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2020-03-19 DASSAULT AVIATION: Amendment 39-19843; Docket No. FAA-2019-0868; Product Identifier 2019-NM-152-AD.
(a) EFFECTIVE DATE

    This AD is effective April 2, 2020.

(b) AFFECTED ADS

    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  Dassault Aviation  Model  MYSTERE-FALCON 20-C5,
    20-D5, 20-E5 and 20-F5 airplanes, certificated in any category, except
    those on which the  Supplemental Structural Inspection Program  (SSIP)
    (Dassault Service Bulletin 730) has been embodied into the  airplane’s
    existing maintenance or inspection program.

(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,  which   could  result  in   reduced  structural
    integrity of the airplane.

(f) COMPLIANCE

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

(g) MAINTENANCE OR INSPECTION PROGRAM REVISION

    Within 90 days after the effective date of this AD,  revise the exist-
    ing maintenance or inspection  program, as applicable, to  incorporate
    the   information   specified   in   Chapter   5-40-00,  Airworthiness
    Limitations,  of  the  Dassault  Falcon  20  Retrofit  731 Maintenance
    Manual, Revision  13, dated  January 1,  2019. The  initial compliance
    time for doing the tasks is at the time specified in Chapter  5-40-00,
    Airworthiness  Limitations,  of  the Dassault  Falcon 20  Retrofit 731
    Maintenance Manual, Revision 13, dated  January 1, 2019, or within  90
    days after the effective date of this AD, whichever occurs later.

(h) NO ALTERNATIVE ACTIONS OR INTERVALS

    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 (j)(1)  of this
    AD.

(i) TERMINATING ACTION FOR CERTAIN REQUIREMENTS OF AD 2010-26-05

    Accomplishing the actions required  by this AD terminates the require-
    ments of paragraph (g)(1) of AD 2010-26-05  only  for  Model  MYSTERE-
    FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes  on which the SSIP has
    not been embodied  into the airplane’s existing maintenance or inspec-
    tion program.

(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)(2) 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  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.

(k) RELATED INFORMATION

(1) Refer  to  Mandatory Continuing Airworthiness Information  (MCAI) EASA
    AD 2019-0200R1,  dated August 29, 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-2019-0868

(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 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) Chapter 5-40-00,  Airworthiness Limitations, of the Dassault Falcon 20
    Retrofit 731 Maintenance Manual, Revision 13, dated January 1, 2019.

(ii) [Reserved]

(3) For service information identified in this AD, contact Dassault Falcon
    Jet Corporation, Teterboro Airport, PO Box 2000,  South Hackensack, NJ
    07606; telephone 201-440-6700; Internet https://www.dassaultfalcon.com

(4) 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.

(5) You  may  view  this  service  information  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  February 12, 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-2019-0868; Product Identifier 2019-NM-152-AD; Amendment
39-19843; AD 2020-03-19]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

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

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Dassault Aviation Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and
20-F5 airplanes. This AD was prompted by a determination that new or
more restrictive airworthiness limitations are necessary. This AD
requires 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 the unsafe condition
on these products.

DATES: This AD is effective April 2, 2020.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 2,
2020.

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 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. It is also available on the internet at https://www.
regulations.gov by searching for and locating Docket No. FAA-2019-0868.

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-
0868; 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
Tom.Rodriguez@faa.gov.

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 2019-0200R1, dated August 29, 2019 (``EASA AD 2019-0200R1'')
(also referred to as the Mandatory Continuing Airworthiness
Information, or ``the MCAI''), to correct an unsafe condition for
certain Dassault Aviation Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and
20-F5 airplanes, except those on which the Supplemental Structural
Inspection Program (SSIP) (Dassault Service Bulletin 730) has been
embodied into the airplane's maintenance program. 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-2019-0868.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Dassault
Aviation Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes.
The NPRM published in the Federal Register on November 18, 2019 (84 FR
63585). 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, which 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:
Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
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, of the Dassault Falcon 20 Retrofit 731 Maintenance Manual,
Revision 13, dated January 1, 2019. This service information describes
procedures for airworthiness limitations for safe life limits and
certification maintenance requirements. 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 56 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD.
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 workhours 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.

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.

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):