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Published 2023-04-13 · Federal Register document 2023-07751

Airworthiness Directives; Dassault Aviation Airplanes

Publication summary

The FAA is superseding Airworthiness Directive (AD) 2017-09-03 and AD 2018-20-07, which applied to all Dassault Aviation Model MYSTERE-FALCON 50 airplanes. AD 2017-09-03 and AD 2018-20-07 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD continues to require the actions in AD 2018-20-07 and requires 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 incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:14.395624+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2023-81e907e5105d0f2c
Source row
results[112]
Raw source SHA-256
81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2023-05-15
Effective date printed in this edition
2023-05-18
Read 15 complete recorded clauses
Effective Date
(a) Effective Date

    This airworthiness directive (AD) is effective May 18, 2023.

Exact source excerpt. Text positions 10611–10697, end exclusive, in the original decoded publication. SHA-256: 2844c2467bc9760770ff3ce82e23e561c2c52c24bbfeb16483685ba1efb7fb83

Affected ADs
(b) Affected ADs

    (1) This AD replaces AD 2017-09-03, Amendment 39-18865 (82 FR 
21467, May 9, 2017) (AD 2017-09-03) and AD 2018-20-07, Amendment 39-
19441 (83 FR 49789, October 3, 2018) (AD 2018-20-07).
    (2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR 
79952, December 21, 2010) (AD 2010-26-05);

Exact source excerpt. Text positions 10697–11015, end exclusive, in the original decoded publication. SHA-256: 2a66685160e836e9a1b49dcd9d6e0cb93e34ce4c548b2f91f5ae5e4bd5c4dfdf

Applicability wording · Applicability
(c) Applicability

    This AD applies to all Dassault Aviation Model MYSTERE-FALCON 50 
airplanes, certificated in any category.

Exact source excerpt. Text positions 11015–11146, end exclusive, in the original decoded publication. SHA-256: 90e9973755037528f7f1b70046a4bdb033dd4deccd167cabad1a9e4432b681f9

Subject
(d) Subject

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

Exact source excerpt. Text positions 11146–11249, end exclusive, in the original decoded publication. SHA-256: b15263823fded4455be00ff56d3a178d819d56a04f0615355cdb43771d1bcef9

Unsafe Condition
(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 reduced structural integrity of the 
airplane.

Exact source excerpt. Text positions 11249–11473, end exclusive, in the original decoded publication. SHA-256: 77efed63cf47fea44f3253e32f34f023d4f4b8840d8e168a1ade3e27743ff3f5

Compliance
(f) Compliance

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

Exact source excerpt. Text positions 11473–11575, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

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

    This paragraph restates the requirements of paragraph (g) of AD 
2018-20-07, with no changes. Within 90 days after November 7, 2018 
(the effective date of AD 2018-20-07), revise the maintenance or 
inspection program, as applicable, to incorporate the information 
specified in Chapter 5-40, Airworthiness Limitations, DGT 113872, 
Revision 24, dated July 2017, of the Dassault Falcon 50/50EX 
Maintenance Manual. The initial compliance times for doing the tasks 
are at the time specified in Chapter 5-40, Airworthiness 
Limitations, DGT 113872, Revision 24, dated July 2017, of the 
Dassault Falcon 50/50EX Maintenance Manual, or within 90 days after 
November 7, 2018, 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.

Exact source excerpt. Text positions 11575–12532, end exclusive, in the original decoded publication. SHA-256: dfbb1d1c8eeb1cb2eef65b557984ae2501b5c1a69adfb9247920a56bcc87329c

Retained Restrictions on Alternative Actions and Intervals With No Changes
(h) Retained Restrictions on Alternative Actions and Intervals With No 
Changes

    This paragraph restates the requirements of paragraph (h) of AD 
2018-20-07, with no changes. After the 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.

Exact source excerpt. Text positions 12532–13054, end exclusive, in the original decoded publication. SHA-256: ad708c972bf21a96e61ec71727ed981d2a26da0b26d089693036d6abe2f0d088

New Revision of the Existing Maintenance or Inspection Program
(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 
2022-0166, dated August 11, 2022 (EASA AD 2022-0166). Accomplishing 
the maintenance or inspection program revision specified in EASA AD 
2022-0166 as required by this paragraph terminates the requirements 
of paragraph (g) of this AD.

Exact source excerpt. Text positions 13054–13555, end exclusive, in the original decoded publication. SHA-256: e6a04efcbe826e47be45e14c6d8706700e00c39b7646ada16925f35468c65c64

Exceptions to EASA AD 2022-0166
(j) Exceptions to EASA AD 2022-0166

    (1) The requirements specified in paragraphs (1) and (2) of EASA 
AD 2022-0166 do not apply to this AD.
    (2) Paragraph (3) of EASA AD 2022-0166 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 2022-0166 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2022-0166, or within 90 
days after the effective date of this AD, whichever occurs later.
    (4) The provisions specified in paragraphs (4) and (5) of EASA 
AD 2022-0166 do not apply to this AD.
    (5) This AD does not adopt the ``Remarks'' section of EASA AD 
2022-0166.

Exact source excerpt. Text positions 13555–14487, end exclusive, in the original decoded publication. SHA-256: 9dff438eeab20dae1676e36a0d44e1500fe0ca838e02c3f02f2cbb963efc51b7

New Provisions for Alternative Actions and Intervals
(k) New Provisions for Alternative Actions and Intervals

    After the maintenance or inspection program has been revised as 
required by paragraph (g) of this AD, no alternative actions (e.g., 
inspections) or intervals are allowed unless they are approved as 
specified in the provisions of the ``Ref. Publications'' section of 
EASA AD 2022-0166.

Exact source excerpt. Text positions 14487–14839, end exclusive, in the original decoded publication. SHA-256: e485629aadf6d45d64e2a72d0875fee35cc8437bce1f01fe4555e3155b2727e2

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

    Accomplishing the actions required by paragraph (g) or (i) of 
this AD terminates the requirements of AD 2010-26-05 for Dassault 
Aviation Model MYSTERE-FALCON 50 airplanes only.

Exact source excerpt. Text positions 14839–15066, end exclusive, in the original decoded publication. SHA-256: 116ea06dd054904ea36ee6b319dc4e8460fc713d2bccd9ea43cdf7c8978728e5

Additional AD Provisions
(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

[[Page 22377]]

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.

Exact source excerpt. Text positions 15066–16270, end exclusive, in the original decoded publication. SHA-256: baa1a37696ff9159a31d6aa172f960113dcc4b3095b5952e1d1e36d13d08344c

Additional Information
(n) Additional Information

    For more information about this AD, contact Tom Rodriguez, 
Aerospace Engineer, Large Aircraft Section, International Validation 
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 
206-231-231-3226; email [email protected].

Exact source excerpt. Text positions 16270–16544, end exclusive, in the original decoded publication. SHA-256: d3900a29abef98a8af42485e91b429b46d8f6e35af66f685db09030d915475d9

Material Incorporated by Reference
(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 
May 18, 2023.
    (i) European Union Aviation Safety Agency (EASA) AD 2022-0166, 
dated August 11, 2022.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on 
November 7, 2018 (83 FR 49789, October 3, 2018).
    (i) Chapter 5-40, Airworthiness Limitations, DGT 113872, 
Revision 24, dated July 2017, of the Dassault Falcon 50/50EX 
Maintenance Manual.
    (ii) [Reserved]
    (5) For EASA AD 2022-0166, 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 at ad.easa.europa.eu.
    (6) For Dassault Falcon 50/50EX service information, contact 
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, 
South Hackensack, NJ 07606; telephone 201-440-6700; website 
dassaultfalcon.com.
    (7) You may view this material at the FAA, Airworthiness 
Products Section, Operational Safety Branch, 2200 South 216th St., 
Des Moines, WA. For information on the availability of this material 
at the FAA, call 206-231-3195.
    (8) You may view this material 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.

Exact source excerpt. Text positions 16544–18353, end exclusive, in the original decoded publication. SHA-256: b01f7f4cccc4356cac81f62eb23db61037ea82435d682ae5939174211eb95afb

No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.

Find all recorded historical references to AD 2023-05-15 · 0 printed reference observations in this pinned collection.

These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.

Why these observations are shown

They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.

Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 5842c7e05875e6a1fc08281400de4d4af6cc1114ef1eca5ee7837f545030a93f. Source manifest: a34950e097c1477091b1a31c4977695f62440013730f010e7e57a39016af5c98.

Official source · 2023-04-13

Publication text

This is the complete recorded text of this dated publication.

Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.

Read the complete official publication text
[Federal Register Volume 88, Number 71 (Thursday, April 13, 2023)]
[Rules and Regulations]
[Pages 22374-22377]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-07751]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-0013; Project Identifier MCAI-2022-01085-T; 
Amendment 39-22384; AD 2023-05-15]
RIN 2120-AA64


Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2017-09-03 
and AD 2018-20-07, which applied to all Dassault Aviation Model 
MYSTERE-FALCON 50 airplanes. AD 2017-09-03 and AD 2018-20-07 required 
revising the existing maintenance or inspection program, as applicable, 
to incorporate new or more restrictive airworthiness limitations. This 
AD was prompted by a determination that new or more restrictive 
airworthiness limitations are necessary. This AD continues to require 
the actions in AD 2018-20-07 and requires 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 incorporated by 
reference. The FAA is issuing this AD to address the unsafe condition 
on these products.

[[Page 22375]]


DATES: This AD is effective May 18, 2023.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of May 18, 
2023.
    The Director of the Federal Register approved the incorporation by 
reference of a certain other publication listed in this AD as of 
November 7, 2018 (83 FR 49789, October 3, 2018).

ADDRESSES: 
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2023-0013; or in person at Docket Operations between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD 
docket contains this final rule, the mandatory continuing airworthiness 
information (MCAI), any comments received, and other information. The 
address for Docket Operations is U.S. Department of Transportation, 
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 
New Jersey Avenue SE, Washington, DC 20590.
    Material Incorporated by Reference:
    <bullet> For the EASA AD incorporated by reference in this AD, 
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 at ad.easa.europa.eu.
    <bullet> For Dassault Falcon 50/50EX service information 
incorporated by reference in this AD, contact Dassault Falcon Jet 
Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 
07606; telephone 201-440-6700; website dassaultfalcon.com.
    <bullet> You may view this material at the FAA, Airworthiness 
Products Section, Operational Safety Branch, 2200 South 216th St., Des 
Moines, WA. For information on the availability of this material at the 
FAA, call 206-231-3195. It is also available in the AD docket at 
regulations.gov under Docket No. FAA-2023-0013.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, 
Large Aircraft Section, International Validation Branch, FAA, 2200 
South 216th St., Des Moines, WA 98198; telephone 206-231-3226; email 
[email protected].

SUPPLEMENTARY INFORMATION: 

Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 to supersede AD 2017-09-03, Amendment 39-18865 (82 FR 
21467, May 9, 2017) (AD 2017-09-03) and AD 2018-20-07, Amendment 39-
19441 (83 FR 49789, October 3, 2018) (AD 2018-20-07). AD 2017-09-03 and 
AD 2018-20-07 applied to all Dassault Aviation Model MYSTERE-FALCON 50 
airplanes. AD 2017-09-03 and AD 2018-20-07 required revising the 
existing maintenance or inspection program, as applicable, to 
incorporate new or more restrictive airworthiness limitations. The FAA 
issued AD 2017-09-03 and AD 2018-20-07 to address reduced structural 
integrity of the airplane.
    AD 2018-20-07 specifies that accomplishing the revision required by 
that AD terminates all requirements of AD 2017-09-03. AD 2018-20-07 
also specifies that it terminates the requirements of AD 2010-26-05, 
Amendment 39-16544 (75 FR 79952, December 21, 2010) (AD 2010-26-05) and 
AD 2012-02-18, Amendment 39-16941 (77 FR 12175, February 29, 2012) (AD 
2012-02-18) for certain Dassault Aviation Model MYSTERE-FALCON 50 
airplanes. AD 2012-02-18 has since been removed (84 FR 11640, March 28, 
2019). This AD therefore supersedes AD 2017-09-03 and terminates the 
requirements of AD 2010-26-05 for Dassault Aviation Model MYSTERE-
FALCON 50 airplanes only.
    The NPRM published in the Federal Register on January 13, 2023 (88 
FR 2292). The NPRM was prompted by AD 2022-0166, dated August 11, 2022, 
issued by EASA, which is the Technical Agent for the Member States of 
the European Union (EASA AD 2022-0166) (also referred to as the MCAI). 
The MCAI states that new or more restrictive airworthiness limitations 
have been developed.
    You may examine the MCAI in the AD docket at regulations.gov under 
Docket No. FAA-2023-0013.
    In the NPRM, the FAA proposed to continue to require the actions in 
AD 2018-20-07 and to require revising the existing maintenance or 
inspection program, as applicable, to incorporate new or more 
restrictive airworthiness limitations, as specified in EASA AD 2022-
0166. The FAA is issuing this AD to address reduced structural 
integrity of the airplane.

Discussion of Final Airworthiness Directive

Comments

    The FAA received no comments on the NPRM or on the determination of 
the cost to the public.

Conclusion

    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 
referenced above. The FAA reviewed the relevant data and determined 
that air safety requires adopting this AD as proposed. Accordingly, the 
FAA is issuing this AD to address the unsafe condition on this product. 
Except for minor editorial changes, this AD is adopted as proposed in 
the NPRM. None of the changes will increase the economic burden on any 
operator.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed EASA AD 2022-0166. This service information 
specifies new or more restrictive airworthiness limitations for 
airplane structures and safe life limits.
    This AD also requires Chapter 5-40, Airworthiness Limitations, DGT 
113872, Revision 24, dated July 2017, of the Dassault Falcon 50/50EX 
Maintenance Manual, which the Director of the Federal Register approved 
for incorporation by reference as of November 7, 2018 (83 FR 49789, 
October 3, 2018).
    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.

Costs of Compliance

    The FAA estimates that this AD affects 239 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:
    The FAA estimates the total cost per operator for the retained 
actions from AD 2018-20-07 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 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

[[Page 22376]]

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

Regulatory Findings

    This AD will not have federalism implications under Executive Order 
13132. This AD will not have a substantial direct effect on the States, 
on the relationship between the national government and the States, or 
on the distribution of power and responsibilities among the various 
levels of government.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Will not affect intrastate aviation in Alaska, and
    (3) Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

The Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by:
0
a. Removing Airworthiness Directive (AD) 2017-09-03, Amendment 39-18865 
(82 FR 21467, May 9, 2017) and AD 2018-20-07, Amendment 39-19441 (83 FR 
49789, October 3, 2018); and
0
b. Adding the following new airworthiness directive:

2023-05-15 Dassault Aviation: Amendment 39-22384; Docket No. FAA-
2023-0013; Project Identifier MCAI-2022-01085-T.

(a) Effective Date

    This airworthiness directive (AD) is effective May 18, 2023.

(b) Affected ADs

    (1) This AD replaces AD 2017-09-03, Amendment 39-18865 (82 FR 
21467, May 9, 2017) (AD 2017-09-03) and AD 2018-20-07, Amendment 39-
19441 (83 FR 49789, October 3, 2018) (AD 2018-20-07).
    (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 all Dassault Aviation Model MYSTERE-FALCON 50 
airplanes, certificated in any category.

(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 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 
2018-20-07, with no changes. Within 90 days after November 7, 2018 
(the effective date of AD 2018-20-07), revise the maintenance or 
inspection program, as applicable, to incorporate the information 
specified in Chapter 5-40, Airworthiness Limitations, DGT 113872, 
Revision 24, dated July 2017, of the Dassault Falcon 50/50EX 
Maintenance Manual. The initial compliance times for doing the tasks 
are at the time specified in Chapter 5-40, Airworthiness 
Limitations, DGT 113872, Revision 24, dated July 2017, of the 
Dassault Falcon 50/50EX Maintenance Manual, or within 90 days after 
November 7, 2018, 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 Restrictions on Alternative Actions and Intervals With No 
Changes

    This paragraph restates the requirements of paragraph (h) of AD 
2018-20-07, with no changes. After the 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 
2022-0166, dated August 11, 2022 (EASA AD 2022-0166). Accomplishing 
the maintenance or inspection program revision specified in EASA AD 
2022-0166 as required by this paragraph terminates the requirements 
of paragraph (g) of this AD.

(j) Exceptions to EASA AD 2022-0166

    (1) The requirements specified in paragraphs (1) and (2) of EASA 
AD 2022-0166 do not apply to this AD.
    (2) Paragraph (3) of EASA AD 2022-0166 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 2022-0166 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2022-0166, or within 90 
days after the effective date of this AD, whichever occurs later.
    (4) The provisions specified in paragraphs (4) and (5) of EASA 
AD 2022-0166 do not apply to this AD.
    (5) This AD does not adopt the ``Remarks'' section of EASA AD 
2022-0166.

(k) New Provisions for Alternative Actions and Intervals

    After the maintenance or inspection program has been revised as 
required by paragraph (g) of this AD, no alternative actions (e.g., 
inspections) or intervals are allowed unless they are approved as 
specified in the provisions of the ``Ref. Publications'' section of 
EASA AD 2022-0166.

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

    Accomplishing the actions required by paragraph (g) or (i) of 
this AD terminates the requirements of AD 2010-26-05 for Dassault 
Aviation Model MYSTERE-FALCON 50 airplanes 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

[[Page 22377]]

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, 
Aerospace Engineer, Large Aircraft Section, International Validation 
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 
206-231-231-3226; 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 
May 18, 2023.
    (i) European Union Aviation Safety Agency (EASA) AD 2022-0166, 
dated August 11, 2022.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on 
November 7, 2018 (83 FR 49789, October 3, 2018).
    (i) Chapter 5-40, Airworthiness Limitations, DGT 113872, 
Revision 24, dated July 2017, of the Dassault Falcon 50/50EX 
Maintenance Manual.
    (ii) [Reserved]
    (5) For EASA AD 2022-0166, 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 at ad.easa.europa.eu.
    (6) For Dassault Falcon 50/50EX service information, contact 
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, 
South Hackensack, NJ 07606; telephone 201-440-6700; website 
dassaultfalcon.com.
    (7) You may view this material at the FAA, Airworthiness 
Products Section, Operational Safety Branch, 2200 South 216th St., 
Des Moines, WA. For information on the availability of this material 
at the FAA, call 206-231-3195.
    (8) You may view this material 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 March 9, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2023-07751 Filed 4-12-23; 8:45 am]
BILLING CODE 4910-13-P


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