Published 2020-03-11 · Federal Register document 2020-04999
Airworthiness Directives; Dassault Aviation Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for certain Dassault Aviation Model FALCON 7X airplanes. This AD was prompted by a report of an incorrect version of EASy "Top-Level System" operational software installed in the avionics system due to use of an improper CD-ROM. This AD requires ensuring that the correct versions of the operational software and CD-ROM are installed, and doing corrective action if necessary, 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 2026-09-03T22:24:04.586324+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2020-f01fbc4d7ab3dbaa
- Source row
- results[61]
- Raw source SHA-256
- f01fbc4d7ab3dbaae6a412acd9ff6cece48db77a6a882e46e8f8087200be3837
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2020-05-10
- Effective date printed in this edition
- 2020-03-26
Read 12 complete recorded clauses
Effective Date
(a) Effective Date
This AD becomes effective March 26, 2020.
Exact source excerpt. Text positions 13849–13916, end exclusive, in the original decoded publication. SHA-256: 19f6d6c0ff69e7e9e7af02e43adc507f3d623d9e8b7d02d45cb92cb6f5f295cc
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 13916–13945, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Dassault Aviation Model FALCON 7X airplanes,
certificated in any category, as identified in European Union
Aviation Safety Agency (EASA) AD 2020-0014, dated January 29, 2020
(``EASA AD 2020-0014'').
Exact source excerpt. Text positions 13945–14190, end exclusive, in the original decoded publication. SHA-256: bfd89f478008a71c997fb4aa3caca37b60bc6dc472004dadc90d0a9bacda834a
Subject
(d) Subject
Air Transport Association (ATA) of America Code 34, Navigation.
Exact source excerpt. Text positions 14190–14272, end exclusive, in the original decoded publication. SHA-256: 0542bcd80d4296f1663f9c1a9ee6733c7599b54c556ebcd2abd87a0d6015adff
Reason
(e) Reason
This AD was prompted by a report of an incorrect version of EASy
``Top-Level System'' operational software installed in the avionics
system due to use of an improper CD-ROM. The FAA is issuing this AD
to address misleading information and erroneous guidance affecting
the functional capabilities of the avionics system, which could
result in reduced control of the airplane.
Exact source excerpt. Text positions 14272–14669, end exclusive, in the original decoded publication. SHA-256: 83d36081d73948c627d4e5d589997945fa9fd7f01638ea22fec50ead90c389a8
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 14669–14771, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Requirements
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, EASA AD 2020-0014.
Exact source excerpt. Text positions 14771–14956, end exclusive, in the original decoded publication. SHA-256: 76ecd3bccdcf215d86918c8b992774195e5606642017fb1a0f3c69d8f2ebdb03
Exceptions to EASA AD 2020-0014
(h) Exceptions to EASA AD 2020-0014
(1) Where EASA AD 2020-0014 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The ``Remarks'' section of EASA AD 2020-0014 does not apply
to this AD.
Exact source excerpt. Text positions 14956–15192, end exclusive, in the original decoded publication. SHA-256: 5dc3e10eba9477afe834251a3df1d491bbbbf657f278df82a19057729f0e250f
No Reporting Requirement
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2020-0014
specifies to submit certain information and send a ``wrong CD-ROM''
to the manufacturer, this AD does not include that requirement.
Exact source excerpt. Text positions 15192–15426, end exclusive, in the original decoded publication. SHA-256: d0d4fa718c42b0d7f0f8b4e9ba709ea50a425518eb910df7cde39382b15183b3
Other FAA AD Provisions
(j) 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 (k) 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 local flight
standards district office/certificate holding district 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
Section, Transport Standards 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 15426–16683, end exclusive, in the original decoded publication. SHA-256: 251982ecb18bd8423ec91668f88bc8806b089eea9aae8035e7ec9de677647261
Related Information
(k) Related Information
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 16683–16952, end exclusive, in the original decoded publication. SHA-256: 78c4dfcefda7b8fcc4494ed9c40af7f6e90d14f4087a0dc43b823ec1af43a53b
Material Incorporated by Reference
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2020-0014,
dated January 29, 2020.
(ii) [Reserved]
(3) For information about EASA AD 2020-0014, contact the EASA,
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221
89990 6017; email [email protected]; internet www.easa.europa.eu.
You may find this EASA AD on the EASA website at https://ad.easa.europa.eu.
(4) You may view this material 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. This
material may be found in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-
2020-0198.
(5) 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: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 16952–18348, end exclusive, in the original decoded publication. SHA-256: ac01fdd51ba9f8df7f7d92a967831b2c771b9fc9de23cdc1dcc553eaf7927dd0
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 2020-05-10 · 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: 59cbe466c10f87a44f49107c1e505da8cc9fa842b3bace36ae3139e548820d0c. Source manifest: 9a1c07af0801284052cf12c0d459288e07b3e8fadb9ff68f1406029a60d86554.
Official source · 2020-03-11
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 48 (Wednesday, March 11, 2020)]
[Rules and Regulations]
[Pages 14143-14145]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-04999]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
========================================================================
Federal Register / Vol. 85, No. 48 / Wednesday, March 11, 2020 /
Rules and Regulations
[[Page 14143]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0198; Product Identifier 2020-NM-018-AD; Amendment
39-19859; AD 2020-05-10]
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Dassault Aviation Model FALCON 7X airplanes. This AD was
prompted by a report of an incorrect version of EASy ``Top-Level
System'' operational software installed in the avionics system due to
use of an improper CD-ROM. This AD requires ensuring that the correct
versions of the operational software and CD-ROM are installed, and
doing corrective action if necessary, 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.
DATES: This AD becomes effective March 26, 2020.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 26,
2020.
The FAA must receive comments on this AD by April 27, 2020.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> 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.
<bullet> Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
For the material incorporated by reference (IBR) in this AD,
contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
telephone +49 221 89990 1000; email [email protected]; internet
www.easa.europa.eu. You may find this IBR material on the EASA website
at https://ad.easa.europa.eu. You may view this IBR material 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. It is also available in the AD docket on the internet at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2020-0198.
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-2020-
0198; 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 AD, the regulatory evaluation, any comments received, and other
information. The street address for Docket Operations is listed above.
Comments will be available in the AD docket shortly after receipt.
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 EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2020-0014, dated January 29, 2020
(``EASA AD 2020-0014'') (also referred to as the Mandatory Continuing
Airworthiness Information, or ``the MCAI''), to correct an unsafe
condition for certain Dassault Aviation Model FALCON 7X airplanes.
This AD was prompted by a report of an incorrect version of EASy
``Top-Level System'' operational software loaded into the avionics
system due to the use of an improper CD-ROM. The FAA is issuing this AD
to address misleading information and erroneous guidance affecting the
functional capabilities of the avionics system, which could result in
reduced control of the airplane. See the MCAI for additional background
information.
Related IBR Material Under 1 CFR Part 51
EASA AD 2020-0014 describes procedures for ensuring that correct
versions of EASy ``Top-Level System'' operational software and CD-ROM
are installed. EASA AD 2020-0014 also describes procedures for
applicable corrective actions, which include amending the applicable
airplane flight manual (AFM) to limit the use of the software during
descent, and installing the correct version of the operational software
and CD-ROM, which eliminates the need for the AFM revision.
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 the 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 a bilateral agreement with the State of Design Authority, the FAA
has been notified of the unsafe condition described in the MCAI
referenced above. The FAA is issuing this AD because the agency
evaluated all pertinent information and determined the unsafe condition
exists and is likely to exist or develop on other products of the same
type design.
Requirements of This AD
This AD requires accomplishing the actions specified in the service
information described previously, as incorporated by reference, except
for any differences identified as exceptions in the regulatory text of
this AD.
[[Page 14144]]
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA initially worked with Airbus and EASA to develop a
process to use certain EASA ADs as the primary source of information
for compliance with requirements for corresponding FAA ADs. The FAA has
since coordinated with other manufacturers and civil aviation
authorities (CAAs) to use this process. As a result, EASA AD 2020-0014
is incorporated by reference in this final rule. This AD, therefore,
requires compliance with EASA AD 2020-0014 in its entirety, through
that incorporation, except for any differences identified as exceptions
in the regulatory text of this AD. Using common terms that are the same
as the heading of a particular section in the EASA AD 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 the
EASA AD. Service information specified in EASA AD 2020-0014 that is
required for compliance with EASA AD 2020-0014 is available on the
internet at https://www.regulations.gov by searching for and locating
Docket No. FAA-2020-0198.
FAA's Justification and Determination of the Effective Date
An unsafe condition exists that requires the immediate adoption of
this AD without providing an opportunity for public comments prior to
adoption. The FAA has found that the risk to the flying public
justifies waiving notice and comment prior to adoption of this rule
because misleading information and erroneous guidance affecting the
functional capabilities of the avionics system could result in reduced
control of the airplane. Therefore, the FAA finds good cause that
notice and opportunity for prior public comment are impracticable. In
addition, for the reasons stated above, the FAA finds that good cause
exists for making this amendment effective in less than 30 days.
Regulatory Flexibility Act (RFA)
The requirements of the RFA do not apply when an agency finds good
cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and
comment. Because the FAA has determined that it has good cause to adopt
this rule without notice and comment, RFA analysis is not required.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and the FAA did not precede it by notice and opportunity for
public comment. The FAA invites you to send any written relevant data,
views, or arguments about this AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2020-0198;
Product Identifier 2020-NM-018-AD'' at the beginning of your comments.
The FAA specifically invites comments on the overall regulatory,
economic, environmental, and energy aspects of this AD. The FAA will
consider all comments received by the closing date and may amend this
AD based on those comments.
The FAA will post all comments received, without change, to https://www.regulations.gov, including any personal information you provide.
The FAA will also post a report summarizing each substantive verbal
contact received about this AD.
Costs of Compliance
The FAA estimates that this AD affects 59 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
1 work-hour x $85 per hour = $85............................. $0 $85 $5,015
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary on-
condition actions that would be required based on the results of any
required actions. The FAA has no way of determining the number of
aircraft that might need these on-condition actions:
Estimated Costs of On-Condition Actions
------------------------------------------------------------------------
Cost per
Labor cost Parts cost product
------------------------------------------------------------------------
Up to 7 work-hours x $85 per hour = $0 $595
$595.................................
------------------------------------------------------------------------
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 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:
[[Page 14145]]
(1) Is not a ``significant regulatory action'' under Executive
Order 12866, and
(2) Will not affect intrastate aviation in Alaska.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2020-05-10 Dassault Aviation: Amendment 39-19859; Docket No. FAA-
2020-0198; Product Identifier 2020-NM-018-AD.
(a) Effective Date
This AD becomes effective March 26, 2020.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Dassault Aviation Model FALCON 7X airplanes,
certificated in any category, as identified in European Union
Aviation Safety Agency (EASA) AD 2020-0014, dated January 29, 2020
(``EASA AD 2020-0014'').
(d) Subject
Air Transport Association (ATA) of America Code 34, Navigation.
(e) Reason
This AD was prompted by a report of an incorrect version of EASy
``Top-Level System'' operational software installed in the avionics
system due to use of an improper CD-ROM. The FAA is issuing this AD
to address misleading information and erroneous guidance affecting
the functional capabilities of the avionics system, which could
result in reduced control of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, EASA AD 2020-0014.
(h) Exceptions to EASA AD 2020-0014
(1) Where EASA AD 2020-0014 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The ``Remarks'' section of EASA AD 2020-0014 does not apply
to this AD.
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2020-0014
specifies to submit certain information and send a ``wrong CD-ROM''
to the manufacturer, this AD does not include that requirement.
(j) 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 (k) 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 local flight
standards district office/certificate holding district 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
Section, Transport Standards 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.
(k) Related Information
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].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2020-0014,
dated January 29, 2020.
(ii) [Reserved]
(3) For information about EASA AD 2020-0014, contact the EASA,
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221
89990 6017; email [email protected]; internet www.easa.europa.eu.
You may find this EASA AD on the EASA website at https://ad.easa.europa.eu.
(4) You may view this material 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. This
material may be found in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-
2020-0198.
(5) 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: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on March 2, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020-04999 Filed 3-6-20; 4:15 pm]
BILLING CODE 4910-13-P
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
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