[Federal Register Volume 87, Number 55 (Tuesday, March 22, 2022)]
[Notices]
[Pages 16183-16184]
[FR Doc No: 2022-06042]

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ENVIRONMENTAL PROTECTION AGENCY

[FRL-9678-01-R5]

Great Lakes Advisory Board Notice for Virtual Meeting

AGENCY: Environmental Protection Agency (EPA).

ACTION: Notice of Public Meeting for Great Lakes Advisory Board.

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SUMMARY: Pursuant to the Federal Advisory Committee Act (FACA), the
Environmental Protection Agency (EPA) provides notice of a public
meeting for the Great Lakes Advisory Board. Pre-registration is
required.

DATES: This virtual public meeting will be held on April 6th, 2022,
from 1:00 p.m. to 2:30 p.m. Central Daylight Time. Members of the
public seeking to view the meeting must register by 3:00 p.m. Central
Daylight Time on April 1st, 2022. Members of the public seeking to make
comments relevant to issues discussed at the virtual meeting must
register and indicate a request to make oral and/or written public
comments in advance of the meeting. For information on how to register,
please see [How do I participate in the meeting] below.

FOR FURTHER INFORMATION CONTACT: Todd Nettesheim, Acting Designated
Federal Officer (DFO), at [email protected] or<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

I. General Information

    The GLAB is chartered in accordance with the Federal Advisory
Committee Act (FACA) of 1972 (5 U.S.C., Appendix 2, as amended) and 41
CFR 102-3.50(d). The Advisory Board provides advice and recommendations
on matters related to the Great Lakes Restoration Initiative. The
Advisory Board also advises on domestic matters related to
implementation of the Great Lakes Water Quality Agreement between the
U.S. and Canada. The major objectives are to provide advice and
recommendations on: Great Lakes protection and restoration activities;
long-term goals, objectives, and priorities for Great Lakes protection
and restoration; and other issues identified

by the Great Lakes Interagency Task Force/Regional Working Group.

II. How do I participate in the remote public meeting?

A. Remote Meeting

    This meeting will be conducted as a virtual meeting on April 6th,
2022, from 1:00 p.m. to 2:30 p.m. Central Daylight Time. You must
register by 3:00 p.m. Central Daylight Time on April 1st, 2022 to
receive information on how to participate. You may also submit written
or oral comments for the committee by following the processes outlined
below.

B. Registration

    Individual registration is required for participation in this
meeting. Information on registration for this meeting can be found at
https://event.capconcorp.com/form/view.php?id=135500. When registering,
please provide your name, email, organization, city, and state. Please
also indicate whether you would like to provide oral and/or written
comments during the meeting at the time of registration.

C. Procedures for Providing Public Comments

    Oral Statements: In general, oral comments at this virtual
conference will be limited to the Public Comments portions of the
meeting agenda. Members of the public may provide oral comments limited
to up to three minutes per individual or group and may submit further
information as written comments. Persons interested in providing oral
statements should register at https://event.capconcorp.com/form/view.php?id=135500 for the meeting and indicate your interest to
provide public comments. Oral commenters will be provided an
opportunity to speak in the order in which their request was received
by the DFO and to the extent permitted by the number of comments and
the scheduled length of the meeting. Persons not able to provide oral
comments during the meeting will be given an opportunity to provide
written comments after the meeting.
    Written Statements: Persons interested in providing written
statements pertaining to this committee meeting may do so by indicating
at https://event.capconcorp.com/form/view.php?id=135500. Written
comments will be accepted before and during the public meeting for
consideration by the Great Lakes Advisory Board members.

D. Availability of Meeting Materials

    The meeting agenda and other materials for the virtual conference
will be posted on the GLAB website at www.glri.us/glab.

E. Accessibility

    Persons with disabilities who wish to request reasonable
accommodations to participate in this event may contact the Acting DFO
at [email protected] or<PHONE_NUMBER> by 3:00 p.m. Central
Daylight Time on April 1st, 2022. All final meeting materials will be
posted to the GLAB website in an accessible format following the
meeting, as well as a written summary of this meeting.

    Dated: March 16, 2022.
Debra Shore,
Regional Administrator & Great Lakes National Program Manager, U.S. EPA
Region 5.
[FR Doc. 2022-06042 Filed 3-21-22; 8:45 am]
BILLING CODE 6560-50-P


[Federal Register: December 3, 2009 (Volume 74, Number 231)]
[Rules and Regulations]
[Page 63284-63288]
[DOCID:fr03de09-3]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2009-1022; Directorate Identifier 2009-NM-163-AD;
Amendment 39-16078; AD 2008-11-02 R1]
RIN 2120-AA64

Airworthiness Directives; Lockheed Model L-1011 Series Airplanes

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

ACTION: Final rule; request for comments.

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SUMMARY: The FAA is revising an existing airworthiness directive (AD),
which applies to all Lockheed Model L-1011 series airplanes. That AD
currently requires revising the FAA-approved maintenance program by
incorporating new airworthiness limitations for fuel tank systems to
satisfy Special Federal Aviation Regulation No. 88 requirements. That
AD also requires the accomplishment of certain fuel system
modifications, the initial inspections of certain repetitive fuel
system limitations to phase in those inspections, and repair if
necessary. This AD clarifies the intended effect of the AD on spare and
on-airplane fuel tank system components. This AD results from a design
review of the fuel tank systems. We are issuing this AD to prevent the
potential for ignition sources inside fuel tanks caused by latent
failures, alterations, repairs, or maintenance actions, which, in
combination with flammable fuel vapors, could result in a fuel tank
explosion and consequent loss of the airplane.

DATES: This AD is effective December 18, 2009.
    On June 25, 2008 (73 FR 29410, May 21, 2008), the Director of the
Federal

Register approved the incorporation by reference of a certain
publication listed in the AD.
    We must receive any comments on this AD by January 19, 2010.

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 AD, contact Lockheed
Continued Airworthiness Project Office, Attention Airworthiness, 86
South Cobb Drive, Marietta, Georgia 30063-0567; telephone<PHONE_NUMBER>;
fax<PHONE_NUMBER>; e-mail<EMAIL_ADDRESS>Internet http://
www.lockheedmartin.com/ams/tools/TechPubs.html.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://
www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Office (telephone<PHONE_NUMBER>) is in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Robert A. Bosak, Aerospace Engineer,
Propulsion and Services Branch, ACE-118A, FAA, Atlanta Aircraft
Certification Office, 1701 Columbia Avenue, College Park, Georgia
30337; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    On May 8, 2008, we issued AD 2008-11-02, Amendment 39-15524 (73 FR
29410, May 21, 2008). That AD applied to all Lockheed Model L-1011
series airplanes. That AD required revising the FAA-approved
maintenance program by incorporating new airworthiness limitations for
fuel tank systems to satisfy Special Federal Aviation Regulation No. 88
requirements. That AD also required the accomplishment of certain fuel
system modifications, the initial inspections of certain repetitive
fuel system limitations to phase in those inspections, and repair if
necessary. That AD resulted from a design review of the fuel tank
systems. The actions specified in that AD are intended to prevent the
potential for ignition sources inside fuel tanks caused by latent
failures, alterations, repairs, or maintenance actions, which, in
combination with flammable fuel vapors, could result in a fuel tank
explosion and consequent loss of the airplane.
    Critical design configuration control limitations (CDCCLs) are
limitation requirements to preserve a critical ignition source
prevention feature of the fuel tank system design that is necessary to
prevent the occurrence of an unsafe condition. The purpose of a CDCCL
is to provide instruction to retain the critical ignition source
prevention feature during configuration change that may be caused by
alterations, repairs, or maintenance actions. A CDCCL is not a periodic
inspection.

Actions Since AD Was Issued

    Since we issued that AD, we have determined that it is necessary to
clarify the AD's intended effect on spare and on-airplane fuel tank
system components, regarding the use of maintenance manuals and
instructions for continued airworthiness.
    Section 91.403(c) of the Federal Aviation Regulations (14 CFR
91.403(c)) specifies the following:

    No person may operate an aircraft for which a manufacturer's
maintenance manual or instructions for continued airworthiness has
been issued that contains an airworthiness limitation section unless
the mandatory * * * procedures * * * have been complied with.

Some operators have questioned whether existing components affected by
the new CDCCLs must be reworked. We did not intend for the AD to
retroactively require rework of components that had been maintained
using acceptable methods before the effective date of the AD. Owners
and operators of the affected airplanes therefore are not required to
rework affected components identified as airworthy or installed on the
affected airplanes before the required revisions of the FAA-approved
maintenance program. But once the CDCCLs are incorporated into the FAA-
approved maintenance program, future maintenance actions on components
must be done in accordance with those CDCCLs.

FAA's Determination and Requirements of This AD

    The unsafe condition described previously is likely to exist or
develop on other airplanes of the same type design. For this reason, we
are issuing this AD to revise AD 2008-11-02. This new AD retains the
requirements of the existing AD, and adds a new note to clarify the
intended effect of the AD on spare and on-airplane fuel tank system
components.

Explanation of Additional Changes to AD

    AD 2008-11-02 allowed the use of alternative CDCCLs if they are
part of a later revision of Lockheed Service Bulletin 093-28-098,
Revision 1, dated January 22, 2008. That provision has been removed
from this AD. Allowing the use of ``a later revision'' of a specific
service document violates Office of the Federal Register regulations
for approving materials that are incorporated by reference. Affected
operators, however, may request approval to use an alternative CDCCL
that is part of a later revision of the referenced service document as
an alternative method of compliance, under the provisions of paragraph
(k) of this AD.
    We have revised paragraph (g)(2) of this AD to remove information
on certain approved methods. Instead we have added Note 3 to this AD to
specify that guidance on certain CDCCLs can be found in the documents
identified in Table 1 of this AD. We have re-identified subsequent
notes accordingly. We have approved the documents in Table 1 of this
AD. Operators may contact the Manager, Atlanta Aircraft Certification
Office, for guidance regarding the use of the documents in Table 1 of
this AD.

Explanation of Further Change to This AD

    We have revised paragraphs (g), (g)(2), (h), (h)(1), and (h)(2),
Note 4, and Tables 1 and 2 of this AD to remove the term ``the service
bulletin,'' which is defined in paragraph (f) of this AD. We have
provided the full service bulletin citation throughout this AD to avoid
any confusion about which specific service bulletin is being
referenced. However, we have not removed the ``Service Bulletin
Reference'' paragraph from this AD. Because this AD revises AD 2008-11-
02, we cannot change paragraph references, which would adversely affect
compliance. Therefore, we have determined that leaving paragraph (f) of
this AD unchanged is a less burdensome

approach for operators, while still adhering to standard drafting
guidance.

Costs of Compliance

    This revision imposes no additional economic burden. The current
costs for this AD are repeated for the convenience of affected
operators, as follows:
    There are about 108 airplanes of the affected design in the
worldwide fleet. The following table provides the estimated costs, at
an average labor rate of $80 per work hour, for U.S. operators to
comply with this AD.

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Number of U.S.-
             Action                 Work hours         Parts         Cost per       registered      Fleet cost
                                                                     airplane        airplanes
----------------------------------------------------------------------------------------------------------------
Maintenance program revision to                4            None            $320              63         $20,160
 incorporate FSLs and CDCCLs....
Removal of auxiliary fuel tank                40            None           3,200               8          25,600
 No. 4, if applicable...........
Modification and inspection of                19            $974           2,494              63         157,122
 the wiring harnesses of the
 fuel level control switch......
Inspection of the airplane fuel              370          18,491          48,091              63       3,029,733
 tanks, vent boxes, and bonding
 jumpers, and the addition of
 bonding jumpers to the fuel/
 vent tube fittings.............
Identification and inspection of               4             336             656              63          41,328
 the FQIS wiring harnesses......
----------------------------------------------------------------------------------------------------------------

FAA's Justification and Determination of the Effective Date

    This revision merely clarifies the intended effect on spare and on-
airplane fuel tank system components, and makes no substantive change
to the AD's requirements. For this reason, it is found that notice and
opportunity for prior public comment for this action are unnecessary,
and good cause exists for making this amendment effective in less than
30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments before it becomes effective. However, we invite
you to send any written data, views, or arguments about this AD. Send
your comments to an address listed under the ADDRESSES section. Include
``Docket No. FAA-2009-1022; Directorate Identifier 2009-NM-163-AD'' at
the beginning of your comments. We specifically invite comments on the
overall regulatory, economic, environmental, and energy aspects of this
AD. We will consider all comments received by the closing date and may
amend this AD because of 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 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 have determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the national government and the States, or on the distribution of power
and responsibilities among the various levels of government.
    For the reasons discussed above, I certify that the 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); and
    3. 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.
    We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket. See the ADDRESSES
section for a location to examine the regulatory evaluation.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends part 39 of the Federal Aviation Regulations (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 removing Amendment 39-15524 (73 FR
29410, May 21, 2008) and adding the following new AD:

2008-11-02 R1 Lockheed: Amendment 39-16078. Docket No. FAA-2009-
1022; Directorate Identifier 2009-NM-163-AD.

Effective Date

    (a) This airworthiness directive (AD) is effective December 18,
2009.

Affected ADs

    (b) This AD revises AD 2008-11-02, Amendment 39-15524.

Applicability

    (c) This AD applies to all Lockheed Model L-1011 series
airplanes, certificated in any category.

    Note 1:  This AD requires revisions to certain operator
maintenance documents to include new inspections. Compliance with
these inspections is required by 14 CFR 91.403(c). For airplanes
that have been

previously modified, altered, or repaired in the areas addressed by
these inspections, the operator may not be able to accomplish the
inspections described in the revisions. In this situation, to comply
with 14 CFR 91.403(c), the operator must request approval for an
alternative method of compliance (AMOC) in accordance with paragraph
(k) of this AD. The request should include a description of changes
to the required inspections that will ensure the continued
operational safety of the airplane.

Unsafe Condition

    (d) This AD results from a design review of the fuel tank
systems. We are issuing this AD to prevent the potential for
ignition sources inside fuel tanks caused by latent failures,
alterations, repairs, or maintenance actions, which, in combination
with flammable fuel vapors, could result in a fuel tank explosion
and consequent loss of the airplane.

Compliance

    (e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.

Restatement of Requirements of AD 2008-11-02 With Changes to Compliance
Method

Service Bulletin Reference

    (f) The term ``service bulletin,'' as used in this AD, means the
Accomplishment Instructions of Lockheed Service Bulletin 093-28-098,
Revision 1, dated January 22, 2008.

Maintenance Program Revision

    (g) Before December 16, 2008, revise the FAA-approved
maintenance program to incorporate the fuel system limitations
(FSLs) specified in paragraphs 2.B.(1)(b), 2.B.(1)(e), 2.B.(1)(f),
and 2.B.(1)(g) of Lockheed Service Bulletin 093-28-098, Revision 1,
dated January 22, 2008, and the critical design configuration
control limitations (CDCCLs) specified in paragraph 2.C. of Lockheed
Service Bulletin 093-28-098, Revision 1, dated January 22, 2008;
except as provided by paragraphs (g)(1), (g)(2), and (h) of this AD.
    (1) Where the FSLs specify to inspect, this AD would require
doing a general visual inspection.

    Note 2:  For the purposes of this AD, a general visual
inspection is: ``A visual examination of an interior or exterior
area, installation, or assembly to detect obvious damage, failure,
or irregularity. This level of inspection is made from within
touching distance unless otherwise specified. A mirror may be
necessary to ensure visual access to all surfaces in the inspection
area. This level of inspection is made under normally available
lighting conditions such as daylight, hangar lighting, flashlight,
or droplight and may require removal or opening of access panels or
doors. Stands, ladders, or platforms may be required to gain
proximity to the area being checked.''

    (2) For the CDCCLs specified in paragraphs 2.C.(2)(c),
2.C.(2)(d), and 2.C.(15)(a) of Lockheed Service Bulletin 093-28-098,
Revision 1, dated January 22, 2008, do the applicable actions using
a method approved in accordance with a method approved by the
Manager, Atlanta Aircraft Certification Office, FAA.

    Note 3:  Guidance on certain CDCCLs can be found in the
documents identified in Table 1 of this AD.

              Table 1--Approved Methods for Certain CDCCLs
------------------------------------------------------------------------
 For the CDCCL identified in
  Lockheed Service Bulletin
   093-28-098, Revision 1,       Guidance can be            For--
 dated January 22, 2008, in        found in--
         paragraph--
------------------------------------------------------------------------
2.C.(2)(c)..................  Hamilton Sundstrand   Overhauling and
                               Overhaul Manual 28-   repairing the
                               24-03, Revision 14,   electrically
                               dated May 15, 2000.   operated fuel boost
                                                     pumps.
2.C.(2)(d)..................  Lockheed L-1011       Keeping the
                               Service Information   electrical conduit
                               Letter 28-12, dated   for the
                               March 17, 1998.       electrically
                                                     operated fuel boost
                                                     pumps open and
                                                     unplugged at the
                                                     wing rear spar.
2.C.(15)(a).................  Lockheed Drawing      Installing the fuel
                               1527514, Revision     tank valves,
                               D, dated September    auxiliary power
                               26, 1981.             unit pump, sight
                                                     gauges, fuel
                                                     quantity indicating
                                                     system tank units,
                                                     over[dash]wing
                                                     filler cap adapter
                                                     ring, boost pump
                                                     mounting plate, and
                                                     access doors for
                                                     the boost pump,
                                                     vent box, vent
                                                     valve, and fuel
                                                     level control
                                                     switch.
------------------------------------------------------------------------

Initial Accomplishment of FSLs and Repair if Necessary

    (h) At the applicable compliance time specified in paragraph
(h)(1) or (h)(2) of this AD, do the applicable FSLs specified in
paragraphs 2.B.(1)(b), 2.B.(1)(e), 2.B.(1)(f), and 2.B.(1)(g) of
Lockheed Service Bulletin 093-28-098, Revision 1, dated January 22,
2008, and repair any discrepancy, in accordance with Lockheed
Service Bulletin 093-28-098, Revision 1, dated January 22, 2008. Any
repair must be done before further flight.
    (1) For the FSL identified in paragraph 2.B.(1)(b) of Lockheed
Service Bulletin 093-28-098, Revision 1, dated January 22, 2008, do
the FSL before December 16, 2008.
    (2) For the FSLs identified in paragraphs 2.B.(1)(e),
2.B.(1)(f), and 2.B.(1)(g) of Lockheed Service Bulletin 093-28-098,
Revision 1, dated January 22, 2008, do the applicable FSLs within 60
months after June 25, 2008 (the effective date AD 2008-11-02).

    Note 4:  Lockheed Service Bulletin 093-28-098, Revision 1, dated
January 22, 2008, refers to the service information listed in Table
2 of this AD as additional sources of guidance for doing the FSLs
and repair.

        Table 2--Additional Sources of Guidance for Certain FSLs
------------------------------------------------------------------------
    The FSL identified in
  Lockheed Service Bulletin
   093-28-098, Revision 1,     Refers to Lockheed           For--
 dated January 22, 2008, in    Service Bulletin--
         paragraph--
------------------------------------------------------------------------
2.B.(1)(b)..................  093-28-089, Revision  Removing auxiliary
                               3, dated October 4,   fuel tank No. 4, if
                               2006.                 applicable.

2.B.(1)(e)..................  093-28-095, dated     Inspecting the
                               September 13, 2006.   airplane fuel tanks
                                                     and vent boxes for
                                                     cleanliness and
                                                     evidence of
                                                     deteriorated or
                                                     damaged fuel/vent
                                                     tubes and
                                                     components;
                                                     inspecting bonding
                                                     jumpers for proper
                                                     installation,
                                                     corrosion, frayed
                                                     or broken strands,
                                                     and the condition
                                                     of the
                                                     environmental
                                                     sealing or bonding
                                                     clamps and
                                                     hardware;
                                                     correcting any
                                                     discrepant
                                                     conditions; adding
                                                     bonding jumpers to
                                                     the fuel/vent tube
                                                     fittings; and
                                                     inspecting the
                                                     bonding jumpers on
                                                     the fuel/vent tube
                                                     fittings.
2.B.(1)(f)..................  093-28-096, Revision  Inspecting the
                               2, dated June 23,     wiring harnesses of
                               2006.                 the No. 1 and No. 3
                                                     engine tank valves
                                                     for evidence of
                                                     damage and fuel
                                                     contamination;
                                                     replacing any
                                                     damaged wire with
                                                     new wire; and
                                                     repairing or
                                                     replacing any
                                                     contaminated wires
                                                     as applicable.
2.B.(1)(g)..................  093-28-097, dated     Identifying the
                               August 3, 2006.       wiring harnesses
                                                     for the fuel
                                                     quantity indicator
                                                     system (FQIS);
                                                     inspecting the FQIS
                                                     wiring harnesses
                                                     for any visible
                                                     damage, wear,
                                                     chafing, or
                                                     indications of
                                                     electrical arcing;
                                                     and replacing or
                                                     repairing any
                                                     damaged wires as
                                                     applicable.
------------------------------------------------------------------------

No Reporting Requirement

    (i) Although Lockheed Service Bulletin 093-28-095, dated
September 13, 2006; Lockheed Service Bulletin 093-28-096, Revision
2, dated June 23, 2006; and Lockheed Service Bulletin 093-28-097,
dated August 3, 2006; specify to notify Lockheed of any
discrepancies found during inspection or any evidence of damage or
wire replacement, this AD does not require that action.

No Alternative Inspections, Inspection Intervals, or CDCCLs

    (j) After accomplishing the actions specified in paragraphs (g)
and (h) of this AD, no alternative inspections, inspection
intervals, or CDCCLs may be used unless the inspections, intervals,
or CDCCLs are approved as an AMOC in accordance with the procedures
specified in paragraph (k) of this AD.

New Information

Explanation of CDCCL Requirements

    Note 5: Notwithstanding any other maintenance or operational
requirements, components that have been identified as airworthy or
installed on the affected airplanes before the revision of the FAA-
approved maintenance program, as required by paragraph (g) of this
AD, do not need to be reworked in accordance with the CDCCLs.
However, once the FAA-approved maintenance program has been revised,
future maintenance actions on these components must be done in
accordance with the CDCCLs.

Alternative Methods of Compliance (AMOCs)

    (k)(1) The Manager, Atlanta Aircraft Certification 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:
Robert Bosak, Aerospace Engineer, Propulsion Branch, ACE-118A, FAA,
Atlanta Aircraft Certification Office, 1701 Columbia Avenue, College
Park, GA 30337; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.
    (2) To request a different method of compliance or a different
compliance time for this AD, follow the procedures in 14 CFR 39.19.
Before using any approved AMOC on any airplane to which the AMOC
applies, notify your principal maintenance inspector (PMI) or
principal avionics inspector (PAI), as appropriate, or lacking a
principal inspector, your local Flight Standards District Office.
The AMOC approval letter must specifically reference this AD.

Material Incorporated by Reference

    (l) You must use Lockheed Service Bulletin 093-28-098, Revision
1, dated January 22, 2008, to do the actions required by this AD,
unless the AD specifies otherwise.
    (1) The Director of the Federal Register previously approved the
incorporation by reference of this service information on June 25,
2008 (73 FR 29410 May 21, 2008).
    (2) For service information identified in this AD, contact
Lockheed Continued Airworthiness Project Office, Attention
Airworthiness, 86 South Cobb Drive, Marietta, Georgia 30063-0567;
telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>; e-mail
<EMAIL_ADDRESS>Internet http://www.lockheedmartin.com/ams/
tools/TechPubs.html.
    (3) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the availability of this material at
the FAA, call<PHONE_NUMBER> or<PHONE_NUMBER>.
    (4) You may also review copies of the 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/code_of_federal_regulations/
ibr_locations.html.

    Issued in Renton, Washington, on October 26, 2009.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E9-28301 Filed 12-2-09; 8:45 am]

BILLING CODE 4910-13-P


[Federal Register Volume 79, Number 96 (Monday, May 19, 2014)]
[Notices]
[Page 28710]
[FR Doc No: 2014-11467]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. ER14-1934-000]

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

    This is a supplemental notice in the above-referenced proceeding of
Rising Tree 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 June 2, 2014.
    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
5 copies of the intervention or protest to the Federal Energy
Regulatory Commission, 888 First Street 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 email notification
when a document is added to a subscribed docket(s). For assistance with
any FERC Online service, please email<EMAIL_ADDRESS>or
call<PHONE_NUMBER> (toll free). For TTY, call<PHONE_NUMBER>.

    Dated: May 12, 2014.
Kimberly D. Bose,
Secretary.
[FR Doc. 2014-11467 Filed 5-16-14; 8:45 am]
BILLING CODE 6717-01-P