[Federal Register Volume 84, Number 26 (Thursday, February 7, 2019)]
[Proposed Rules]
[Pages 2484-2485]
[FR Doc No: 2019-01366]

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ENVIRONMENTAL PROTECTION AGENCY

40 CFR Part 60

[EPA-HQ-OAR-2018-0195; FRL-9988-89-OAR]
RIN 2060-AU00

Standards of Performance for New Residential Wood Heaters, New
Residential Hydronic Heaters and Forced-Air Furnaces

AGENCY: Environmental Protection Agency (EPA).

ACTION: Reopen comment period.

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SUMMARY: On November 30, 2018, the Environmental Protection Agency
(EPA) proposed a rule titled ``Standards of Performance for New
Residential Wood Heaters, New Residential Hydronic Heaters and Forced-
Air Furnaces.'' The EPA is reopening the public comment period on the
proposed rule that closed on January 14, 2019. The EPA is taking this
action to allow time for the public to comment on the proposed rule for
at least 30 days following the public hearing, which was held on
December 17, 2018.

DATES: The public comment period for the proposed rule published in the
Federal Register on November 30, 2018 is being reopened. Written
comments must be received on or before February 12, 2019.

ADDRESSES: Comments. Submit your comments, identified by Docket ID No.
EPA-HQ-OAR-2018-0195, at https://www.regulations.gov. Follow the online
instructions for submitting comments. Once submitted, comments cannot
be edited or removed from Regulations.gov.
    Regulations.gov is our preferred method for receiving comments.
However, the following other submission methods are also accepted:
     Email<EMAIL_ADDRESS>Include Docket ID No. EPA-
HQ-OAR-2018-0195 in the subject line of the message.
     Fax:<PHONE_NUMBER>. Attention Docket ID No. EPA-HQ-OAR-
2018-0195.
     Mail: To ship or send mail via the United States Postal
Service, use the following address: U.S. Environmental Protection
Agency, EPA Docket Center, Docket ID No. EPA-HQ-OAR-2018-0195, Mail
Code 28221T, 1200 Pennsylvania Avenue NW, Washington, DC 20460.
     Hand/Courier Delivery: Use the following Docket Center
address if you are using express mail, commercial delivery, hand
delivery, or courier: EPA Docket Center, EPA WJC West Building, Room
3334, 1301 Constitution Avenue NW, Washington, DC 20004. Delivery
verification signatures will be available only during regular business
hours.
    Do not submit electronically any information you consider to be
Confidential Business Information (CBI) or other information whose
disclosure is restricted by statute. If you need to include CBI as part
of your comment, send or deliver information identified as CBI only 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-2018-0195.
    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://www2.epa.gov/dockets/commenting-epa-dockets.

FOR FURTHER INFORMATION CONTACT: For additional information on this
action, contact Rochelle Boyd, Sector Policies and Programs Division,
Office of Air Quality Planning and Standards (D243-02), Environmental
Protection Agency, Research Triangle Park, NC 27711; telephone number:
(919) 541-1390; and email address<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION: To allow for additional time for
stakeholders to provide comments, the EPA has decided to reopen the
public comment period until February 12, 2019.

     Dated: February 1, 2019.
Panagiotis Tsirigotis,
Director, Office of Air Quality Planning and Standards.
[FR Doc. 2019-01366 Filed 2-6-19; 8:45 am]
 BILLING CODE 6560-50-P


[Federal Register: July 17, 2009 (Volume 74, Number 136)]
[Notices]
[Page 34748]
[DOCID:fr17jy09-46]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Project No. 13497-000]

FFP Project 66, LLC; Notice of Preliminary Permit Application
Accepted for Filing and Soliciting Comments, Motions To Intervene, and
Competing Applications

July 10, 2009.
    On May 22, 2009, FFP Project 66, LLC filed an application for a
preliminary permit, pursuant to section 4(f) of the Federal Power Act,
proposing to study the feasibility of the Saint Catherine Bend
Hydrokinetic Project, to be located on the Mississippi River, in
Concordia Parish, Louisiana and Adams County, Mississippi.
    The sole purpose of a preliminary permit, if issued, is to grant
the permit holder priority to file a license application during the
permit term. A preliminary permit does not authorize the permit holder
to perform any land disturbing activities or otherwise enter upon lands
or waters owned by others without the owners' express permission.
    The proposed Saint Catherine Bend Hydrokinetic Project consists of:
(1) 4,752 proposed 40 kilowatt Free Flow generating units having a
total installed capacity of 190.08 megawatts; (2) a 6.5-mile-long, 69
kilovolt transmission line; and (3) appurtenant facilities. The
proposed Saint Catherine Bend Hydrokinetic Project would have an
average annual generation of 833 gigawatt-hours.
    Applicant Contact: Ramya Swaminathan, Vice President of
Development, Free Flow Power Corporation, 33 Commercial Street,
Gloucester, MA 01930; phone:<PHONE_NUMBER>.
    FERC Contact: Kim Carter,<PHONE_NUMBER>.
    Deadline for filing comments, motions to intervene, competing
applications (without notices of intent), or notices of intent to file
competing applications: 60 days from the issuance of this notice.
Comments, motions to intervene, notices of intent, and competing
applications may be filed electronically via the Internet. See 18 CFR
385.2001(a)(1)(iii) and the instructions on the Commission's Web site
under the ``e-Filing'' link. If unable to be filed electronically,
documents may be paper-filed. To paper-file, an original and eight
copies should be mailed to: Kimberly D. Bose, Secretary, Federal Energy
Regulatory Commission, 888 First Street, NE., Washington, DC 20426. For
more information on how to submit these types of filings, please go to
the Commission's Web site located at http://www.ferc.gov/filing-
comments.asp. More information about this project, including a copy of
the application, can be viewed or printed on the ``eLibrary'' link of
Commission's Web site at http://www.ferc.gov/docs-filing/elibrary.asp.
Enter the docket number (P-13497) in the docket number field to access
the document. For assistance, call toll-free 1-866-208-3372.

Kimberly D. Bose,
Secretary.
[FR Doc. E9-16989 Filed 7-16-09; 8:45 am]

BILLING CODE 6717-01-P


[Federal Register Volume 88, Number 137 (Wednesday, July 19, 2023)]
[Proposed Rules]
[Pages 46115-46118]
[FR Doc No: 2023-15192]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1495; Project Identifier MCAI-2023-00492-T]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2020-03-24, which applies certain Dassault Aviation Model MYSTERE-
FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes. AD 2020-03-24 requires
revising the existing maintenance or inspection program, as applicable,
to incorporate new or more restrictive airworthiness limitations. Since
the FAA issued AD 2020-03-24, the FAA has determined that new or more
restrictive airworthiness limitations are necessary. This proposed AD
would continue to require the actions in AD 2020-03-24 and require
revising the existing maintenance or inspection program, as applicable,
to incorporate new or more restrictive airworthiness limitations, as
specified in a European Union Aviation Safety Agency (EASA) AD, which
is proposed for incorporation by reference (IBR). The FAA is proposing
this AD to address the unsafe condition on these products.

DATES: The FAA must receive comments on this proposed AD by September
5, 2023.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to regulations.gov. Follow
the instructions for submitting comments.
     Fax:<PHONE_NUMBER>.
     Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
     Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-1495; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this NPRM, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
street address for Docket Operations is listed above.
    Material Incorporated by Reference:
     For material that is proposed for IBR in this NPRM,
contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone
+49 221 8999 000; email: [email protected]; website: easa.europa.eu.
You may find this material on the EASA website: ad.easa.europa.eu. It
is also available at regulations.gov under Docket No. FAA-2023-1495.
     For service information identified in this NPRM, contact
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000,
South Hackensack, NJ 07606; telephone<PHONE_NUMBER>; website:
dassaultfalcon.com.
     You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200 South
216th Street, Des Moines, WA. For information on the availability of
this material at the FAA, call<PHONE_NUMBER>.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone:<PHONE_NUMBER>; email: [email protected].

SUPPLEMENTARY INFORMATION:

Comments Invited

    The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2023-1495; Project Identifier
MCAI-2023-00492-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider

all comments received by the closing date and may amend this proposal
because of those comments.
    Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this NPRM.

Confidential Business Information

    CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to Tom
Rodriguez, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; phone:<PHONE_NUMBER>; email:
[email protected]. Any commentary that the FAA receives that is not
specifically designated as CBI will be placed in the public docket for
this rulemaking.

Background

    The FAA issued AD 2020-03-24, Amendment 39-19848 (85 FR 11289,
February 27, 2020) (AD 2020-03-24), for certain Dassault Aviation Model
MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes. AD 2020-03-24
was prompted by an MCAI originated by EASA, which is the Technical
Agent for the Member States of the European Union. EASA issued AD 2019-
0201, dated August 20, 2019 (EASA 2019-0201) (which corresponds to FAA
AD 2020-03-24), to correct an unsafe condition.
    AD 2020-03-24 requires revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. The FAA issued AD 2020-03-24 to
address fatigue cracking, damage, and corrosion in principal structural
elements, which could result in reduced structural integrity of the
airplane. AD 2020-03-24 specifies that accomplishing the revision
required by that AD terminates the requirements of paragraph (g)(1) of
AD 2010-26-05, Amendment 39-16544 (75 FR 79952, December 21, 2010), for
Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes on which
the SSIP [Supplemental Structural Inspection Program (Dassault Service
Bulletin 730)] has been embodied into the airplane's existing
maintenance or inspection program only. This proposed AD would
therefore continue to allow that terminating action.

Actions Since AD 2020-03-04 Was Issued

    Since the FAA issued AD 2020-03-04, EASA superseded AD 2019-0201
and issued EASA AD 2023-0062, dated March 20, 2023 (EASA AD 2023-0062)
(referred to after this as the MCAI), for certain Dassault Aviation
Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes. The MCAI
states that new or more restrictive airworthiness limitations have been
developed.
    The FAA is proposing this AD to address fatigue cracking, damage,
and corrosion in principal structural elements, which could result in
reduced structural integrity of the airplane. You may examine the MCAI
in the AD docket at regulations.gov under Docket No. FAA-2023-1495.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed EASA AD 2023-0062. This service information
specifies new or more restrictive airworthiness limitations for
airplane structures and safe life limits.
    This proposed AD would also require Chapter 5-40-01, Airworthiness
Limitations, of the Dassault Falcon 20 Retrofit 731 Maintenance Manual,
Revision 10, dated January 1, 2019, which the Director of the Federal
Register approved for incorporation by reference as of April 2, 2020
(85 FR 11289, February 27, 2020).
    This material is reasonably available because the interested
parties have access to it through their normal course of business or by
the means identified in ADDRESSES section.

FAA's Determination

    This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI and
service information referenced above. The FAA is issuing this NPRM
after determining that the unsafe condition described previously is
likely to exist or develop in other products of the same type design.

Proposed AD Requirements in This NPRM

    This proposed AD would retain the requirements of AD 2020-03-04.
This proposed AD would also require revising the existing maintenance
or inspection program, as applicable, to incorporate additional new or
more restrictive airworthiness limitations, which are specified in EASA
AD 2023-0062 already described, as proposed for incorporation by
reference. Any differences with EASA AD 2023-0062 are identified as
exceptions in the regulatory text of this AD.
    This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections).
Compliance with these actions is required by 14 CFR 91.403(c). For
airplanes that have been previously modified, altered, or repaired in
the areas addressed by this proposed AD, the operator may not be able
to accomplish the actions described in the revisions. In this
situation, to comply with 14 CFR 91.403(c), the operator must request
approval for an alternative method of compliance (AMOC) according to
paragraph (m)(1) of this proposed AD.

Explanation of Required Compliance Information

    In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some civil aviation
authority (CAA) ADs as the primary source of information for compliance
with requirements for corresponding FAA ADs. The FAA has been
coordinating this process with manufacturers and CAAs. As a result, the
FAA proposes to incorporate EASA AD 2023-0062 by reference in the FAA
final rule. This proposed AD would, therefore, require compliance with
EASA AD 2023-0062 through that incorporation, except for any
differences identified as exceptions in the regulatory text of this
proposed AD. Using common terms that are the same as the heading of a
particular section in EASA AD 2023-0062 does not mean that operators
need comply only with that section. For example, where the AD
requirement refers to ``all required actions and compliance times,''
compliance with this AD requirement is not limited to the section
titled ``Required Action(s) and Compliance Time(s)'' in EASA AD 2023-
0062.

Service information required by EASA AD 2023-0062 for compliance will
be available at regulations.gov by searching for and locating Docket
No. FAA-2023-1495 after the FAA final rule is published.

Airworthiness Limitation ADs Using the New Process

    The FAA's process of incorporating by reference MCAI ADs as the
primary source of information for compliance with corresponding FAA ADs
has been limited to certain MCAI ADs (primarily those with service
bulletins as the primary source of information for accomplishing the
actions required by the FAA AD). However, the FAA is now expanding the
process to include MCAI ADs that require a change to airworthiness
limitation documents, such as airworthiness limitation sections.
    For these ADs that incorporate by reference an MCAI AD that changes
airworthiness limitations, the FAA requirements are unchanged.
Operators must revise the existing maintenance or inspection program,
as applicable, to incorporate the information specified in the new
airworthiness limitation document. The airworthiness limitations must
be followed according to 14 CFR 91.403(c) and 91.409(e).
    The previous format of the airworthiness limitation ADs included a
paragraph that specified that no alternative actions (e.g.,
inspections) or intervals may be used unless the actions and intervals,
are approved as an AMOC in accordance with the procedures specified in
the AMOCs paragraph under ``Additional AD Provisions.'' This new format
includes a ``New Provisions for Alternative Actions and Intervals''
paragraph that does not specifically refer to AMOCs, but operators may
still request an AMOC to use an alternative action or interval.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would
affect 57 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
    The FAA estimates the total cost per operator for the retained
actions from AD 2020-03-24 to be $7,650 (90 work-hours x $85 per work-
hour).
    The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the agency recognizes that this number may vary from operator
to operator. Since operators incorporate maintenance or inspection
program changes for their affected fleet(s), the FAA has determined
that a per-operator estimate is more accurate than a per-airplane
estimate.
    The FAA estimates the total cost per operator for the new proposed
actions to be $7,650 (90 work-hours x $85 per work-hour).

Authority for This Rulemaking

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

Regulatory Findings

    The FAA 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 this proposed
regulation:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866,
    (2) Would not affect intrastate aviation in Alaska, and
    (3) Would 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:
0
a. Removing Airworthiness Directive 2020-03-24, Amendment 39-19848 (85
FR 11289, February 27, 2020); and
0
b. Adding the following new Airworthiness Directive:

Dassault Aviation: Docket No. FAA-2023-1495; Project Identifier
MCAI-2023-00492-T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive
(AD) by September 5, 2023.

(b) Affected ADs

    (1) This AD replaces AD 2020-03-24, Amendment 39-19848 (85 FR
11289, February 27, 2020) (AD 2020-03-24).
    (2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR
79952, December 21, 2010) (AD 2010-26-05).

(c) Applicability

    This AD applies to Dassault Aviation Model MYSTERE-FALCON 20-C5,
20-D5, 20-E5, and 20-F5 airplanes, certificated in any category, on
which the Supplemental Structural Inspection Program (SSIP)
(Dassault Service Bulletin 730) has been embodied into the
airplane's existing maintenance or inspection program.

(d) Subject

    Air Transport Association (ATA) of America Code: 05, Time
Limits/Maintenance Checks.

(e) Unsafe Condition

    This AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
issuing this AD to address fatigue cracking, damage, and corrosion
in principal structural elements, which could result in reduced
structural integrity of the airplane.

(f) Compliance

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

(g) Retained Revision of the Existing Maintenance or Inspection
Program, With No Changes

    This paragraph restates the requirements of paragraph (g) of AD
2020-03-24, with no changes. Within 90 days after April 2, 2020 (the
effective date of AD 2020-03-24), revise the existing maintenance or
inspection program, as applicable, to incorporate the information
specified in Chapter 5-40-01, Airworthiness Limitations, of the
Dassault Falcon 20 Retrofit 731 Maintenance Manual, Revision 10,
dated January 1, 2019. The initial compliance time for doing the
tasks is at the applicable time specified in Chapter 5-

40-01, Airworthiness Limitations, of the Dassault Falcon 20 Retrofit
731 Maintenance Manual, Revision 10, dated January 1, 2019; or
within 90 days after April 2, 2020; whichever occurs later.
Accomplishing the revision of the existing maintenance or inspection
program required by paragraph (i) of this AD terminates the
requirements of this paragraph.

(h) Retained No Alternative Actions or Intervals, With a New Exception

    This paragraph restates the requirements of paragraph (h) of AD
2020-03-24, with a new exception. Except as required by paragraph
(i) of this AD, after the existing maintenance or inspection program
has been revised as required by paragraph (g) of this AD, no
alternative actions (e.g., inspections) or intervals may be used
unless the actions or intervals are approved as an alternative
method of compliance (AMOC) in accordance with the procedures
specified in paragraph (m)(1) of this AD.

(i) New Revision of the Existing Maintenance or Inspection Program

    Except as specified in paragraph (j) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, European Union Aviation Safety Agency (EASA) AD
2023-0062, dated March 20, 2023 (EASA AD 2023-0062). Accomplishing
the revision of the existing maintenance or inspection program
required by this paragraph terminates the requirements of paragraph
(g) of this AD.

(j) Exceptions to EASA AD 2023-0062

    (1) This AD does not adopt the requirements specified in
paragraphs (1) and (2) of EASA AD 2023-0062.
    (2) Paragraph (3) of EASA AD 2023-0062 specifies revising ``the
approved AMP'' within 12 months after its effective date, but this
AD requires revising the existing maintenance or inspection program,
as applicable, within 90 days after the effective date of this AD.
    (3) The initial compliance time for doing the tasks specified in
paragraph (3) of EASA AD 2023-0062 is at the applicable
``limitations'' and ``associated thresholds'' as incorporated by the
requirements of paragraph (3) of EASA AD 2023-0062 or within 90 days
after the effective date of this AD, whichever occurs later.
    (4) This AD does not adopt the provisions specified in
paragraphs (4) and (5) of EASA AD 2023-0062.
    (5) This AD does not adopt the ``Remarks'' section of EASA AD
2023-0062.

(k) New Provisions for Alternative Actions and Intervals

    After the existing maintenance or inspection program has been
revised as required by paragraph (i) of this AD, no alternative
actions (e.g., inspections) and intervals are allowed unless they
are approved as specified in the provisions of the ``Ref.
Publications'' section of EASA AD 2023-0062.

(l) Terminating Action for AD 2010-26-05

    Accomplishing the actions required by paragraph (g) or (i) of
this AD terminates the requirements of paragraph (g)(1) of AD 2010-
26-05, for Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5
airplanes on which the SSIP has been embodied into the airplane's
existing maintenance or inspection program only.

(m) Additional AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
International Validation Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the procedures found in 14 CFR
39.19. In accordance with 14 CFR 39.19, send your request to your
principal inspector or responsible Flight Standards Office, as
appropriate. If sending information directly to the International
Validation Branch, send it to the attention of the person identified
in paragraph (n) of this AD. Information may be emailed to: [email protected]. Before using any approved AMOC, notify your
appropriate principal inspector, or lacking a principal inspector,
the manager of the responsible Flight Standards Office.
    (2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
Validation Branch, FAA; or EASA; or Dassault Aviation's EASA Design
Organization Approval (DOA). If approved by the DOA, the approval
must include the DOA-authorized signature.

(n) Additional Information

    For more information about this AD, contact Tom Rodriguez,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone:<PHONE_NUMBER>; email:
[email protected].

(o) 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.
    (3) The following service information was approved for IBR on
[DATE 35 DAYS AFTER PUBLICATION OF THE FINAL RULE].
    (i) European Union Aviation Safety Agency (EASA) AD 2023-0062,
dated March 20, 2023.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on
April 2, 2020 (85 FR 11289, February 27, 2020).
    (i) Chapter 5-40-01, Airworthiness Limitations, of the Dassault
Falcon 20 Retrofit 731 Maintenance Manual, Revision 10, dated
January 1, 2019.
    (ii) [Reserved]
    (5) For EASA AD 2023-0062, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email:
[email protected]; website: easa.europa.eu. You may find this EASA
AD on the EASA website: ad.easa.europa.eu.
    (6) For service information identified in this AD, contact
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000,
South Hackensack, NJ 07606; telephone<PHONE_NUMBER>; website
dassaultfalcon.com.
    (7) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th Street, Des Moines, WA. For information on the
availability of this material at the FAA, call<PHONE_NUMBER>.
    (8) 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, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on July 12, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-15192 Filed 7-18-23; 8:45 am]
BILLING CODE 4910-13-P