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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 al-
    ready done.

(g) REQUIREMENTS

    Except as specified  in paragraph (h) of this AD:  Comply with all re-
    quired 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: 9-ANM-116
    -AMOC-REQUESTS@faa.gov. 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
    Aviationís 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 tom.rodriguez@faa.gov.

(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 ADs@easa.europa.eu; 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 avail-
    ability 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 fedreg.legal@nara.
    gov,   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

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, Inter-
national Section,  Transport Standards Branch, FAA,  2200 South 216th St.,
Des Moines, WA 98198; telephone and fax 206-231-3226; email tom.rodriguez@
faa.gov.
PREAMBLE 

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:
Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions
for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: 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 ADs@easa.europa.eu; 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
tom.rodriguez@faa.gov.

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.

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

Labor cost
Parts cost
Cost per product
Cost on U.S. 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

Labor cost
Parts cost
Cost per product
Up to 7 work-hours x $85 per hour = $595
$0
$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:

(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

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]

2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):