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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 air-
    planes, 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 exist-
    ing 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 para-
    graph (m)(2) of this AD. Information may be emailed to: 9-ANM-116-AMOC
    -REQUESTS@faa.gov.

(i) Before using any approved AMOC,  notify your appropriate principal in-
    spector,  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 Tom.Rodriguez@faa.gov.

(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,  PO 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 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 January 15, 2020.  Dionne Palermo, Acting Director, System Over-
sight 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-2019-0857; 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 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
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 2019-0153, 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:
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, 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
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 removing Airworthiness Directive (AD)
2018-19-26, Amendment 39-19427 (83 FR 49275, October 1, 2018), and
adding the following new AD: