM-058-AD; Amendment
39-19508; AD 2018-24-04]
RIN 2120-AA64

Airworthiness Directives; Airbus SAS Airplanes

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

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Airbus SAS Model A330-200 Freighter, A330-200, and A330-300 series
airplanes. This AD was prompted by a revision of a certain
airworthiness limitations item (ALI) document, which specifies new or
more restrictive maintenance instructions and airworthiness
limitations, and a determination that those maintenance instructions
and airworthiness limitations are necessary. This AD requires revising
the existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive maintenance instructions and
airworthiness limitations. We are issuing this AD to address the unsafe
condition on these products.

DATES: This AD is effective January 2, 2019.
    The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 2,
2019.

ADDRESSES: For service information identified in this final rule,
contact Airbus SAS, Airworthiness Office--EAL, Rond-Point Emile
Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36
96; fax +33 5 61 93 45 80; email [email protected];
internet http://www.airbus.com. You may view this service information
at the FAA, Transport Standards Branch, 2200 South 216th St., Des
Moines, 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-2018-
0639.

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-2018-
0639; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, the regulatory evaluation, any comments received, and
other information. The address for Docket Operations (phone: 800-647-
5527) is 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: Vladimir Ulyanov, Aerospace Engineer,
International Section, Transport Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; telephone and fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Airbus SAS Model
A330-200 Freighter, A330-200, and A330-300 series airplanes. The NPRM
published in the Federal Register on August 10, 2018 (83 FR 39633). The
NPRM was prompted by a revision of a certain ALI document, which
specifies new or more restrictive maintenance instructions and
airworthiness limitations, and a determination that those maintenance
instructions and airworthiness limitations are necessary. The NPRM
proposed to require revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive
maintenance instructions and airworthiness limitations.
    We are issuing this AD to address fatigue cracking, damage, and
corrosion in principal structural elements; such fatigue cracking,
damage, and corrosion could result in reduced structural integrity 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
2018-0068, dated March 26, 2018 (referred to after this as the
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to
correct an unsafe condition for certain Airbus SAS Model A330-200
Freighter, A330-200, and A330-300 series airplanes. The MCAI states:

    The airworthiness limitations for Airbus A330 and A340
aeroplanes, which are approved by EASA, are currently defined and
published in the A330 and A340 [Airworthiness Limitations Section]
ALS document(s). The Damage Tolerant Airworthiness Limitation Items
(DT ALI) are specified in the ALS Part 2. These instructions have
been identified as mandatory actions for continued airworthiness.
    Failure to comply with these instructions could result in an
unsafe condition [i.e., fatigue cracking, damage, and corrosion in
principal structural elements] which could result in reduced
structural integrity of the airplane.
    Previously, EASA issued AD 2016-0152 [which corresponds to FAA
AD 2017-19-13, Amendment 39-19043 (82 FR 43837, September 20, 2017)
(``AD 2017-19-13'')] for A330 and A340 aeroplanes to require
accomplishment of all maintenance tasks as described in ALS Part 2
Revision 01 (A330 aeroplanes) and Revision 02 (A340 aeroplanes).
    Since that [EASA] AD was issued, Airbus published Revision 02 of
the ALS Part 2 for A330 aeroplanes, including new and/or more
restrictive items.
    For the reason described above, this [EASA] AD takes over the
requirements from EASA AD 2016-0152 for A330 aeroplanes, and
requires accomplishment of all maintenance tasks as described in the
ALS. EASA AD 2016-0152 has been revised accordingly, removing A330
aeroplanes from the Applicability.

    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-2018-
0639.

Comments

    We gave the public the opportunity to participate in developing
this final rule. The following presents the comment received on the
NPRM and the FAA's response to that comment.

Request To Clarify or Remove Previously Approved Alternative Method of
Compliance (AMOC)

    American Airlines requested that we clarify the applicability of
the AMOC approved in letter AIR-676-18-111 R1, dated January 29, 2018,
or remove the previously approved AMOC from the proposed AD. The
commenter stated that, as currently written, paragraph (j)(1)(ii) of
the proposed AD is confusing because it states that the AMOC approved
in letter AIR-676-18-111 R1, dated January 29, 2018, previously
approved for AD 2017-19-13, would still be approved for the
corresponding provisions of the final rule. The commenter explained
that this AMOC is limited to a specific organization and is not
applicable to all operators.
    We agree with the commenter's request for the reasons provided by
the commenter. AMOC letter AIR-676-18-111 R1, dated January 29, 2018,
was issued specifically to Singapore Technologies Aerospace Limited and
is not a global AMOC. We have revised paragraph (j)(1)(ii) of this AD
to clarify that the AMOC granted in letter AIR-676-18-111 R1, dated
January 29, 2018, is approved as an AMOC for Model A330-300 series
airplanes modified from a passenger to freighter configuration under
the provisions of FAA Supplemental Type Certificate ST04038NY.

Conclusion

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

Related Service Information Under 1 CFR Part 51

    Airbus SAS has issued Airbus A330 Airworthiness Limitations Section
(ALS) Part 2--Damage Tolerant Airworthiness Limitation Items (DT-ALI),
Revision 02, Issue 2, dated November 22, 2017. This service information
describes maintenance instructions and airworthiness limitations
applicable to the DT-ALI. 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 105 airplanes of U.S. registry. We
estimate the following costs to comply with this AD:
    We have determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although we recognize that this number may vary from operator to
operator. In the past, we have estimated that this action takes 1 work-
hour per airplane. Since operators incorporate maintenance or
inspection program changes for their affected fleet(s), we have
determined that a per-operator estimate is more accurate than a per-
airplane estimate. Therefore, we estimate the total cost per operator
to be $7,650 (90 work-hours x $85 per work-hour).

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 and
associated appliances to the Director of the System Oversight Division.

Regulatory Findings

    This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866,
    (2) Is not a ``significant rule'' under 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):

2018-24-04 Airbus SAS: Amendment 39-19508; Docket No. FAA-2018-0639;
Product Identifier 2018-NM-058-AD.

(a) Effective Date

    This AD is effective January 2, 2019.

(b) Affected ADs

    This AD affects AD 2017-19-13, Amendment 39-19043 (82 FR 43837,
September 20, 2017) (``AD 2017-19-13'').

(c) Applicability

    This AD applies to the Airbus SAS airplanes specified in
paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in
any category, with an original certificate of airworthiness or
original export certificate of airworthiness issued on or before
November 22, 2017.
    (1) Model A330-223F and -243F airplanes.
    (2) Model A330-201, -202, -203, -223, and -243 airplanes.
    (3) Model A330-301, -302, -303, -321, -322, -323, -341, -342,
and -343 airplanes.

(d) Subject

    Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.

(e) Reason

    This AD was prompted by a revision of a certain airworthiness
limitations item (ALI) document, which specifies new or more
restrictive maintenance instructions and airworthiness limitations,
and a determination that those maintenance instructions and
airworthiness limitations are necessary. We are issuing this AD to
address fatigue cracking, damage, and corrosion in principal
structural elements; such fatigue cracking, damage, and corrosion
could result in reduced structural integrity of the airplane.

(f) Compliance

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

(g) Maintenance or Inspection Program Revision

    Within 90 days after the effective date of this AD, revise the
existing maintenance or inspection program, as applicable, to
incorporate the information specified in Airbus A330 Airworthiness
Limitations Section (ALS) Part 2--Damage Tolerant Airworthiness
Limitation Items (DT-ALI), Revision 02, Issue 2, dated November 22,
2017. The initial compliance time for accomplishing the tasks is at
the applicable times specified in Airbus A330 Airworthiness
Limitations Section (ALS) Part 2--Damage Tolerant Airworthiness
Limitation Items (DT-ALI), Revision 02, Issue 2, dated November 22,
2017, or within 90 days after the effective date of this AD,
whichever occurs later.

(h) No Alternative Actions or Intervals

    After the existing maintenance or inspection program has been
revised, as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections) or intervals may be used unless the
actions or intervals are approved as an alternative method of
compliance (AMOC) in accordance with the procedures specified in
paragraph (j)(1) of this AD.

(i) Terminating Action for the Requirements of AD 2017-19-13

    Accomplishing the action required by paragraph (g) of this AD
terminates all requirements of AD 2017-19-13.

(j) 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. If sending information
directly to the International Section, send it to the attention of
the person identified in paragraph (k)(2) of this AD. Information
may be emailed to: [email protected].
    (i) 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.
    (ii) The AMOC specified in letter AIR-676-18-111 R1, dated
January 29, 2018, approved previously for AD 2017-19-13, is approved
as an AMOC for the corresponding provisions of this AD for Model
A330-300 series airplanes that have been modified from a passenger
to freighter configuration under the provisions of FAA Supplemental
Type Certificate ST04038NY.
    (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 SAS's EASA Design Organization
Approval (DOA). If approved by the DOA, the approval must include
the DOA-authorized signature.

(k) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2018-0068, dated March 26, 2018, 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-2018-0639.
    (2) For more information about this AD, contact Vladimir
Ulyanov, Aerospace Engineer, International Section, Transport
Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198;
telephone and fax<PHONE_NUMBER>.

(l) 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 A330 Airworthiness Limitations Section (ALS) Part 2--
Damage Tolerant Airworthiness Limitation Items (DT-ALI),

Revision 02, Issue 2, dated November 22, 2017.
    (ii) [Reserved]
    (3) For service information identified in this AD, contact
Airbus SAS, Airworthiness Office--EAL, Rond-Point Emile Dewoitine
No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax
+33 5 61 93 45 80; email [email protected];
internet http://www.airbus.com.
    (4) You may view this service information at the FAA, Transport
Standards Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call
206-231-3195.
    (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 Des Moines, Washington, on November 15, 2018.
Dionne Palermo,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2018-25663 Filed 11-26-18; 8:45 am]
 BILLING CODE 4910-13-P


[Federal Register: May 11, 2006 (Volume 71, Number 91)]
[Notices]
[Page 27486]
[DOCID:fr11my06-61]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. RP06-344-000]

Williston Basin Interstate Pipeline Company; Notice of Proposed
Changes in FERC Gas Tariff

May 4, 2006.
    Take notice that on May 1, 2006, Williston Basin Interstate
Pipeline Company (Williston Basin) tendered for filing as part of its
FERC Gas Tariff, Second Revised Volume No. 1, the following tariff
sheets, to become effective June 2, 2006:

Fourth Revised Sheet No. 179B
Second Revised Sheet No. 181
First Revised Sheet No. 181A
Third Revised Sheet No. 182
First Revised Sheet No. 182A
First Revised Sheet No. 184
First Revised Sheet No. 185
Second Revised Sheet No. 186
Seventh Revised Sheet No. 225
Eighth Revised Sheet No. 226
Third Revised Sheet No. 226A
Third Revised Sheet No. 226B
Third Revised Sheet No. 233
Fourth Revised Sheet No. 368
Third Revised Sheet No. 369
Second Revised Sheet No. 730
Second Revised Sheet No. 731

    Williston Basin states that it is proposing to make certain tariff
modifications which it believes are necessary to correct and/or clarify
terms used in its tariff.
    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 online 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 e-mail
notification when a document is added to a subscribed docket(s). For
assistance with any FERC Online service, please e-mail
<EMAIL_ADDRESS>or call<PHONE_NUMBER> (toll free). For

TTY, call<PHONE_NUMBER>.

Magalie R. Salas,
Secretary.
 [FR Doc. E6-7166 Filed 5-10-06; 8:45 am]

BILLING CODE 6717-01-P