  U.S. Environmental Protection Agency
    stratospheric ozone protection program
                         class i controlled substance

      certification of order/purchase
of qps methyl bromide
(Sec 82.13)
SECTION 1
PURCHASER IDENTIFICATION AND METHYL BROMIDE USE
1.1   Date of Submission

1.2  Quantity of Methyl Bromide Ordered/ Purchased (kg)

1.3   Company Information
Purchaser Name
Street Address

City
State
Zip Code
1.4   Company Contact Identification
Reporting Company Contact Person

Phone Number

Fax Number

E-mail Address
Quarantine Applications, with respect to Class I, Group VI controlled substances (methyl bromide), are treatments to prevent the introduction, establishment and/or spread of quarantine pests (including diseases), or to ensure their official control, where: (1) Official control is that performed by, or authorized by, a national (including state, tribal or local) plant, animal or environmental protection or health authority; (2) quarantine pests are pests of potential importance to the areas endangered thereby and not yet present there, or present but not widely distributed and being officially controlled. This definition excludes treatments of commodities not entering or leaving the United States or any State (or political subdivision thereof).
Preshipment Applications, with respect to Class I, Group VI controlled substances (methyl bromide), are those non-quarantine applications applied within 21 days prior to export to meet the official requirements of the importing country or existing official requirements of the exporting country. Official requirements are those which are performed by, or authorized by, a national plant, animal, environmental, health or stored product authority.
1.5   Signature of Reporting Company Representative
I certify that the quantities of methyl bromide specified in Section 1.2 of this form are ordered/purchased and will be used exclusively for quarantine & preshipment applications as defined above, and not sold/ transferred to another person. I certify under penalty of law that I have personally examined and am familiar with the information submitted in this and all attached documents, and that based on my inquiry of those individuals immediately responsible for obtaining the information, I believe that the submitted information is true, accurate, and complete.  I am aware that there are significant penalties for submitting false information, including the possibility of fine and imprisonment.
Name
Title
Signature

Date

SEND COMPLETED FORMS TO:
The Company from Whom the
Methyl Bromide is Being Ordered/Purchased

The public reporting and recordkeeping burden for this collection of information is estimated to average 2.1 hours per response.  Send comments on the Agency's need for this information, the accuracy of the provided burden estimates, and any suggested methods for minimizing respondent burden, including through the use of automated collection techniques to the Director, Collection Strategies Division, U.S. Environmental Protection Agency (2822T), 1200 Pennsylvania Ave., NW, Washington, D.C. 20460.  Include the OMB control number in any correspondence.  Do not send the completed form to this address.


[Federal Register Volume 77, Number 129 (Thursday, July 5, 2012)]
[Notices]
[Page 39793]
[FR Doc No: 2012-16400]

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

DEPARTMENT OF TRANSPORTATION

Office of the Secretary

Notice of Applications for Certificates of Public Convenience and
Necessity and Foreign Air Carrier Permits Filed Under Subpart B
(Formerly Subpart Q) During the Week Ending June 23, 2012

    The following Applications for Certificates of Public Convenience
and Necessity and Foreign Air Carrier Permits were filed under Subpart
B (formerly Subpart Q) of the Department of Transportation's Procedural
Regulations (See 14 CFR 301.201 et seq.). The due date for Answers,
Conforming Applications, or Motions to Modify Scope are set forth below
for each application. Following the Answer period DOT may process the
application by expedited procedures. Such procedures may consist of the
adoption of a show-cause order, a tentative order, or in appropriate
cases a final order without further proceedings.
    Docket Number: DOT-OST-2007-0066.
    Date Filed: June 18, 2012.
    Due Date for Answers, Conforming Applications, or Motion to Modify
Scope: July 9, 2012.
    Description: Application of Hainan Airlines Co., Ltd. (``Hainan
Airlines'') requesting the Department amend its foreign air carrier
permit to enable it to engage in scheduled air transportation of
persons, property, and mail between Beijing, People's Republic of China
(PEK), on the one hand, and Chicago, Illinois (ORD), on the other hand.
Hainan Airlines also requests exemption authority to the extent
necessary so that it may exercise the rights requested in this
application prior to the issuance of an amended foreign air carrier
permit.

Renee V. Wright,
Program Manager, Docket Operations, Federal Register Liaison.
[FR Doc. 2012-16400 Filed 7-3-12; 8:45 am]
BILLING CODE 4910-9X-P


To: Stephanie Plummer/ DC/ USEPA/ US@ EPA, Allen_ Jennings@ USDA. Gov From: russ1212@ tennessee. edu Date: 07/ 11/ 2006 08: 45AM cc: Rick. K_ Kesler@ fmc. com Subject: Furadan Support Dear Fellow Scientist:

I am writing to you in reference to the use and value of Furadan 4F to corn and alfalfa growers. I have worked for many years using Furadan in my plot work. In all cases my data showed that Furadan was as good or better than the other products I was using at the time. I have used Furadan 4F to control grasshoppers in soybeans with execellent results, even with larger specimens. The use in alfalfa to control alfalfa weevil was impressive especially when you had to only use it once to control the insects. I did not have to use a second application because the first was sufficient.

The above is the gist of what my data showed when using Furadan 4F in plot work. I hope it is enough to help you decide to keep it in our arsenol for future use.

Sincerely,

Charles Patrick, Professor University of Tennessee Entomology Plant Pathology Dept. 605 Airways Blvd. Jackson, TN 38301


 MEMORANDUM

DATE: 7/29/15

FROM: 		Ken Mitchell/EPA Region 4

TO:CLEAN POWER PLAN FOR EXISTING POWER PLANTS; DOCKET ID: OAR - 2013-0602

SUBJECT:DISCUSSION OF THE CLEAN POWER Plan at the GA AWMA Regulatory Update Conference             March 25, 2015

SUMMARY:         REGION 4 PROVIDED INFORMATION ON THE CLEAN POWER PLAN to participants at the Georgia AWMA Regulatory Update Conference in Atlanta, GA, on March 25, 2015.  The Clean Power Plan for Existing Power Plants was proposed on June 2, 2014.   ATTENDEES:

EPA Beverly Banister/EPA R4 Several additional Region 4 staff

External Stakeholders Approximately 75 participants

ATTACHMENT


[Federal Register Volume 78, Number 89 (Wednesday, May 8, 2013)]
[Proposed Rules]
[Pages 26720-26727]
[FR Doc No: 2013-10905]

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2013-0366; Directorate Identifier 2011-NM-024-AD]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to supersede an existing airworthiness directive
(AD) that applies to certain The Boeing Company Model 747-100, 747-
100B, 747-100B SUD, 747-200B, 747-200C, 747-300, 747-400, 747-400D, and
747SR series airplanes. The existing AD requires, for certain
airplanes, inspection to determine the material of a main entry door
(MED) reveal; repetitive inspections of certain reveals for cracking; a
detailed inspection of certain reveals for a sharp edge and cracking;
and corrective action if necessary. That AD also allows a certain
replacement as an optional action for certain inspections of certain
airplanes. Since we issued that AD, an operator reported a crack found
in a 6061 machined aluminum one-piece corner reveal. This proposed AD
would add, for certain airplanes, an inspection to determine material
type of MED reveals, repetitive inspections for cracking of 6061
machined aluminum one-piece corner reveals, and replacement with 6061
machined aluminum two-piece corner reveals if necessary. This

proposed AD would also allow replacement with two-piece corner reveals
as an option for certain repetitive inspections. This proposed AD would
also revise the applicability by removing a certain airplane. We are
proposing this AD to detect and correct fatigue cracking of the lower
forward corner reveal of the number 3 MEDs, which could lead to the
door escape slide departing the airplane when the door is opened and
the slide is deployed, and consequent injuries to passengers and crew
using the door escape slide during an emergency evacuation.

DATES: We must receive comments on this proposed AD by June 24, 2013.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Fax:<PHONE_NUMBER>.
     Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this proposed AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management, P.
O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206-
544-5000, extension 1; fax<PHONE_NUMBER>; Internet https://www.myboeingfleet.com. You may review copies of the referenced 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>.

Examining the AD Docket

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

FOR FURTHER INFORMATION CONTACT: Bill Ashforth, Aerospace Engineer,
Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office
(ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: (425) 917-
6432; fax:<PHONE_NUMBER>; email<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2013-0366;
Directorate Identifier 2011-NM-024-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.

Discussion

    On August 20, 2008, we issued AD 2008-18-07, Amendment 39-15664 (73
FR 56960, October 1, 2008), for certain The Boeing Company Model 747-
100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-300, 747-400, 747-
400D, and 747SR series airplanes. The existing AD requires, for certain
airplanes, an inspection to determine the material of an MED reveal;
repetitive inspections of certain reveals for cracking; a detailed
inspection of certain reveals for a sharp edge and cracking; and
corrective action if necessary. That AD also allows a certain
replacement as an optional action for certain inspections of certain
airplanes. The existing AD resulted from reports of cracking and/or a
sharp edge in the lower forward corner reveal of the number 3 MEDs. We
issued that AD to detect and correct fatigue cracking of the lower
forward corner reveal of the number 3 MEDs, which could lead to the
door escape slide departing the airplane when the door is opened and
the slide is deployed, and possible consequent injuries to passengers
and crew using the door escape slide during an emergency evacuation.

Actions Since Existing AD (73 FR 56960, October 1, 2008) Was Issued

    Since we issued AD 2008-18-07, Amendment 39-15664 (73 FR 56960,
October 1, 2008), an operator reported a crack found in a 6061 machined
aluminum one-piece corner reveal. Certain airplanes were equipped with
either 356 cast aluminum or 6061 machined aluminum one-piece corner
reveals at delivery. The existing AD allowed 356 cast aluminum reveals
to be replaced with one-piece machined aluminum corner reveals. We have
determined that inspections are necessary on airplanes having these
one-piece reveals.

Relevant Service Information

    AD 2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008),
referred to Boeing Special Attention Service Bulletin 747-53-2460,
Revision 1, dated February 13, 2007, as the appropriate source of
service information for the required actions. Boeing has since revised
this service information.
    We reviewed Boeing Special Attention Service Bulletin 747-53-2460,
Revision 2, dated December 22, 2010. No new airplanes were added to the
effectivity of Boeing Special Attention Service Bulletin 747-53-2460,
Revision 2, dated December 22, 2010, but airplane groups were changed
based on the material composition of the corner reveals. This service
information describes procedures for a material type inspection of one-
piece or two-piece corner reveals; inspection for sharp edges and
cracking; and replacement of reworked 356 cast aluminum corner reveals
and 6061 machined aluminum one-piece corner reveals with 6061 machined
aluminum two-piece corner reveals, which would eliminate the need for
repetitive inspections.
    Boeing Special Attention Service Bulletin 747-53-2460, Revision 2,
dated December 22, 2010, also specifies a revised effectivity that
clarifies the cargo configuration exceptions by excluding airplanes
modified to the Boeing converted freighter and large cargo freighter
configurations and removing an exception for Groups 2 and 3 of
airplanes modified to the special freighter configuration. This service
information also removes line number (L/N) 1271, a Model 747-400F
series airplane, from the effectivity because it is a freighter
airplane.

FAA's Determination

    We are proposing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of the same type design.

Proposed AD Requirements

    This proposed AD would retain all of the requirements of AD 2008-
18-07, Amendment 39-15664 (73 FR 56960,

October 1, 2008). The proposed AD would require the actions specified
in the service information described previously. The proposed AD would
add, for certain airplanes, an inspection to determine material type of
MED reveals, repetitive inspections for cracking of 6061 machined
aluminum one-piece corner reveals, and replacement with 6061 machined
aluminum two-piece corner reveals if necessary. This proposed AD would
also allow replacement with two-piece corner reveals as an option for
certain repetitive inspections. Also, the proposed AD would remove
airplane L/N 1271, a Model 747-400F series airplane, from the AD
applicability.

Changes To Existing AD (73 FR 56960, October 1, 2008)

    This proposed AD would retain all of the requirements of AD 2008-
18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008). However, we
have removed the ``Service Bulletin Reference'' paragraph from this
proposed AD. That paragraph was identified as paragraph (f) in AD 2008-
18-07. That paragraph provided operators with a one-time citation of
the referenced service bulletin in AD 2008-18-07. Instead, we have
provided the full service bulletin citation throughout this proposed
AD.
    We have revised the heading and wording for paragraph (l) of this
proposed AD, to clarify that the only exception to the procedures in
Boeing Special Attention Service Bulletin 747-53-2460, Revision 1,
dated February 13, 2007; and Boeing Special Attention Service Bulletin
747-53-2460, Revision 2, dated December 22, 2010; is that, as of the
effective date of this proposed AD, an operator's equivalent procedure
may no longer be used without requesting approval of an alternative
method of compliance (AMOC).
    We have also re-designated Notes 1 and 2 of AD 2008-18-07,
Amendment 39-15664 (73 FR 56960, October 1, 2008), as paragraphs (p)
and (q) of this proposed AD. This change does not affect the intent of
those paragraphs.

Costs of Compliance

    We estimate that this proposed AD affects 166 airplanes of U.S.
registry. We estimate the following costs to comply with this proposed
AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Cost on U.S.
              Action                    Labor cost        Parts cost    Cost per product          operators
----------------------------------------------------------------------------------------------------------------
Material type inspection and       4 work-hours x $85             $0  $340 per inspection   $40,460 per
 inspection for cracks (retained    per hour = $340 per                cycle.                inspection cycle.
 actions from AD 2008-18-07,        inspection cycle.
 Amendment 39[dash]15664 (73 FR
 56960, October 1, 2008)) (119
 airplanes).
New Material type inspection and   14 work-hours x $85            $0  $1,190 per            $197,540 per
 inspection for cracks [new         per hour = $1,190                  inspection cycle.     inspection cycle.
 proposed action] (166 airplanes).  per inspection
                                    cycle.
----------------------------------------------------------------------------------------------------------------

    We estimate the following costs to do any necessary on-condition
actions that would be required based on the results of the proposed
inspections. We have no way of determining the number of aircraft that
might need these actions:

                                               On-Condition Costs
----------------------------------------------------------------------------------------------------------------
                 Action                            Labor cost           Parts cost         Cost per product
----------------------------------------------------------------------------------------------------------------
Corner reveal removal and replacement     17 work-hours x $85 per           $9,525   $10,970 per inspection
 [new proposed action].                    hour = $1,445 per                          cycle.
                                           inspection cycle.
----------------------------------------------------------------------------------------------------------------

Authority for This Rulemaking

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

Regulatory Findings

    We have determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and responsibilities among the various levels of government.
    For the reasons discussed above, I certify that the proposed
regulation:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866,
    (2) Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

The Proposed Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by removing airworthiness directive (AD)
2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008), and
adding the following new AD:

The Boeing Company: Docket No. FAA-2013-0366; Directorate Identifier
2011-NM-024-AD.

(a) Comments Due Date

    The FAA must receive comments on this AD action by June 24,
2013.

(b) Affected ADs

    This AD supersedes AD 2008-18-07, Amendment 39-15664 (73 FR
56960, October 1, 2008).

(c) Applicability

    This AD applies to The Boeing Company Model 747-100, 747-100B,
747-100B SUD, 747-200B, 747-200C, 747-300, 747-400, 747-400D, and
747SR series airplanes, certificated in any category, as identified
in Boeing Special Attention Service Bulletin 747-53-2460, Revision
2, dated December 22, 2010, except airplanes that have been
converted to an all-cargo configuration. The requirements of this AD
also become applicable at the time when a converted airplane
operating in an all-cargo configuration is converted back to a
passenger or passenger/cargo configuration.

(d) Subject

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

(e) Unsafe Condition

    This AD was prompted by a report of a crack found in a 6061
machined aluminum one-piece corner reveal. We are proposing this AD
to detect and correct fatigue cracking of the lower forward corner
reveal of the number 3 main entry doors (MEDs), which could lead to
the door escape slide departing the airplane when the door is opened
and the slide is deployed, and consequent injuries to passengers and
crew using the door escape slide during an emergency evacuation.

(f) Compliance

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

(g) Retained Actions for Group 3 Airplanes

    This paragraph restates the requirements of paragraph (g) of AD
2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008), with
revised service information. For airplanes identified as Group 3
airplanes in Boeing Special Attention Service Bulletin 747-53-2460,
Revision 1, dated February 13, 2007: Before the accumulation of
10,000 total flight cycles, or within 1,000 flight cycles after
November 5, 2008 (the effective date of AD 2008-18-07), whichever
occurs later, do a detailed inspection for cracking of the lower
forward corner reveals, in accordance with Part 8 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; or Part 2
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.
As of the effective date of this AD, only Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010,
may be used to accomplish the actions required by this paragraph.
    (1) If no cracking is found, repeat the inspection thereafter at
intervals not to exceed 6,000 flight cycles until a new or reworked
two-piece reveal is installed in accordance with Part 2 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; or Part 3
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.
As of the effective date of this AD, only Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010,
may be used to accomplish the actions required by this paragraph. No
further action is required by this paragraph for that location only
after the replacement.
    (2) If cracking is found, do the replacement specified in
paragraph (g)(2)(i) or (g)(2)(ii) of this AD.
    (i) Before further flight, replace the reveal with a new or
reworked two-piece reveal, in accordance with Part 2 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; or Part 3
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.
No further action is required by this paragraph for that location
only after the replacement. As of the effective date of this AD,
only Boeing Special Attention Service Bulletin 747-53-2460, Revision
2, dated December 22, 2010, may be used to accomplish the actions
required by this paragraph.
    (ii) Before further flight, replace the reveal with a new or
reworked one-piece machined aluminum reveal without a sharp edge, in
accordance with Part 3 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 1, dated
February 13, 2007; or Part 4 of the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 747-53-2460, Revision 2,
dated December 22, 2010. Before the accumulation of 10,000 flight
cycles since new on the replacement reveal, do the inspection for
cracking specified in Part 8 of the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 747-53-2460, Revision 1,
dated February 13, 2007; or Part 2 of the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-53-
2460, Revision 2, dated December 22, 2010. Repeat the inspection
thereafter at intervals not to exceed 6,000 flight cycles until a
new or reworked two-piece reveal is installed in accordance with
Part 2 of the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-53-2460, Revision 1, dated February
13, 2007; or Part 3 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 2, dated
December 22, 2010. If any cracking is found during any inspection
required by this paragraph, before further flight, do the actions
specified in paragraph (g)(2) of this AD. No further action is
required by this paragraph for that location only after the
replacement with a two-piece reveal. As of the effective date of
this AD, only Boeing Special Attention Service Bulletin 747-53-2460,
Revision 2, dated December 22, 2010, may be used to accomplish the
actions required by this paragraph.

(h) Retained Actions for Group 2 Airplanes

    This paragraph restates the requirements of paragraph (h) of AD
2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008), with
revised service information. For airplanes identified as Group 2
airplanes in Boeing Special Attention Service Bulletin 747-53-2460,
Revision 1, dated February 13, 2007; or Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010:
Before the accumulation of 1,500 total flight cycles, or within
1,000 flight cycles after November 5, 2008 (the effective date of AD
2008-18-07), whichever occurs later, do the inspection specified in
paragraph (j) of this AD.

(i) Retained Actions for Group 1, Configuration 2 Airplanes

    This paragraph restates the requirements of paragraph (i) of AD
2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008), with
revised service information. For airplanes identified as Group 1,
Configuration 2 airplanes in Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; or Boeing
Special Attention Service Bulletin 747-53-2460, Revision 2, dated
December 22, 2010: Within 1,500 flight cycles after the lower
forward corner reveal was last replaced, or 1,000 flight cycles
after November 5, 2008 (the effective date of AD 2008-18-07),
whichever occurs later, do the inspection specified in paragraph (j)
of this AD.

(j) Retained Inspection for Cracking and Sharp Edge

    This paragraph restates the requirements of paragraph (j) of AD
2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008), with
revised service information. At the applicable times specified in
paragraphs (h) and (i) of this AD: Do a detailed inspection of the
lower forward corner reveal for cracking and a sharp edge, in
accordance with Part 5 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 1, dated
February 13, 2007; or Part 1 and Part 2 of the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-53-
2460, Revision 2, dated December 22, 2010. As of the effective date
of this AD, only Boeing Special Attention Service Bulletin 747-53-
2460, Revision 2, dated December 22, 2010, may be used to accomplish
the actions required by this paragraph.
    (1) If no cracking and no sharp edge are found, before the
accumulation of 10,000 flight cycles on the lower forward corner
reveal since new, or within 6,000 flight

cycles after doing the inspection required by paragraph (j) of this
AD, whichever occurs later, do a detailed inspection for cracking,
in accordance with Part 8 of the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 747-53-2460, Revision 1,
dated February 13, 2007; or Part 2 of the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-53-
2460, Revision 2, dated December 22, 2010. Inspect thereafter at
intervals not to exceed 6,000 flight cycles, until a new or reworked
two-piece reveal is installed in accordance with Part 2 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; or Part 3
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.
If any cracking is found during any inspection required by this
paragraph, before further flight, do the actions specified in
paragraph (j)(3) of this AD. No further action is required by this
paragraph for that location only after the replacement with a two-
piece reveal. As of the effective date of this AD, only Boeing
Special Attention Service Bulletin 747-53-2460, Revision 2, dated
December 22, 2010, may be used to accomplish the actions required by
this paragraph.
    (2) If no cracking is found, but a sharp edge is found, do the
actions specified in paragraph (j)(2)(i) or (j)(2)(ii) of this AD.
    (i) Before further flight, replace the lower forward corner
reveal with a new or reworked two-piece reveal, in accordance with
Part 2 of the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-53-2460, Revision 1, dated February
13, 2007; or Part 3 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 2, dated
December 22, 2010. No further action is required by this paragraph
for that location only after the replacement. As of the effective
date of this AD, only Boeing Special Attention Service Bulletin 747-
53-2460, Revision 2, dated December 22, 2010, may be used to
accomplish the actions required by this paragraph.
    (ii) Before further flight, replace the reveal with a new or
reworked one-piece machined aluminum reveal without a sharp edge, in
accordance with Part 3 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 1, dated
February 13, 2007; or Part 4 of the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 747-53-2460, Revision 2,
dated December 22, 2010. Before the accumulation of 10,000 flight
cycles on the replacement reveal since new, do the inspection for
cracking, in accordance with Part 8 of the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-53-
2460, Revision 1, dated February 13, 2007; or Part 2 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 2, dated December 22, 2010. Inspect
thereafter at intervals not to exceed 6,000 flight cycles, until a
new or reworked two-piece reveal is installed in accordance with
Part 2 of the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-53-2460, Revision 1, dated February
13, 2007; or Part 3 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 2, dated
December 22, 2010. If any cracking is found during any inspection
required by this paragraph, before further flight, do the actions
specified in paragraph (j)(3) of this AD. No further action is
required by this paragraph for that location only after the
replacement with a two-piece reveal. As of the effective date of
this AD, only Boeing Special Attention Service Bulletin 747-53-2460,
Revision 2, dated December 22, 2010, may be used to accomplish the
actions required by this paragraph.
    (3) If cracking is found, do the actions specified in paragraph
(j)(3)(i) or (j)(3)(ii) of this AD.
    (i) Before further flight, replace the reveal with a new or
reworked two-piece reveal, in accordance with Part 2 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; or Part 3
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.
No further action is required by this paragraph for that location
only after the replacement. As of the effective date of this AD,
only Boeing Special Attention Service Bulletin 747-53-2460, Revision
2, dated December 22, 2010, may be used to accomplish the actions
required by this paragraph.
    (ii) Before further flight, replace the lower forward corner
reveal with a new or reworked one-piece machined aluminum reveal
without a sharp edge, in accordance with Part 3 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; or Part 4
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.
Before the accumulation of 10,000 flight cycles since new on the
replacement reveal, do the inspection for cracking, in accordance
with Part 8 of the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-53-2460, Revision 1, dated February
13, 2007; or Part 2 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 2, dated
December 22, 2010. Inspect thereafter at intervals not to exceed
6,000 flight cycles, until a new or reworked two-piece reveal is
installed in accordance with Part 2 of the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-53-
2460, Revision 1, dated February 13, 2007; or Part 3 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 2, dated December 22, 2010. If any
cracking is found during any inspection required by this paragraph,
before further flight, do the actions required by paragraph (j)(3)
of this AD. No further action is required by this paragraph for that
location only after the replacement with a two-piece reveal. As of
the effective date of this AD, only Boeing Special Attention Service
Bulletin 747-53-2460, Revision 2, dated December 22, 2010, may be
used to accomplish the actions required by this paragraph.

(k) Retained Actions for Group 1, Configuration 1 Airplanes

    This paragraph restates the requirements of paragraph (k) of AD
2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008), with
revised service information. For airplanes identified as Group 1,
Configuration 1 airplanes in Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007: Before
the accumulation of 1,500 total flight cycles, or within 1,000
flight cycles after November 5, 2008 (the effective date of AD 2008-
18-07), whichever occurs later, do a material type inspection to
determine if the lower forward corner reveals are castings, in
accordance with Part 1 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 1, dated
February 13, 2007; or Part 6 of the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 747-53-2460, Revision 2,
dated December 22, 2010. As an alternative to the material type
inspection, replacing a reveal with a new or reworked two-piece
lower forward corner reveal, in accordance with Part 2 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; or Part 3
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010;
is terminating action for the requirements of this paragraph for
that location only. As of the effective date of this AD, only Boeing
Special Attention Service Bulletin 747-53-2460, Revision 2, dated
December 22, 2010, may be used to accomplish the actions required by
this paragraph.
    (1) If the forward corner reveal is not a casting: Before
further flight, do the actions specified in paragraph (j) of this AD
except for the inspection for a sharp edge.
    (2) If the forward corner reveal is a casting: Before the
accumulation of 7,000 total flight cycles, within 2,000 flight
cycles after November 5, 2008 (the effective date of AD 2008-18-07),
or within 3,000 flight cycles since the forward corner reveal was
inspected as specified in Boeing Service Bulletin 747-53A2378,
Revision 3, dated August 11, 2005; or Boeing Service Bulletin 747-
53A2378, Revision 4, dated June 10, 2010; whichever occurs latest;
do a detailed inspection for cracking of the lower forward corner
reveal, in accordance with Part 1 of the Accomplishment Instructions
of Boeing Special Attention Service Bulletin 747-53-2460, Revision
1, dated February 13, 2007; or Part 2 of the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-53-
2460, Revision 2, dated December 22, 2010. As of the effective date
of this AD, only Boeing Special Attention Service Bulletin 747-53-
2460, Revision 2, dated December 22, 2010, may be used to accomplish
the actions required by this paragraph.

    (i) If no cracking is found: Repeat the inspection specified in
paragraph (k)(2) of this AD thereafter at intervals not to exceed
3,000 flight cycles until a new or reworked two-piece lower forward
corner reveal is installed in accordance with Part 2 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; or Part 3
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.
No further action is required by this paragraph for that location
only after the replacement.
    (ii) If cracking is found: Do the actions specified in paragraph
(k)(2)(ii)(A), (k)(2)(ii)(B), or (k)(2)(ii)(C) of this AD.
    (A) Before further flight, weld repair the reveal, in accordance
with Part 4 of the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-53-2460, Revision 1, dated February
13, 2007; or Part 4 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 2, dated
December 22, 2010. Repeat the inspection specified in paragraph
(k)(2) of this AD thereafter at intervals not to exceed 3,000 flight
cycles until a new or reworked two-piece reveal is installed in
accordance with Part 2 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 1, dated
February 13, 2007; or Part 3 of the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 747-53-2460, Revision 2,
dated December 22, 2010. No further action is required by this
paragraph for that location only after the replacement. As of the
effective date of this AD, only Boeing Special Attention Service
Bulletin 747-53-2460, Revision 2, dated December 22, 2010, may be
used to accomplish the actions required by this paragraph.
    (B) Before further flight, replace the reveal with a new or
reworked two-piece reveal, in accordance with Part 2 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; or Part 3
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.
No further action is required by this paragraph for that location
only after the replacement. As of the effective date of this AD,
only Boeing Special Attention Service Bulletin 747-53-2460, Revision
2, dated December 22, 2010, may be used to accomplish the actions
required by this paragraph.
    (C) Before further flight, replace the reveal with a new or
reworked one-piece machined aluminum reveal without a sharp edge, in
accordance with Part 3 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 1, dated
February 13, 2007; or Part 4 of the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 747-53-2460, Revision 2,
dated December 22, 2010. Before the accumulation of 10,000 flight
cycles since new on the replacement reveal, do the inspection for
cracking, in accordance with Part 8 of the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-53-
2460, Revision 1, dated February 13, 2007; or Part 2 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 2, dated December 22, 2010. Inspect
thereafter at intervals not to exceed 6,000 flight cycles, until a
new or reworked two-piece reveal is installed in accordance with
Part 2 of the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-53-2460, Revision 1, dated February
13, 2007; or Part 3 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 2, dated
December 22, 2010. If any cracking is found during any inspection
required by this paragraph, before further flight, do the actions
specified in paragraph (k)(2)(ii)(B) or (k)(2)(ii)(C) of this AD. No
further action is required by this paragraph for that location only
after the replacement with a two-piece reveal. As of the effective
date of this AD, only Boeing Special Attention Service Bulletin 747-
53-2460, Revision 2, dated December 22, 2010, may be used to
accomplish the actions required by this paragraph.

(l) Retained Requirement Regarding Operator's Equivalent Procedure

    This paragraph restates the requirements of paragraph (l) of AD
2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008).
Although Step 5 of Figure 8 of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007, specifies
that operators may accomplish the actions in accordance with ``an
operator's equivalent procedure,'' this AD does not allow using an
``operator equivalent procedure unless approved as an alternative
method of compliance in accordance with paragraph (w) of this AD.

(m) Retained Provisions for Compliance With AD 2007-12-11, Amendment
39-15089 (72 FR 31984, June 11, 2007), for MED 3 Only

    This paragraph restates the provisions of paragraph (m) of AD
2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008), with
revised information. Accomplishment of the applicable repair
required by AD 2008-18-07, Amendment 39-15664 (73 FR 56960, October
1, 2008), constitutes compliance with the repair of the lower
forward corner casting (reveal) of the number 3 MEDs only, as
required by paragraph (q)(2)(ii) of AD 2007-12-11, Amendment 39-
15089 (72 FR 31984, June 11, 2007), which specifies the actions must
be done in accordance with Boeing Service Bulletin 747-53A2378,
Revision 1, dated March 10, 1994; Boeing Service Bulletin 747-
53A2378, Revision 3, dated August 11, 2005; or Boeing Service
Bulletin 747-53A2378, Revision 4, dated June 10, 2010. As of the
effective date of this AD, only Boeing Service Bulletin 747-53A2378,
Revision 4, dated June 10, 2010, may be used to accomplish the
actions specified in this paragraph. Accomplishment of the actions
of this AD does not terminate the remaining requirements of AD 2007-
12-11.

(n) Retained Parts Installation Prohibition (Cast 356 Aluminum) Reveals

    This paragraph restates the requirement of paragraph (n) of AD
2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008). As of
November 5, 2008 (the effective date of AD 2008-18-07), no person
may install a door lower forward corner reveal made of cast 356
aluminum on any airplane at a location specified by AD 2008-18-07.

(o) Retained Parts Installation Limitation (Machined 6061 Aluminum)
Reveals

    This paragraph restates the limitation specified by paragraph
(o) of AD 2008-18-07, Amendment 39-15664 (73 FR 56960, October 1,
2008), with revised service information. As of November 5, 2008 (the
effective date of AD 2008-18-17), no person may install a door lower
forward corner reveal made of machined 6061 aluminum on any airplane
at a location specified by this AD, unless it has been confirmed/
reworked to be without a sharp edge, in accordance with Part 5 of
the Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; or Part 1
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.
As of the effective date of this AD, only Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010,
may be used to accomplish the actions required by this paragraph.

(p) Retained Optional Rework of One-Piece and Two-Piece Machined 6061
Aluminum Reveals

    This paragraph restates the information provided in ``Note 1''
of AD 2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008),
with revised information. For the purpose of this AD, a one-piece
machined 6061 aluminum reveal may be reworked into a two-piece
reveal in accordance with the Accomplishment Instructions of the
applicable service bulletin identified in paragraph of (p)(1) or
(p)(2) of this AD, after it was verified to be crack free and
without a sharp edge, or after it was confirmed to be crack free and
reworked to remove a sharp edge. As of the effective date of this
AD, only Boeing Special Attention Service Bulletin 747-53-2460,
Revision 2, dated December 22, 2010, may be used to accomplish the
actions provided by this paragraph.
    (1) Boeing Special Attention Service Bulletin 747-53-2460,
Revision 1, dated February 13, 2007.
    (2) Boeing Special Attention Service Bulletin 747-53-2460,
Revision 2, dated December 22, 2010.

(q) Retained Optional Rework of One-Piece 6061 Aluminum Reveals With a
Sharp Edge

    This paragraph restates the information provided in ``Note 2''
of AD 2008-18-07, Amendment 39-15664 (73 FR 56960, October 1, 2008),
with revised service information. For the purpose of this AD, a one-
piece machined 6061 aluminum reveal with a sharp edge may be
reworked into a one-piece machined 6061 aluminum reveal without a

sharp edge, in accordance with Part 6 of the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-53-
2460, Revision 1, dated February 13, 2007; or Part 1 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 2, dated December 22, 2010; after it
is confirmed to be crack free in accordance with Part 5 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007, or Part 2
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.
After the sharp edge is removed, the one-piece machined 6061
aluminum reveal without a sharp edge may be further reworked into a
two-piece reveal, in accordance with Part 7 of the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-53-
2460, Revision 1, dated February 13, 2007; or Part 5 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 2, dated December 22, 2010. As of the
effective date of this AD, only Boeing Special Attention Service
Bulletin 747-53-2460, Revision 2, dated December 22, 2010, may be
used to accomplish the actions specified by this paragraph.

(r) New Actions for Previously Inspected Group 4 Airplanes: Corner
Reveal Not Replaced, or Replaced With Two-Piece Reveal

    For Group 4 airplanes identified in Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010,
that have been inspected previously in accordance with the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 1, dated February 13, 2007; and on
which the corner reveal either has not been replaced, or has been
replaced with a two-piece reveal that was made by reworking an
existing one-piece reveal: Before the accumulation of 7,000 total
flight cycles, or within 3,000 flight cycles after the most recent
inspection or rework done in accordance with Boeing Special
Attention Service Bulletin 747-53-2460, Revision 1, dated February
13, 2007; or Boeing Special Attention Service Bulletin 747-53-2460,
Revision 2, dated December 22, 2010; or within 1,000 flight cycles
after the effective date of this AD, whichever occurs latest; do a
material type inspection to determine if the corner reveal is a
casting, in accordance with Part 6 of the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-53-
2460, Revision 2, dated December 22, 2010. Doing the inspection
specified in this paragraph terminates the inspections required by
paragraph (j) of this AD for these airplanes.
    (1) If, during any inspection required by paragraph (r) of this
AD, any corner reveal is found to be a casting: Before further
flight, do a detailed inspection for cracking of the corner reveal,
in accordance with Part 2 of the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 747-53-2460, Revision 2,
dated December 22, 2010; and repeat the inspection thereafter at
intervals not to exceed 3,000 flight cycles until a new two-piece
reveal in installed in accordance with the requirements of paragraph
(r)(1)(i) of this AD. If any cracking is found, do the actions
specified in paragraph (r)(1)(i) or (r)(1)(ii) of this AD.
    (i) Replace the cast reveal with a new 6061 machined aluminum
two-piece corner reveal, before further flight, in accordance with
Part 3 of the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-53-2460, Revision 2, dated December
22, 2010.
    (ii) Repair all cracking, before further flight, in accordance
with Part 4 of the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-53-2460, Revision 2, dated December
22, 2010.
    (2) If, during any inspection required by paragraph (r) of this
AD, any one-piece corner reveal is found to be installed and is not
a casting: Before the accumulation of 10,000 total flight cycles; or
within 6,000 flight cycles after the most recent inspection done in
accordance with Boeing Special Attention Service Bulletin 747-53-
2460, Revision 1, dated February 13, 2007; or Boeing Special
Attention Service Bulletin 747-53-2460, Revision 2, dated December
22, 2010; whichever occurs later; do a detailed inspection of the
corner reveal for cracking, in accordance with Part 2 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 2, dated December 22, 2010. Repeat
the inspection for cracking thereafter at intervals not to exceed
6,000 flight cycles until the corner reveal is replaced with a 6061
machined aluminum two-piece corner reveal. If any cracking is found
during any inspection required by paragraph (r)(2) of this AD,
before further flight, replace the corner reveal with a 6061
machined aluminum two-piece corner reveal, in accordance with Part 3
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.

(s) New Actions for Previously Inspected Group 4 Airplanes: Corner
Reveal Replaced With One-Piece Reveal

    For Group 4 airplanes identified in Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010,
that have been inspected previously in accordance with Boeing
Service Bulletin 747-53-2460, Revision 1, dated February 13, 2007,
and on which the corner reveal has been replaced with a one-piece
reveal: Within 10,000 flight cycles after the date the reveal was
replaced with a one-piece corner reveal, do a detailed inspection
for cracking of the corner reveal, in accordance with Part 2 of the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 747-53-2460, Revision 2, dated December 22, 2010. Repeat
the inspection for cracking thereafter at intervals not to exceed
6,000 flight cycles until the corner reveal is replaced with a 6061
machined aluminum two-piece corner reveal, in accordance with the
requirements of paragraph (u) of this AD. If any cracking is found
during any inspection required this paragraph of this AD, before
further flight, replace the one-piece corner reveal with a 6061
machined aluminum two-piece corner reveal, in accordance with Part 3
of the Accomplishment Instructions of Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010.

(t) New Actions for Group 4 Airplanes: Not Previously Inspected or
Changed

    For Group 4 airplanes identified in Boeing Special Attention
Service Bulletin 747-53-2460, Revision 2, dated December 22, 2010,
that have not been previously inspected or changed in accordance
with Boeing Special Attention Service Bulletin 747-53-2460, Revision
1, dated February 13, 2007: Before the accumulation of 1,500 total
flight cycles, or within 1,000 flight cycles after the effective
date of this AD, whichever occurs later, do a material type
inspection to determine if the lower forward corner reveal is made
from 6061 machined aluminum plate or 356 aluminum casting, in
accordance with Part 6 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 747-53-2460, Revision 2, dated
December 22, 2010. Doing the inspection specified in this paragraph
terminates the inspections required by paragraph (j) of this AD for
these airplanes.
    (1) If, during any inspection required by paragraph (t) of this
AD, any corner reveal is found to be a casting: Before the
accumulation of 7,000 total flight cycles; or within 2,000 flight
cycles after the effective date of this AD; or within 3,000 flight
cycles after the most recent inspection of the MED 3 corner reveal
was done in accordance with Boeing Service Bulletin 747-53A2378,
Revision 4, dated June 10, 2010; whichever occurs latest; do a
detailed inspection for cracking of the corner reveal, in accordance
with Part 2 of the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-53-2460, Revision 2, dated December
22, 2010. Repeat the inspection for cracking thereafter at intervals
not to exceed 3,000 flight cycles until the corner reveal is
replaced with a 6061 machined aluminum two-piece corner reveal. If
any cracking is found during any inspection required by this
paragraph of this AD, before further flight, replace the casting
with a 6061 machined aluminum two-piece corner reveal, in accordance
with Part 3 of the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-53-2460, Revision 2, dated December
22, 2010.
    (2) If, during any inspection required by paragraph (t) of this
AD, a corner reveal is found that is not a casting: Before further
flight, do a detailed inspection for a sharp edge, in accordance
with Part 1 of the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-53-2460, Revision 2, dated December
22, 2010; and do a detailed inspection for cracking of the corner
reveal, in accordance with Part 2 of the Accomplishment Instructions
of Boeing Special Attention Service Bulletin 747-53-2460, Revision
2, dated December 22, 2010. Repeat the inspection for cracking
thereafter at intervals not to exceed 6,000 flight cycles until the
corner reveal is replaced with a 6061 machined aluminum

two-piece corner reveal in accordance with the requirements of
paragraph (u) of this AD.
    (i) If any sharp edge is found during any inspection required by
paragraph (t)(2) of this AD, before further flight, rework the
corner reveal, in accordance with Part 1 of the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-53-
2460, Revision 2, dated December 22, 2010.
    (ii) If any cracking is found during any inspection required by
paragraph (t)(2) of this AD, before further flight, replace the
corner reveal with a 6061 machined aluminum two-piece corner reveal,
in accordance with Part 3 of the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 747-53-2460, Revision 2,
dated December 22, 2010.

(u) New Terminating Action for Repetitive Inspections

    Installation of a 6061 machined aluminum two-piece corner reveal
in accordance with Part 3 of the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 747-53-2460, Revision 2,
dated December 22, 2010, terminates the repetitive inspections
required by paragraphs (r), (s), and (t) of this AD.

(v) Credit for Previous Actions

    This paragraph provides credit for actions required by
paragraphs (g) through (m) and (o) through (q) of this AD, if those
actions were performed before the effective date of this AD using
Boeing Special Attention Service Bulletin 747-53-2460, Revision 1,
dated February 13, 2007; or Boeing Service Bulletin 747-53A2378,
Revision 3, dated August 11, 2005; as applicable, which are not
incorporated by reference in this AD.

(w) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Seattle Aircraft Certification Office (ACO),
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 manager of the ACO, send it to the
attention of the person identified in the Related Information
section of this AD. Information may be emailed to<EMAIL_ADDRESS>    (2) 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.
    (3) An AMOC that provides an acceptable level of safety may be
used for any repair required by this AD if it is approved by the
Boeing Commercial Airplanes Organization Designation Authorization
(ODA) that has been authorized by the Manager, Seattle ACO, to make
those findings. For a repair method to be approved, the repair must
meet the certification basis of the airplane, and the approval must
specifically refer to this AD.
    (4) AMOCs previously approved in accordance with AD 2008-18-07,
Amendment 39-15664 (73 FR 56960, October 1, 2008), are approved as
AMOCs for the corresponding requirements of this AD for Group 2 and
Group 3 airplanes identified in Boeing Special Attention Service
Bulletin 747-53-2460, Revision 2, dated December 22, 2010.
Previously approved AMOCs for Group 1 and Group 4 airplanes
identified in Boeing Special Attention Service Bulletin 747-53-2460,
Revision 2, dated December 22, 2010, are not approved for compliance
with the actions required by this AD.

(x) Related Information

    (1) For more information about this AD, contact Bill Ashforth,
Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft
Certification Office, 1601 Lind Avenue SW., Renton, WA 98057-3356;
phone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
<EMAIL_ADDRESS>    (2) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
P. O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone
206-544-5000, extension 1; fax<PHONE_NUMBER>; Internet https://www.myboeingfleet.com. You may review copies of the referenced
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>.

    Issued in Renton, Washington, on April 26, 2013.
Ali Bahrami,
Manager, Transport Aircraft Directorate, Aircraft Certification
Service.
[FR Doc. 2013-10905 Filed 5-7-13; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 87, Number 133 (Wednesday, July 13, 2022)]
[Proposed Rules]
[Pages 41639-41640]
[FR Doc No: 2022-14897]

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ENVIRONMENTAL PROTECTION AGENCY

40 CFR Part 63

[EPA-HQ-OAR-2002-0049; FRL-8150-03-OAR]
RIN 2060-AU96

Standards of Performance for Steel Plants: Electric Arc Furnaces
Constructed After 10/21/74 & On or Before 8/17/83; Standards of
Performance for Steel Plants: Electric Arc Furnaces & Argon-Oxygen
Decarburization Constructed After 8/17/83; Extension of Comment Period

AGENCY: Environmental Protection Agency (EPA).

ACTION: Proposed rule; extension of comment period.

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SUMMARY: On May 16, 2022, the U.S. Environmental Protection Agency
(EPA) proposed a rule titled ``Standards of Performance for Steel
Plants: Electric Arc Furnaces Constructed After 10/21/74 & On or Before
8/17/83; Standards of Performance for Steel Plants: Electric Arc
Furnaces & Argon-Oxygen Decarburization Constructed After 8/17/83.''
The EPA is extending the comment period on this proposed rule that
currently closes on July 15, 2022, by 30 days. The comment period will
now remain open until August 14, 2022, to allow additional time for
stakeholders to review and comment on the proposal.

DATES: The public comment period for the proposed rule published in the
Federal Register on May 16, 2022 (87 FR 29710), originally ending July
15, 2022, is being extended by 30 days. Written comments must be
received on or before August 14, 2022.

ADDRESSES: Submit comments, identified by Docket ID No. EPA-HQ-OAR-
2002-0049, by any of the following methods:
     Federal eRulemaking Portal: https://www.regulations.gov/
(our preferred method). Follow the online instructions for submitting
comments.
     Email: [email protected]. Include Docket ID No. EPA-
HQ-OAR-2002-0049 in the subject line of the message.
     Fax:<PHONE_NUMBER>. Attention Docket ID No. EPA-HQ-OAR-
2002-0049.
     Mail: U.S. Environmental Protection Agency, EPA Docket
Center, Docket ID No. EPA-HQ-OAR-2002-0049, Mail Code 28221T, 1200
Pennsylvania Avenue NW, Washington, DC 20460.
     Hand Delivery or Courier (by scheduled appointment only):
EPA Docket Center, WJC West Building, Room 3334, 1301 Constitution
Avenue NW, Washington, DC 20004. The Docket Center's hours of operation
are 8:30 a.m.-4:30 p.m., Monday-Friday (except Federal holidays).
    Instructions. All submissions received must include the Docket ID
No. for this rulemaking. Comments received may be posted without change
to https://www.regulations.gov/, including any personal information
provided. For detailed instructions on sending comments and additional
information on the rulemaking process, see the SUPPLEMENTARY
INFORMATION section of this document. Out of an abundance of caution
for members of the public and our staff, the EPA Docket Center and
Reading Room are open to the public by appointment only to reduce the
risk of transmitting COVID-19. Our Docket Center staff also continues
to provide remote customer service via email, phone, and webform. Hand
deliveries and couriers may be received by scheduled appointment only.
For further information on EPA Docket Center services and the current
status, please visit us online at https://www.epa.gov/dockets.

FOR FURTHER INFORMATION CONTACT: For questions about this action,
contact Donna Lee Jones, Metals and Inorganic Chemicals Group, Sector
Policies and Programs Division (D243-02), Environmental Protection
Agency, Research Triangle Park, North Carolina 27711; telephone number:
(919) 541-5251 fax number:<PHONE_NUMBER> email address:
[email protected].

SUPPLEMENTARY INFORMATION:
    Rationale. Based on consideration of requests received from
environmental organizations (GASP (AL), GASP (PA), Fairfield
Environmental Justice Alliance, and California Communities Against
Toxics) and industry (Steel Manufacturers Association, American Iron
and Steel Institute, and Specialty Steel Industry of North America),
the EPA is extending the public comment period for an additional 30
days. Therefore, the public comment period will end on August 15, 2022.
    Docket. The EPA has established a docket for this rulemaking under
Docket ID No. EPA-HQ-OAR-2002-0049. All documents in the docket are
listed in https://www.regulations.gov/. Although listed, some
information is not publicly available, e.g., Confidential Business
Information (CBI) or other information whose disclosure is restricted
by statute. Certain other material, such as copyrighted material, is
not placed on the internet and will be publicly available only in hard
copy. With the exception of such material, publicly available docket
materials are available electronically in Regulations.gov.
    Instructions. Direct your comments to Docket ID No. EPA-HQ-OAR-
2002-0049. The EPA's policy is that all comments received will be
included in the public docket without change and may be made available
online at https://www.regulations.gov/, including any personal
information provided, unless the comment includes information claimed
to be CBI or other information whose disclosure is restricted by
statute. Do not submit electronically to https://www.regulations.gov/
any information that you consider to be CBI or other information whose
disclosure is restricted by statute. This type of

information should be submitted as discussed below.
    The EPA may publish any comment received to its public docket.
Multimedia submissions (audio, video, etc.) must be accompanied by a
written comment. The written comment is considered the official comment
and should include discussion of all points you wish to make. The EPA
will generally not consider comments or comment contents located
outside of the primary submission (i.e., on the Web, cloud, or other
file sharing system). For additional submission methods, the full EPA
public comment policy, information about CBI or multimedia submissions,
and general guidance on making effective comments, please visit https://www.epa.gov/dockets/commenting-epa-dockets.
    The https://www.regulations.gov/ website allows you to submit your
comment anonymously, which means the EPA will not know your identity or
contact information unless you provide it in the body of your comment.
If you send an email comment directly to the EPA without going through
https://www.regulations.gov/, your email address will be automatically
captured and included as part of the comment that is placed in the
public docket and made available on the internet. If you submit an
electronic comment, the EPA recommends that you include your name and
other contact information in the body of your comment and with any
digital storage media you submit. If the EPA cannot read your comment
due to technical difficulties and cannot contact you for clarification,
the EPA may not be able to consider your comment. Electronic files
should not include special characters or any form of encryption and be
free of any defects or viruses. For additional information about the
EPA's public docket, visit the EPA Docket Center homepage at https://www.epa.gov/dockets.
    Due to public health concerns related to COVID-19, the EPA Docket
Center and Reading Room are open to the public by appointment only. Our
Docket Center staff also continues to provide remote customer service
via email, phone, and webform. Hand deliveries or couriers will be
received by scheduled appointment only. For further information and
updates on EPA Docket Center and Reading Room services, please visit us
online at https://www.epa.gov/dockets.
    The EPA continues to carefully and continuously monitor information
from the Centers for Disease Control and Prevention (CDC), local area
health departments, and our federal partners so that we can respond
rapidly as conditions change regarding COVID-19.
    Submitting CBI. Do not submit information containing CBI to the EPA
through https://www.regulations.gov/. Clearly mark the part or all of
the information that you claim to be CBI. For CBI information on any
digital storage media that you mail to the EPA, note the Docket ID No.,
mark the outside of the digital storage media as CBI, and identify
electronically within the digital storage media the specific
information that is claimed as CBI. In addition to one complete version
of the comments that includes information claimed as CBI, you must
submit a copy of the comments that does not contain the information
claimed as CBI directly to the public docket through the procedures
outlined in Instructions above. If you submit any digital storage media
that does not contain CBI, mark the outside of the digital storage
media clearly that it does not contain CBI and note the Docket ID No.
Information not marked as CBI will be included in the public docket and
the EPA's electronic public docket without prior notice. Information
marked as CBI will not be disclosed except in accordance with
procedures set forth in 40 Code of Federal Regulations (CFR) part 2.
    Our preferred method to receive CBI is for it to be transmitted
electronically using email attachments, File Transfer Protocol (FTP),
or other online file sharing services (e.g., Dropbox, OneDrive, Google
Drive). Electronic submissions must be transmitted directly to the
OAQPS CBI Office at the email address [email protected], and as
described above, should include clear CBI markings and note the Docket
ID No. If assistance is needed with submitting large electronic files
that exceed the file size limit for email attachments, and if you do
not have your own file sharing service, please email [email protected]
to request a file transfer link. If sending CBI information through the
postal service, please send it to the following address: OAQPS Document
Control Officer (C404-02), OAQPS, U.S. Environmental Protection Agency,
Research Triangle Park, North Carolina 27711, Attention Docket ID No.
EPA-HQ-OAR-2002-0049. The mailed CBI material should be double wrapped
and clearly marked. Any CBI markings should not show through the outer
envelope.

Panagiotis Tsirigotis,
Director, Office of Air Quality Planning and Standards.
[FR Doc. 2022-14897 Filed 7-12-22; 8:45 am]
BILLING CODE 6560-50-P


[Federal Register: July 18, 2007 (Volume 72, Number 137)]
[Notices]
[Page 39472-39474]
[DOCID:fr18jy07-121]

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SECURITIES AND EXCHANGE COMMISSION

[Release No. 34-56050; File No. SR-CBOE-2007-76]

Self-Regulatory Organizations; Chicago Board Options Exchange,
Incorporated; Notice of Filing and Immediate Effectiveness of Proposed
Rule Change To Extend the Short Term Option Series Pilot Program

July 11, 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 July 2, 2007, the Chicago Board Options Exchange, Incorporated
(``Exchange'' or ``CBOE'') 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 Exchange. The Exchange has designated this proposal as non-
controversial under Section 19(b)(3)(A)(iii) of the Act \3\ and Rule
19b-4(f)(6) thereunder,\4\ which renders the proposed rule change
effective upon filing with the Commission. The Commission is publishing
this notice to solicit comments on the proposed rule change from
interested persons.
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    \1\ 15 U.S.C. 78s(b)(1).
    \2\ 17 CFR 240.19b-4.
    \3\ 15 U.S.C. 78s(b)(3)(A)(iii).
    \4\ 17 CFR 240.19b-4(f)(6).
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I. Self-Regulatory Organization's Statement of the Terms of Substance
of the Proposed Rule Change

    The Exchange proposes to extend the period for its Short Term
Options Series pilot program (``Pilot Program'') through July 12, 2008,
and to amend the Pilot Program related to a restriction on overlapping
expirations of Short Term Option Series with Quarterly Options Series
and Quarterly Index Options (``QIX''). The text of the proposed rule
change is available on the Exchange's Web site (http://www.cboe.org/Legal
), at the Exchange's principal office, and at

the Commission's Public Reference Room.

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, the 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 IV 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
    On July 12, 2005, the Commission approved the Pilot Program.\5\ The
Pilot Program has since been extended and is currently scheduled to
expire on July 12, 2007.\6\
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    \5\ See Securities Exchange Act Release No. 52011 (July 12,
2005), 70 FR 41451 (July 19, 2005) (File No. SR-CBOE-2004-63)
(``Pilot Program Approval Order'').
    \6\ See Securities Exchange Act Release No. 53984 (June 14,
2006), 71 FR 35718 (June 21, 2006) (File No. SR-CBOE-2006-48); see
also Securities Exchange Act Release No. 54338 (August 21, 2006), 71
FR 50952 (August 28, 2006) (File No. SR-CBOE-2006-49) (order
approving a modification to the Pilot Program that increased the
number of series that may be listed for each class selected to
participate in the Pilot Program from five series to seven series).
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    The Exchange has selected the following four options classes to
participant in the Pilot Program: S&P 500 Index options (SPX); S&P 100
Index American-style options (OEX); Mini-S&P 500 Index options (XSP);
and S&P 100 Index European-style options (XEO). CBOE believes the Pilot
Program has been successful and well received by its members and the
investing public. Thus, CBOE proposes to extend the Pilot Program
through July 12, 2008.
    In support of the proposed rule change, and as required by the
Pilot Program Approval Order, the Exchange is submitting to the
Commission a Pilot Program report (the ``Report'') detailing the
Exchange's experience with the Pilot Program. Specifically, the Report
contains data and written analysis regarding the four options classes
included in the Pilot Program. The Report is being submitted under
separate cover and seeks confidential treatment under the Freedom of
Information Act.
    The Exchange believes there is sufficient investor interest and
demand to extend the Pilot Program another year. The Exchange believes
that the Pilot Program has provided investors with additional means of
managing their risk exposures and carrying out their investment
objectives. Furthermore, the Exchange has not experienced any capacity-
related problems with respect to Short Term Option Series. The Exchange
also represents that is has the necessary system capacity to support
the option series listed under the Pilot Program.
    Finally, the Exchange is proposing to amend the Pilot Program to
provide that no Short Term Option Series may have an expiration that
coincides with an expiration of Quarterly Options Series on the same
class. Currently, the Exchange's rules do not have such a restriction.
The Exchange is also proposing to amend the Pilot Program as it
pertains to index options to provide that no Short Term Option Series
may have an expiration that coincides with an expiration of QIX option
series on the same class. Currently, the Exchange's rules provide that
no Short Term Option Series may expire in the same week during which
the QIXs expire. The Exchange believes these changes should provide
consistency in the Exchange's rules with those of other exchanges
sponsoring similar pilot programs.\7\
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    \7\ See, e.g., American Stock Exchange Rule 903, Commentary
.09(b); International Securities Exchange Rule 504, Supplementary
Material .03(b); and NYSE Arca Rule 5.19(a)(3).
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2. Statutory Basis
    The Exchange believes the proposed rule change is consistent with
Section 6(b) of the Act.\8\ Specifically, the Exchange believes the
proposed rule change is consistent with Section 6(b)(5) of the Act,\9\
which requires that the rules of an exchange be designed to promote
just and equitable principles of trade, to prevent fraudulent and
manipulative acts, to remove impediments to and to perfect the
mechanism for a free and open market and a national market system, and,
in general, to protect investors and the public interest. The Exchange
believes that extension of the Pilot Program will result in a
continuing benefit to investors by allowing them additional means to
manage their risk exposures and carry out their investment objectives,
and will allow the Exchange to further study investor interest in Short
Term Option Series.
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    \8\ 15 U.S.C. 78f(b).
    \9\ 15 U.S.C. 78f(b)(5).
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B. Self-Regulatory Organization's Statement on Burden on Competition

    The Exchange does not believe that the proposed rule change will
impose any 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 neither solicited nor received comments on the
proposal.

III. Date of Effectiveness of the Proposed Rule Change and Timing for
Commission Action

    The Exchange has designated the proposed rule change as one that:
(1) Does not significantly affect the protection of investors or the
public interest; (2) does not impose any significant burden on
competition; and (3) does not become operative for 30 days from the
date of filing, or such shorter time as the Commission may designate if
consistent with the protection of investors and the public interest.
Therefore, the foregoing rule change has become effective pursuant to
Section 19(b)(3)(A) of the Act \10\ and subparagraph (f)(6) of Rule
19b-4 thereunder.\11\ The Exchange has asked the Commission to waive
the operative delay to permit the Pilot Program extension to become
operative prior to the 30th day after filing.\12\
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    \10\ 15 U.S.C. 78s(b)(3)(A).
    \11\ 17 CFR 240.19b-4(f)(6).
    \12\ As required under Rule 19b-4(f)(6)(iii), the Exchange
provided the Commission with written notice of its intent to file
the proposed rule change at least five business before doing so.
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    The Commission believes that waiving the 30-day operative delay is
consistent with the protection of investors and the public interest
because it will allow the benefits of the Pilot Program to continue
without interruption.\13\ Therefore, the Commission designates the
proposal operative upon filing.\14\
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    \13\ For purposes only of waiving the 30-day operative delay,
the Commission has considered the proposed rule's impact on
efficiency, competition, and capital formation. See 15 U.S.C.
78c(f).
    \14\ As set forth in the Commission's original release providing
notice filing of CBOE's proposal to adopt the Pilot Program, if the
Exchange were to propose an extension, an expansion, or permanent
approval of the Pilot Program, the Exchange would submit, along with
any filing proposing such amendments to the program, a report that
would provide an analysis of the Pilot Program covering the entire
period during which the Pilot Program was in effect. The report
would include, at a minimum: (1) Data and written analysis on the
open interest and trading volume in the classes for which Short Term
Option Series were opened; (2) an assessment of the appropriateness
of the option classes selected for the Pilot Program; (3) an
assessment of the impact of the Pilot Program on the capacity of the
Exchange, OPRA, and market data vendors (to the extent data from
market data vendors is available); (4) any capacity problems or
other problems that arose during the operation of the Pilot Program
and how the Exchange addressed such problems; (5) any complaints
that the Exchange received during the operation of the Pilot Program
and how the Exchange addressed them; and (6) any additional
information that would assist in assessing the operation of the
Pilot Program. The report must be submitted to the Commission at
least sixty (60) days prior to the expiration date of the Pilot
Program. See Securities Exchange Act Release No. 51172 (February 9,
2005), 70 FR 7979 (February 16, 2005) (File No. SR-CBOE-2004-63).

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    At any time within 60 days of the filing of the proposed rule
change, the Commission may summarily abrogate the rule change if it
appears to the Commission that such action is necessary or appropriate
in the public interest, for the protection of investors, or other CBOE
in furtherance of the purposes of the Act.

IV. 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 No. SR-CBOE-2007-76 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-CBOE-2007-76. 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 Commissions Internet Web site (http://www.sec.gov/rules/sro.shtml).

Copies of the submission, 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 such filing also will be available for inspection and
copying at the principal office 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 Number SR-CBOE-2007-76 and should be submitted on
or before August 8, 2007.\15\
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    \15\ 17 CFR 200.30-3(a)(12).

    For the Commission, by the Division of Market Regulation,
pursuant to delegated authority.
J. Lynn Taylor,
Assistant Secretary. 7
 [FR Doc. E7-13874 Filed 7-17-07; 8:45 am]

BILLING CODE 8010-01-P