Rule2023-07751

Airworthiness Directives; Dassault Aviation Airplanes

Primary source

Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.

Published
April 13, 2023
Effective
May 18, 2023

Issuing agencies

Transportation DepartmentFederal Aviation Administration

Abstract

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.

Full Text

<html>
<head>
<title>Federal Register, Volume 88 Issue 71 (Thursday, April 13, 2023)</title>
</head>
<body><pre>
[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 [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[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 <a href="http://regulations.gov">regulations.gov</a> 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 <a href="/cdn-cgi/l/email-protection#a2e3e6d1e2c7c3d1c38cc7d7d0cdd2c38cc7d7"><span class="__cf_email__" data-cfemail="e7a6a394a782869486c9829295889786c98292">[email&#160;protected]</span></a>; 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 <a href="http://dassaultfalcon.com">dassaultfalcon.com</a>.
    <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 
<a href="http://regulations.gov">regulations.gov</a> 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 
<a href="/cdn-cgi/l/email-protection#2652494b08544942544f4153435c6640474708414950"><span class="__cf_email__" data-cfemail="a1d5cecc8fd3cec5d3c8c6d4c4dbe1c7c0c08fc6ced7">[email&#160;protected]</span></a>.

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 <a href="http://regulations.gov">regulations.gov</a> 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: <a href="/cdn-cgi/l/email-protection#360f1b7760651b777f641b0105061b777b79757650575718515940"><span class="__cf_email__" data-cfemail="84bda9c5d2d7a9c5cdd6a9b3b7b4a9c5c9cbc7c4e2e5e5aae3ebf2">[email&#160;protected]</span></a>. 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 <a href="/cdn-cgi/l/email-protection#82f6edefacf0ede6f0ebe5f7e7f8c2e4e3e3ace5edf4"><span class="__cf_email__" data-cfemail="d0a4bfbdfea2bfb4a2b9b7a5b5aa90b6b1b1feb7bfa6">[email&#160;protected]</span></a>.

(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 
<a href="/cdn-cgi/l/email-protection#5312172013363220327d3626213c23327d3626"><span class="__cf_email__" data-cfemail="2160655261444052400f4454534e51400f4454">[email&#160;protected]</span></a>; 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 
<a href="http://dassaultfalcon.com">dassaultfalcon.com</a>.
    (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 
<a href="/cdn-cgi/l/email-protection#bfd9cd91d6d1cccfdadccbd6d0d1ffd1decdde91d8d0c9"><span class="__cf_email__" data-cfemail="2345510d4a4d50534640574a4c4d634d4251420d444c55">[email&#160;protected]</span></a>, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">www.archives.gov/federal-register/cfr/ibr-locations.html</a>.

    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


</pre><script data-cfasync="false" src="/cdn-cgi/scripts/5c5dd728/cloudflare-static/email-decode.min.js"></script></body>
</html>
Indexed from Federal Register on April 13, 2023.

This is legal information, not legal advice. Laws vary by jurisdiction and change frequently. Always verify current law with official sources and consult a licensed attorney in your jurisdiction for advice on your specific situation.