62965 Federal Register / Vol. 67, No. 196 / Wednesday, October 9, 2002 / Notices or charges under the Interchange Agreement as previously approved and on file with this Commission. Comment Date: October 18, 2002.

Standard Paragraph Any person desiring to intervene or to protest this filing should file with the Federal Energy Regulatory Commission, 888 First Street, NE., Washington, DC 20426, in accordance with rules 211 and 214 of the Commission's rules of practice and procedure (18 CFR 385.211 and 385.214). Protests will be considered by the Commission in determining the appropriate action to be taken, but will not serve to make protestants parties to the proceeding. Any person wishing to become a party must file a motion to intervene. All such motions or protests should be filed on or before the comment date, and, to the extent applicable, must be served on the applicant and on any other person designated on the official service list. This filing is available for review at the Commission or may be viewed on the Commission's Web site at http:// www. ferc. gov using the `` RIMS'' link, select `` Docket #'' and follow the instructions (call 202– 208– 2222 for assistance). Protests and interventions may be filed electronically via the Internet in lieu of paper; see 18 CFR 385.2001( a)( 1)( iii) and the instructions on the Commission's web site under the `` e Filing'' link.

Linwood A. Watson, Jr., Deputy Secretary. [FR Doc. 02– 25646 Filed 10– 8– 02; 8: 45 am]

BILLING CODE 6717– 01– P DEPARTMENT OF ENERGY Federal Energy Regulatory Commission Notice of Meeting, Notice of Vote, Explanation of Action Closing Meeting and List of Persons To Attend October 2, 2002. The following notice of meeting is published pursuant to Section 3( a) of the Government in the Sunshine Act (Pub. L. No. 94– 409), 5 U. S. C. 552b: AGENCY HOLDING MEETING: Federal Energy Regulatory Commission. DATE AND TIME: October 9, 2002 (30 Minutes Following Regular Commission Meeting). PLACE: Hearing Room 5, 888 First Street, NE., Washington, DC 20426. STATUS: Closed. MATTERS TO BE CONSIDERED: Non Public, Investigations and Inquiries and Enforcement Related Matters. CONTACT PERSON FOR MORE INFORMATION: Magalie R. Salas, Secretary, Telephone (202) 502– 8400. Chairman Wood and Commissioners Massey, Breathitt and Brownell voted to hold a closed meeting on October 9, 2002. The certification of the General Counsel explaining the action closing the meeting is available for public inspection in the Commission's Public Reference Room at 888 First Street, NE., Washington, DC 20426. The Chairman and the Commissioners, their assistants, the Commission's Secretary and her assistant, the General Counsel and members of her staff, and a stenographer are expected to attend the meeting. Other staff members from the Commission's program offices who will advise the Commissioners in the matters discussed will also be present.

Magalie R. Salas, Secretary. [FR Doc. 02– 25735 Filed 10– 4– 02; 8: 45 am]

BILLING CODE 6717– 01– P ENVIRONMENTAL PROTECTION AGENCY [FRL– 7392– 8]

Gulf of Mexico Program Citizens Advisory Committee Meeting AGENCY: Environmental Protection Agency ( EPA).

ACTION: Notice of meeting.

SUMMARY: Under the Federal Advisory Committee Act (Pub. L. 92– 463), EPA gives notice of a meeting of the Gulf of Mexico Program (GMP) Citizens Advisory Committee (CAC).

DATES: The meeting will be held on Wednesday, November 6, 2002, from 1 p. m. to 5 p. m., and on Thursday, November 7, 2002, from 8: 30 a. m. to 12 p. m.

ADDRESSES: The meeting will be held at the Bay Tower Hotel and Conference Center, 711 Casino Magic Drive, Bay St. Louis, MS 39520 (1– 800– 5– MAGIC– 5)

FOR FURTHER INFORMATION CONTACT: Gloria D. Car, Designated Federal Officer, Gulf of Mexico Program Office, Mail Code EPA/ GMPO, Stennis Space Center, MS 39529– 6000 at (228) 688– 2421.

SUPPLEMENTARY INFORMATION: Proposed agenda is attached. The meeting is open to the public. Dated: September 30, 2002. Gloria D. Car, Designated Federal Officer.

Gulf of Mexico Program— Citizens Advisory Committee Meeting— Bay Towers Hotel and Conference Center, Bay St. Louis, Mississippi, November 6– 7, 2002 Draft Agenda Wednesday, November 6 11: 45– 1: 00 CAC Members Networking Luncheon (at hotel) 1: 00– 1: 20 p. m. Opening Remarks/ Introductions (Jim Kachtick, Chair), Review and approval of November 7– 8, 2001 and June 11– 13, 2002, Meeting Summaries, Jim Kachtick, Chair 1: 20– 1: 45 Chair Report, Jim Kachtick, Chair   Follow up on CAC Action Items 1: 45– 2: 15 GMP Director's Report, Gloria Car, GMPO Associate Director 2: 15– 2: 30 Break 2: 30– 3: 15 Presentation: Dockwatch Update (Jellyfish), Dr. William Graham, Dauphin Island Sea Lab 3: 15– 5: 00 Casino Magic Golf Course Gulf Guardian Award Video Golf Course Tour (tentative) Evening Dinner Sponsored by Hancock County Board of Supervisors— location to be announced Thursday, November 7 7: 30– 8: 30 Continental Breakfast 8: 30– 9: 15 CAC Projects Report, Jennyfer Smith, Battelle   Dockwatch Project   Coastal Bird Trail   FFA Environmental Speech Project   GMP Presentation for CAC Members   CAC Web Page and Status of Bulletin Board 9: 15– 9: 45 Election of Officers 9: 45– 10: 30 Members Roundtable and Participation Reports 10: 30– 10: 45 Break 10: 45– 11: 30 Presentation on the Gulf Restoration Network, Cynthia Sarthou, Gulf Restoration Network 11: 15– 11: 30 Meeting Calendar for 2003 11: 30– 12: 00 Citizens Advisory Committee Wrap up   Discussion and Recommendations 12: 00 Adjourn [FR Doc. 02– 25683 Filed 10– 8– 02; 8: 45 am]

BILLING CODE 6560– 50– P ENVIRONMENTAL PROTECTION AGENCY [OPP– 2002– 0270; FRL– 7276– 7]

Pesticide Product; Registration Application AGENCY: Environmental Protection Agency (EPA). ACTION: Notice.

SUMMARY: This notice announces receipt of an application to register a pesticide product containing a new active ingredient not included in any VerDate 0ct< 02> 2002 19: 03 Oct 08, 2002 Jkt 200001 PO 00000 Frm 00020 Fmt 4703 Sfmt 4703 E:\ FR\ FM\ 09OCN1. SGM 09OCN1 62966 Federal Register / Vol. 67, No. 196 / Wednesday, October 9, 2002 / Notices previously registered products pursuant to the provisions of section 3( c)( 4) of the Federal Insecticide, Fungicide, and Rodenticide Act (FIFRA), as amended. DATES: Written comments, identified by the docket ID number OPP– 2002– 0270, must be received on or before November 8, 2002. ADDRESSES: Comments may be submitted electronically, by mail, or through hand delivery/ courier. Follow the detailed instructions as provided in Unit I. of the SUPPLEMENTARY INFORMATION.

FOR FURTHER INFORMATION CONTACT: Alan Reynolds, Biopesticides and Pollution Prevention Division (7511C), Office of Pesticide Programs, Environmental Protection Agency, 1200 Pennsylvania Ave., NW., Washington, DC 20460– 0001; telephone number: (703) 605– 0515; e mail address: reynolds. alan@ epa. gov.

SUPPLEMENTARY INFORMATION:

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

You may be potentially affected by this action if you are a pesticide manufacturer. Potentially affected entities may include, but are not limited to: Pesticide manufacturers (NAICS 32532) This listing is not intended to be exhaustive, but rather provides a guide for readers regarding entities likely to be affected by this action. Other types of entities not listed in this unit could also be affected. The North American Industrial Classification System (NAICS) codes have been provided to assist you and others in determining whether this action might apply to certain entities. If you have any questions regarding the applicability of this action to a particular entity, consult the person 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 OPP– 2002– 0270. 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 Public Information and Records Integrity Branch (PIRIB), Rm. 119, Crystal Mall #2, 1921 Jefferson Davis Hwy., Arlington, VA. This docket facility is open from 8: 30 a. m. to 4 p. m., Monday through Friday, excluding legal holidays. The docket telephone number is (703) 305– 5805. 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. Once in the system, select `` search, '' then key in the appropriate docket ID number. Certain types of information will not be placed in EPA's Dockets. Information claimed as CBI and other information whose disclosure is restricted by statute, which is not included in the official public docket, will not be available for public viewing in EPA's electronic public docket. EPA's policy is that copyrighted material will not be placed in EPA's electronic public docket but will be available only in printed, paper form in the official public docket. To the extent feasible, publicly available docket materials will be made available in EPA's electronic public docket. When a document is selected from the index list in EPA Dockets, the system will identify whether the document is available for viewing in EPA's electronic public docket. 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. EPA intends to work towards providing electronic access to all of the publicly available docket materials through EPA's electronic public docket. For public commenters, it is important to note that EPA's policy is that public comments, whether submitted electronically or in paper, will be made available for public viewing in EPA's electronic public docket as EPA receives them and without change, unless the comment contains copyrighted material, CBI, or other information whose disclosure is restricted by statute. When EPA identifies a comment containing copyrighted material, EPA will provide a reference to that material in the version of the comment that is placed in EPA's electronic public docket. The entire printed comment, including the copyrighted material, will be available in the public docket. Public comments submitted on computer disks that are mailed or delivered to the docket will be transferred to EPA's electronic public docket. Public comments that are mailed or delivered to the Docket will be scanned and placed in EPA's electronic public docket. Where practical, physical objects will be photographed, and the photograph will be placed in EPA's electronic public docket along with a brief description written by the docket staff.

C. How and To Whom Do I Submit Comments? You may submit comments electronically, by mail, or through hand delivery/ courier. To ensure proper receipt by EPA, identify the appropriate docket ID number in the subject line on the first page of your comment. Please ensure that your comments are submitted within the specified comment period. Comments received after the close of the comment period will be marked `` late. '' EPA is not required to consider these late comments. If you wish to submit CBI or information that is otherwise protected by statute, please follow the instructions in Unit I. D. Do not use EPA Dockets or e mail to submit CBI or information protected by statute. 1. Electronically. If you submit an electronic comment as prescribed in this unit, EPA recommends that you include your name, mailing address, and an email address or other contact information in the body of your comment. Also include this contact information on the outside of any disk or CD ROM you submit, and in any cover letter accompanying the disk or CD ROM. This ensures that you can be identified as the submitter of the comment and allows EPA to contact you in case EPA cannot read your comment due to technical difficulties or needs further information on the substance of your comment. EPA's policy is that EPA will not edit your comment, and any identifying or contact information provided in the body of a comment will be included as part of the comment that is placed in the official public docket, and made available in EPA's electronic public docket. If EPA cannot read your comment due to technical difficulties and cannot contact you for clarification, EPA may not be able to consider your comment. i. EPA Dockets. Your use of EPA's electronic public docket to submit VerDate 0ct< 02> 2002 19: 03 Oct 08, 2002 Jkt 200001 PO 00000 Frm 00021 Fmt 4703 Sfmt 4703 E:\ FR\ FM\ 09OCN1. SGM 09OCN1 62967 Federal Register / Vol. 67, No. 196 / Wednesday, October 9, 2002 / Notices comments to EPA electronically is EPA's preferred method for receiving comments. Go directly to EPA Dockets at http:// www. epa. gov/ edocket, and follow the online instructions for submitting comments. Once in the system, select `` search, '' and then key in docket ID number OPP– 2002– 0270. The system is an `` anonymous access'' system, which means EPA will not know your identity, e mail address, or other contact information unless you provide it in the body of your comment. ii. E mail. Comments may be sent by e mail to opp docket@ epa. gov, Attention: Docket ID Number OPP– 2002– 0270. In contrast to EPA's electronic public docket, EPA's e mail system is not an `` anonymous access'' system. If you send an e mail comment directly to the docket without going through EPA's electronic public docket, EPA's e mail system automatically captures your e mail address. E mail addresses that are automatically captured by EPA's e mail system are included as part of the comment that is placed in the official public docket, and made available in EPA's electronic public docket. iii. Disk or CD ROM. You may submit comments on a disk or CD ROM that you mail to the mailing address identified in Unit I. C. 2. These electronic submissions will be accepted in WordPerfect or ASCII file format. Avoid the use of special characters and any form of encryption. 2. By mail. Send your comments to: Public Information and Records Integrity Branch (PIRIB), Office of Pesticide Programs (OPP), Environmental Protection Agency (7502C), 1200 Pennsylvania Ave., NW., Washington, DC 20460– 0001, Attention: Docket ID Number OPP– 2002– 0270. 3. By hand delivery or courier. Deliver your comments to: Public Information and Records Integrity Branch (PIRIB), Office of Pesticide Programs (OPP), Environmental Protection Agency, Rm. 119, Crystal Mall #2, 1921 Jefferson Davis Hwy., Arlington, VA, Attention: Docket ID Number OPP– 2002– 0270. Such deliveries are only accepted during the docket's normal hours of operation as identified in Unit I. B. 1.

D. How Should I Submit CBI To the Agency? Do not submit information that you consider to be CBI electronically through EPA's electronic public docket or by e mail. You may claim information that you submit to EPA as CBI by marking any part or all of that information as CBI (if you submit CBI on disk or CD ROM, mark the outside of the disk or CD ROM as CBI and then identify electronically within the disk or CD ROM the specific information that is CBI). Information so marked will not be disclosed except in accordance with procedures set forth in 40 CFR part 2. In addition to one complete version of the comment that includes any information claimed as CBI, a copy of the comment that does not contain the information claimed as CBI must be submitted for inclusion in the public docket and EPA's electronic public docket. If you submit the copy that does not contain CBI on disk or CD ROM, mark the outside of the disk or CD ROM clearly that it does not contain CBI. Information not marked as CBI will be included in the public docket and EPA's electronic public docket without prior notice. If you have any questions about CBI or the procedures for claiming CBI, please consult the person listed under FOR FURTHER INFORMATION CONTACT.

E. What Should I Consider as I Prepare My Comments for EPA?

You may find the following suggestions helpful for preparing your comments: 1. Explain your views as clearly as possible. 2. Describe any assumptions that you used. 3. Provide copies of any technical information and/ or data you used that support your views. 4. If you estimate potential burden or costs, explain how you arrived at the estimate that you provide. 5. Provide specific examples to illustrate your concerns. 6. Offer alternative ways to improve the registration activity. 7. Make sure to submit your comments by the deadline in this notice. 8. To ensure proper receipt by EPA, be sure to identify the docket ID number assigned to this action in the subject line on the first page of your response. You may also provide the name, date, and Federal Register citation.

II. Registration Application EPA received an application as follows to register a pesticide product containing an active ingredient not included in any previously registered products pursuant to the provision of section 3( c)( 4) of FIFRA. Notice of receipt of this application does not imply a decision by the Agency on the application.

Product Containing an Active Ingredient Not Included in any Previously Registered Products File symbol: 74411– R. Applicant: Insect Biotechnology, Inc., 100 Capitola Drive, Suite 307, Durham, NC 27713. Product name: Technical Trypsin Modulating Oostatic Factor (TMOF). Product type: Insecticide. Active ingredient: Trypsin Modulating Oostatic Factor at 100%. Proposed classification/ Use: Manufacturing use product for formulation into insecticidal products for mosquito control.

List of Subjects Environmental protection, Pesticides and pest.

Dated: September 30, 2002. Janet L. Andersen, Director, Biopesticides and Pollution Prevention Division, Office of Pesticide Programs. [FR Doc. 02– 25684 Filed 10– 8– 02; 8: 45 am]

BILLING CODE 6560– 50– S ENVIRONMENTAL PROTECTION AGENCY [OPP– 2002– 0244; FRL– 7198–– 2]

Notice of Filing a Pesticide Petition to Establish a Tolerance for a Certain Pesticide Chemical in or on Food AGENCY: Environmental Protection Agency (EPA). ACTION: Notice.

SUMMARY: This notice announces the initial filing of a pesticide petition proposing the establishment of regulations for residues of a certain pesticide chemical in or on various food commodities. DATES: Comments, identified by docket ID number OPP– 2002– 0244, must be received on or before November 8, 2002. ADDRESSES: Comments may be submitted electronically, by mail, or through hand delivery/ courier. Follow the detailed instructions as provided in Unit I. of the SUPPLEMENTARY INFORMATION. To ensure proper receipt by EPA, it is imperative that you identify docket ID number OPP– 2002– 0244 in the subject line on the first page of your response. FOR FURTHER INFORMATION CONTACT: By mail: Leonard Cole, Biopesticide and Pollution Prevention Division, Office of Pesticide Programs, (7511C) Environmental Protection Agency, 1200 Pennsylvania Ave., NW., Washington, DC 20460; telephone number: (703) 305– 5412; e mail address: cole. leonard@ epa. gov.

SUPPLEMENTARY INFORMATION:

I. General Information A. Does this Action Apply to Me? You may be affected by this action if you are an agricultural producer, food VerDate 0ct< 02> 2002 19: 03 Oct 08, 2002 Jkt 200001 PO 00000 Frm 00022 Fmt 4703 Sfmt 4703 E:\ FR\ FM\ 09OCN1. SGM 09OCN1


[Federal Register: November 10, 2005 (Volume 70, Number 217)]
[Notices]
[Page 68417]
[DOCID:fr10no05-63]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. RP06-60-000]

Columbia Gas Transmission Corporation; Notice of Filing

November 2, 2005.
    Take notice that on October 28, 2005, Columbia Gas Transmission
Corporation (Columbia) tendered for filing the following Service
Agreement for consideration and approval:

    FTS Service Agreement No. 85207 between Columbia Gas
Transmission Corporation and Columbia Gas of Kentucky, Inc., Dated
October 27, 2005

    In addition, Columbia tendered for filing as part of its FERC Gas
Tariff, Second Revised Volume No. 1, Twelfth Revised Sheet No. 500B,
with a proposed effective date of November 1, 2005.
    Any person desiring to intervene or to protest this filing must
file in accordance with Rules 211 and 214 of the Commission's Rules of
Practice and Procedure (18 CFR 385.211 and 385.214). Protests will be
considered by the Commission in determining the appropriate action to
be taken, but will not serve to make protestants parties to the
proceeding. Any person wishing to become a party must file a notice of
intervention or motion to intervene, as appropriate. Such notices,
motions, or protests must be filed in accordance with the provisions of
Section 154.210 of the Commission's regulations (18 CFR 154.210).
Anyone filing an intervention or protest must serve a copy of that
document on the Applicant. Anyone filing an intervention or protest on
or before the intervention or protest date need not serve motions to
intervene or protests on persons other than the Applicant.
    The Commission encourages electronic submission of protests and
interventions in lieu of paper using the ``eFiling'' link at http://www.ferc.gov.
 Persons unable to file electronically should submit an

original and 14 copies of the protest or intervention to the Federal
Energy Regulatory Commission, 888 First Street, NE., Washington, DC
20426.
    This filing is accessible on-line at http://www.ferc.gov, using the

``eLibrary'' link and is available for review in the Commission's
Public Reference Room in Washington, DC. There is an ``eSubscription''
link on the Web site that enables subscribers to receive e-mail
notification when a document is added to a subscribed docket(s). For
assistance with any FERC Online service, please e-mail
<EMAIL_ADDRESS>or call<PHONE_NUMBER> (toll free). For

TTY, call<PHONE_NUMBER>.

Magalie R. Salas,
Secretary.
[FR Doc. E5-6196 Filed 11-9-05; 8:45 am]

BILLING CODE 6717-01-P


  From: Lydia Wegman/RTP/USEPA/US  To: "King, Heidi R."<EMAIL_ADDRESS> Cc: Deirdre Murphy/RTP/USEPA/US@EPA, Karen Martin/RTP/USEPA/US@EPA  Date: 01/18/2011 11:07 AM  Subject: RE: Checking in on the CO NAAQS

Thanks Heidi.  I'm happy to schedule some time to tomorrow to talk about the comments, if we receive them early enough today that we can consider them.   I want to make sure we have enough time to discuss the internally before meeting with you.  We can aim for a meeting later tomorrow afternoon if you think we'll receive the comments early this afternoon.  Thanks a lot.


[Federal Register Volume 86, Number 181 (Wednesday, September 22, 2021)]
[Notices]
[Page 52669]
[FR Doc No: 2021-20487]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. TX21-6-000]

EnerSmart Chula Vista BESS LLC; Notice of Filing

    Take notice that on September 14, 2021, pursuant to section 211 of
the Federal Power Act,\1\ EnerSmart Chula Vista BESS LLC (EnerSmart
Chula Vista) filed an application requesting that the Federal Energy
Regulatory Commission (Commission) issue an order requiring San Diego
Gas & Electric Company (SDG&E) to provide interconnection and
transmission services for delivery of the output from EnerSmart Chula
Vista's two (2) 3 MW battery energy storage system across SDG&E
Participating Transmission Owner's Interconnection Facilities to Points
of Interconnection with the California Independent System Operator
Corporation Controlled Grid, including Network Upgrades to be
constructed to accommodate service to EnerSmart Chula Vista.
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    \1\ 16 U.S.C. 824j (2018).
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    Any person desiring to intervene or to protest this filing must
file in accordance with Rules 211 and 214 of the Commission's Rules of
Practice and Procedure (18 CFR 385.211 and 385.214). Protests will be
considered by the Commission in determining the appropriate action to
be taken, but will not serve to make protestants parties to the
proceeding. Any person wishing to become a party must file a notice of
intervention or motion to intervene, as appropriate. Such notices,
motions, or protests must be filed on or before the comment date.
Anyone filing a motion to intervene or protest must serve a copy of
that document on the Applicant. On or before the comment date, it is
not necessary to serve motions to intervene or protests on persons
other than the Applicant.
    In addition to publishing the full text of this document in the
Federal Register, the Commission provides all interested persons an
opportunity to view and/or print the contents of this document via the
internet through the Commission's Home Page (http://ferc.gov) using the
``eLibrary'' link. Enter the docket number excluding the last three
digits in the docket number field to access the document. At this time,
the Commission has suspended access to the Commission's Public
Reference Room, due to the proclamation declaring a National Emergency
concerning the Novel Coronavirus Disease (COVID-19), issued by the
President on March 13, 2020. For assistance, contact FERC at
<EMAIL_ADDRESS>or call toll-free,<PHONE_NUMBER> or TYY,
(202) 502-8659.
    The Commission strongly encourages electronic filings of comments,
protests and interventions in lieu of paper using the ``eFiling'' link
at http://www.ferc.gov. Persons unable to file electronically may mail
similar pleadings to the Federal Energy Regulatory Commission, 888
First Street NE, Washington, DC 20426. Hand delivered submissions in
docketed proceedings should be delivered to Health and Human Services,
12225 Wilkins Avenue, Rockville, Maryland 20852.
    Comment Date: 5:00 p.m. Eastern Time on October 5, 2021.

    Dated: September 16, 2021.
Kimberly D. Bose,
Secretary.
[FR Doc. 2021-20487 Filed 9-21-21; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register Volume 76, Number 151 (Friday, August 5, 2011)]
[Rules and Regulations]
[Pages 47430-47435]
[FR Doc No: 2011-19433]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-0388; Directorate Identifier 2010-NM-004-AD;
Amendment 39-16761; AD 2011-16-03]
RIN 2120-AA64

Airworthiness Directives; Airbus Model A300 B4-600, A300 B4-600R,
and A300 F4-600R Series Airplanes, and Model A300 C4-605R Variant F
Airplanes (Collectively Called Model A300-600 Series Airplanes); Model
A310 Series Airplanes; Model A318 Series Airplanes; Model A319 Series
Airplanes; Model A320-211, -212, -214, -231, -232, and -233 Airplanes;
Model A321 Series Airplanes; Model A330-200 and A330-300 Series
Airplanes; and Model A340-200, A340-300, A340-500, and A340-600 Series
Airplanes

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

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. This AD results from mandatory continuing
airworthiness information (MCAI) originated by an aviation authority of
another country to identify and correct an unsafe condition on an
aviation product. For Model A310 and A300-600 series airplanes, the
MCAI describes the unsafe condition as:

    Hamilton Sundstrand (HS), the manufacturer of the RAT [ram air
turbine], reported the failure during a wind tunnel test of a
balance weight fastening screw on the RAT turbine cover. After
investigation, it has been discovered that a batch of screws, which
are used to attach the balance washers of the HS RAT Turbine
Assembly, has not been subject to the correct heat treatment and are
consequently exposed to potential fracture.
    This condition, if not corrected, might lead to the ejection of
screw heads and consequently to the detachment of the associated
balance washers. The loss of balance washers could increase RAT
vibrations, which might lead to a possible detachment of RAT parts
and consequent loss of RAT functionality. The loss of the RAT, in
combination with a total engine flame out, could result in loss of
control of the aeroplane.
* * * * *
    For Model A318, A319, A320, and A321 series airplanes, the MCAI
describes the unsafe condition as:

    Hamilton Sundstrand (HS) reported the failure of a balance
weight fastening screw on the RAT turbine cover during a wind tunnel
test. After investigation, it has been discovered that a batch of
screws, used to attach the balance washers of the RAT Turbine
assembly, has not received the correct heat treatment, making them
more subject to a potential failure.
    This condition, if left uncorrected, could lead to the ejection
of screw heads and detachment of the associated balance washers. The
loss of balance washers would increase RAT vibrations, which could
lead to a possible detachment of RAT parts and loss of RAT
functionality. The loss of the RAT, in combination with a double
engine failure, or a total loss of normal electrical power
generation, could result in loss of control of the aeroplane.
* * * * *
    For Model A330 and A340 series airplanes, the MCAI describes the
unsafe condition as:

    Hamilton Sundstrand (HS), the manufacturer of the RAT, reported
the failure of a balance weight fastening screw on the RAT cover
during a wind tunnel test. After investigation, it has been
discovered that a batch of screws, which are used to attach the
balance washers of the HS RAT turbine lower gear box assembly, has
not been subject to the correct heat treatment and the screws are
consequently exposed to potential fracture.
    This condition, if not corrected, might lead to the ejection of
screw heads and consequently to the detachment of the associated
balance washers. The loss of balance washers could increase RAT
vibrations, which might lead to a possible detachment of RAT parts,
and thus to damage to the aeroplane and risk of injury to persons on
the ground.
* * * * *
    We are issuing this AD to require actions to correct the unsafe
condition on these products.

DATES: This AD becomes effective September 9, 2011.
    The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of September 9,
2011.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC.

FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Branch, ANM-116,

Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on May 4, 2011 (76 FR
25259). That NPRM proposed to correct an unsafe condition for the
specified products.
    The MCAI for Model A300-600 and A310 series airplanes states:

    Hamilton Sundstrand (HS), the manufacturer of the RAT [ram air
turbine], reported the failure during a wind tunnel test of a
balance weight fastening screw on the RAT turbine cover. After
investigation, it has been discovered that a batch of screws, which
are used to attach the balance washers of the HS RAT Turbine
Assembly, has not been subject to the correct heat treatment and are
consequently exposed to potential fracture.
    This condition, if not corrected, might lead to the ejection of
screw heads and consequently to the detachment of the associated
balance washers. The loss of balance washers could increase RAT
vibrations, which might lead to a possible detachment of RAT parts
and consequent loss of RAT functionality. The loss of the RAT, in
combination with a total engine flame out, could result in loss of
control of the aeroplane.
    For the reasons described above, this AD requires the
identification of the affected RAT turbine assemblies and
replacement of all balance weight screws or, in case balance washer
detachment is found, replacement of the RAT turbine assembly.

    The MCAI for Model A318, A319, A320, and A321 series airplanes
states:

    Hamilton Sundstrand (HS) reported the failure of a balance
weight fastening screw on the RAT turbine cover during a wind tunnel
test. After investigation, it has been discovered that a batch of
screws, used to attach the balance washers of the RAT Turbine
assembly, has not received the correct heat treatment, making them
more subject to a potential failure.
    This condition, if left uncorrected, could lead to the ejection
of screw heads and detachment of the associated balance washers. The
loss of balance washers would increase RAT vibrations, which could
lead to a possible detachment of RAT parts and loss of RAT
functionality. The loss of the RAT, in combination with a double
engine failure, or a total loss of normal electrical power
generation, could result in loss of control of the aeroplane.
    For the reasons described above, EASA AD 2009-0259 was issued in
December 2009 to require the replacement of all balance weight
screws on the affected RAT turbine assemblies, or replacement of the
RAT, if any balancing washer was found missing.
    This AD retains some of the requirements of AD 2009-0259, which
is superseded, and corrects its applicability by adding Airbus model
A320-215 and A320-216 aeroplanes which were inadvertently omitted.
Also, this AD requires the replacement of the set of balancing
weights screws before the next operational or functional check of
the RAT assembly.

    The MCAI for Model A330 and A340 series airplanes states:

    Hamilton Sundstrand (HS), the manufacturer of the RAT, reported
the failure of a balance weight fastening screw on the RAT cover
during a wind tunnel test. After investigation, it has been
discovered that a batch of screws, which are used to attach the
balance washers of the HS RAT turbine lower gear box assembly, has
not been subject to the correct heat treatment and the screws are
consequently exposed to potential fracture.
    This condition, if not corrected, might lead to the ejection of
screw heads and consequently to the detachment of the associated
balance washers. The loss of balance washers could increase RAT
vibrations, which might lead to a possible detachment of RAT parts,
and thus to damage to the aeroplane and risk of injury to persons on
the ground.
    For the reasons described above, this AD requires the
identification of the affected RAT turbine lower gear box assemblies
and replacement of all balance screws or, in case balance washer
detachment is found, replacement of the RAT turbine lower gear box
assembly. * * *

    You may obtain further information by examining the MCAI in the AD
docket.

Comments

    We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.

Conclusion

    We reviewed the available data and determined that air safety and
the public interest require adopting the AD as proposed.

Differences Between This AD and the MCAI or Service Information

    We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable. In making these
changes, we do not intend to differ substantively from the information
provided in the MCAI and related service information.
    We might also have required different actions in this AD from those
in the MCAI in order to follow our FAA policies. Any such differences
are highlighted in a NOTE within the AD.

Costs of Compliance

    Based on the service information, we estimate that this AD will
affect about 1,004 products of U.S. registry. We also estimate that it
will take about 2 work-hours per product to comply with the basic
requirements of this AD. The average labor rate is $85 per work-hour.
Required parts will cost about $100 per product. Where the service
information lists required parts costs that are covered under warranty,
we have assumed that there will be no charge for these costs. As we do
not control warranty coverage for affected parties, some parties may
incur costs higher than estimated here. Based on these figures, we
estimate the cost of the AD on U.S. operators to be $271,080, or $270
per product.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
    We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.

Regulatory Findings

    We determined that this 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 this AD:
    1. Is not a ''significant regulatory action'' under Executive Order
12866;
    2. Is not a ''significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); 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.

Examining the AD Docket

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

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new AD:

2011-16-03 Airbus: Amendment 39-16761. Docket No. FAA-2011-0388;
Directorate Identifier 2010-NM-004-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective
September 9, 2011.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to the Airbus airplanes listed in paragraphs
(c)(1), (c)(2), (c)(3), (c)(4), and (c)(5) of this AD, certificated
in any category.
    (1) Airbus Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R,
B4-622R, F4-605R, F4-622R, and C4-605R Variant F airplanes; and
Model A310-203, -204, -221, -222, -304, -322, -324, and -325
airplanes; all certified models, all manufacturer serial numbers, if
equipped with a Hamilton Sundstrand ram air turbine (RAT) turbine
assembly, as identified by part number (P/N) in Hamilton Sundstrand
Service Bulletin 730816-29-15, dated August 4, 2009 (for Model A310
airplanes), and Hamilton Sundstrand Service Bulletin 732365-29-7,
dated August 4, 2009 (for Model A300-600 series airplanes); or
equipped with a Hamilton Sundstrand RAT turbine lower gear box
assembly on which the part number cannot be determined.
    (2) Airbus Model A318-111, -112, -121, and -122 airplanes; Model
A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes;
Model A320-211, -212, -214, -231, -232, and -233 airplanes; and
Model A321-111, -112, -131, -211, -212, -213, -231, and -232
airplanes; all manufacturer serial numbers, if equipped with a
Hamilton Sundstrand RAT turbine assembly Model ERPS08M, as
identified by part number in Hamilton Sundstrand Service Bulletin
ERPS08M-29-8, dated June 17, 2009; or equipped with a Hamilton
Sundstrand RAT turbine lower gear box assembly on which the part
number cannot be determined.
    (3) Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -
303, -321, -322, -323, -341, -342, and -343 airplanes; all
manufacturer serial numbers, if equipped with a Hamilton Sundstrand
RAT turbine lower gearbox assembly, as identified by part number in
Hamilton Sundstrand Service Bulletin ERPS06G-29-6, dated July 20,
2009; or equipped with a Hamilton Sundstrand RAT turbine lower gear
box assembly on which the part number cannot be determined.
    (4) Model A340-211, -212, -213, -311, -312, and -313 airplanes;
all manufacturer serial numbers, if equipped with a Hamilton
Sundstrand RAT turbine lower gearbox assembly, as identified by part
number in Hamilton Sundstrand Service Bulletin ERPS06G-29-6, dated
July 20, 2009; or equipped with a Hamilton Sundstrand RAT turbine
lower gear box assembly on which the part number cannot be
determined.
    (5) Model A340-541 and -642 airplanes, all manufacturer serial
numbers, if equipped with a Hamilton Sundstrand RAT turbine lower
gearbox assembly, as identified by part number in Hamilton
Sundstrand Service Bulletin ERPS33G-29-1, dated July 20, 2009; or
equipped with a Hamilton Sundstrand RAT turbine lower gear box
assembly on which the part number cannot be determined.

Subject

    (d) Air Transport Association (ATA) of America Code 29:
Hydraulic power.

Reason

    (e) For Model A310 and A300-600 series airplanes, the MCAI
describes the unsafe condition as:

    Hamilton Sundstrand (HS), the manufacturer of the RAT, reported
the failure during a wind tunnel test of a balance weight fastening
screw on the RAT turbine cover. After investigation, it has been
discovered that a batch of screws, which are used to attach the
balance washers of the HS RAT Turbine Assembly, has not been subject
to the correct heat treatment and are consequently exposed to
potential fracture.
    This condition, if not corrected, might lead to the ejection of
screw heads and consequently to the detachment of the associated
balance washers. The loss of balance washers could increase RAT
vibrations, which might lead to a possible detachment of RAT parts
and consequent loss of RAT functionality. The loss of the RAT, in
combination with a total engine flame out, could result in loss of
control of the aeroplane.
* * * * *
    For Model A318, A319, A320, and A321 series airplanes, the MCAI
describes the unsafe condition as:

    Hamilton Sundstrand (HS) reported the failure of a balance
weight fastening screw on the RAT turbine cover during a wind tunnel
test. After investigation, it has been discovered that a batch of
screws, used to attach the balance washers of the RAT Turbine
assembly, has not received the correct heat treatment, making them
more subject to a potential failure.
    This condition, if left uncorrected, could lead to the ejection
of screw heads and detachment of the associated balance washers. The
loss of balance washers would increase RAT vibrations, which could
lead to a possible detachment of RAT parts and loss of RAT
functionality. The loss of the RAT, in combination with a double
engine failure, or a total loss of normal electrical power
generation, could result in loss of control of the aeroplane.
* * * * *
    For Model A330 and A340 series airplanes, the MCAI describes the
unsafe condition as:

    Hamilton Sundstrand (HS), the manufacturer of the RAT, reported
the failure of a balance weight fastening screw on the RAT cover
during a wind tunnel test. After investigation, it has been
discovered that a batch of screws, which are used to attach the
balance washers of the HS RAT turbine lower gear box assembly, has
not been subject to the correct heat treatment and the screws are
consequently exposed to potential fracture.
    This condition, if not corrected, might lead to the ejection of
screw heads and consequently to the detachment of the associated
balance washers. The loss of balance washers could increase RAT
vibrations, which might lead to a possible detachment of RAT parts,
and thus to damage to the aeroplane and risk of injury to persons on
the ground.
* * * * *

Compliance

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

Actions

    (g) At the applicable time specified in paragraph (g)(1),
(g)(2), or (g)(3) of this AD: Inspect to determine the part number
and serial number of the RAT turbine lower gear box assembly, in
accordance with the applicable Airbus all operator telex (AOT)
identified in table 1 of this AD. If the RAT turbine lower gear box
assembly has a part number and a serial number that are not listed
in the applicable Hamilton Sundstrand service bulletin identified in
table 2 of this AD, no further action is required by this AD, except
as required by paragraph (k) of this AD. A review of airplane
maintenance

records is acceptable in lieu of this inspection if the part and
serial numbers of the RAT turbine lower gear box assembly can be
conclusively determined from that review.

                                              Table 1--Airbus AOTs
----------------------------------------------------------------------------------------------------------------
                  Model                              Document                              Date
----------------------------------------------------------------------------------------------------------------
Model A300-600 series airplanes..........  Airbus AOT A300-29A6062.....  September 1, 2009.
Model A310 series airplanes..............  Airbus AOT A310-29A2098.....  September 1, 2009.
Model A318 series airplanes; Model A319    Airbus AOT A320-29A1150.....  June 24, 2009.
 series airplanes; Model A320-211, -212, -
 214, -231, -232, and -233 airplanes;
 Model A321 series airplanes.
Model A330-200 and A330-300 series         Airbus AOT A330-29A3110.....  September 1, 2009.
 airplanes.
Model A340-200 and A340n-300 series        Airbus AOT A340-29A4085.....  September 1, 2009.
 airplanes.
Model A340-500 and A340-600 series         Airbus AOT A340-500/600-      September 1, 2009.
 airplanes.                                 29A5015.
----------------------------------------------------------------------------------------------------------------

    (1) For airplanes identified in paragraph (c)(1) of this AD:
Before the next RAT spin test, or within 1,500 flight hours or 9
months after the effective date of this AD, whichever occurs first.
    (2) For airplanes identified in paragraph (c)(2) of this AD:
Before the next RAT spin test, or within 3,000 flight hours or 12
months after the effective date of this AD, whichever occurs first.
    (3) For airplanes identified in paragraph (c)(3), (c)(4), and
(c)(5) of this AD: Before the next RAT spin test, or within 3,000
flight hours or 8 months after the effective date of this AD,
whichever occurs first.
    (h) If, during the inspection required by paragraph (g) of this
AD, the RAT turbine lower gear box assembly has a part number and a
serial number identified in the applicable Hamilton Sundstrand
service bulletin specified in table 2 of this AD; or if the part
number or serial number of the RAT turbine lower gear box assembly
cannot be determined: Before further flight, inspect the RAT turbine
lower gear box assembly to determine if the nameplate is identified
with the applicable symbol specified in table 3 of this AD, in
accordance with the applicable Airbus AOT specified in table 1 of
this AD. If the RAT turbine lower gear box assembly nameplate has
the applicable symbol that is identified in table 3 of this AD, no
further action is required by this AD except as required by
paragraph (k) of this AD. A review of airplane maintenance records
is acceptable in lieu of this inspection if the symbol identified on
the nameplate can be conclusively determined from that review.

                            Table 2--Applicable Hamilton Sundstrand Service Bulletins
----------------------------------------------------------------------------------------------------------------
                  Model                              Document                              Date
----------------------------------------------------------------------------------------------------------------
Model A300-600 series airplanes..........  Hamilton Sundstrand Service   August 4, 2009.
                                            Bulletin 732365-29-7.
Model A310 series airplanes..............  Hamilton Sundstrand Service   August 4, 2009.
                                            Bulletin 730816-29-15.
Model A318 series airplanes; Model A319    Hamilton Sundstrand Service   June 17, 2009.
 series airplanes; Model A320-211, -212, -  Bulletin ERPS08M-29-8.
 214, -231, -232, and -233 airplanes;
 Model A321 series airplanes.
Model A330-200 and A330-300 series         Hamilton Sundstrand Service   July 20, 2009.
 airplanes and Model A340-200 and A340-     Bulletin ERPS06G-29-6.
 300 series airplanes.
Model A340-500 and A340-600 series         Hamilton Sundstrand Service   July 20, 2009.
 airplanes.                                 Bulletin ERPS33G-29-1.
----------------------------------------------------------------------------------------------------------------

                    Table 3--Nameplate Identification
------------------------------------------------------------------------
                         Model                               Symbol
------------------------------------------------------------------------
Model A300-600 series airplanes.......................              29-7
Model A310 series airplanes...........................             29-15
Model A318 series airplanes; Model A319 series                      29-8
 airplanes; Model A320-211, -212, -214, -231, -232,
 and -233 airplanes; Model A321 series airplanes......
Model A330-200 and A330-300 series airplanes..........              29-6
Model A340-200 and A340-300 series airplanes..........              29-6
Model A340-500 and A340-600 series airplanes..........              29-1
------------------------------------------------------------------------

    (i) If, during the inspection required by paragraph (h) of this
AD, the RAT turbine lower gear box assembly does not have the
applicable symbol specified in table 3 of this AD: Before further
flight, do a general visual inspection for the missing and fractured
balance screws and for missing washers in accordance with the
applicable Airbus AOT specified in table 1 of this AD.
    (1) If all balance screws are fitted on the turbine and are not
fractured or missing, at the applicable time specified in paragraph
(i)(1)(i), (i)(1)(ii), or (i)(1)(iii) of this AD: Replace the RAT
turbine lower gear box assembly with a new or serviceable RAT
turbine lower gear box assembly, or replace all balance screws on
the RAT turbine lower gear box assembly with new or serviceable
balance screws, in accordance with the applicable Airbus AOT
specified in table 1 of this AD.
    (i) For airplanes identified in paragraph (c)(1) of this AD:
Within 1,500 flight hours or 9 months after the effective date of
this AD, whichever occurs first.
    (ii) For airplanes identified in paragraph (c)(2) of this AD:
Within 3,000 flight hours or 12 months after the effective date of
this AD, whichever occurs first.
    (iii) For airplanes identified in paragraphs (c)(3), (c)(4), and
(c)(5) of this AD: Within 3,000 flight hours or 8 months after the
effective date of this AD, whichever occurs first.
    (2) If one or more screws are fractured but the associated
balance washers are still fitted on the RAT turbine lower gear box
assembly, before further flight, do the actions specified in
paragraph (i)(2)(i) or (i)(2)(ii) of this AD, in accordance with the
applicable Airbus AOT specified in table 1 of this AD.
    (i) Replace the RAT turbine lower gear box assembly with a new
or serviceable RAT turbine lower gear box assembly.
    (ii) Replace all balance screws on the RAT turbine lower gear
box assembly with new or serviceable balance screws, including
replacing any missing washers.

    (3) If one or more screws are fractured and any balance washer
is missing, before further flight, replace the RAT turbine lower
gear box assembly with new or serviceable RAT turbine lower gear box
assembly, in accordance with the applicable Airbus AOT specified in
table 1 of this AD.

Reporting Requirement

    (j) At the applicable time specified in paragraph (j)(1) or
(j)(2) of this AD, submit a report of the findings (both positive
and negative) of the inspection required by paragraph (i) of this AD
to Airbus, as specified in Paragraph 7 of the applicable AOT
specified in table 1 of this AD. The report must include the
inspection results, a description of any discrepancies found, the
airplane serial number, and the number of landings and flight hours
on the airplane.
    (1) If the inspection was done on or after the effective date of
this AD: Submit the report within 30 days after the inspection.
    (2) If the inspection was done before the effective date of this
AD: Submit the report within 30 days after the effective date of
this AD.

Parts Installation

    (k) As of the effective date of this AD, no person may install,
on any airplane, a RAT turbine lower gear box assembly, as
identified by part number in the applicable Hamilton Sundstrand
service bulletin specified in table 2 of this AD, unless it has been
inspected and all applicable corrective actions have been done, in
accordance with the requirements of this AD.

FAA AD Differences

    Note 1: This AD differs from the MCAI and/or service information
as follows: No differences.

Other FAA AD Provisions

    (l) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
has the authority to approve AMOCs for this AD, if requested using
the procedures found in 14 CFR 39.19. In accordance with 14 CFR
39.19, send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the International Branch, send it to Attn: Dan Rodina,
Aerospace Engineer, International Branch, ANM-116, Transport
Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington
98057-3356; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>. Before
using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
local flight standards district office/certificate holding district
office. The AMOC approval letter must specifically reference this
AD.
    (2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
    (3) Reporting Requirements: A Federal agency may not conduct or
sponsor, and a person is not required to respond to, nor shall a
person be subject to a penalty for failure to comply with a
collection of information subject to the requirements of the
Paperwork Reduction Act unless that collection of information
displays a current valid OMB Control Number. The OMB Control Number
for this information collection is 2120-0056. Public reporting for
this collection of information is estimated to be approximately 5
minutes per response, including the time for reviewing instructions,
completing and reviewing the collection of information. All
responses to this collection of information are mandatory. Comments
concerning the accuracy of this burden and suggestions for reducing
the burden should be directed to the FAA at: 800 Independence Ave.,
SW., Washington, DC 20591, Attn: Information Collection Clearance
Officer, AES-200.

Related Information

    (m) Refer to the applicable MCAI European Aviation Safety Agency
(EASA) AD specified in table 4 of this AD, the Airbus AOTs specified
in table 1 of this AD, and the Hamilton Sundstrand service bulletins
specified in table 2 of this AD, for related information.

                            Table 4--EASA ADs
------------------------------------------------------------------------
          For model--               EASA AD--             Dated--
------------------------------------------------------------------------
A300-600 and A310 series               2009-0258  December 10, 2009.
 airplanes.
A318, A319, A320, and A321             2010-0120  June 21, 2010.
 series airplanes.
A330 and A340 series airplanes         2009-0260  December 10, 2009
                                                   (corrected December
                                                   14, 2009).
------------------------------------------------------------------------

Material Incorporated by Reference

    (n) You must use the service information contained in table 5 of
this AD, as applicable, to do the actions required by this AD,
unless the AD specifies otherwise.

               Table 5--Material Incorporated by Reference
------------------------------------------------------------------------
              Document                               Date
------------------------------------------------------------------------
Airbus All Operator Telex A300-       September 1, 2009.
 29A6062.
Airbus All Operator Telex A310-       September 1, 2009.
 29A2098.
Airbus All Operator Telex A320-       June 24, 2009.
 29A1150.
Airbus All Operator Telex A330-       September 1, 2009.
 29A3110.
Airbus All Operator Telex A340-       September 1, 2009.
 29A4085.
Airbus All Operator Telex A340-500/   September 1, 2009.
 600-29A5015.
Hamilton Sundstrand Service Bulletin  August 4, 2009.
 732365-29-7.
Hamilton Sundstrand Service Bulletin  August 4, 2009.
 730816-29-15.
Hamilton Sundstrand Service Bulletin  June 17, 2009.
 ERPS08M-29-8.
Hamilton Sundstrand Service Bulletin  July 20, 2009.
 ERPS06G-29-6.
Hamilton Sundstrand Service Bulletin  July 20, 2009.
 ERPS33G-29-1.
------------------------------------------------------------------------

    (1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
    (2) For Airbus service information identified in this AD,
contact the appropriate office listed below.
    (i) For Model A300-600 and A310 series airplanes: Airbus SAS--
EAW (Airworthiness Office), 1 Rond Point Maurice Bellonte, 31707
Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93
44 51; e-mail<EMAIL_ADDRESS>Internet http://www.airbus.com.
    (ii) For Model A318, A319, A320, and A321 series airplanes:
Airbus, Airworthiness

Office--EAS, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex,
France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; e-mail:
<EMAIL_ADDRESS>Internet http://www.airbus.com.
    (iii) For Model A330 and A340 series airplanes: Airbus SAS--
Airworthiness Office--EAL, 1 Rond Point Maurice Bellonte, 31707
Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93
45 80; e-mail<EMAIL_ADDRESS>Internet http://www.airbus.com.
    (3) For Hamilton Sundstrand service information identified in
this AD, contact Hamilton Sundstrand, Technical Publications, Mail
Stop 302-9, 4747 Harrison Avenue, P.O. Box 7002, Rockford, Illinois
61125-7002; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>; e-mail
<EMAIL_ADDRESS>Internet http://www.hamiltonsundstrand.com.
    (4) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the availability of this material at
the FAA, call<PHONE_NUMBER>.
    (5) You may also review copies of the service information that
is incorporated by reference at the National Archives and Records
Administration (NARA). For information on the availability of this
material at NARA, call<PHONE_NUMBER>, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

    Issued in Renton, Washington, on July 20, 2011.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-19433 Filed 8-4-11; 8:45 am]
BILLING CODE 4910-13-P


Year State Species Metric TonsPounds $ 1980 Delaware CRAB, BLU 968.1 2,134,300 723,601 1980 Delaware CRAB, BLU 11.5 25,400 48,064 1980 New JerseyCRAB, BLU 855.2 1,885,300 778,134 1980 New JerseyCRAB, BLU 7.1 15,700 9,213 1980 New York CRAB, BLU 90 198,400 90,804 1981 Delaware CRAB, BLU 442.5 975,500 251,262 1981 Delaware CRAB, BLU 25.3 55,800 80,381 1981 New JerseyCRAB, BLU 698.3 1,539,500 560,885 1981 New JerseyCRAB, BLU 21.6 47,700 49,544 1981 New York CRAB, BLU 14.9 32,900 14,145 1982 Delaware CRAB, BLU 350.9 773,500 284,184 1982 Delaware CRAB, BLU 6.2 13,700 29,613 1982 New JerseyCRAB, BLU 359.5 792,500 274,485 1982 New JerseyCRAB, BLU 4.4 9,800 11,402 1982 New York CRAB, BLU 20.8 45,800 23,839 1983 Delaware CRAB, BLU 532.8 1,174,600 448,637 1983 Delaware CRAB, BLU 5.3 11,600 19,548 1983 New JerseyCRAB, BLU 535.3 1,180,100 518,782 1983 New JerseyCRAB, BLU 8 17,600 25,120 1983 New York CRAB, BLU 60.4 133,100 58,474 1984 Delaware CRAB, BLU 497.4 1,096,500 434,992 1984 Delaware CRAB, BLU 18 39,700 64,096 1984 New JerseyCRAB, BLU 763.9 1,684,200 701,091 1984 New JerseyCRAB, BLU 13.7 30,200 40,980 1984 New York CRAB, BLU 60.8 134,100 69,069 1985 Delaware CRAB, BLU 1,270.60 2,801,100 982,473 1985 Delaware CRAB, BLU 17.5 38,500 62,199 1985 New JerseyCRAB, BLU 1,045.90 2,305,800 978,003 1985 New JerseyCRAB, BLU 46 101,400 142,767 1985 New York CRAB, BLU 127 280,070 134,712 1986 Delaware CRAB, BLU 1,409.30 3,107,000 1,031,311 1986 Delaware CRAB, BLU 37.5 82,600 136,892 1986 New JerseyCRAB, BLU 1,183.90 2,610,100 1,195,576 1986 New JerseyCRAB, BLU 40.8 90,000 111,607 1986 New York CRAB, BLU 65.3 143,900 70,137 1987 Delaware CRAB, BLU 1,757.10 3,873,800 1,151,724 1987 Delaware CRAB, BLU 19.6 43,100 65,044 1987 New JerseyCRAB, BLU 1,292.60 2,849,600 1,419,168 1987 New JerseyCRAB, BLU 33.7 74,200 89,103 1987 New York CRAB, BLU 140.7 310,165 183,766 1988 Delaware CRAB, BLU 1,760.50 3,881,200 1,748,899 1988 Delaware CRAB, BLU 71.2 157,000 307,734 1988 New JerseyCRAB, BLU 2,210.00 4,872,200 2,233,014 1988 New JerseyCRAB, BLU 108 238,100 320,317 1988 New York CRAB, BLU 93.2 205,360 131,260 1989 Delaware CRAB, BLU 2,355.30 5,192,400 2,125,116 1989 Delaware CRAB, BLU 53.1 117,000 300,924 1989 New JerseyCRAB, BLU 2,495.40 5,501,300 2,603,623 1989 New JerseyCRAB, BLU 81.1 178,900 236,220 1989 New York CRAB, BLU 297 654,700 388,713 1990 Delaware CRAB, BLU 3,178.30 7,006,800 2,758,009 1990 Delaware CRAB, BLU 88.7 195,500 331,564 1990 New JerseyCRAB, BLU 2,051.50 4,522,699 1,996,876 1990 New JerseyCRAB, BLU 143.8 316,946 284,829 1990 New York CRAB, BLU 232.6 512,715 269,438 1991 Delaware CRAB, BLU 3,068.50 6,764,900 2,482,275 1991 Delaware CRAB, BLU 11.1 24,400 61,000 1991 New JerseyCRAB, BLU 2,232.60 4,922,077 2,138,588 1991 New JerseyCRAB, BLU 22.5 49,524 51,277 1991 New York CRAB, BLU 370.8 817,545 441,034 1992 Delaware CRAB, BLU 2,047.00 4,512,800 1,945,376 1992 Delaware CRAB, BLU 200.5 442,000 654,160 1992 New JerseyCRAB, BLU 2,793.00 6,157,459 3,248,324 1992 New JerseyCRAB, BLU 168.8 372,182 371,688 1992 New York CRAB, BLU 347.3 765,565 447,033 1993 Delaware CRAB, BLU 2,888.40 6,367,800 3,339,422 1993 Delaware CRAB, BLU 128.3 282,900 297,045 1993 New JerseyCRAB, BLU 3,411.00 7,519,941 3,906,317 1993 New JerseyCRAB, BLU 100 220,506 275,141 1993 New York CRAB, BLU 551 1,214,840 759,350 1994 Delaware CRAB, BLU 2,805.50 6,185,094 3,824,040 1994 Delaware CRAB, BLU 138.3 304,800 493,996 1994 New JerseyCRAB, BLU 2,338.90 5,156,361 3,500,600 1994 New JerseyCRAB, BLU 203.1 447,695 577,965 1994 New York CRAB, BLU 402.3 886,840 558,718 1995 Delaware CRAB, BLU 3,405.00 7,506,600 6,077,256 1995 Delaware CRAB, BLU 235 518,000 690,224 1995 New JerseyCRAB, BLU 3,056.90 6,739,199 5,190,101 1995 New JerseyCRAB, BLU 434.5 957,814 1,061,742 1995 New York CRAB, BLU 790.7 1,743,111 1,481,783 1996 Delaware CRAB, BLU 1,672.20 3,686,520 2,277,664 1996 Delaware CRAB, BLU 99.9 220,207 478,210 1996 New JerseyCRAB, BLU 1,632.60 3,599,275 2,375,078 1996 New JerseyCRAB, BLU 101.4 223,609 260,592 1996 New York CRAB, BLU 1,042.50 2,298,351 1,717,982 1997 Delaware CRAB, BLU 2,429.00 5,354,880 3,342,899 1997 Delaware CRAB, BLU 43.9 96,713 212,953 1997 New JerseyCRAB, BLU 1,946.20 4,290,678 2,874,543 1997 New JerseyCRAB, BLU 123.3 271,913 492,046 1997 New York CRAB, BLU 534.6 1,178,622 883,950 1998 Delaware CRAB, BLU 1,889.50 4,165,492 3,594,116 1998 Delaware CRAB, BLU 88.1 194,330 423,708 1998 New JerseyCRAB, BLU 2,424.50 5,345,074 4,359,892 1998 New JerseyCRAB, BLU 219.7 484,257 918,922 1998 New York CRAB, BLU 693.2 1,528,285 1,146,114 1999 Delaware CRAB, BLU 2,222.00 4,898,564 4,375,998 1999 Delaware CRAB, BLU 42.9 94,601 223,383 1999 New JerseyCRAB, BLU 2,381.90 5,251,058 4,211,931 1999 New JerseyCRAB, BLU 148.8 328,130 698,718 1999 New York CRAB, BLU 53.3 117,572 65,868 2000 Delaware CRAB, BLU 1,821.30 4,015,346 4,899,394 2000 Delaware CRAB, BLU 34.9 76,849 187,027 2000 New JerseyCRAB, BLU 2,206.20 4,863,858 4,924,705 2000 New JerseyCRAB, BLU 103.8 228,906 565,246 2000 New York CRAB, BLU 672.1 1,481,728 744,072 2001 Delaware CRAB, BLU 1,826.60 4,026,904 5,001,256 2001 Delaware CRAB, BLU 26.2 57,664 138,798 2001 New JerseyCRAB, BLU 2,009.60 4,430,330 4,098,293 2001 New JerseyCRAB, BLU 133.4 294,022 703,515 2001 New York CRAB, BLU 565 1,245,544 648,308 2002 Delaware CRAB, BLU 1,372.60 3,026,054 3,424,805 2002 Delaware CRAB, BLU 16.3 35,870 85,850 2002 New JerseyCRAB, BLU 2,721.40 5,999,612 6,173,797 2002 New JerseyCRAB, BLU 104.1 229,470 551,516 2002 New York CRAB, BLU 1.7 3,713 2,731 2003 Delaware CRAB, BLU 804.6 1,773,774 1,849,098 2003 Delaware CRAB, BLU 8.1 17,903 49,607 2003 New JerseyCRAB, BLU 1,726.60 3,806,480 4,243,576 2003 New JerseyCRAB, BLU 93.1 205,214 492,492 2003 New York CRAB, BLU 437 963,407 502,089