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Published 2020-01-30 · Federal Register document 2020-01638

Airworthiness Directives; Dassault Aviation Airplanes

Publication summary

The FAA is superseding Airworthiness Directive (AD) 2018-19- 26, which applied to all Dassault Aviation Model MYSTERE-FALCON 200 airplanes. AD 2018-19-26 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive maintenance requirements and airworthiness limitations. This AD continues to require 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. 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 2026-09-03T22:24:04.586324+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2020-f01fbc4d7ab3dbaa
Source row
results[19]
Raw source SHA-256
f01fbc4d7ab3dbaae6a412acd9ff6cece48db77a6a882e46e8f8087200be3837

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2020-01-13
Effective date printed in this edition
2020-03-05
Read 14 complete recorded clauses
Effective Date
(a) Effective Date

    This AD is effective March 5, 2020.

Exact source excerpt. Text positions 9940–10001, end exclusive, in the original decoded publication. SHA-256: 4e4d65988a770c5839150706cbebd9ac51f433f5d9b36208af11d733b57743ae

Affected ADs
(b) Affected ADs

    (1) This AD replaces AD 2018-19-26, Amendment 39-19427 (83 FR 
49275, October 1, 2018) (``AD 2018-19-26'').
    (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 10001–10245, end exclusive, in the original decoded publication. SHA-256: b0131ac27c9ef94a804c7510baa8b749c8e186788d5cf4f86c4981d19437753f

Applicability wording · Applicability
(c) Applicability

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

Exact source excerpt. Text positions 10245–10377, end exclusive, in the original decoded publication. SHA-256: 7a9598b577de6f9f1297a63fb532488b29ee1f73cdd9488e0cf863fd8d453311

Subject
(d) Subject

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

Exact source excerpt. Text positions 10377–10480, end exclusive, in the original decoded publication. SHA-256: b15263823fded4455be00ff56d3a178d819d56a04f0615355cdb43771d1bcef9

Reason
(e) Reason

    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; such fatigue cracking, damage, and 
corrosion could result in reduced structural integrity of the 
airplane.

Exact source excerpt. Text positions 10480–10831, end exclusive, in the original decoded publication. SHA-256: fbcc0450dcab683e28bd1d7c34d8620ea6efe0d1d903a20548dd8331b39d995e

Compliance
(f) Compliance

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

Exact source excerpt. Text positions 10831–10933, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

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

    This paragraph restates the requirements of paragraph (g) of AD 
2018-19-26, with no changes. Within 90 days after November 5, 2018 
(the effective date of AD 2018-19-26), revise the existing 
maintenance or inspection program, as applicable, to incorporate 
Chapter 5-40-00, Airworthiness Limitations, Revision 17, dated 
December 20, 2017, of the Dassault Falcon 200 Maintenance Manual. 
The initial compliance time for accomplishing the actions is at the 
applicable time specified in Chapter 5-40-00, Airworthiness 
Limitations, Revision 17, dated December 20, 2017, of the Dassault 
Falcon 200 Maintenance Manual; or within 90 days after November 5, 
2018; whichever occurs later.

Exact source excerpt. Text positions 10933–11702, end exclusive, in the original decoded publication. SHA-256: fec2ee490e65a11537edc2bef39792d779754d148c914f46d23b880c473b2dd3

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

    This paragraph restates the requirements of paragraph (h) of AD 
2018-19-26, 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 (l)(1) of this AD.

Exact source excerpt. Text positions 11702–12278, end exclusive, in the original decoded publication. SHA-256: c00be720335eb6871e9973557e52a0708f38f182103dbdef36f56313e4c90c88

New Maintenance or Inspection Program Revision
(i) New Maintenance or Inspection Program Revision

    Within 90 days after the effective date of this AD, revise the 
existing maintenance or inspection program, as applicable, to 
incorporate the information specified in Chapter 5-40-00, 
Airworthiness Limitations, Revision 18, dated January 15, 2019, of 
the Dassault Falcon 200 Maintenance Manual. The initial compliance 
time for doing the tasks is at the time specified in Chapter 5-40-
00, Airworthiness Limitations, Revision 18, dated January 15, 2019, 
of the Dassault Falcon 200 Maintenance Manual, or within 90 days 
after the effective date of this AD, whichever occurs later.

Exact source excerpt. Text positions 12278–12920, end exclusive, in the original decoded publication. SHA-256: e6e5d042587ef003394a8571dc67d3d087d96e7df977ba8f5d55c08dec26ce06

New No Alternative Actions or Intervals
(j) New No Alternative Actions or 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) or intervals may be used unless the 
actions or intervals are approved as an AMOC in accordance with the 
procedures specified in paragraph (l)(1) of this AD.

Exact source excerpt. Text positions 12920–13285, end exclusive, in the original decoded publication. SHA-256: 3f7d41e2c038c79b3d3be31c00e1387dbbc3bb2e069949309f1e15e73e73f4e6

Terminating Action for Certain Actions in AD 2010-26-05
(k) Terminating Action for Certain Actions in 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 Dassault Aviation Model MYSTERE-FALCON 200 airplanes.

Exact source excerpt. Text positions 13285–13547, end exclusive, in the original decoded publication. SHA-256: 9eb3f2df5dc48eab6fe23ee24816d311ef6e068e898b0416077b3054faf52520

Other FAA AD Provisions
(l) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Section, Transport Standards 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 local Flight 
Standards District Office, as appropriate. If sending information 
directly to the International Section, send it to the attention of 
the person identified in paragraph (m)(2) of this AD. Information 
may be emailed to: [email protected].
    (i) 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.
    (ii) AMOCs approved previously for AD 2018-19-26, are approved 
as AMOCs for the corresponding provisions of 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, International 
Section, Transport Standards Branch, FAA; or the European Union 
Aviation Safety Agency (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 13547–14982, end exclusive, in the original decoded publication. SHA-256: 2bb7d0f84ec6e59f946309421b89e0062fed11164ee785ad5301b417e9d671ee

Related Information
(m) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA AD 2019-0153, dated July 3, 2019, for related 
information. This MCAI may be found in the AD docket on the internet 
at https://www.regulations.gov by searching for and locating Docket 
No. FAA-2019-0857.
    (2) For more information about this AD, contact Tom Rodriguez, 
Aerospace Engineer, International Section, Transport Standards 
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 
and fax 206-231-3226; email [email protected].

Exact source excerpt. Text positions 14982–15537, end exclusive, in the original decoded publication. SHA-256: 3b3b47e06cea5406ac016e50f2573089d2578b31cab56f911fe795b158422842

Material Incorporated by Reference
(n) 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 
March 5, 2020.
    (i) Chapter 5-40-00, Airworthiness Limitations, Revision 18, 
dated January 15, 2019, of the Dassault Falcon 200 Maintenance 
Manual.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on 
November 5, 2018 (83 FR 49275, October 1, 2018).
    (i) Chapter 5-40-00, Airworthiness Limitations, Revision 17, 
dated December 20, 2017, of the Dassault Falcon 200 Maintenance 
Manual.
    (ii) [Reserved]
    (5) For service information identified in this AD, contact 
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, 
South Hackensack, NJ 07606; telephone 201-440-6700; internet https://www.dassaultfalcon.com.
    (6) You may view this service information at the FAA, Transport 
Standards Branch, 2200 South 216th St., Des Moines, WA. For 
information on the availability of this material at the FAA, call 
206-231-3195.
    (7) You may view this service information that is incorporated 
by reference at the

[[Page 5316]]

National Archives and Records Administration (NARA). For information 
on the availability of this material at NARA, email 
[email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

Exact source excerpt. Text positions 15537–17173, end exclusive, in the original decoded publication. SHA-256: ce6b3cdbd1d528c33e8abe3148fdc6e5ac10588dd2bbb6d0a7b0eda4d08d8044

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 2020-01-13 · 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: 027fb29cedf631352e75f4f941a10775c0ec49c9217eb2d7cd5f839cf7596f6d. Source manifest: c4051460d909966a5caa6628a9a81583dbe308513f57be00a10f75a77b6ca2e5.

Official source · 2020-01-30

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 85, Number 20 (Thursday, January 30, 2020)]
[Rules and Regulations]
[Pages 5313-5316]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-01638]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0857; Product Identifier 2019-NM-124-AD; Amendment 
39-19819; AD 2020-01-13]
RIN 2120-AA64


Airworthiness Directives; Dassault Aviation Airplanes

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

ACTION: Final rule.

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

SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2018-19-
26, which applied to all Dassault Aviation Model MYSTERE-FALCON 200 
airplanes. AD 2018-19-26 required revising the existing maintenance or 
inspection program, as applicable, to incorporate new or more 
restrictive maintenance requirements and airworthiness limitations. 
This AD continues to require 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. The FAA is issuing this AD to address the unsafe 
condition on these products.

DATES: This AD is effective March 5, 2020.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of March 5, 
2020.
    The Director of the Federal Register approved the incorporation by 
reference of a certain other publication listed in this AD as of 
November 5, 2018 (83 FR 49275, October 1, 2018).

ADDRESSES: For service information identified in this final rule, 
contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 
2000, South Hackensack, NJ 07606; telephone 201-440-6700; internet 
https://www.dassaultfalcon.com. You may view this referenced service 
information at the FAA, Transport Standards Branch, 2200 South 216th 
St., Des

[[Page 5314]]

Moines, WA. For information on the availability of this material at the 
FAA, call 206-231-3195. It is also available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0857.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0857; 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 regulatory evaluation, 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.

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

SUPPLEMENTARY INFORMATION:

Discussion

    The European Union Aviation Safety Agency (EASA), which is the 
Technical Agent for the Member States of the European Union, has issued 
EASA AD 2019-0153, dated July 3, 2019 (``EASA AD 2019-0153'') (also 
referred to as the Mandatory Continuing Airworthiness Information, or 
``the MCAI''), to correct an unsafe condition for all Dassault Aviation 
Model MYSTERE-FALCON 200 airplanes. You may examine the MCAI in the AD 
docket on the internet at https://www.regulations.gov by searching for 
and locating Docket No. FAA-2019-0857.
    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 to supersede AD 2018-19-26, Amendment 39-19427 (83 FR 
49275, October 1, 2018) (``AD 2018-19-26''). AD 2018-19-26 applied to 
all Dassault Aviation Model MYSTERE-FALCON 200 airplanes. The NPRM 
published in the Federal Register on October 30, 2019 (84 FR 58070). 
The NPRM was prompted by a determination that new or more restrictive 
airworthiness limitations are necessary. The NPRM proposed to require 
revising the existing maintenance or inspection program, as applicable, 
to incorporate new or more restrictive airworthiness limitations. The 
FAA is issuing this AD to address fatigue cracking, damage, and 
corrosion in principal structural elements; such fatigue cracking, 
damage, and corrosion could result in reduced structural integrity of 
the airplane. See the MCAI for additional background information.

Comments

    The FAA gave the public the opportunity to participate in 
developing this final rule. The FAA received no comments on the NPRM or 
on the determination of the cost to the public.

Conclusion

    The FAA reviewed the relevant data and determined that air safety 
and the public interest require adopting this final rule as proposed, 
except for minor editorial changes. The FAA has determined that these 
minor changes:
    <bullet> Are consistent with the intent that was proposed in the 
NPRM for addressing the unsafe condition; and
    <bullet> Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

    Dassault Aviation has issued Chapter 5-40-00, Airworthiness 
Limitations, Revision 18, dated January 15, 2019, of the Dassault 
Falcon 200 Maintenance Manual. This service information describes 
mandatory maintenance tasks that operators must perform at specified 
intervals.
    This AD also requires Chapter 5-40-00, Airworthiness Limitations, 
Revision 17, dated December 20, 2017, of the Dassault Falcon 200 
Maintenance Manual, which the Director of the Federal Register approved 
for incorporation by reference as of November 5, 2018 (83 FR 49275, 
October 1, 2018).
    This service information is reasonably available because the 
interested parties have access to it through their normal course of 
business or by the means identified in the ADDRESSES section.

Costs of Compliance

    The FAA estimates that this AD affects 9 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 2018-19-26 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 FAA recognizes that this number may vary from operator to 
operator. In the past, the FAA has estimated that this action takes 1 
work-hour per airplane. 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. Therefore, the FAA estimates the total cost per 
operator 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.
    This AD is issued in accordance with authority delegated by the 
Executive Director, Aircraft Certification Service, as authorized by 
FAA Order 8000.51C. In accordance with that order, issuance of ADs is 
normally a function of the Compliance and Airworthiness Division, but 
during this transition period, the Executive Director has delegated the 
authority to issue ADs applicable to transport category airplanes and 
associated appliances to the Director of the System Oversight Division.

Regulatory Findings

    The FAA has 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) 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

[[Page 5315]]

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.

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 removing Airworthiness Directive (AD) 
2018-19-26, Amendment 39-19427 (83 FR 49275, October 1, 2018), and 
adding the following new AD:

2020-01-13 Dassault Aviation: Amendment 39-19819; Docket No. FAA-
2019-0857; Product Identifier 2019-NM-124-AD.

(a) Effective Date

    This AD is effective March 5, 2020.

(b) Affected ADs

    (1) This AD replaces AD 2018-19-26, Amendment 39-19427 (83 FR 
49275, October 1, 2018) (``AD 2018-19-26'').
    (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 
200 airplanes, certificated in any category.

(d) Subject

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

(e) Reason

    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; such fatigue cracking, damage, and 
corrosion 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 Maintenance or Inspection Program, With No 
Changes

    This paragraph restates the requirements of paragraph (g) of AD 
2018-19-26, with no changes. Within 90 days after November 5, 2018 
(the effective date of AD 2018-19-26), revise the existing 
maintenance or inspection program, as applicable, to incorporate 
Chapter 5-40-00, Airworthiness Limitations, Revision 17, dated 
December 20, 2017, of the Dassault Falcon 200 Maintenance Manual. 
The initial compliance time for accomplishing the actions is at the 
applicable time specified in Chapter 5-40-00, Airworthiness 
Limitations, Revision 17, dated December 20, 2017, of the Dassault 
Falcon 200 Maintenance Manual; or within 90 days after November 5, 
2018; whichever occurs later.

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

    This paragraph restates the requirements of paragraph (h) of AD 
2018-19-26, 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 (l)(1) of this AD.

(i) New Maintenance or Inspection Program Revision

    Within 90 days after the effective date of this AD, revise the 
existing maintenance or inspection program, as applicable, to 
incorporate the information specified in Chapter 5-40-00, 
Airworthiness Limitations, Revision 18, dated January 15, 2019, of 
the Dassault Falcon 200 Maintenance Manual. The initial compliance 
time for doing the tasks is at the time specified in Chapter 5-40-
00, Airworthiness Limitations, Revision 18, dated January 15, 2019, 
of the Dassault Falcon 200 Maintenance Manual, or within 90 days 
after the effective date of this AD, whichever occurs later.

(j) New No Alternative Actions or 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) or intervals may be used unless the 
actions or intervals are approved as an AMOC in accordance with the 
procedures specified in paragraph (l)(1) of this AD.

(k) Terminating Action for Certain Actions in 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 Dassault Aviation Model MYSTERE-FALCON 200 airplanes.

(l) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Section, Transport Standards 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 local Flight 
Standards District Office, as appropriate. If sending information 
directly to the International Section, send it to the attention of 
the person identified in paragraph (m)(2) of this AD. Information 
may be emailed to: [email protected].
    (i) 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.
    (ii) AMOCs approved previously for AD 2018-19-26, are approved 
as AMOCs for the corresponding provisions of 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, International 
Section, Transport Standards Branch, FAA; or the European Union 
Aviation Safety Agency (EASA); or Dassault Aviation's EASA Design 
Organization Approval (DOA). If approved by the DOA, the approval 
must include the DOA-authorized signature.

(m) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA AD 2019-0153, dated July 3, 2019, for related 
information. This MCAI may be found in the AD docket on the internet 
at https://www.regulations.gov by searching for and locating Docket 
No. FAA-2019-0857.
    (2) For more information about this AD, contact Tom Rodriguez, 
Aerospace Engineer, International Section, Transport Standards 
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 
and fax 206-231-3226; email [email protected].

(n) 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 
March 5, 2020.
    (i) Chapter 5-40-00, Airworthiness Limitations, Revision 18, 
dated January 15, 2019, of the Dassault Falcon 200 Maintenance 
Manual.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on 
November 5, 2018 (83 FR 49275, October 1, 2018).
    (i) Chapter 5-40-00, Airworthiness Limitations, Revision 17, 
dated December 20, 2017, of the Dassault Falcon 200 Maintenance 
Manual.
    (ii) [Reserved]
    (5) For service information identified in this AD, contact 
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, 
South Hackensack, NJ 07606; telephone 201-440-6700; internet https://www.dassaultfalcon.com.
    (6) You may view this service information at the FAA, Transport 
Standards Branch, 2200 South 216th St., Des Moines, WA. For 
information on the availability of this material at the FAA, call 
206-231-3195.
    (7) You may view this service information that is incorporated 
by reference at the

[[Page 5316]]

National Archives and Records Administration (NARA). For information 
on the availability of this material at NARA, email 
[email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on January 15, 2020.
Dionne Palermo,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2020-01638 Filed 1-29-20; 8:45 am]
BILLING CODE 4910-13-P


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