[Federal Register Volume 81, Number 32 (Thursday, February 18, 2016)]
[Proposed Rules]
[Pages 8160-8164]
[FR Doc No: 2016-03137]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-0465; Directorate Identifier 2015-NM-096-AD]
RIN 2120-AA64

Airworthiness Directives; Airbus Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to adopt a new airworthiness directive (AD) for
certain Airbus Model A330-200 and -300 series airplanes; and Model
A340-200 and -300 series airplanes. This proposed AD was prompted by a
determination that the compliance times for certain post-repair
inspections and certain allowable damage limits (ADLs) must be reduced
in order to address fatigue. This proposed AD would require identifying
any repairs and ADLs used to assess or control any structural damage on
certain structural areas, and corrective action if necessary. We are
proposing this AD to prevent fatigue damage on primary structure and
structural repairs, which could result in reduced structural integrity
of the airplane.

DATES: We must receive comments on this proposed AD by April 4, 2016.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, 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, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
    For service information identified in this NPRM, contact Airbus
SAS, Airworthiness Office--EAL, 1 Rond Point Maurice Bellonte, 31707
Blagnac Cedex, France; telephone: +33 5 61 93 36 96; fax: +33 5 61 93
45 80; email<EMAIL_ADDRESS>Internet: http://www.airbus.com. You may view this referenced service information at the
FAA, Transport

Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information
on the availability of this material at the FAA, call<PHONE_NUMBER>.

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-
0465; 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
Operations office (telephone:<PHONE_NUMBER>) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.

FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone:<PHONE_NUMBER>;
fax:<PHONE_NUMBER>.

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-2016-0465;
Directorate Identifier 2015-NM-096-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 based on those comments.
    We will post all comments we receive, without change, to http://www.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 Union, has issued EASA AD
2015-0101R1, dated June 12, 2015 (referred to after this as the
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to
correct an unsafe condition for certain Airbus Model A330-200 and -300
series airplanes; and Model A340-200 and -300 series airplanes. The
MCAI states:

    Result of a fleet survey accomplished in 2008 identified that
the nature of flight missions of A330 and A340-200/300 fleets had
significantly changed in comparison with assumed usage during the
type certification. Consequently, it was decided to recalculate the
Structural Repair Manual (SRM) fatigue values to ensure that the
given threshold and intervals remain valid.
    The results of this recalculation identified reduced thresholds
and intervals applicable for repairs and Allowable Damage Limits
(ADL) affecting the following areas:

--Door cut-out corners of door surrounding panels (forward cargo
door, forward passenger (PAX) door, mid PAX door, emergency exit
door/PAX door 3, aft cargo door, bulk cargo door, aft PAX door), on
both Left Hand (LH) and Right Hand (RH) sides,
--Stringer (STGR) 9 junction between Frame (FR) 10 and FR13 on both
LH and RH sides, and
--Fuselage skin doubler repairs on both LH and RH sides.

    Failing to apply the reduced thresholds and intervals, could
adversely affect the structural integrity of the aeroplane.
    To address this unsafe condition, Airbus issued SRM revision
dated April 2013 and temporary revision (TR) 53-001 for the STGR9
junction between FR10 and FR13 area (and subsequent revisions) to
introduce reduced thresholds and intervals for the affected ADLs and
repairs and issued a set of Service Bulletins (SB) to identify the
ADLs used and repairs made, as well as to enable operators to update
aeroplane repair records.
    Consequently EASA issued AD * * *, to require identification of
any repairs and/or ADL used to assess or control any structural
damage on certain structural areas and, depending on findings,
accomplishment of corrective action(s) [including revising the
maintenance or inspection program as applicable to incorporate
revised thresholds and intervals and repair].
    Since that [EASA] AD was issued, data review confirmed that A330
freighter versions are not affected by the unsafe condition.
    This [EASA] AD is revised to remove A330-223F and A330-243F 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-2016-
0465.

Related Service Information Under 1 CFR Part 51

    Airbus has issued the following service information. The service
information describes procedures for updating the airplane repair
records with revised thresholds and intervals.
     Airbus Service Bulletin A330-53-3232, dated November 4,
2014.
     Airbus Service Bulletin A330-53-3233, dated September 26,
2014.
     Airbus Service Bulletin A330-53-3234, dated December 8,
2014.
     Airbus Service Bulletin A330-53-3235, Revision 01, dated
January 14, 2015.
     Airbus Service Bulletin A340-53-4222, dated November 25,
2014.
     Airbus Service Bulletin A340-53-4223, dated September 26,
2014.
     Airbus Service Bulletin A340-53-4224, dated December 15,
2014.
     Airbus Service Bulletin A340-53-4225, Revision 01, dated
January 14, 2015.
    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.

FAA's Determination and Requirements of This 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 the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are proposing this AD because we
evaluated all pertinent information and determined an unsafe condition
exists and is likely to exist or develop on other products of these
same type designs.

Costs of Compliance

    We estimate that this proposed AD affects 95 airplanes of U.S.
registry. We also estimate that it would take about 2 work-hours 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 this proposed AD on U.S. operators to be $16,150,
or $170 per product.
    We have received no definitive data that would enable us to provide
cost estimates for the on-condition actions specified in this proposed
AD.

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 airworthiness
directive (AD):

Airbus: Docket No. FAA-2016-0465; Directorate Identifier 2015-NM-
096-AD.

(a) Comments Due Date

    We must receive comments by April 4, 2016.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to the airplanes, certificated in any category,
identified in paragraphs (c)(1) and (c)(2) of this AD; manufacturer
serial numbers (MSNs) 1 through 1,600 inclusive.
    (1) Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -
303, -321, -322, -323, -341, -342, and -343 airplanes.
    (2) Airbus Model A340-211, -212, -213, -311, -312, and -313
airplanes.

(d) Subject

    Air Transport Association (ATA) of America Code 53, Fuselage.

(e) Reason

    This AD was prompted by a determination that the compliance
times for certain post-repair inspections and certain allowable
damage limits (ADLs) must be reduced in order to address fatigue. We
are issuing this AD to prevent fatigue damage on primary structure
and structural repairs, which could result in reduced structural
integrity of the airplane.

(f) Compliance

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

(g) Records Review

    At the applicable times in table 1 to paragraph (g) of this AD,
review the airplane maintenance records to identify any structural
repair manual (SRM) ADLs used to assess or control any structural
damage or any structural repair accomplished as specified in an SRM,
as applicable, that have been applied on the areas as specified in
table 2 to paragraph (g) of this AD.

                              Table 1 to Paragraph (g) of This AD--Compliance Times
----------------------------------------------------------------------------------------------------------------
                                                                                Related Service
          Affected airplanes             ADL location/repair        Compliance time              Bulletin
----------------------------------------------------------------------------------------------------------------
A330-200 Pre-mod 49144...............  Mid passenger (PAX)      Within 12 months after   Airbus Service Bulletin
                                        door surround panels.    the effective date of    A330-53-3232, dated
                                                                 this AD.                 November 4, 2014.
A330-200 Pre-mod 49144...............  Forward cargo door,      Within 24 months after   Airbus Service Bulletin
                                        emergency exit door/     the effective date of    A330-53-3232, dated
                                        PAX door 3, aft cargo    this AD.                 November 4, 2014.
                                        door, bulk cargo door,
                                        and aft PAX door
                                        surround panels.
A330-300 Pre-mod 49144 and A340-200/-  Mid PAX door surround    Within 24 months after   Airbus Service Bulletin
 300 pre-mod 49144.                     panels, forward cargo    the effective date of    A330-53-3232, dated
                                        door, emergency exit     this AD.                 November 4, 2014 or
                                        door/PAX door 3, aft                              Airbus Service
                                        cargo door, bulk cargo                            Bulletin A340-53-4222,
                                        door, and aft PAX door                            dated November 25,
                                        surround panels.                                  2014.
All, Post-mod 40347..................  Forward PAX door         Within 12 months after   Airbus Service Bulletin
                                        surround panels with     the effective date of    A330-53-3233, dated
                                        an ADL with a            this AD.                 September 26, 2014 or
                                        Temporary Life Limit.                             Airbus Service
                                                                                Bulletin A340-53-4223,
                                                                                dated September 26,
                                                                                2014.
All, Post-mod 40347..................  Forward PAX door         Within 24 months after   Airbus Service Bulletin
                                        surround panels with     the effective date of    A330-53-3233, dated
                                        an ADL with a            this AD.                 September 26, 2014 or
                                        Permanent Acceptance.                             Airbus Service
                                                                                Bulletin A340-53-4223,
                                                                                dated September 26,
                                                                                2014.
All..................................  STGR9 junction between   Within 12 months after   Airbus Service Bulletin
                                        frame (FR) 10 and FR13.  the effective date of    A330-53-3235, Revision
                                                                 this AD.                 01, dated January 14,
                                                                                2015 or Airbus Service
                                                                                Bulletin A340-53-4225,
                                                                                Revision 01, dated
                                                                                January 14, 2015.
A340-200/-300 Weight Variant (WV)00s.  Forward and rear         Within 12 months after   Airbus Service Bulletin
                                        fuselage.                the effective date of    A340-53-4224, dated
                                                                 this AD.                 December 15, 2014.
A340-200/-300 WV00s..................  Nose forward and center  Within 24 months after   Airbus Service Bulletin
                                        fuselage.                the effective date of    A340-53-4224, dated
                                                                 this AD.                 December 15, 2014.

A330-200/-300 pre-MOD 49144 and A340-  Forward and rear         Within 24 months after   Airbus Service Bulletin
 200/-300 WV20s.                        fuselage, nose forward   the effective date of    A330-53-3234, dated
                                        and center fuselage.     this AD.                 December 8, 2014 or
                                                                                Airbus Service
                                                                                Bulletin A340-53-4224,
                                                                                dated December 15,
                                                                                2014.
A330-200/-300 post-MOD 49144 and A340- Nose forward and center  Within 24 months after   Airbus Service Bulletin
 200/-300 post-MOD 49144.               fuselage.                the effective date of    A330-53-3234, dated
                                                                 this AD.                 December 8, 2014 or
                                                                                Airbus Service
                                                                                Bulletin A340-53-4224,
                                                                                dated December 15,
                                                                                2014.
----------------------------------------------------------------------------------------------------------------

           Table 2 to Paragraph (g) of This AD--Affected Areas
------------------------------------------------------------------------
                                                                  As
                                                               specified
   Affected areas (on both left-hand and right-hand sides)     in Airbus
                                                                Service
                                                              Bulletin--
------------------------------------------------------------------------
Door cut-out corners of door surrounding panels (forward      A330-53-32
 cargo door, mid PAX door, emergency exit door/PAX door 3,    32, dated
 aft cargo door, bulk cargo door, aft PAX door).............  November
                                                              4, 2014
                                                              (for Model
                                                               A330
                                                              series
                                                              airplanes)
                                                              or A340-53-
                                                              4222,
                                                              dated
                                                              November
                                                              25, 2014
                                                              (for Model
                                                               A340
                                                              series
                                                              airplanes)
                                                                  .
Forward PAX door surround panels............................  A330-53-32
                                                              33, dated
                                                              September
                                                              26, 2014
                                                              (for Model
                                                               A330
                                                              series
                                                              airplanes)
                                                              or A340-53-
                                                              4223,
                                                              dated
                                                              September
                                                              26, 2014
                                                              (for Model
                                                               A340
                                                              series
                                                              airplanes)
                                                                  .
Fuselage skin doubler repairs...............................  A330-53-32
                                                              34, dated
                                                              December
                                                              8, 2014
                                                              (for Model
                                                               A330
                                                              series
                                                              airplanes)
                                                              or A340-53-
                                                              4224,
                                                              dated
                                                              December
                                                              15, 2014
                                                              (for Model
                                                               A340
                                                              series
                                                              airplanes)
                                                                  .
STGR9 junction between FR10 and FR13........................  A330-53-32
                                                                35,
                                                              Revision
                                                              01, dated
                                                              January
                                                              14, 2015
                                                              (for Model
                                                               A330
                                                              series
                                                              airplanes)
                                                              or A340-53-
                                                              4225,
                                                              Revision
                                                              01, dated
                                                              January
                                                              14, 2015
                                                              (for Model
                                                               A340
                                                              series
                                                              airplanes)
                                                                  .
------------------------------------------------------------------------

(h) Corrective Actions

    If, during any review required by paragraph (g) of this AD, it
is determined that an SRM ADL was used on an area specified in table
2 to paragraph (g) of this AD to assess or control any structural
damage, or any structural repair of an area specified in table 2 to
paragraph (g) of this AD was accomplished as specified in the
instructions of the applicable SRM revision, dated before April 2013
or SRM temporary revision (TR) dated before November 28, 2014:
Within the applicable compliance time specified in table 1 to
paragraph (g) of this AD, do the actions specified in paragraph
(h)(1) or (h)(2) of this AD, as applicable.
    (1) Revise the maintenance or inspection program, as applicable,
with the applicable revised thresholds and intervals for the
identified structural repairs embodied on the airplane, and
accomplish all updated inspections, in accordance with the
Accomplishment Instructions of the applicable service information
identified in table 2 to paragraph (g) of this AD, except as
required by paragraphs (h)(1)(i) and (h)(1)(ii) of this AD.
    (i) Where the applicable Airbus service information identified
in table 2 to paragraph (g) of this AD specifies to contact Airbus
for specific assessment, revise the maintenance or inspection
program and accomplish all updated inspections, as applicable, using
a method approved by the Manager, International Branch, ANM-116,
Transport Airplane Directorate, FAA; or the European Aviation Safety
Agency (EASA); or Airbus's EASA Design Organization Approval (DOA).
    (ii) Where the Airbus applicable service information identified
in table 2 to paragraph (g) of this AD specifies ``current SRM,'' no
SRM revision dated before April 2013 or SRM TR dated before November
28, 2014, is considered a ``current SRM.''
    (2) For any repair that was previously allowed in any revision
of the Airbus A330 or A340 SRM, as applicable, dated before April
2013; or in any SRM TR dated before November 28, 2014, to the
applicable SRM: Make an assessment using a method approved by the
Manager, International Branch, ANM-116, Transport Airplane
Directorate, FAA; or the EASA; or Airbus's EASA DOA and perform
necessary corrective actions at the applicable times identified
therein.

(i) Limitation on Repair/Replacement

    As of the effective date of this AD, for any structural damage
in the areas identified in table 2 to paragraph (g) of this AD that
has exceeded the ADL, no repair or replacement may be done using an
Airbus A330 or A340 SRM dated before April 2013, or any SRM TR dated
before November 28, 2014.

(j) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, 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
Branch, send it to ATTN: Vladimir Ulyanov, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone: 425-227-
1138; fax:<PHONE_NUMBER>. Information may be emailed to<EMAIL_ADDRESS>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. The AMOC approval letter must
specifically reference this AD.
    (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
Branch, ANM-116, Transport Airplane Directorate, FAA; or EASA; or
Airbus's EASA Design Organization Approval (DOA). If approved by the
DOA, the approval must include the DOA-authorized signature.
    (3) Required for Compliance (RC): Except as required by
paragraphs (h)(1)(i), (h)(1)(ii), and (h)(2) of this AD: If any
service information contains procedures or tests that are identified
as RC, those procedures and tests must be done to comply with this
AD; any procedures or tests that are not identified as RC are
recommended. Those procedures and tests that are not identified as
RC may be deviated from using accepted methods in accordance with
the operator's maintenance or inspection program without obtaining
approval of an AMOC, provided the procedures and tests identified as
RC can be done and the airplane can be put back in an airworthy
condition. Any substitutions or changes to procedures or tests
identified as RC require approval of an AMOC.

(k) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD

2015-0101R1, dated June 12, 2015, 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-
2016-0465.
    (2) For service information identified in this AD, contact
Airbus SAS, Airworthiness Office--EAL, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France; telephone: +33 5 61 93 36 96;
fax: +33 5 61 93 45 80; email<EMAIL_ADDRESS>
Internet: http://www.airbus.com. You may view this service
information at the FAA, Transport Airplane Directorate, 1601 Lind
Avenue SW., Renton, WA. For information on the availability of this
material at the FAA, call<PHONE_NUMBER>.

    Issued in Renton, Washington, on February 6, 2016.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-03137 Filed 2-17-16; 8:45 am]
 BILLING CODE 4910-13-P


[Federal Register: October 7, 2009 (Volume 74, Number 193)]
[Notices]
[Page 51574-51576]
[DOCID:fr07oc09-47]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

Combined Notice of Filings 1

September 29, 2009.
    Take notice that the Commission received the following electric
corporate filings:
    Docket Numbers: EC09-110-000
    Applicants: Monmouth Energy, Inc., Montauk Energy Capital, LLC,
Johnnic Holdings USA LLC, Johnnic Holdings Limited, Tsogo Investment
Holding Company, Hosken Consolidated Investments Limited
    Description: Application for authorization under Section 203 of the
federal power act request for expedited consideration and confidential
treatment re Monmouth Energy, Inc. et al.
    Filed Date: 09/28/2009.
    Accession Number: 20090929-0123.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Take notice that the Commission received the following exempt
wholesale generator filings:
    Docket Numbers: EG09-95-000.
    Applicants: Raleigh Wind Power Partnership.
    Description: Notice of Self-Certification of Exempt Wholesale
Status of Raleigh Wind Power Partnership.
    Filed Date: 09/29/2009.
    Accession Number: 20090929-5049.

    Comment Date: 5 p.m. Eastern Time on Tuesday, October 20, 2009.

    Take notice that the Commission received the following electric
rate filings:
    Docket Numbers: ER97-3359-014.
    Applicants: Florida Power & Light Company.
    Description: Florida Power & Light Company submits notice of change
in status.
    Filed Date: 09/25/2009.
    Accession Number: 20090928-0087.
    Comment Date: 5 p.m. Eastern Time on Friday, October 16, 2009.

    Docket Numbers: ER02-537-025; ER07-758-017.
    Applicants: Inland Empire Energy Center, L.L.C., Shady Hills Power
Company, L.L.C.
    Description: Notice of Non-Material Change in Status for Shady
Hills Power Company, L.L.C. et al.
    Filed Date: 09/29/2009.
    Accession Number: 20090929-5045.
    Comment Date: 5 p.m. Eastern Time on Tuesday, October 20, 2009.

    Docket Numbers: ER03-774-013.
    Applicants: Eagle Energy Partners I, LP.
    Description: Notice of Non-Material Change in Status of Eagle
Energy Partners I, LP.
    Filed Date: 09/25/2009.
    Accession Number: 20090925-5104.
    Comment Date: 5 p.m. Eastern Time on Friday, October 16, 2009.

    Docket Numbers: ER08-1113-006.
    Applicants: California Independent System Operator Corporation.
    Description: The California Independent System Operator Corp
submits a compliance filing re FERC's 7/30/09 Order on Rehearing and
Clarification.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0100.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER08-1272-002.
    Applicants: New York Independent System Operator, Inc.
    Description: New York Independent System Operator, Inc. submits
Fourth Revised Sheet 751 et al. to FERC Electric Tariff, Original
Volume 1.
    Filed Date: 09/28/2009.
    Accession Number: 20090929-0086.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER08-83-002.
    Applicants: Idaho Power Company.
    Description: Idaho Power Co submits a compliance filing re the 7/
30/09 Order.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0099.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1590-001.
    Applicants: Xcel Energy Services Inc.
    Description: Amendment to Application of Xcel Energy Services Inc.
    Filed Date: 09/28/2009.
    Accession Number: 20090925-5103.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1699-001.
    Applicants: Eurus Combine Hills II LLC.
    Description: Eurus Combine Hills II LLC submits an amended
application for market based rate authority and associated waivers and
Blanket Approvals.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0101.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1749-000.
    Applicants: PacifiCorp.
    Description: PacifiCorp submits Large Generator Interconnection
Agreement Facilities Maintenance Agreement.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0102.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1750-000.
    Applicants: American Electric Power Service Corporation.
    Description: American Electric Power submits Nineteenth Revised
Interconnection and Local Delivery Service Agreement between AEP and
Buckeye Power, Inc.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0088.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1751-000.
    Applicants: Westar Energy, Inc.
    Description: Westar Energy, Inc. et al. submit Third Revised Sheet
No. 9 et al. to First Revised Rate Schedule FERC No 169.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0089.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1752-000.
    Applicants: Westar Energy, Inc.
    Description: Westar Energy, Inc. et al. submits Third Revised Sheet
11 & 1 to the Wholesale Electric Service Agreement, designated as First
Revised Rate Schedule FERC 170 between Kansas Gas and Electric Co and
the City of Elsmore, KS.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0090.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1753-000.
    Applicants: Westar Energy, Inc.
    Description: Westar Energy, Inc. submits Third Revised No. 11 et
al. to the Wholesale Electric Service Agreement with the City of Blue
Mound, Kansas.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0091.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1754-000.
    Applicants: Westar Energy, Inc.
    Description: Westar Energy, Inc. et al. submits Third Revised Sheet
No. 10 et al. to the Wholesale Electric Service Agreement.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0092.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1755-000.
    Applicants: Westar Energy, Inc.
    Description: Westar Energy, Inc. submits Third Revised No. 8 et al.
to the Wholesale Electric Service Agreement with the City of Mulberrry,
Kansas.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0094.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1756-000.
    Applicants: Westar Energy, Inc.
    Description: Westar Energy, Inc. submits Third Revised No. 12 et
al. to the Wholesale Electric Service Agreement with the City of
Bronson, Kansas.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0093.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1757-000.
    Applicants: Westar Energy, Inc.
    Description: Westar Energy, Inc. submits Third Revised No. 11 et
al. to the Wholesale Electric Service Agreement with the City of
Savonburg, Kansas.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0095.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1758-000.
    Applicants: Westar Energy, Inc.
    Description: Westar Energy, Inc. submits Third Revised No. 10 et
al. to the Wholesale Electric Service Agreement with the City of
Mindenmines, Kansas.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0096.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1759-000.
    Applicants: Westar Energy, Inc.
    Description: Westar Energy, Inc. submits Eighth Revised Sheet No. 4
et

al. to the Wholesale Electric Service Agreement.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0097.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1761-000.
    Applicants: Westar Energy, Inc.
    Description: Westar Energy, Inc. submits Third Revised No. 4 et al.
to the Wholesale Electric Service Agreement with the City of
Vermillion, Kansas.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0098.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1762-000.
    Applicants: Westar Energy, Inc.
    Description: Westar Energy, Inc. submits its Full Requirements
Electric Service Rate Schedule and Electric Service Agreement.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-0104.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Docket Numbers: ER09-1763-000.
    Applicants: PacifiCorp.
    Description: PacifiCorp submits Notice of Cancellation for Service
Agreement 425 with Bonneville Power Administration.
    Filed Date: 09/28/2009.
    Accession Number: 20090929-0088.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.
    Take notice that the Commission received the following foreign
utility company status filings:

    Docket Numbers: FC09-1-000.
    Applicants: SunEdison Canada, LLC.
    Description: Notice of Self Certification of Foreign Utility
Company Status of SunEdison Canada, LLC as FUCO.
    Filed Date: 09/28/2009.
    Accession Number: 20090928-5098.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Take notice that the Commission received the following open access
transmission tariff filings:

    Docket Numbers: OA08-32-005.
    Applicants: PJM Interconnection L.L.C.
    Description: PJM Interconnection, LLC submits Second Substitute
Seventh Revised Sheet 183 et al. to Third Revised Rate Schedule FERC
24.
    Filed Date: 09/28/2009.
    Accession Number: 20090929-0087.
    Comment Date: 5 p.m. Eastern Time on Monday, October 19, 2009.

    Any person desiring to intervene or to protest in any of the above
proceedings 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) on or before 5 p.m. Eastern time on the specified comment
date. It is not necessary to separately intervene again in a subdocket
related to a compliance filing if you have previously intervened in the
same docket. 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. Anyone filing a motion to
intervene or protest must serve a copy of that document on the
Applicant. In reference to filings initiating a new proceeding,
interventions or protests submitted on or before the comment deadline
need not be served on persons other than the Applicant.
    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 proceedings 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>.

Nathaniel J. Davis, Sr.,
Deputy Secretary.
[FR Doc. E9-24114 Filed 10-6-09; 8:45 am]

BILLING CODE 6717-01-P


 [Federal Register Volume 76, Number 218 (Thursday, November 10, 2011)] [Rules and Regulations] [Page 70062] [FR Doc No: C1-2011-25035]

======================================================================= -----------------------------------------------------------------------

DEPARTMENT OF HOMELAND SECURITY

Coast Guard

46 CFR Parts 160, 180, and 199

[Docket No. USCG-2010-0048] RIN 1625-AB46

Lifesaving Equipment: Production Testing and Harmonization With  International Standards

Correction

    In rule document 2011-25035, appearing on pages 62962-63015 in the  issue of Monday, October 11, 2011, make the following corrections:

Sec.  160.051-1  [Corrected]

0 1. On page 62975, in the second column, in Sec.  160.051-1(b), in the  fifth through seventh lines, ``[INSERT DATE 30 DAYS AFTER DATE OF  PUBLICATION OF INTERIM RULE]'' should read ``November 10, 2011''.

Sec.  160.151-1  [Corrected]

0 2. On page 62996, in the second column, in Sec.  160.151-1, in the  sixth through eighth lines, ``[INSERT DATE 30 DAYS AFTER DATE OF  PUBLICATION OF INTERIM RULE]'' should read ``November 10, 2011''.

Sec.  180.150  [Corrected]

0 3. On page 63015, in the third column, in Sec.  180.150(c)(2), in the  second through fourth lines, ``[INSERT DATE 30 DAYS AFTER DATE OF  PUBLICATION OF INTERIM RULE]'' should read ``November 10, 2011''.

Sec.  199.150  [Corrected]

0 4. On page 63015, in the third column, in Sec.  199.150(a)(2)(ii), in  the second through fourth lines, ``[INSERT DATE 30 DAYS AFTER DATE OF  PUBLICATION OF INTERIM RULE]'' should read ``November 10, 2011''.

[FR Doc. C1-2011-25035 Filed 11-9-11; 8:45 am] BILLING CODE 1505-01-D