[Federal Register Volume 79, Number 160 (Tuesday, August 19, 2014)]
[Rules and Regulations]
[Pages 48954-48957]
[FR Doc No: 2014-18863]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0120; Directorate Identifier 2013-NM-056-AD;
Amendment 39-17932; AD 2014-16-08]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc. Airplanes

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

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Bombardier, Inc. Model CL-215-6B11 (CL-215T Variant), and CL-215-6B11
(CL-415 Variant) airplanes. This AD was prompted by several reports
indicating that shorter nacelle strut bushings were inadvertently
installed on certain airplanes. This AD requires a general visual
inspection of the left and right nacelle upper strut bushings;
installation of the bolts and preload indicating (PLI) washers, if
necessary; and replacement of the bushing or repair of the bushing
installation, if necessary. We are issuing this AD to detect and
correct inadequate nacelle strut bushings, which provide insufficient
engagement in the strut fork end, and could deform under the bearing
load and lead to the failure of the joint.

DATES: This AD becomes effective September 23, 2014.
    The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of September 23,
2014.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0120; or in person at the
Docket Management Facility, U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC.
    For service information identified in this AD, contact Bombardier,
Inc., 400 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9,
Canada; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>; email
<EMAIL_ADDRESS>Internet http://www.bombardier.com. You
may view this referenced service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information
on the availability of this material at the FAA, call<PHONE_NUMBER>.

FOR FURTHER INFORMATION CONTACT: Ricardo Garcia, Aerospace Engineer,
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft
Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; phone<PHONE_NUMBER>; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Bombardier, Inc.
Model CL-215-6B11 (CL-215T Variant), and CL-215-6B11 (CL-415 Variant)
airplanes. The NPRM published in the Federal Register on February 27,
2014 (79 FR 11022).
    Transport Canada Civil Aviation, which is the aviation authority
for

Canada, has issued Canadian Airworthiness Directive CF-2013-06, dated
February 27, 2013 (referred to after this as the Mandatory Continuing
Airworthiness Information, or ``the MCAI''), to correct an unsafe
condition certain Bombardier, Inc. Model CL-215-6B11 (CL-215T Variant),
and CL-215-6B11 (CL-415 Variant) airplanes. The MCAI states:

    It was discovered in several cases that nacelle strut bushings
with part number (P/N), 85410265-105, have been inadvertently
installed in lieu of P/N 85410265-103. Bushing P/N 85410265-105 is
shorter than bushing P/N 85410265-103 and provides for less
engagement in the strut fork end, P/N 215T16534-12/-13, which may
deform under the bearing load leading to the failure of the joint.

    The actions for this AD include a general visual inspection of the
left and right nacelle upper strut bushings; installation of the bolts
and PLI washers, if necessary; and replacement of the bushing or repair
of the bushing installation, if necessary. You may examine the MCAI in
the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0120-0002.

Comments

    We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (79 FR 11022, February 27,
2014) or on the determination of the cost to the public.

``Contacting the Manufacturer'' Paragraph in This AD

    Since late 2006, we have included a standard paragraph titled
``Airworthy Product'' in all MCAI ADs in which the FAA develops an AD
based on a foreign authority's AD.
    The MCAI or referenced service information in an FAA AD often
directs the owner/operator to contact the manufacturer for corrective
actions, such as a repair. Briefly, the Airworthy Product paragraph
allowed owners/operators to use corrective actions provided by the
manufacturer if those actions were FAA-approved. In addition, the
paragraph stated that any actions approved by the State of Design
Authority (or its delegated agent) are considered to be FAA-approved.
    In the NPRM (79 FR 11022, February 27, 2014), we proposed to
prevent the use of repairs that were not specifically developed to
correct the unsafe condition, by requiring that the repair approval
provided by the State of Design Authority or its delegated agent
specifically refer to this FAA AD. This change was intended to clarify
the method of compliance and to provide operators with better
visibility of repairs that are specifically developed and approved to
correct the unsafe condition. In addition, we proposed to change the
phrase ``its delegated agent'' to include a design approval holder
(DAH) with State of Design Authority design organization approval
(DOA), as applicable, to refer to a DAH authorized to approve required
repairs for the proposed AD.
    No comments were provided to the NPRM (79 FR 11022, February 27,
2014) about these proposed changes. However, a comment was provided for
another NPRM having Directorate Identifier 2012-NM-101-AD (78 FR 78285,
December 26, 2013). The commenter stated the following: ``The proposed
wording, being specific to repairs, eliminates the interpretation that
Airbus messages are acceptable for approving minor deviations
(corrective actions) needed during accomplishment of an AD mandated
Airbus service bulletin.''
    This comment has made the FAA aware that some operators have
misunderstood or misinterpreted the Airworthy Product paragraph to
allow the owner/operator to use messages provided by the manufacturer
as approval of deviations during the accomplishment of an AD-mandated
action. The Airworthy Product paragraph does not approve messages or
other information provided by the manufacturer for deviations to the
requirements of the AD-mandated actions. The Airworthy Product
paragraph only addresses the requirement to contact the manufacturer
for corrective actions for the identified unsafe condition and does not
cover deviations from other AD requirements. However, deviations to AD-
required actions are addressed in 14 CFR 39.17, and anyone may request
the approval for an alternative method of compliance to the AD-required
actions using the procedures found in 14 CFR 39.19.
    To address this misunderstanding and misinterpretation of the
Airworthy Product paragraph, we have changed the paragraph and retitled
it ``Contacting the Manufacturer.'' This paragraph now clarifies that
for any requirement in this AD to obtain corrective actions from a
manufacturer, the action must be accomplished using a method approved
by the FAA, TCCA, or Bombardier's TCCA Design Approval Organization
(DAO).
    The Contacting the Manufacturer paragraph also clarifies that, if
approved by the DAO, the approval must include the DAO-authorized
signature. The DAO signature indicates that the data and information
contained in the document are TCCA-approved, which is also FAA-
approved. Messages and other information provided by the manufacturer
that do not contain the DAO-authorized signature approval are not TCCA-
approved, unless TCCA directly approves the manufacturer's message or
other information.
    This clarification does not remove flexibility previously afforded
by the Airworthy Product paragraph. Consistent with long-standing FAA
policy, such flexibility was never intended for required actions. This
is also consistent with the recommendation of the Airworthiness
Directive Implementation Aviation Rulemaking Committee to increase
flexibility in complying with ADs by identifying those actions in
manufacturers' service instructions that are ``Required for
Compliance'' with ADs. We continue to work with manufacturers to
implement this recommendation. But once we determine that an action is
required, any deviation from the requirement must be approved as an
alternative method of compliance.
    Other commenters to the NPRM having Directorate Identifier 2012-NM-
101-AD (78 FR 78285, December 26, 2013) pointed out that in many cases
the foreign manufacturer's service bulletin and the foreign authority's
MCAI might have been issued some time before the FAA AD. Therefore, the
DOA might have provided U.S. operators with an approved repair,
developed with full awareness of the unsafe condition, before the FAA
AD is issued. Under these circumstances, to comply with the FAA AD, the
operator would be required to go back to the manufacturer's DOA and
obtain a new approval document, adding time and expense to the
compliance process with no safety benefit.
    Based on these comments, we removed the requirement that the DAH-
provided repair specifically refer to this AD. Before adopting such a
requirement, the FAA will coordinate with affected DAHs and verify they
are prepared to implement means to ensure that their repair approvals
consider the unsafe condition addressed in this AD. Any such
requirements will be adopted through the normal AD rulemaking process,
including notice-and-comment procedures, when appropriate.
    We also have decided not to include a generic reference to either
the ``delegated agent'' or ``DAH with State of Design Authority design
organization approval,'' but instead we have provided the specific
delegation approval granted by the State of Design

Authority for the DAH in the Contacting the Manufacturer paragraph of
this AD.

Conclusion

    We reviewed the relevant data and determined that air safety and
the public interest require adopting this AD with the changes described
previously and minor editorial changes. We have determined that these
minor changes:
     Are consistent with the intent that was proposed in the
NPRM (79 FR 11022, February 27, 2014) for correcting the unsafe
condition; and
     Do not add any additional burden upon the public than was
already proposed in the NPRM (79 FR 11022, February 27, 2014).
    We also determined that these changes will not increase the
economic burden on any operator or increase the scope of this AD.

Costs of Compliance

    We estimate that this AD affects 5 airplanes of U.S. registry.
    We also estimate that it will take about 4 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 $0 per
product. Based on these figures, we estimate the cost of this AD on
U.S. operators to be $1,700, or $340 per product.
    In addition, we estimate that any necessary follow-on actions will
take about 4 work-hours and require parts costing $0, for a cost of
$340 per product. We have no way of determining the number of aircraft
that might need these actions.

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 that 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);
    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.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0120; or in person at the
Docket Management Facility between 9 a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The AD docket contains this AD, the
regulatory evaluation, any comments received, and other information.
The street address for the Docket Operations office (telephone 800-647-
5527) is in the ADDRESSES section.

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 airworthiness
directive (AD):

2014-16-08 Bombardier, Inc.: Amendment 39-17932. Docket No. FAA-
2014-0120; Directorate Identifier 2013-NM-056-AD.

(a) Effective Date

    This AD becomes effective September 23, 2014.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to the Bombardier, Inc. airplanes, certificated
in any category, identified in paragraphs (c)(1) and (c)(2) of this
AD.
    (1) Model CL-215-6B11 (CL-215T Variant) airplanes, serial
numbers 1056, 1057, 1061, 1080, 1109, 1113, 1114, 1115, 1116, 1117,
1118, 1119, 1120, 1121, 1122, and 1125.
    (2) Model CL-215-6B11 (CL-415 Variant) airplanes, serial numbers
2001 through 2067 inclusive.

(d) Subject

    Air Transport Association (ATA) of America Code 54, Nacelles/
Pylons.

(e) Reason

    This AD was prompted by several reports indicating that shorter
nacelle strut bushings were inadvertently installed on certain
airplanes. We are issuing this AD to detect and correct inadequate
nacelle strut bushings, which provide insufficient engagement in the
strut fork end, and could deform under the bearing load and lead to
the failure of the joint.

(f) Compliance

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

(g) Inspection of the Bushing

    Within 3 months after the effective date of this AD: Do a
general visual inspection to determine the part number of the left
and right nacelle upper strut bushings, in accordance with the
Accomplishment Instructions of Bombardier Alert Service Bulletin
215-A3173, dated April 11, 2012 (for Model CL-215-6B11 (CL-215T
Variant) airplanes); or Bombardier Alert Service Bulletin 215-A4453,
dated April 10, 2012 (for Model CL-215-6B11 (CL-415 Variant)
airplanes).
    (1) If any bushing with part number (P/N) 85410265-103 is
installed: Before further flight, install the bolts and preload
indicating (PLI) washers, in accordance with paragraph 2.G. of the
Accomplishment Instructions of Bombardier Alert Service Bulletin
215-A3173, dated April 11, 2012 (for Model CL-215-6B11 (CL-215T
Variant) airplanes); or Bombardier Alert Service Bulletin 215-A4453,
dated April 10, 2012 (for Model CL-215-6B11 (CL-415 Variant)
airplanes).
    (2) If any bushing with P/N 85410265-105 is installed in either
the left or right nacelle: Do the actions in paragraph (h) of this
AD.

(h) Replacement or Repair of the Bushing

    If any bushing with P/N 85410265-105 is found installed during
the inspection required by paragraph (g) of this AD: Before further
flight, do the actions specified in paragraph (h)(1) or (h)(2) of
this AD.
    (1) Replace the bushing in accordance with paragraph 2.E. of the
Accomplishment Instructions of Bombardier Alert Service Bulletin
215-A3173, dated April 11, 2012 (for Model CL-215-6B11 (CL-215T
Variant) airplanes); or Bombardier Alert Service Bulletin 215-A4453,
dated April 10, 2012

(for Model CL-215-6B11 (CL-415 Variant) airplanes); and continue
with the installation of the bolt and PLI washer, in accordance with
paragraph 2.G. of the Accomplishment Instructions of Bombardier
Alert Service Bulletin 215-A3173, dated April 11, 2012 (for Model
CL-215-6B11 (CL-215T Variant) airplanes); or Bombardier Alert
Service Bulletin 215-A4453, dated April 10, 2012 (for Model CL-215-
6B11 (CL-415 Variant) airplanes).
    (2) Repair the bushing in accordance with paragraph 2.F. of the
Accomplishment Instructions of Bombardier Alert Service Bulletin
215-A3173, dated April 11, 2012 (for Model CL-215-6B11 (CL-215T
Variant) airplanes); or Bombardier Alert Service Bulletin 215-A4453,
dated April 10, 2012 (for Model CL-215-6B11 (CL-415 Variant)
airplanes); and continue with the installation of the bolt and PLI
washer, in accordance with paragraph 2.G. of the Accomplishment
Instructions of Bombardier Alert Service Bulletin 215-A3173, dated
April 11, 2012 (for Model CL-215-6B11 (CL-215T Variant) airplanes);
or Bombardier Alert Service Bulletin 215-A4453, dated April 10, 2012
(for Model CL-215-6B11 (CL-415 Variant) airplanes).

(i) Replacement of Repaired Bushing

    For any bushing that has been repaired as specified in paragraph
(h)(2) of this AD: Within 5,000 flight hours after accomplishing the
repair or at the next engine removal, whichever occurs first,
replace the bushing with P/N 85410265-103, in accordance with
paragraph 2.E. of the Accomplishment Instructions of Bombardier
Alert Service Bulletin 215-A3173, dated April 11, 2012 (for Model
CL-215-6B11 (CL-215T Variant) airplanes); or Bombardier Alert
Service Bulletin 215-A4453, dated April 10, 2012 (for Model CL-215-
6B11 (CL-415 Variant) airplanes); and continue with the installation
of the bolt and PLI washer, in accordance with paragraph 2.G. of the
Accomplishment Instructions of Bombardier Alert Service Bulletin
215-A3173, dated April 11, 2012 (for Model CL-215-6B11 (CL-215T
Variant) airplanes); or Bombardier Alert Service Bulletin 215-A4453,
dated April 10, 2012 (for Model CL-215-6B11 (CL-415 Variant)
airplanes).

(j) Airplanes for Which No Further Action Is Required

    (1) For airplanes on which a general visual inspection specified
in paragraph (g) of this AD is done and it is determined that
nacelle strut bushings having P/N 85410265-103 are installed in the
airplane: No further actions are required by this AD, provided the
actions specified in paragraph (g)(1) of this AD have been done.
    (2) For airplanes on which nacelle strut bushings having P/N
85410265-103 are installed as specified in paragraph (h)(1) or (i)
of this AD: No further actions are required by this AD.

(k) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, New
York Aircraft Certification Office (ACO), ANE-170, 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 ACO, send it to ATTN: Program Manager, Continuing
Operational Safety, FAA, New York ACO, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; 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) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, New York ACO,
ANE-170, Engine and Propeller Directorate, FAA; or Transport Canada
Civil Aviation (TCCA); or Bombardier, Inc.'s TCCA Design Approval
Organization (DAO). If approved by the DAO, the approval must
include the DAO-authorized signature.

(l) Related Information

    Refer to Mandatory Continuing Airworthiness Information (MCAI)
Canadian Airworthiness Directive CF-2013-06, dated February 27,
2013, for related information. This MCAI may be found in the AD
docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0120-0002.

(m) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
    (i) Bombardier Alert Service Bulletin 215-A3173, dated April 11,
2012.
    (ii) Bombardier Alert Service Bulletin 215-A4453, dated April
10, 2012.
    (3) For service information identified in this AD, contact
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; telephone<PHONE_NUMBER>; fax 514-855-
7401; email<EMAIL_ADDRESS>Internet http://www.bombardier.com.
    (4) You may view this service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
    (5) You may view this 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/cfr/ibr-locations.html.

    Issued in Renton, Washington, on July 30, 2014.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2014-18863 Filed 8-18-14; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 87, Number 145 (Friday, July 29, 2022)]
[Notices]
[Pages 45810-45811]
[FR Doc No: 2022-16258]

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SECURITIES AND EXCHANGE COMMISSION

[SEC File No. 270-93, OMB Control No. 3235-0087]

Submission for OMB Review; Comment Request: Extension: Rule
15Bc3-1 and Form MDSW, Withdrawal From Registration of Municipal
Securities Dealers

Upon Written Request, Copies Available From: Securities and Exchange
Commission, Office of FOIA Services, 100 F Street NE, Washington, DC
20549-2736

    Notice is hereby given that, pursuant to the Paperwork Reduction
Act of 1995 (``PRA'') (44 U.S.C. 3501 et seq.), the Securities and
Exchange Commission (``Commission'') has submitted to the Office of
Management and Budget (``OMB'') a request for approval of extension of
the previously approved collection of information provided for in Rule
15Bc3-1 (17 CFR 240.15Bc3-1) and Form MSDW (17 CFR 249.1110) under the
Securities Exchange Act of 1934 (15 U.S.C. 78a et seq.).
    Rule 15Bc3-1 provides that a notice of withdrawal from registration
with the Commission as a bank municipal securities dealer must be filed
on Form MSDW. The Commission uses the information contained in Form
MSDW in determining whether it is in the public interest to permit a
bank municipal securities dealer to withdraw its registration. This
information is also important to the municipal securities dealer's
customers and to the public because it provides, among other things,
the name and address of a person to contact regarding any of the
municipal securities dealer's unfinished business.
    Based upon past submissions of two filings in 2019, zero filings in
2020, zero filings in 2021, and zero filings so far in 2022, the
Commission estimates that approximately one respondent will use Form
MSDW annually, with a total hour burden for all respondents of
approximately 1 hour per year (0.5 hours rounded up to 1 hour). This
estimate is based on the Commission staff's experience in administering
the form. The form is available from the Commission, and can usually be
completed by checking appropriate boxes and writing the name and
address of the bank municipal securities dealer, and the name and
address of the person who has or will have custody of the bank
municipal securities dealer's books and records. The staff estimates
that the average internal compliance cost per hour is approximately
$406.\1\ Therefore, the estimated total annual internal cost of
compliance is approximately $203 per year (0.5 hours/year x $406/hour =
$203/year).
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    \1\ The estimate of $406 per hour is for a compliance attorney,
based on the Securities Industry and Financial Markets Association's
Management & Professional Earnings in the Securities Industry 2013,
modified by Commission staff to account for an 1800-hour work-year
and inflation, and multiplied by 5.35 to account for bonuses, firm
size, employee benefits and overhead.
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    Rule 15Bc3-1 does not contain an explicit recordkeeping
requirement, but the instructions for filing Form MSDW state that an
exact copy should be retained by the registrant. Providing the
information on the application is mandatory in order to withdraw from
registration with the Commission as a bank municipal securities dealer.
The information contained in the notice will not be kept confidential.
    An agency may not conduct or sponsor, and a person is not required
to respond to, a collection of information under the PRA unless it
displays a currently valid OMB control number.
    The public may view background documentation for this information
collection at the following website: www.reginfo.gov. Find this
particular information collection by selecting ``Currently under 30-day
Review--Open for Public Comments'' or by using the search function.
Written comments and recommendations for the proposed information
collection should be sent by August 29, 2022 to (i) www.reginfo.gov/public/do/PRAMain and (ii) David Bottom, Director/Chief Information
Officer, Securities and Exchange Commission, c/o John Pezzullo, 100 F
Street NE, Washington, DC 20549, or by sending an email to:
[email protected].

    July 25, 2022.
J. Matthew DeLesDernier,
Deputy Secretary.
[FR Doc. 2022-16258 Filed 7-28-22; 8:45 am]
BILLING CODE 8011-01-P