[Federal Register: December 4, 2007 (Volume 72, Number 232)]
[Notices]
[Page 68225-68226]
[DOCID:fr04de07-115]

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SECURITIES AND EXCHANGE COMMISSION

[Release No. 34-56850; File No. SR-Amex-2007-123]

Self-Regulatory Organizations; American Stock Exchange LLC;
Notice of Filing and Order Granting Accelerated Approval of a Proposed
Rule Change, as Modified by Amendment No.1 Thereto, To Send P/A Orders
Through Linkage Prior to the Opening of Trading

November 27, 2007.
    Pursuant to Section 19(b)(1) of the Securities Exchange Act of 1934
(``Act'') \1\ and Rule 19b-4 thereunder,\2\ notice is hereby given that
on November 16, 2007, the American Stock Exchange LLC (``Exchange'' or
``Amex'') filed with the Securities and Exchange Commission
(``Commission'') the proposed rule change as described in Items I and
II below, which items have been substantially prepared by the Amex. On
November 26, 2008, the Exchange filed Amendment No. 1 to the proposed
rule change. The Commission is publishing this notice to solicit
comments on the proposed rule change, as amended, from interested
persons and is approving the proposed rule change on an accelerated
basis.
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    \1\ 15 U.S.C. 78s(b)(l).
    \2\ 17 CFR 240. 19b-4.
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I. Self-Regulatory Organization's Statement of the Terms of Substance
of the Proposed Rule Change

    The Exchange proposes to adopt Commentary .06 to Amex Rule 918 to
permit the sending of Principal Acting as Agent Orders (``P/A Orders'')
\3\ through the Intermarket Options Linkage (``Linkage'') prior to the
opening of trading. This proposal would conform Amex Rule 918 to Joint
Amendment No. 23 \4\ (``Amendment No. 23'') to the Plan for the Purpose
of Creating and Operating an Intermarket Options Linkage (the ``Linkage
Plan'').\5\ The text of the proposed rule change is available at the
Amex, at the Commission's Public Reference Room, and at http://www.amex.com
.

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    \3\ See Section 2(16)(a) of the Plan for the Purpose of Creating
and Operating an Intermarket Option Linkage (``Linkage Plan'') .
    \4\ See Securities Exchange Act Release No. 56780 (November 13,
2007), 72 FR 65113 (November 19, 2007) (File No. 4-429).
    \5\ On July 28, 2000, the Commission approved a national market
system plan for the purpose of creating and operating an intermarket
options market linkage proposed by the Amex, CBOE, and ISE. See
Securities Exchange Act Release No. 43086 (July 28, 2000), 65 FR
48023 (August 4, 2000). Subsequently, Phlx, Pacific Exchange, Inc.
(n/k/a NYSE Arca, Inc.), and BSE joined the Linkage Plan. See
Securities Exchange Act Release Nos. 43573 (November 16, 2000), 65
FR 70851 (November 28, 2000); 43574 (November 16, 2000), 65 FR 70850
(November 28, 2000); and 49198 (February 5, 2004), 69 FR 7029
(February 12, 2004).
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II. Self-Regulatory Organization's Statement of the Purpose of, and
Statutory Basis for, the Proposed Rule Change

    In its filing with the Commission, the Exchange included statements
concerning the purpose of, and basis for, its proposed rule change and
discussed any comments it received on the proposed rule change. The
text of these statements may be examined at the places specified in
Item III below. The Exchange has prepared summaries, set forth in
Sections A, B, and C below, of the most significant aspects of such
statements.

A. Self-Regulatory Organization's Statement of the Purpose of, and
Statutory Basis for, the Proposed Rule Change

1. Purpose
    The Amex proposes to adopt Commentary .06 to Amex Rule 918 to amend
its rule to conform to Amendment No. 23 to the Linkage Plan. The
proposal will permit the use of the Linkage prior to the opening of
trading. Prior to the adoption of Amendment No. 23, the Linkage Plan
did not comtemplate the use of the Linkage before a Linkage Plan
participant (a ``Participant'') opened for trading and disseminated a
quotation in an options series. In addition, there was no trade-through
protection for opening trades. As a result, if there was a better
market away at the time a Plan Participant opens its market, the Amex
specialist, responsible both for the opening and for protecting
customer orders, could not access that market for a customer. The
customer accordingly could receive a price inferior to the national
best bid and offer (``NBBO''). This proposal, along with Amendment No.
23 to the Linkage Plan, will permit the sending of P/A Orders prior to
the opening, allowing the Amex specialist to access better markets on
behalf of customers prior to the Exchange's opening.
    In implementing this proposed rule change, the Exchange represented
that it will ensure that customers receive the best price for their
orders. Under the Linkage Plan, a Participant receiving market has five
(5) seconds to respond to a P/A Order, and the Participant receiving
market can then reject a response it receives more than five (5)
seconds after sending the order. In the unlikely event that the Amex
opens its market during this five (5) second period, it is possible
that the opening price could differ from the price of an executed P/A
Order. In that case, the Amex represented that it will ensure that the
specialist provides the customer with the most advantageous price.
Therefore, the proposal will only benefit customers by providing them
with potential price improvement at the opening.
2. Statutory Basis
    The Exchange believes the proposed rule change is consistent with
the Act and the rules and regulations under the Act applicable to
national securities exchanges and, in particular, the

requirements of Section 6(b) of the Act.\6\ Specifically, the Exchanges
believe the proposed rule change is consistent with the requirements of
Section 6(b)(5) of the Act\7\ that the rules of an exchange be designed
to prevent fraudulent and manipulative acts, to promote just and
equitable principles of trade, to remove impediments to and perfect the
mechanism of a free and open market and a national market system, and,
in general, to protect investors and the public interest.
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    \6\ 15 U.S.C. 78f(b).
    \7\ 15 U.S.C. 78f(b)(5).
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B. Self-Regulatory Organization's Statement on Burden on Competition

    The Exchange believes that the proposed rule change would impose no
burden on competition that is not necessary or appropriate in
furtherance of the purposes of the Act.

C. Self-Regulatory Organization's Statement on Comments on the Proposed
Rule Change Received From Members, Participants or Others

    The Exchange has neither solicited nor received comments on this
proposal.

III. Solicitation of Comments

    Interested persons are invited to submit written data, views, and
arguments concerning the foregoing, including whether the proposed rule
change is consistent with the Act. Comments may be submitted by any of
the following methods:

Electronic Comments

     Use the Commission's Internet comment form (http://www.sec.gov/rules/sro.shtml.
 ); or     Send an e-mail to<EMAIL_ADDRESS>Please include

File Number SR-Amex-2007-123 on the subject line.

Paper Comments

     Send paper comments in triplicate to Nancy M. Morris,
Secretary, Securities and Exchange Commission, 100 F Street, NE.,
Washington, DC 20549-1090.

All submissions should refer to File Number SR-Amex-2007-123. This file
number should be included on the subject line if e-mail is used. To
help the Commission process and review your comments more efficiently,
please use only one method. The Commission will post all comments on
the Commission's Internet Web site (http://www.sec.gov/rules/sro.shtml

). Copies of the submissions, all subsequent amendments, all written
statements with respect to the proposed rule change that are filed with
the Commission, and all written communications relating to the proposed
rule change between the Commission and any person, other than those
that may be withheld from the public in accordance with the provisions
of 5 U.S.C. 552, will be available for inspection and copying in the
Commission's Public Reference Room, 100 F Street, NE., Washington, DC
20549, on official business days between the hours of 10 a.m. and 3
p.m. Copies of the filings also will be available for inspection and
copying at the principal offices of the Exchange. All comments received
will be posted without change; the Commission does not edit personal
identifying information from submissions. You should submit only
information that you wish to make available publicly. All submissions
should refer to File No. SR-Amex-2007-123 and should be submitted on or
before December 26, 2007.

IV. Commission's Findings and Order Granting Accelerated Approval of
Proposed Rule Changes

    After careful consideration, the Commission finds that the proposed
rule change is consistent with the requirements of the Act and the
rules and regulations thereunder, applicable to national securities
exchanges.\8\ In particular, the Commission finds that the proposal is
consistent with the provisions of Section 6(b)(5) of the Act\9\ in that
it is designed to prevent fraudulent and manipulative acts and
practices, to promote just and equitable principles of trade, to remove
impediments to and perfect the mechanism of a free and open market and
a national market system, and, in general, to protect investors and the
public interest. The Commission believes that allowing the Exchange to
send P/A Orders to the Linkage prior to the opening should facilitate
investors' intermarket access to superior prices.
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    \8\ In approving this proposal, the Commission has considered
its impact on efficiency, competition, and capital formation. See
U.S.C. 78c(f).
    \9\ 15 U.S.C. 78f(b)(5).
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    The Commission finds good cause for approving the proposed rule
change before the 30th day after the date of publication of notice of
filing thereof in the Federal Register. Granting accelerated approval
would facilitate the implementation of the proposed rule change in
conjunction with Amendment No. 23 to the Linkage Plan.\10\ In addition,
the Commission notes that the Exchange has committed to ensuring that,
for Linkage P/A Orders sent prior to the opening, Amex specialists will
provide customers with the most advantageous price in the event that
the Amex opens its market while the Exchange is awaiting a response to
such a P/A Order. Therefore, the Commission finds good cause,
consistent with Section 19(b)(2) of the Act,\11\ to approve the
proposed rule change on an accelerated basis.
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    \10\ See supra note 4.
    \11\ 15 U.S.C. 78s(b)(2).
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V. Conclusion

    It is therefore ordered, pursuant to Section 19(b)(2) of the
Act,\12\ that the proposed rule change (SR-Amex-2007-123) be, and it
hereby is, approved on an accelerated basis.
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    \12\ 17 CFR 200.30-3(a)(12).

    For the Commission, by the Division of Trading and Markets,
pursuant to delegated authority.\13\
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    \13\ 15 U.S.C. 78s(b)(2).
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Nancy M. Morris,
Secretary.
 [FR Doc. E7-23396 Filed 12-3-07; 8:45 am]

BILLING CODE 8011-01-P


Facility name Address City State Zip County Latitude Longitude SIC code NAICS code Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Page 1 Facility name Address City State Zip County Latitude Longitude SIC code NAICS code Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Quantegy Inc. 2230 Marvyn Parkway Opelika AL 36801 Lee 32 37 20 85 22 09 3695 334613 Total Quantegy JVC Magnetics America Co. 1 JVC Road Tuscaloosa AL 35405 Tuscaloosa 33 10 29 87 27 30 3695 334613 JVC Magnetics America Co. 1 JVC Road Tuscaloosa AL 35405 Tuscaloosa 33 10 29 87 27 30 3695 334613 JVC Magnetics America Co. 1 JVC Road Tuscaloosa AL 35405 Tuscaloosa 33 10 29 87 27 30 3695 334613 JVC Magnetics America Co. 1 JVC Road Tuscaloosa AL 35405 Tuscaloosa 33 10 29 87 27 30 3695 334613 JVC Magnetics America Co. 1 JVC Road Tuscaloosa AL 35405 Tuscaloosa 33 10 29 87 27 30 3695 334613 JVC Magnetics America Co. 1 JVC Road Tuscaloosa AL 35405 Tuscaloosa 33 10 29 87 27 30 3695 334613 JVC Magnetics America Co. 1 JVC Road Tuscaloosa AL 35405 Tuscaloosa 33 10 29 87 27 30 3695 334613 JVC Magnetics America Co. 1 JVC Road Tuscaloosa AL 35405 Tuscaloosa 33 10 29 87 27 30 3695 334613 Total JVC 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 3M Magnetic Tape Manufacturin905  915 Adam Street S. Hutchinson MN 55350 McLeod 44 52 49 94 21 32 3695; 2672 334613; 32222 Total 3M Eastman Kodak Co.  Kodak Par1669 Lake Avenue Rochester NY 14652 Monroe 43 12 10 77 37 45 3861 325992 Eastman Kodak Co.  Kodak Par1669 Lake Avenue Rochester NY 14652 Monroe 43 12 10 77 37 45 3861 325992 Eastman Kodak Co.  Kodak Par1669 Lake Avenue Rochester NY 14652 Monroe 43 12 10 77 37 45 3861 325992 Eastman Kodak Co.  Kodak Par1669 Lake Avenue Rochester NY 14652 Monroe 43 12 10 77 37 45 3861 325992 Eastman Kodak Co.  Kodak Par1669 Lake Avenue Rochester NY 14652 Monroe 43 12 10 77 37 45 3861 325992 Total Eastman Kodak Imation Enterprises Corp. 2700 East Frontage RoadWeatherford OK 73096 Custer 35 31 15 98 41 01 3695 334613 Imation Enterprises Corp. 2700 East Frontage RoadWeatherford OK 73096 Custer 35 31 15 98 41 01 3695 334613 Imation Enterprises Corp. 2700 East Frontage RoadWeatherford OK 73096 Custer 35 31 15 98 41 01 3695 334613 Imation Enterprises Corp. 2700 East Frontage RoadWeatherford OK 73096 Custer 35 31 15 98 41 01 3695 334613 Page 2 Facility name Address City State Zip County Latitude Longitude SIC code NAICS code Imation Enterprises Corp. 2700 East Frontage RoadWeatherford OK 73096 Custer 35 31 15 98 41 01 3695 334613 Imation Enterprises Corp. 2700 East Frontage RoadWeatherford OK 73096 Custer 35 31 15 98 41 01 3695 334613 Imation Enterprises Corp. 2700 East Frontage RoadWeatherford OK 73096 Custer 35 31 15 98 41 01 3695 334613 Imation Enterprises Corp. 2700 East Frontage RoadWeatherford OK 73096 Custer 35 31 15 98 41 01 3695 334613 Imation Enterprises Corp. 2700 East Frontage RoadWeatherford OK 73096 Custer 35 31 15 98 41 01 3695 334613 Total Imation Using TRI Emissions Data Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Total Sony ( TRI)

Using TRI and Alabama DEM Emissions Data Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Sony Magnetics Products Inc. of4275 W. Main Street Dothan AL 36305 Houston 31 13 00 85 27 30 3695 334613 Total Sony ( TRI/ Alabama DEM) Page 3 Facility name Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc. Mag tape products Equipment Emission type Control devices Audio, video, and datatape Stack 1  storage tanks, mix tanks, coatiStack Carbon adsorber 1 Audio, video, and datatape Stack 1  storage tanks, mix tanks, coatiStack Carbon adsorber 1 Audio, video, and datatape Stack 2  storage tanks, mix tanks, coatiStack Carbon adsorber 2 Audio, video, and datatape Stack 2  storage tanks, mix tanks, coatiStack Carbon adsorber 2 Audio, video, and datatape Stack 3  storage tanks, mix tanks, coatiStack Carbon adsorber 3 Audio, video, and datatape Stack 3  storage tanks, mix tanks, coatiStack Carbon adsorber 3 Audio, video, and datatape Stack 4  storage tanks, mix tanks, coatiStack Carbon adsorber 4 Audio, video, and datatape Stack 4  storage tanks, mix tanks, coatiStack Carbon adsorber 4 Audio, video, and datatape Stack 5  storage tanks, mix tanks, coatiStack Carbon adsorber 5 Audio, video, and datatape Stack 5  storage tanks, mix tanks, coatiStack Carbon adsorber 5 Audio, video, and datatape Stack 6  storage tanks, mix tanks, coatiStack Carbon adsorber 6 Audio, video, and datatape Stack 6  storage tanks, mix tanks, coatiStack Carbon adsorber 6 Audio, video, and datatape Emission unit 014 Stack Audio, video, and datatape Emission unit 104121 Stack Audio, video, and datatape Plant 1  coating lines Fugitive None Audio, video, and datatape Plant 1  coating lines Fugitive None Audio, video, and datatape Plant 1  ovens Fugitive None Audio, video, and datatape Plant 1  ovens Fugitive None Audio, video, and datatape Plant 1  mix prep area Fugitive None Audio, video, and datatape Plant 1  mix prep area Fugitive None Audio, video, and datatape Plant 1  mix prep area Fugitive None Audio, video, and datatape Plant 2  coating line 1 Fugitive None Audio, video, and datatape Plant 2  coating line 1 Fugitive None Audio, video, and datatape Plant 2  coating line 2 Fugitive None Audio, video, and datatape Plant 2  coating line 2 Fugitive None Audio, video, and datatape Plant 2  ovens Fugitive None Audio, video, and datatape Plant 2  ovens Fugitive None Audio, video, and datatape Plant 2  mix prep area Fugitive None Audio, video, and datatape Plant 2  mix prep area Fugitive None Audio, video, and datatape Plant 2  mix prep area Fugitive None Audio, video, and datatape R& D bldg  coating line 1 Fugitive None Audio, video, and datatape R& D bldg  coating line 1 Fugitive None Audio, video, and datatape R& D bldg  coating line 2 Fugitive None Audio, video, and datatape R& D bldg  coating line 2 Fugitive None Audio, video, and datatape R& D bldg  oven 1 Fugitive None Audio, video, and datatape R& D bldg  oven 1 Fugitive None Audio, video, and datatape R& D bldg  oven 2 Fugitive None Audio, video, and datatape R& D bldg  oven 2 Fugitive None Page 4 Facility name Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Total Quantegy JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

Total JVC 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin Total 3M Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Total Eastman Kodak Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp. Mag tape products Equipment Emission type Control devices Audio, video, and datatape R& D bldg  mix prep area Fugitive None Audio, video, and datatape R& D bldg  mix prep area Fugitive None Audio, video, and datatape R& D bldg  mix prep area Fugitive None Audio and videotape Area 1  mixing room Fugitive Condenser Audio and videotape Area 1  mixing room Fugitive Condenser Audio and videotape Area 2  coating and rewind room Fugitive Condenser Audio and videotape Area 2  coating and rewind room Fugitive Condenser Audio and videotape Area 3  coating cleanroom Fugitive Condenser Audio and videotape Area 3  coating cleanroom Fugitive Condenser Audio and videotape Area 4  K room Fugitive Condenser Audio and videotape Area 4  K room Fugitive Condenser Audio and videotape Stack Audio and videotape Stack Audio and videotape Stack Audio and videotape Fugitive Audio and videotape Stack Audio and videotape Stack Audio and videotape Fugitive Audio and videotape Stack Audio and videotape Stack Audio and videotape Fugitive Audio and videotape Stack Audio and videotape Fugitive Audio and videotape Stack Audio and videotape Stack Advantix film Source A  coater Stack RTO with caustic scr Advantix film Source A  coater Stack RTO with caustic scr Advantix film Source B  mix prep area Stack Fabric filter with non Advantix film Source B  mix prep area Stack Fabric filter with non Advantix film Source C  mix prep area Stack Fabric filter Diskettes, datatape Emission unit 1  miscellaneous Stack Thermal oxidizer Diskettes, datatape Emission unit 1  miscellaneous Stack Thermal oxidizer Diskettes, datatape Emission unit 4A  coater, curing ovens, Stack Thermal oxidizer Diskettes, datatape Emission unit 4A  coater, curing ovens, Stack Thermal oxidizer Page 5 Facility name Quantegy Inc.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Total Imation Using TRI Emissions Data Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Total Sony ( TRI)

Using TRI and Alabama DEM E Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Total Sony ( TRI/ Alabama DEM Mag tape products Equipment Emission type Control devices Diskettes, datatape Emission unit 4A  coater, curing ovens, Stack Thermal oxidizer Diskettes, datatape Emission unit 4B  coater, curing ovens, Stack Thermal oxidizer Diskettes, datatape Emission unit 4B  coater, curing ovens, Stack Thermal oxidizer Diskettes, datatape Emission unit 4B  coater, curing ovens, Stack Thermal oxidizer Diskettes, datatape Emission unit 3  mixing Fugitive Audio, video, and datatape SR001  mixing room Fugitive Audio, video, and datatape SR001  mixing room Fugitive Audio, video, and datatape SR001  mixing room Fugitive Audio, video, and datatape SR004  coating line Fugitive Audio, video, and datatape SR004  coating line Fugitive Audio, video, and datatape SR002  oven Fugitive Audio, video, and datatape SR002  oven Fugitive Audio, video, and datatape SR003  control equipment Stack/ fugitive Audio, video, and datatape SR003  control equipment Stack/ fugitive Audio, video, and datatape SR003  control equipment Fugitive Audio, video, and datatape Misc. fugitives Fugitive Audio, video, and datatape Misc. fugitives Fugitive Audio, video, and datatape Misc. fugitives Fugitive Audio, video, and datatape Misc. fugitives Fugitive Audio, video, and datatape SR001  mixing room Fugitive Audio, video, and datatape SR001  mixing room Fugitive Audio, video, and datatape SR001  mixing room Fugitive Audio, video, and datatape SR002  coating line Fugitive Audio, video, and datatape SR002  coating line Fugitive Audio, video, and datatape SR003  oven Fugitive Audio, video, and datatape SR003  oven Fugitive Audio, video, and datatape SR004  control equipment Stack/ fugitive Audio, video, and datatape SR004  control equipment Stack/ fugitive Audio, video, and datatape SR004  control equipment Fugitive Audio, video, and datatape Misc. fugitives Fugitive Audio, video, and datatape Misc. fugitives Fugitive Audio, video, and datatape Misc. fugitives Fugitive Audio, video, and datatape Misc. fugitives Fugitive Page 6 Facility name Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc. Pollutant Emissions,

tpy Emissions,

lb/ yr Stack diameter, ft Stack flowrate,

ft3/ s Stack height, ft Stack velocity,

ft/ s Stack temperature,

deg F Toluene 0.8 1,647 2.7 1479 17 4.3 100 Methyl ethyl ketone 1.2 2,461 2.7 1479 17 4.3 100 Toluene 0.8 1,647 2.7 1479 17 4.3 100 Methyl ethyl ketone 1.2 2,461 2.7 1479 17 4.3 100 Toluene 0.8 1,647 2.7 1479 17 4.3 100 Methyl ethyl ketone 1.2 2,461 2.7 1479 17 4.3 100 Toluene 0.8 1,647 2.7 1479 17 4.3 100 Methyl ethyl ketone 1.2 2,461 2.7 1479 17 4.3 100 Toluene 0.8 1,647 2.7 1479 17 4.3 100 Methyl ethyl ketone 1.2 2,461 2.7 1479 17 4.3 100 Toluene 0.8 1,647 2.7 1479 17 4.3 100 Methyl ethyl ketone 1.2 2,461 2.7 1479 17 4.3 100 Methyl ethyl ketone 1.0 2,000 1.5 42 25 0.4 120 Cobalt 0.0025 5.0 2.9 263 52 0.7 217 Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Cobalt 0.0008 1.7 Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Cobalt 0.0008 1.7 Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Page 7 Facility name Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Total Quantegy JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

Total JVC 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin Total 3M Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Total Eastman Kodak Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp. Pollutant Emissions,

tpy Emissions,

lb/ yr Stack diameter, ft Stack flowrate,

ft3/ s Stack height, ft Stack velocity,

ft/ s Stack temperature,

deg F Toluene 1.2 2,384 Methyl ethyl ketone 1.8 3,559 Cobalt 0.0008 1.7 49 97,971 Toluene 27 54,880 Methyl ethyl ketone 42 83,729 Toluene 24 47,196 Methyl ethyl ketone 36 72,007 Toluene 2.7 5,488 Methyl ethyl ketone 4.2 8,373 Toluene 1.1 2,195 Methyl ethyl ketone 1.7 3,349 139 277,217 Ethyl benzene 0.05 90 Ethylene glycol 0.007 14 n Hexane 2.6 5,100 n Hexane 0.05 90 Methanol 12 23,400 MEK 24 48,000 MEK 15 29,400 MIBK 0.2 300 Toluene 21 42,000 Toluene 5.1 10,200 Xylenes 0.2 300 Xylenes 0.02 39 Antimony 0.003 6.3 Lead compounds 0.004 7.2 79 158,946 Methyl ethyl ketone 1.21711292 2,434 12 169,697 100 25 100 Toluene 3.03288708 6,066 12 169,697 100 25 100 Hydrogen chloride 0.035 70 0.5 30 73 2.5 ambient Cobalt 0.0000005 0.001 0.5 30 73 2.5 ambient Cobalt 0.000001 0.002 1.25 3,700 74 50 ambient 4.3 8,570 Methyl ethyl ketone 0.005 10 3.5 30,000 30 52 400 Acrylonitrile 0.004 8 3.5 30,000 30 52 400 Toluene 0.2 390 3.5 30,000 30 52 400 Methanol 0.01 20 3.5 30,000 30 52 400 Page 8 Facility name Quantegy Inc.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Total Imation Using TRI Emissions Data Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Total Sony ( TRI)

Using TRI and Alabama DEM E Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Total Sony ( TRI/ Alabama DEM Pollutant Emissions,

tpy Emissions,

lb/ yr Stack diameter, ft Stack flowrate,

ft3/ s Stack height, ft Stack velocity,

ft/ s Stack temperature,

deg F Methyl ethyl ketone 2.7 5,420 3.5 30,000 30 52 400 Toluene 0.2 390 3.5 30,000 30 52 400 Methanol 0.01 20 3.5 30,000 30 52 400 Methyl ethyl ketone 2.7 5,420 3.5 30,000 30 52 400 Methyl ethyl ketone 0.004 8 5.8 11,686 Toluene 9.1 18,180 Methyl ethyl ketone 38 75,060 Cobalt compounds 0.1 200 Toluene 14 27,270 Methyl ethyl ketone 56 112,590 Toluene 16 31,815 Methyl ethyl ketone 66 131,355 Toluene 2.9 5,745 Methyl ethyl ketone 12 23,645 Cobalt 0.1 288 Toluene 4.5 9,090 Methyl ethyl ketone 19 37,530 Cobalt 0.4 863 Cobalt compounds 0.03 50 237 473,680 Toluene 9.1 18,180 Methyl ethyl ketone 38 75,060 Cobalt compounds 0.2 397 Toluene 14 27,270 Methyl ethyl ketone 56 112,590 Toluene 16 31,815 Methyl ethyl ketone 66 131,355 Toluene 2.9 5,745 Methyl ethyl ketone 12 23,645 Cobalt 0.3 571 Toluene 4.5 9,090 Methyl ethyl ketone 19 37,530 Cobalt 0.9 1,713 Cobalt compounds 0.05 99 238 475,060 Page 9 Facility name Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Quantegy Inc. Building volume, ft3 Operating hr/ yr Notes 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Estimated emissions assuming equal fraction of emissions throu 6,257 Data from 1999 NEI; used operating hours from facility.

6,257 Data from 1999 NEI; used operating hours from facility.

4,312 6,257 Estimated emissions assuming equal fraction of emissions throu 4,312 6,257 Estimated emissions assuming equal fraction of emissions throu 33,750 6,257 Estimated emissions assuming equal fraction of emissions throu 33,750 6,257 Estimated emissions assuming equal fraction of emissions throu 171,110 8,760 Estimated emissions assuming equal fraction of emissions throu 171,110 8,760 Estimated emissions assuming equal fraction of emissions throu 171,110 8,760 Estimated emissions assuming equal fraction of emissions throu 878 6,257 Estimated emissions assuming equal fraction of emissions throu 878 6,257 Estimated emissions assuming equal fraction of emissions throu 1,440 6,257 Estimated emissions assuming equal fraction of emissions throu 1,440 6,257 Estimated emissions assuming equal fraction of emissions throu 165,835 6,257 Estimated emissions assuming equal fraction of emissions throu 165,835 6,257 Estimated emissions assuming equal fraction of emissions throu 415,538 8,760 Estimated emissions assuming equal fraction of emissions throu 415,538 8,760 Estimated emissions assuming equal fraction of emissions throu 415,538 8,760 Estimated emissions assuming equal fraction of emissions throu 619 6,257 Estimated emissions assuming equal fraction of emissions throu 619 6,257 Estimated emissions assuming equal fraction of emissions throu 2,475 6,257 Estimated emissions assuming equal fraction of emissions throu 2,475 6,257 Estimated emissions assuming equal fraction of emissions throu 14,850 6,257 Estimated emissions assuming equal fraction of emissions throu 14,850 6,257 Estimated emissions assuming equal fraction of emissions throu 7,475 6,257 Estimated emissions assuming equal fraction of emissions throu 7,475 6,257 Estimated emissions assuming equal fraction of emissions throu Page 10 Facility name Quantegy Inc.

Quantegy Inc.

Quantegy Inc.

Total Quantegy JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

JVC Magnetics America Co.

Total JVC 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin 3M Magnetic Tape Manufacturin Total 3M Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Eastman Kodak Co.  Kodak Par Total Eastman Kodak Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp. Building volume, ft3 Operating hr/ yr Notes 53,035 8,760 Estimated emissions assuming equal fraction of emissions throu 53,035 8,760 Estimated emissions assuming equal fraction of emissions throu 53,035 8,760 Estimated emissions assuming equal fraction of emissions throu 290,133 8,760 Estimated to emit 50% of fugitive toluene emissions; assume 24 290,133 8,760 Estimated to emit 50% of fugitive MEK emissions; assume 24 h 283,729 8,760 Estimated to emit 43% of fugitive toluene emissions; assume 24 283,729 8,760 Estimated to emit 43% of fugitive MEK emissions; assume 24 h 253,760 8,760 Estimated to emit 5% of fugitive toluene emissions; assume 24 253,760 8,760 Estimated to emit 5% of fugitive MEK emissions; assume 24 hr/

54,080 8,760 Estimated to emit 2% of fugitive toluene emissions; assume 24 54,080 8,760 Estimated to emit 2% of fugitive MEK emissions; assume 24 hr/

8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 8,760 Estimated emissions by applying 30% factor to 2000 TRI emiss 3,000 Estimated emissions by applying ratio of MEK and toluene emis 3,000 Estimated emissions by applying ratio of MEK and toluene emis 630 Estimated emissions by applying ratio of MEK and toluene emis 630 Estimated emissions by applying ratio of MEK and toluene emis 630 Estimated emissions by applying ratio of MEK and toluene emis 6,240 Data from 1999 NEI; assumed same stack parameters as proce 6,240 Data from 1999 NEI; assumed same stack parameters as proce 6,240 Data from 1999 NEI.

6,240 Data from 1999 NEI.

Page 11 Facility name Quantegy Inc.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Imation Enterprises Corp.

Total Imation Using TRI Emissions Data Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Total Sony ( TRI)

Using TRI and Alabama DEM E Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Sony Magnetics Products Inc. of Total Sony ( TRI/ Alabama DEM Building volume, ft3 Operating hr/ yr Notes 6,240 Data from 1999 NEI.

6,240 Data from 1999 NEI.

6,240 Data from 1999 NEI.

6,240 Data from 1999 NEI.

6,240 Data from 1999 NEI; default stack parameters in NEI not useful See diagram 8,736 Estimated to emit 20% of toluene emissions; assumed to be SR See diagram 8,736 Estimated to emit 20% of MEK emissions; assumed to be SR00 See diagram 8,736 Estimated to emit 80% of cobalt compound emissions; assumed See diagram 8,736 Estimated to emit 30% of toluene emissions; assumed to be SR See diagram 8,736 Estimated to emit 30% of MEK emissions; assumed to be SR00 See diagram 8,736 Estimated to emit 35% of toluene emissions; assumed to be SR See diagram 8,736 Estimated to emit 35% of MEK emissions; assumed to be SR00 See diagram 8,736 Estimated to emit 5% of toluene emissions; added stack toluene See diagram 8,736 Estimated to emit 5% of MEK emissions; added stack MEK emi See diagram 8,736 Estimated to emit 25% of cobalt emissions; assumed to be SR0 8,736 Estimated to emit 10% of toluene emissions.

8,736 Estimated to emit 10% of MEK emissions.

8,736 Estimated to emit 75% of cobalt emissions.

8,736 Estimated to emit 20% of cobalt compound emissions.

See diagram 8,736 Estimated to emit 20% of toluene emissions; assumed to be SR See diagram 8,736 Estimated to emit 20% of MEK emissions; assumed to be SR00 See diagram 8,736 Estimated to emit 14.3% of cobalt and cobalt compound emissio See diagram 8,736 Estimated to emit 30% of toluene emissions; assumed to be SR See diagram 8,736 Estimated to emit 30% of MEK emissions; assumed to be SR00 See diagram 8,736 Estimated to emit 35% of toluene emissions; assumed to be SR See diagram 8,736 Estimated to emit 35% of MEK emissions; assumed to be SR00 See diagram 8,736 Estimated to emit 5% of toluene emissions; added stack toluene See diagram 8,736 Estimated to emit 5% of MEK emissions; added stack MEK emi See diagram 8,736 Eestimated to emit 20.5% of cobalt and cobalt compound emiss 8,736 Estimated to emit 10% of toluene emissions.

8,736 Estimated to emit 10% of MEK emissions.

8,736 Estimated to emit 61.6% of cobalt and cobalt compound emissio 8,736 Estimated to emit 3.6% of cobalt and cobalt compound emission Page 12 Cobalt Emissions Summary Report Month Reported cobalt emissions, lbs Revised cobalt emissions, lbs April 2002 223.91 223.91 May 2002 199.93 199.93 June 2002 254.46 254.46 July 2002 261.31 261.31 August 2002 ( 4.95) 0.00 September 2002 332.02 332.02 October 2002 329.69 329.69 November 2002 399.76 399.76 December 2002 ( 161.26) 0.00 January 2003 493.03 493.03 February 2003 ( 142.52) 0.00 March 2003 ( 173.68) 0.00 April 2003 285.96 285.96 Total Sony 2,780.07 Note: For those months where Alabama DEM data showed negative cobalt emissions, assumed zero.


[Federal Register Volume 88, Number 223 (Tuesday, November 21, 2023)]
[Rules and Regulations]
[Pages 80952-80955]
[FR Doc No: 2023-25762]

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-2140; Project Identifier AD-2023-01071-T;
Amendment 39-22590; AD 2023-22-06]
RIN 2120-AA64

Airworthiness Directives; Lockheed Martin Corporation/Lockheed
Martin Aeronautics Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

-----------------------------------------------------------------------

SUMMARY: The FAA is superseding Airworthiness Directive (AD) 96-12-20,
which applied to certain Lockheed Martin Corporation/Lockheed Martin
Aeronautics Company Model 382, 382B, 382E, 382F, and 382G airplanes. AD
96-12-20 required visual inspections to detect loose, missing, or
deformed fasteners in the upper truss mounts of certain engines, visual
inspections to detect cracking in the associated lugs, repetitive
ultrasonic inspections to detect cracking of the upper lugs, and
replacement of damaged or cracked parts. AD 96-12-20 also provided for
an optional terminating action for the repetitive inspections. This AD
was prompted by reports of fatigue cracking of the lugs of the upper
truss mount, and by reports of cracks found prior to the initial
inspection times required by AD 96-12-20 and the determination that the
terminating action is no longer valid. This AD requires one-time
inspections for cracked or severed engine truss mount upper lugs of the
outboard engines, and replacement of the engine truss mount if
necessary. This AD also revises the applicability to include all Model
382, 382B, 382E, 382F, and 382G airplanes, and all Model

EC-130Q, C-130H, HP-C-130A, C-130A, and C-130B (including Model 282-
44A-05) airplanes. The FAA is issuing this AD to address the unsafe
condition on these products.

DATES: This AD is effective November 21, 2023.
    The FAA must receive comments on this AD by January 5, 2024.

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 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: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    AD Docket: You may examine the AD docket at regulations.gov by
searching for and locating Docket No. FAA-2023-2140; or in person at
Docket Operations between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket contains this final rule, any
comments received, and other information. The street address for Docket
Operations is listed above.

FOR FURTHER INFORMATION CONTACT: Fred Caplan, Aviation Safety Engineer,
FAA, 1701 Columbia Avenue, College Park, GA 30337; phone:<PHONE_NUMBER>;
email: [email protected].

SUPPLEMENTARY INFORMATION:

Comments Invited

    The FAA invites you to send any written data, views, or arguments
about this final rule. Send your comments to an address listed under
ADDRESSES. Include ``Docket No. FAA-2023-2140 and Project Identifier
AD-2023-01071-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the final rule, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this final rule because of those comments.
    Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this final rule.

Confidential Business Information

    CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this AD contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this AD, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this AD. Submissions containing CBI should be sent to Fred
Caplan, Aviation Safety Engineer, FAA, 1701 Columbia Avenue, College
Park, GA 30337; phone:<PHONE_NUMBER>; email: [email protected].
Any commentary that the FAA receives that is not specifically
designated as CBI will be placed in the public docket for this
rulemaking.

Background

    The FAA issued AD 96-12-20, Amendment 39-9663 (61 FR 29279, June
10, 1996; corrected August 16, 1996 (61 FR 42549)) (AD 96-12-20), for
certain Lockheed Martin Corporation/Lockheed Martin Aeronautics Company
Model 382, 382B, 382E, 382F, and 382G airplanes. AD 96-12-20 required
visual inspections to detect loose, missing, or deformed fasteners in
the upper truss mounts of certain engines; inspections to detect
cracking in the associated lugs; repetitive ultrasonic inspections to
detect cracking of the upper lugs; and replacement of damaged and
cracked parts. This amendment also provides for an optional terminating
action for the repetitive inspections. AD 96-12-20 was prompted by
reports of fatigue cracking of the lugs of the upper truss mount. The
FAA issued AD 96-12-20 to prevent multiple failures of the upper truss
mounts due to problems associated with fatigue cracking, which could
adversely affect the integrity of the engine mount structure.

Actions Since AD 96-12-20 Was Issued

    Since the FAA issued AD 96-12-20, the FAA has been notified of
additional crack findings in engine truss mount upper lugs occurring
prior to the initial inspection times required by AD 96-12-20. The
cracks were found to have progressed entirely through these parts and
have been found on multiple airplanes. In addition, modified parts,
required by the terminating action in AD 96-12-20, that were intended
to have a longer operational life have not resulted in longer periods
before cracks occur; therefore, the previous terminating action is not
valid, and airplanes on which the terminating action was done must be
inspected. The restricted category models EC-130Q, C-130H, HP-C-130A,
C-130A, and C-130B (including Model 282-44A-05) were added to the Model
382 airplanes affected by AD 96-12-20, since they share the same type
design in the area where cracking is occurring. Fatigue cracking of a
single engine truss mount upper lug could reduce the static strength of
an engine mount to limit load, while cracking of both lugs can lead to
separation of the engine, catastrophic structural damage, and loss of
control of the airplane.

FAA's Determination

    The FAA is issuing this AD because the agency has determined the
unsafe condition described previously is likely to exist or develop in
other products of the same type design.

AD Requirements

    This AD does not retain the requirements of AD 96-12-20. This AD
revises the applicability of AD 96-12-20 by expanding to all Model 382,
382B, 382E, 382F, and 382G airplanes, and adding Model EC-130Q, C-130H,
HP-C-130A, C-130A, and C-130B (including Model 282-44A-05) airplanes.
This AD requires one-time inspections to detect cracking of the No. 1
and No. 4 engine truss mount upper lugs, lower surfaces, at outer wing
station (OWS) 162 and OWS 197; cracking of the No. 1 and No. 4 engine
truss mount upper lug side surfaces, inboard and outboard, at OWS 162
and OWS 197; and severed engine truss mount upper lugs; and replacement
of the engine truss mount if found with cracked or severed engine truss
mount upper lugs.

Interim Action

    The FAA considers this AD to be an interim action. If final action
is later identified, the FAA might consider further rulemaking then.

Impact on Intrastate Aviation in Alaska

    In light of the heavy reliance on aviation for intrastate
transportation in Alaska, the FAA fully considered the effects of this
AD (including costs to be borne by affected operators) from the
earliest possible stages of AD development. This AD is based on those
considerations, and was developed with

regard to minimizing the economic impact on operators to the extent
possible, consistent with the safety objectives of this AD. In any
event, the Federal Aviation Regulations require operators to correct an
unsafe condition identified on an airplane to ensure operation of that
airplane in an airworthy condition. The FAA has determined in this case
that the requirements are necessary and the indirect costs would be
outweighed by the safety benefits of the AD.

Justification for Immediate Adoption and Determination of the Effective
Date

    Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies to dispense with notice and
comment procedures for rules when the agency, for ``good cause,'' finds
that those procedures are ``impracticable, unnecessary, or contrary to
the public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without providing notice and seeking
comment prior to issuance. Further, section 553(d) of the APA
authorizes agencies to make rules effective in less than thirty days,
upon a finding of good cause.
    An unsafe condition exists that requires the immediate adoption of
this AD without providing an opportunity for public comments prior to
adoption. The FAA has found that the risk to the flying public
justifies forgoing notice and comment prior to adoption of this rule
because fatigue cracking of a single engine truss mount upper lug
reduces the static strength of an engine mount to limit load, while
cracking of both lugs can lead to separation of the engine,
catastrophic structural damage, and loss of control of the airplane.
Further, based upon the additional applicability of affected airplanes
and the previously insufficient service information, it is likely that
further fatigue cracking and reduction in static strength has occurred
and could result in imminent separation of the engine, catastrophic
structural damage, and loss of control of the airplane. Finally, the
compliance time for the required action is shorter than the time
necessary for the public to comment and for publication of the final
rule. Accordingly, notice and opportunity for prior public comment are
impracticable and contrary to the public interest pursuant to 5 U.S.C.
553(b)(3)(B).
    In addition, the FAA finds that good cause exists pursuant to 5
U.S.C. 553(d) for making this amendment effective in less than 30 days,
for the same reasons the FAA found good cause to forgo notice and
comment.

Regulatory Flexibility Act

    The requirements of the Regulatory Flexibility Act (RFA) do not
apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt
a rule without prior notice and comment. Because the FAA has determined
that it has good cause to adopt this rule without notice and comment,
RFA analysis is not required.

Costs of Compliance

    The FAA estimates that this AD affects 41 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Inspections...........................  10 work-hours x $85 per               $0            $850         $34,850
                                         hour = $850.
----------------------------------------------------------------------------------------------------------------

    The FAA has received no definitive data on which to base the cost
estimates for the on-condition actions specified in 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.
    The FAA is 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

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

List of Subjects in 14 CFR Part 39

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

The Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by:
a. Removing Airworthiness Directive (AD) AD 96-12-20, Amendment 39-9663
(61 FR 29279, June 10, 1996; corrected August 16, 1996 (61 FR 42549));
and
b. Adding the following new AD:

2023-22-06 Lockheed Martin Corporation/Lockheed Martin Aeronautics
Company: Amendment 39-22590; Docket No. FAA-2023-2140; Project
Identifier AD-2023-01071-T.

(a) Effective Date

    This airworthiness directive (AD) is effective November 21,
2023.

(b) Affected ADs

    This AD replaces AD 96-12-20, Amendment 39-9663 (61 FR 29279,
June 10, 1996; corrected August 16, 1996 (61 FR 42549)) (AD 96-12-
20).

(c) Applicability

    This AD applies to the airplanes identified in paragraphs (c)(1)
and (2) of this AD.
    (1) All Lockheed Martin Corporation/Lockheed Martin Aeronautics
Company Model 382, 382B, 382E, 382F, and 382G airplanes,
certificated in any category.

    (2) All airplanes specified in paragraphs (c)(2)(i) through (xi)
of this AD, type certificated in the restricted category.
    (i) LeSEA Model C-130A airplanes (transferred from Central Air
Services, Inc.), Type Certificate Data Sheet (TCDS) A34SO, Revision
1.
    (ii) T.B.M., Inc., Model C-130A airplanes, TCDS A39CE, Revision
3.
    (iii) Western International Aviation, Inc., Model C-130A
airplanes, TCDS A33NM.
    (iv) USDA Forest Service Model C-130A airplanes, TCDS A15NM,
Revision 4.
    (v) Snow Aviation International, Inc., Model C-130A airplanes,
TCDS TQ3CH, Revision 1.
    (vi) International Air Response (transferred from Rogers
Helicopters, Inc., and Heavylift Helicopters Inc.) Model C-130A
airplanes, TCDS A31NM, Revision 3.
    (vii) Heavylift Helicopters, Inc., Model C-130B airplanes, TCDS
A35NM, Revision 1.
    (viii) Hawkins & Powers Aviation, Inc., Model HP-C-130A
airplanes, TCDS A30NM, Revision 1.
    (ix) Coulson Aviation (USA), Inc., Model EC-130Q and C-130H
airplanes, TCDS T00019LA, Revision 4.
    (x) Lockheed-Georgia Company Model 282-44A-05 (C-130B)
airplanes, TCDS A5SO.
    (xi) Surplus Model C-130A airplanes.

(d) Subject

    Air Transport Association (ATA) of America Code 71, Powerplant.

(e) Unsafe Condition

    This AD was prompted by reports of fatigue cracking of an upper
lug of the engine truss mount, and by reports of cracks found prior
to the initial inspection times required by AD 96-12-20. The FAA is
issuing this AD to address such fatigue cracking. Fatigue cracking
of a single engine truss mount upper lug could reduce the static
strength of an engine mount to limit load, while cracking of both
lugs can lead to separation of the engine, catastrophic structural
damage, and loss of control of the airplane.

(f) Compliance

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

(g) Required Actions

    Within 35 days after the effective date of this AD, do the
inspections specified in paragraphs (g)(1) and (2) of this AD, using
a method approved in accordance with the procedures specified in
paragraph (i) of this AD. If any cracked or severed engine truss
mount upper lug is found, the engine truss mount must be replaced
before further flight, using a method approved in accordance with
the procedures specified in paragraph (i) of this AD.
    (1) Do a one-time detailed visual inspection for cracking of the
No. 1 and No. 4 engine truss mount upper lugs, lower surfaces, at
outer wing station (OWS) 162 and OWS 197; and for severed engine
truss mount upper lugs; at a total of four locations: two locations
per engine mount, one mount assembly at each OWS.
    (2) Do a one-time borescope inspection for cracking of the No. 1
and No. 4 engine truss mount upper lug side surfaces, inboard and
outboard, at OWS 162 and OWS 197; and for severed engine truss mount
upper lugs; at a total of eight locations: two locations per engine
truss mount lug, two lugs per engine, one mount assembly at each
OWS.
    Note 1 to paragraph (g): Guidance for accomplishing the
inspections and replacement can be found in Lockheed Martin
Aeronautics Company Alert Service Bulletin A382-57-103, dated
October 19, 2023.

(h) Special Flight Permit

    Special flight permits may be issued in accordance with 14 CFR
21.197 and 21.199 to operate the airplane to a location where the
inspections required by this AD can be performed, but special flight
permits may not be issued to operate the airplane after a visual or
borescope inspection has identified a cracked or severed lug, unless
the operator contacts the Manager, East Certification Branch, FAA,
for specific limitations that must be followed and complies with
those limitations.

(i) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, East Certification Branch, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or responsible Flight
Standards Office, as appropriate. If sending information directly to
the manager of the certification office, send it to the attention of
the person identified in paragraph (j) of this AD.
    (2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.

(j) Related Information

    (1) For more information about this AD, contact Fred Caplan,
Aviation Safety Engineer, FAA, 1701 Columbia Avenue, College Park,
GA 30337; phone:<PHONE_NUMBER>; email: [email protected].
    (2) For Lockheed Martin Aeronautics Company service information
identified in this AD that is not incorporated by reference, contact
Lockheed Martin Corporation/Lockheed Martin Aeronautics Company,
Airworthiness Office, Dept. 6A0M, Zone 0252, Column P-58, 86 S Cobb
Drive, Marietta, GA 30063; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>;
email [email protected]. You may view this service information at
the FAA, Airworthiness Products Section, Operational Safety Branch,
2200 South 216th St., Des Moines, WA. For information on the
availability of this material at the FAA, call<PHONE_NUMBER>.

(k) Material Incorporated by Reference

    None.

    Issued on November 16, 2023.
Ross Landes,
Deputy Director for Regulatory Operations, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023-25762 Filed 11-17-23; 4:15 pm]
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