[Federal Register Volume 83, Number 128 (Tuesday, July 3, 2018)]
[Rules and Regulations]
[Pages 31045-31046]
[FR Doc No: 2018-14274]

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DEPARTMENT OF LABOR

Occupational Safety and Health Administration

29 CFR Part 1910

[Docket No. OSHA-2018-0003]
RIN 1218-AB76

Revising the Beryllium Standard for General Industry

AGENCY: Occupational Safety and Health Administration (OSHA), Labor.

ACTION: Final rule; confirmation of effective date.

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SUMMARY: OSHA is confirming the effective date of its direct final rule
(DFR) adopting a number of clarifying amendments to the beryllium
standard for general industry to address the application of the
standard to materials containing trace amounts of beryllium. In the May
7, 2018, DFR, OSHA stated that the DFR would become effective on July
6, 2018, unless one or more significant adverse comments were submitted
by June 6, 2018. OSHA did not receive significant adverse comments on
the DFR, so by this document the agency is confirming that the DFR will
become effective on July 6, 2018.

DATES: The DFR published on May 7, 2018 (83 FR 19936), becomes
effective on July 6, 2018. For purposes of judicial review, OSHA
considers the date of publication of this document as the date of
promulgation of the DFR.

ADDRESSES: For purposes of 28 U.S.C. 2112(a), OSHA designates the
Associate Solicitor of Labor for Occupational Safety and Health as the
recipient of petitions for review of the direct final rule. Contact the
Associate Solicitor at the Office of the Solicitor, Room S-4004, U.S.
Department of Labor, 200 Constitution Avenue NW, Washington, DC 20210;
telephone:<PHONE_NUMBER>.

FOR FURTHER INFORMATION CONTACT:
    Press inquiries: Mr. Frank Meilinger, OSHA Office of
Communications, Room N-3647, U.S. Department of Labor, 200 Constitution
Avenue NW, Washington, DC 20210; telephone:<PHONE_NUMBER>; email:
[email protected].
    General information and technical inquiries: Mr. William Perry or
Ms. Maureen Ruskin, Directorate of Standards and Guidance, Room N-3718,
OSHA, U.S. Department of Labor, 200 Constitution Avenue NW, Washington,
DC 20210; telephone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>.
    Copies of this Federal Register document and news releases:
Electronic copies of these documents are available

at OSHA's web page at http://www.osha.gov.

SUPPLEMENTARY INFORMATION:

I. Confirmation of Effective Date

    On May 7, 2018, OSHA published a DFR in the Federal Register (83 FR
19936) amending the text of the beryllium standard for general industry
to clarify OSHA's intent with respect to certain terms in the standard,
including the definition of Beryllium Work Area (BWA), the definition
of emergency, and the meaning of the terms dermal contact and beryllium
contamination. It also clarifies OSHA's intent with respect to
provisions for disposal and recycling and with respect to provisions
that the agency intends to apply only where skin can be exposed to
materials containing at least 0.1% beryllium by weight. Interested
parties had until June 6, 2018, to submit comments on the DFR.
    The agency stated that it would publish another document confirming
the effective date of the DFR if it received no significant adverse
comments. OSHA received seven comments in the record from Materion
Brush, Inc., Mead Metals Inc., National Association of Manufacturers,
Airborn, Inc., Edison Electric Institute, and two private citizens
(Document IDs OSHA-2018-0003-0004 thru OSHA-2018-0003-0010). The seven
submissions contained comments that were either supportive of the DFR
or were considered not to be significant adverse comments. (Document
IDs OSHA-2018-0003-0004 thru OSHA-2018-0003-0010). Three of these
submissions also contained comments that were outside the scope of the
DFR and OSHA is not considering the portions of those submissions that
are outside the scope (OSHA-2018-0003-0004 thru OSHA-2018-0003-0006).
    OSHA has determined this DFR will maintain safety and health
protections for workers while reducing employers' compliance burdens.
As the agency did not receive any significant adverse comments, OSHA is
hereby confirming that the DFR published on May 7, 2018, will become
effective on July 6, 2018.

II. OMB Review Under the Paperwork Reduction Act of 1995

    This action does not add or change any information collection
requirements subject to OMB approval under the Paperwork Reduction Act
of 1995 (PRA), 44 U.S.C. 3501 et seq., and its implementing regulations
at 5 CFR part 1320. The PRA defines a collection of information as the
obtaining, causing to be obtained, soliciting, or requiring the
disclosure to third parties or the public of facts or opinions by or
for an agency regardless of form or format. See 44 U.S.C. 3502(3)(A).
While not affected by this rulemaking, the Department has cleared
information collections related to occupational exposure to beryllium
standards--general industry, 29 CFR 1910.1024; construction, 29 CFR
1926.1124; and shipyards, 29 CFR 1915.1024--under control number 1218-
0267. The existing approved information collections are unchanged by
this rulemaking.
    In the DFR published on May 7, 2018, OSHA provided 30 days for the
public to comment on whether approved information collections would be
affected by this rulemaking. The agency did not receive any comments on
paperwork in response to that notice.

List of Subjects in 29 CFR Part 1910

    Beryllium, General industry, Health, Occupational safety and
health.

Authority and Signature

    Loren Sweatt, Deputy Assistant Secretary of Labor for Occupational
Safety and Health, directed the preparation of this direct final rule.
The agency is issuing this rule under Sections 4, 6, and 8 of the
Occupational Safety and Health Act of 1970 (29 U.S.C. 653, 655, 657),
Secretary of Labor's Order 5-2007 (72 FR 31159), and 29 CFR part 1911.

    Signed at Washington, DC, on June 27, 2018.
Loren Sweatt,
Deputy Assistant Secretary of Labor for Occupational Safety and Health.
[FR Doc. 2018-14274 Filed 7-2-18; 8:45 am]
BILLING CODE 4510-26-P


[Federal Register: June 25, 2009 (Volume 74, Number 121)]
[Notices]
[Page 30289]
[DOCID:fr25jn09-37]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. CP09-427-000]

Columbia Gas Transmission, LLC; Notice of Request Under Blanket
Authorization

June 18, 2009.
    Take notice that on June 4, 2009, Columbia Gas Transmission, LLC
(Columbia), 5151 San Felipe, Suite 2500, Houston, Texas 77056, filed a
prior notice request pursuant to sections 157.205, 157.208, and 157.216
of the Commission's regulations under the Natural Gas Act (NGA) and
Columbia's blanket certificate issued in Docket No. CP83-76-000, for
NGA certification to construct, uprate, replace, relocate, and abandon
certain natural gas facilities, all as more fully set forth in the
application, which is on file with the Commission and open to public
inspection. The filing may also be viewed on the Web at http://
www.ferc.gov using the ``eLibrary'' link. Enter the docket number
excluding the last three digits in the docket number field to access
the document. For assistance, contact FERC at
<EMAIL_ADDRESS>or call toll-free,<PHONE_NUMBER> or TTY,
(202) 502-8659.
    Columbia states that Range Resources Appalachia LLC (Range
Resources) has requested Columbia to transport 150,000 dekatherms per
day (Dth/d) of natural gas from Range Resources' production fields in
the Marcellus Shale in southwestern Pennsylvania to Leach, Kentucky.
Columbia asserts that, as a result of that request and to meet the
market demands in the Marcellus Shale region, it has determined that it
will need to make certain modifications to its pipeline system in
Washington and Greene Counties, Pennsylvania. Columbia states that it
will: (i) Isolate a portion of its transmission Line 1570 from Sharp
Farm MS to Waynesburg Compressor Station; (ii) provide alternate
sources of supply to continue service to the markets currently being
served from Line 1570; and (iii) make minor modifications to other
Columbia facilities in order to accommodate those alternate sources of
supply.
    More specifically, Columbia seeks approval to: (i) Increase the
maximum allowable operating pressure (MAOP) on approximately 1.3 miles
of 4-inch pipeline on Line 10331 from 206 pounds per square inch gauge
(psig) to 330 psig; (ii) increase the MAOP on approximately 13.4 miles
of 10-inch pipeline on Line 40 from 150 psig to 330 psig; (iii)
increase the MAOP on approximately 0.82 miles of 8-inch pipeline of
Line 708 from 280 psig to 330 psig; (iv) replace approximately 0.4
miles of 4-inch pipeline and appurtenances with a like amount of 10-
inch pipeline and appurtenances on Line 36; (v) replace approximately
2.8 miles of 3-inch pipeline and appurtenances with a like amount of
10-inch pipeline and appurtenances on Line 628; (vi) replace
approximately 0.07 miles of 10-inch pipeline and appurtenances with a
like amount of 10-inch pipeline and appurtenances on Line 40; (vii)
construct approximately 1.8 miles of 12-inch pipeline and appurtenances
to extend Line 7215; (viii) construct approximately 1.14 miles of 6-
inch pipeline and appurtenances on Line 10366; (ix) abandon the
pipeline segments being replaced; and (x) abandon 23 mainline taps.
Columbia estimates the cost associated with the construction of the
subject facilities as approximately $16,500,000.
    Any questions regarding the application should be directed to
Frederic J. George, Senior Counsel, Columbia Gas Transmission, LLC, PO
Box 1273, Charleston, West Virginia 22030-0146, at<PHONE_NUMBER>.
    Any person may, within 60 days after the issuance of the instant
notice by the Commission, file pursuant to Rule 214 of the Commission's
Procedural Rules (18 CFR 385.214) a motion to intervene or notice of
intervention. Any person filing to intervene or the Commission's staff
may, pursuant to Sec.  157.205 of the Commission's regulations under
the NGA (18 CFR 157.205), file a protest to the request. If no protest
is filed within the time allowed therefore, the proposed activity shall
be deemed to be authorized effective the day after the time allowed for
protest. If a protest is filed and not withdrawn within 30 days after
the time allowed for filing a protest, the instant request shall be
treated as an application for authorization pursuant to section 7 of
the NGA.
    The Commission strongly encourages electronic filings of comments,
protests, and interventions via the Internet in lieu of paper. See 18
CFR 385.2001(a)(1)(iii) and the instructions on the Commission's Web
site (http://www.ferc.gov) under the ``e-Filing'' link.

Kimberly D. Bose,
Secretary.
[FR Doc. E9-14937 Filed 6-24-09; 8:45 am]

BILLING CODE 6717-01-P


[Federal Register: September 21, 2007 (Volume 72, Number 183)]
[Rules and Regulations]
[Page 53939-53942]
[DOCID:fr21se07-13]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-29263; Directorate Identifier 2007-NM-198-AD;
Amendment 39-15210; AD 2007-19-19]
RIN 2120-AA64

Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-
100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP
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 superseding an existing airworthiness directive
(AD) that applies to certain Boeing Model 747 series airplanes. The
existing AD currently requires repetitive inspections and torque checks
of the hanger fittings and strut forward bulkhead of the forward engine
mount and adjacent support structure, and corrective actions if
necessary. The existing AD also currently requires a terminating action
for the repetitive inspections and checks. This new AD requires, among
other actions, new repetitive inspections in the existing area and new
areas. This new AD also provides for an optional inspection and no
longer allows the existing fastener replacement to terminate repetitive
inspections. This AD results from new reports of under-torqued or loose
fasteners, a cracked bulkhead chord, and a fractured back-up angle
after operators accomplished the terminating action required by the
existing AD. We are issuing this AD to detect and correct loose
fasteners and/or damaged or cracked hanger fittings, back-up angles,
and bulkhead of the forward engine mount, which could lead to failure
of the hanger fitting and bulkhead and consequent separation of the
engine from the airplane.

DATES: This AD becomes effective October 9, 2007.
    The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of October 9,
2007.
    On December 6, 2000 (65 FR 69862, November 21, 2000), the Director
of the Federal Register approved the incorporation by reference of
Boeing Alert Service Bulletin 747-54A2203, dated August 31, 2000.
    We must receive any comments on this AD by November 20, 2007.

ADDRESSES: Use one of the following addresses to submit comments on
this AD.
     DOT Docket Web site: Go to http://dms.dot.gov and follow

the instructions for sending your comments electronically.
     Government-wide rulemaking Web site: Go to http://www.regulations.gov
 and follow the instructions for sending your

comments electronically.
     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.
     Fax:<PHONE_NUMBER>.
     Hand Delivery: Room W12-140 on the ground floor of the
West Building, 1200 New Jersey Avenue, SE., Washington, DC, between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle,
Washington 98124-2207, for service information identified in this AD.

FOR FURTHER INFORMATION CONTACT: Tamara Anderson, Aerospace Engineer,
Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
917-6421; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    On July 13, 2001, we issued AD 2001-15-02, amendment 39-12336 (66
FR 37884, July 20, 2001). That AD applies to certain Boeing Model 747
series airplanes. That AD requires repetitive inspections and torque
checks of the hanger fittings and strut forward bulkhead of the forward
engine mount and adjacent support structure, and corrective actions if
necessary. That AD also requires a terminating action for the
repetitive inspections and checks. That AD resulted from reports
indicating the detection of loose fasteners of the hanger fittings and
strut forward bulkhead of the forward engine mount. The actions
specified in that AD are intended to prevent loose fasteners and
associated damage to the hanger fittings

and bulkhead of the forward engine mount, which could result in
separation of the engine from the airplane.

Actions Since AD Was Issued

    Since we issued that AD, we have received new reports of under-
torqued or loose fasteners after operators accomplished the terminating
action required by AD 2001-15-02 (i.e., Part 6 specified in Boeing
Alert Service Bulletin 747-54A2203, dated August 31, 2000). In
addition, we have received a report of a crack approximately 1.5-inch
in length in the bulkhead chord adjacent to an upper fastener on a
number 2 strut with approximately 20,050 total flight cycles and
110,000 total flight hours. Further investigation revealed that the
back-up angle inside the strut adjacent to the crack had fractured at
its bend radius. The fracture initiated as a result of fatigue at
multiple locations on the inner diameter of the bend radius. The cause
of the loose fasteners of the hanger fittings of the bulkhead of the
forward engine mount is their location in an area of high vibration and
the design of the bulkhead. Loose fasteners and/or damaged or cracked
hanger fittings, back-up angles, and bulkhead of the forward engine
mount, if not corrected, could lead to failure of the hanger fitting
and bulkhead and consequent separation of the engine from the airplane.

Relevant Service Information

    We have reviewed Boeing Alert Service Bulletin 747-54A2203,
Revision 1, dated August 9, 2007. The service information describes the
following new procedures:
     Repetitive detailed inspections of the torque stripes and
bulkhead of the forward engine mount and the adjacent support structure
on the inboard and outboard struts and repetitive torque inspections
(checks) of the bulkhead for cracks and/or fretting damage of the
hanger fittings and bulkhead and for loose or under-torqued fasteners,
as applicable; and applicable related investigative and corrective
actions (i.e., Part 2 of the Accomplishment Instructions).
     Repetitive high frequency eddy current (HFEC), detailed,
or fluorescent penetrant inspections of the bulkhead of the forward
engine mount on the inboard and outboard struts for cracks of the
bulkhead chords, evidence of a fractured internal angle, or cracks/
fracture of the internal angles; as applicable (i.e., Part 8 of the
Accomplishment Instructions); and detailed and HFEC inspections to
detect cracks or fracture of the internal angle and stiffener (i.e.,
Part 7 of the Accomplishment Instructions), and applicable related
investigative and corrective actions.
    The related investigative actions involve doing applicable
inspections described previously. The corrective actions include
applying optional torque stripes; reworking, repairing, and/or
replacing any discrepant part with a new part; replacing all fasteners
with new fasteners; and contacting Boeing for certain conditions; as
applicable.
    For the inspections specified in Parts 2 and 8 of the
Accomplishment Instructions, the service information specifies an
initial compliance time of 90 days and repeat intervals of 6 and 18
months, depending on the inspection type. For the inspections specified
in Part 7 of the Accomplishment Instructions, the service information
specifies an initial compliance time of 18 months and repeat intervals
of 36 months. The service bulletin specifies a compliance time of
before further flight or 18 months for doing the related investigative
and corrective actions, as applicable.

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 supersede AD 2001-15-02. This new AD retains the
required fastener replacement, except that action no longer terminates
any repetitive inspections and torque inspections (checks). This AD
also requires accomplishing the actions specified in Parts 2 and 8 of
the Accomplishment Instructions of the service information described
previously, except as discussed under ``Differences Between the AD and
Service Information.'' This AD also provides, as an option, the
inspections specified in Part 7 of the Accomplishment Instructions of
the service information described previously.

Interim Action

    This is considered to be interim action. We are currently
considering requiring the inspections and applicable related
investigative and corrective actions specified in Part 7 of the
Accomplishment Instructions of Boeing Alert Service Bulletin 747-
54A2203, Revision 1. However, the planned compliance time for the
inspections is sufficiently long so that notice and opportunity for
prior public comment will be practicable.

Differences Between the AD and Service Information

    The service information specifies to contact the manufacturer for
instructions on how to repair certain conditions, but this AD requires
repairing those conditions in one of the following ways:
     Using a method that we approve; or
     Using data that meet the certification basis of the
airplane, and that have been approved by an Authorized Representative
for the Boeing Commercial Airplanes Delegation Option Authorization
Organization whom we have authorized to make those findings.

Change to Existing AD

    This AD will retain certain requirements of AD 2001-15-02. Since AD
2001-15-02 was issued, we have revised the AD format and rearranged
certain paragraphs. As a result, we reidentified paragraph (c) of AD
2001-15-02 as paragraph (f) in this AD.
    Boeing Commercial Airplanes has received a Delegation Option
Authorization (DOA). We have revised paragraph (f) of this AD to
delegate the authority to approve an alternative method of compliance
for any repair required by this AD to an Authorized Representative for
the Boeing Commercial Airplanes DOA rather than a Designated
Engineering Representative (DER).

FAA's Determination of the Effective Date

    An unsafe condition exists that requires the immediate adoption of
this AD; therefore, providing notice and opportunity for public comment
before the AD is issued is impracticable, and good cause exists to make
this AD effective in less than 30 days.

Comments Invited

    This AD is a final rule that involves requirements that affect
flight safety and was not preceded by notice and an opportunity for
public comment; however, we invite you to submit any relevant written
data, views, or arguments regarding this AD. Send your comments to an
address listed in the ADDRESSES section. Include ``Docket No. FAA-2007-
29263; Directorate Identifier 2007-NM-198-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of the AD that might
suggest a need to modify it.
    We will post all comments we receive, without change, to http://dms.dot.gov
, including any personal information you provide. We will

also

post a report summarizing each substantive verbal contact with FAA
personnel concerning this AD. Using the search function of that web
site, anyone can find and read the comments in any of our dockets,
including the name of the individual who sent the comment (or signed
the comment on behalf of an association, business, labor union, etc.).
You may review the DOT's complete Privacy Act Statement in the Federal
Register published on April 11, 2000 (65 FR 19477-78), or you may visit
http://dms.dot.gov.

Examining the Docket

    You may examine the AD docket on the Internet at http://dms.dot.gov
, or in person at the Docket Operations office between 9

a.m. and 5 p.m., Monday through Friday, except Federal holidays. The
Docket Operations office (telephone<PHONE_NUMBER>) is located on the
ground level of the West Building at the DOT street address stated in
the ADDRESSES section. Comments will be available in the AD docket
shortly after the Docket Management System receives them.

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 Federal Aviation Administration (FAA) amends Sec.  39.13 by
removing amendment 39-12336 (66 FR 37884, July 20, 2001) and adding the
following new airworthiness directive (AD):

2007-19-19 Boeing: Docket No. FAA-2007-29263; Directorate Identifier
2007-NM-198-AD; Amendment 39-15210.

Effective Date

    (a) This AD becomes effective October 9, 2007.

Affected ADs

    (b) This AD supersedes AD 2001-15-02.

Applicability

    (c) This AD applies to Boeing Model 747-100, 747-100B, 747-100B
SUD, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP series
airplanes, certificated in any category; as identified in Boeing
Alert Service Bulletin 747-54A2203, Revision 1, dated August 9,
2007.

Unsafe Condition

    (d) This AD results from new reports of under-torqued or loose
fasteners, a cracked bulkhead chord, and a fractured back-up angle
after operators accomplished the terminating action required by the
existing AD. We are issuing this AD to detect and correct loose
fasteners and/or damaged or cracked hanger fittings, back-up angles,
and bulkhead of the forward engine mount, which could lead to
failure of the hanger fitting and bulkhead and consequent separation
of the engine from 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.

Certain Requirement of AD 2001-15-02

    (f) Within 60 months after August 24, 2001 (the effective date
of AD 2001-15-02): Accomplish all actions specified in Part 6 of the
Accomplishment Instructions of Boeing Alert Service Bulletin 747-
54A2203, dated August 31, 2000. Where the alert service bulletin
specifies that the manufacturer may be contacted for disposition of
certain corrective actions (rework or replacement of fittings), this
AD requires such rework and/or replacement to be done in accordance
with a method approved by the Manager, Seattle Aircraft
Certification Office (ACO); or in accordance with data meeting the
type certification basis of the airplane approved by a Boeing
Company Designated Engineering Representative (DER) who has been
authorized by the Manager, Seattle ACO, to make such findings. For a
repair method to be approved by the Manager, Seattle ACO, as
required by this paragraph, the Manager's approval letter must
specifically reference this AD. As of the effective date of this AD,
the rework and/or replacement must be done using a method approved
in accordance with the procedures specified in paragraph (k) of this
AD.

    Note 1: Installation of two BACW10BP*APU washers on Group A
fasteners accomplished during modification in accordance with Boeing
Service Bulletin 747-54A2159, dated November 3, 1994, Revision 1,
dated June 1, 1995, or Revision 2, dated March 14, 1996; and pin or
bolt protrusion as specified in the 747 Structural Repair Manual,
Chapter 51-30-02 (both referenced in Boeing Alert Service Bulletin
747-54A2203, dated August 31, 2000); is considered acceptable for
compliance with the action required by paragraph (f) of this AD.

New Actions Required by This AD

Inspections and Related Investigative and Corrective Actions

    (g) Except as provided by paragraphs (i) and (j) of this AD: At
the applicable compliance times and repeat intervals listed in
Tables 1 and 2 of paragraph 1.E., ``Compliance,'' of Boeing Alert
Service Bulletin 747-54A2203, Revision 1, dated August 9, 2007, do
the inspections and applicable related investigative and corrective
actions by accomplishing all the actions specified in Parts 2 and 8
of the Accomplishment Instructions of the service bulletin.

Optional Initial and Repetitive Inspections and Related Investigative
and Corrective Actions

    (h) Do the initial and repetitive inspections and related
investigative and corrective actions by accomplishing all the
actions specified in Part 7 of the Accomplishment Instructions of
Boeing Alert Service Bulletin 747-54A2203, Revision 1, dated August
9, 2007, except as provided by paragraph (j) of this AD.

Exceptions to Service Bulletin

    (i) Where Boeing Alert Service Bulletin 747-54A2203, Revision 1,
dated August 9, 2007, specifies a compliance time after the date of
the service bulletin, this AD requires compliance within the
specified compliance time after the effective date of this AD.
    (j) Where Boeing Alert Service Bulletin 747-54A2203, Revision 1,
dated August 9, 2007, specifies to contact Boeing for appropriate
action, this AD requires, before further flight, repair of the
discrepancy or replacement of the discrepant part using a method
approved in accordance with the procedures specified in paragraph
(k) of this AD.

Alternative Methods of Compliance (AMOCs)

    (k)(1) The Manager, Seattle Aircraft Certification Office (ACO),
FAA, has the authority to approve AMOCs for this AD, if requested in
accordance with the procedures found in 14 CFR 39.19.
    (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 appropriate principal inspector (PI) in the FAA
Flight Standards District Office (FSDO), or lacking a PI, your local
FSDO.
    (3) An AMOC that provides an acceptable level of safety may be
used for any repair required by this AD, if it is approved by an
Authorized Representative for the Boeing Commercial Airplanes
Delegation Option Authorization Organization who has been authorized
by the Manager, Seattle ACO, to make those findings. For a repair
method to be approved, the repair must meet the certification basis
of the airplane, and the approval must specifically refer to this
AD.

Material Incorporated by Reference

    (l) You must use Boeing Alert Service Bulletin 747-54A2203,
dated August 31, 2000; and Boeing Alert Service Bulletin 747-
54A2203, Revision 1, dated August 9, 2007; to perform the actions
that are required by this AD, unless the AD specifies otherwise.
    (1) The Director of the Federal Register approved the
incorporation by reference of Boeing Alert Service Bulletin 747-
54A2203, Revision 1, dated August 9, 2007, in accordance with 5
U.S.C. 552(a) and 1 CFR part 51.
    (2) On December 6, 2000 (65 FR 69862, November 21, 2000), the
Director of the Federal Register approved the incorporation by
reference of Boeing Alert Service Bulletin 747-54A2203, dated August
31, 2000.
    (3) Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle,
Washington 98124-2207, for a copy of this service information. You
may review copies at the FAA, Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington; or at the National Archives
and Records Administration (NARA). For information on the
availability of this material at NARA, call<PHONE_NUMBER>, or go to:
http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on September 14, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-18541 Filed 9-20-07; 8:45 am]

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[Federal Register Volume 86, Number 193 (Friday, October 8, 2021)]
[Notices]
[Pages 56261-56262]
[FR Doc No: 2021-22065]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Project No. 7590-015]

City of Nashua, New Hampshire; Notice of Effectiveness of
Withdrawal of Exemption Amendment Application

    On June 1, 2021, the City of Nashua, New Hampshire (City of Nashua)
filed an application to amend the exemption from licensing for the
Jackson Mills Project No. 7590. On September 14, 2021, the City of
Nashua notified the Commission that it was withdrawing its application.
    No motion in opposition to the notice of withdrawal has been filed,
and the Commission has taken no action to disallow the withdrawal.
Pursuant to Rule 216(b) of the Commission's Rules of Practice and
Procedure,\1\ the withdrawal of the amendment application became
effective on September 29, 2021, and this proceeding is hereby
terminated.
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    \1\ 18 CFR 385.216(b) (2020).

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    Dated: October 4, 2021.
Kimberly D. Bose,
Secretary.
[FR Doc. 2021-22065 Filed 10-7-21; 8:45 am]
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[ Federal Register: September 3, 2004 ( Volume 69, Number 171)] [ Notices] [ Page 53916 53917] From the Federal Register Online via GPO Access [ wais. access. gpo. gov] [ DOCID: fr03se04 75]

ENVIRONMENTAL PROTECTION AGENCY [ OPPT 2004 0103; FRL 7673 7]

National Advisory Committee for Acute Exposure Guideline Levels for Hazardous Substances; Notice of Public Meeting and Proposed AEGL Chemicals AGENCY: Environmental Protection Agency ( EPA).

ACTION: Notice.

SUMMARY: A meeting of the National Advisory Committee for Acute Exposure Guideline Levels for Hazardous Substances ( NAC/ AEGL Committee) will be held on September 21 23, 2004, in Washington, DC. At this meeting, the NAC/ AEGL Committee will address, as time permits, the various aspects of the acute toxicity and the development of Acute Exposure Guideline Levels ( AEGLs) for the following chemicals: 1,1,1 trichloroethane; acetaldehyde; acetone cyanohydrin; chloromethyl methyl ether; cumene; dibromoethane; diketene; disulfur dichloride; ethylene oxide ( 10 minute AEGL 2 value); hydroxylamine; jet fuel 8; propionaldehyde; propylene oxide; tetranitromethane and vinyl acetate. Regarding one chemical scheduled for the December, 2004 NAC/ AEGL Committee meeting, methylene chloride, the public is requested to provide comment on the Draft Technical Support Document, which is available upon request from the technical information contact ( see FOR FURTHER INFORMATION CONTACT below). All comments and suggestions including alternative pharmacokinetic and pharmacodynamic modeling for the derived methylene chloride draft provisional AEGL values should be directed to the technical information contact. Any comments should be submitted no later than October 29, 2004. Requests for short presentations regarding methylene chloride AEGL derivation should also be directed to the technical information contact. Proposed AEGL values for methylene chloride are scheduled to be balloted at the December 13 15, 2004 NAC/ AEGL Committee meeting currently planned to be held in Research Triangle Park, North Carolina.

DATES: A meeting of the NAC/ AEGL Committee will be held from 10: 00 a. m. to 5: 30 p. m. on September 21, 2004; 8: 30 a. m. to 5: 30 p. m. on September 22, 2004 and from 8: 00 a. m. to 12: 00 p. m. on September 23, 2004.

ADDRESSES: The meeting will be held at the U. S. Department of Labor, 200 Constitution Avenue, NW., Washington, DC 20210, Room numbers C5515 1A and 1B.

FOR FURTHER INFORMATION CONTACT: For general information contact: Colby Lintner, Regulatory Coordinator, Environmental Assistance Division ( 7408M), Office of Pollution Prevention and Toxics, Environmental Protection Agency, 1200 Pennsylvania Ave., NW., Washington, DC 20460 0001; telephone number: ( 202) 554 1404; e mail address: TSCA Hotline@ epa. gov.

[[ Page 53917]] For technical information contact: Paul S. Tobin, Designated Federal Officer ( DFO), Economics, Exposure, and Technology Division ( 7406M), Office of Pollution Prevention and Toxics, 1200 Pennsylvania Ave., NW., Washington, DC 20460 0001; telephone number: ( 202) 564 8557; e mail address: tobin. paul@ epa. gov.

SUPPLEMENTARY INFORMATION:

I. General Information A. Does this Action Apply to Me?

This action is directed to the public in general. This action may be of particular interest to anyone who may be affected if the AEGL values are adopted by government agencies for emergency planning, prevention, or response programs, such as EPA's Risk Management Program under the Clean Air Act and Amendments Section 112r. It is possible that other Federal agencies besides EPA, as well as State agencies and private organizations, may adopt the AEGL values for their programs. As such, the Agency has not attempted to describe all the specific entities that may be affected by this action. If you have any questions regarding the applicability of this action to a particular entity, consult the DFO listed under FOR FURTHER INFORMATION CONTACT.

B. How Can I Get Copies of this Document and Other Related Information?

1. Docket. EPA has established an official public docket for this action under docket identification ( ID) number OPPT 2004 0103. The official public docket consists of the documents specifically referenced in this action, any public comments received, and other information related to this action. Although a part of the official docket, the public docket does not include Confidential Business Information ( CBI) or other information whose disclosure is restricted by statute. The official public docket is the collection of materials that is available for public viewing at the EPA Docket Center, Rm. B102 Reading Room, EPA West, 1301 Constitution Ave., NW., Washington, DC. The EPA Docket Center is open from 8: 30 a. m. to 4: 30 p. m., Monday through Friday, excluding legal holidays. The EPA Docket Center Reading Room telephone number is ( 202) 566 1744 and the telephone number for the OPPT Docket, which is located in EPA Docket Center, is ( 202) 566 0280. 2. Electronic access. You may access this Federal Register document electronically through the EPA Internet under the `` Federal Register'' listings at http:// www. epa. gov/ fedrgstr/.

An electronic version of the public docket is available through EPA's electronic public docket and comment system, EPA Dockets. You may use EPA Dockets at http:// www. epa. gov/ edocket/ to submit or view public comments, access the index listing of the contents of the official public docket, and to access those documents in the public docket that are available electronically. Although not all docket materials may be available electronically, you may still access any of the publicly available docket materials through the docket facility identified in Unit I. B. 1. Once in the system, select `` search,'' then key in the appropriate docket ID number.

II. Meeting Procedures For additional information on the scheduled meeting, the agenda of the NAC/ AEGL Committee, or the submission of information on chemicals to be discussed at the meeting, contact the DFO listed under FOR FURTHER INFORMATION CONTACT. The meeting of the NAC/ AEGL Committee will be open to the public. Oral presentations or statements by interested parties will be limited to 10 minutes. Interested parties are encouraged to contact the DFO to schedule presentations before the NAC/ AEGL Committee. Since seating for outside observers may be limited, those wishing to attend the meeting as observers are also encouraged to contact the DFO at the earliest possible date to ensure adequate seating arrangements. Inquiries regarding oral presentations and the submission of written statements or chemical specific information should be directed to the DFO.

III. Future Meetings Another meeting of the NAC/ AEGL Committee is scheduled for December 13 15, 2004.

List of Subjects Environmental protection, Chemicals, Hazardous substances, Health.

Dated: August 30, 2004. Wendy C. Hamnett, Acting Director, Office of Pollution Prevention and Toxics. [ FR Doc. 04 20138 Filed 9 2 04; 8: 45 am]

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