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PROPOSED AD DASSAULT AVIATION: Docket No. FAA-2018-0549; Product Identifier 2018-NM-014-AD.
(a) COMMENTS DUE DATE

    We must receive comments by August 6, 2018.

(b) AFFECTED ADS

    None.

(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/Maint-
    enance Checks.

(e) REASON

    This  AD  was  prompted  by  a  determination  that  more  restrictive
    maintenance requirements and airworthiness limitations are  necessary.
    We  are  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) MAINTENANCE OR INSPECTION PROGRAM REVISION

    Within  90  days after  the  effective date  of  this AD,  revise  the
    maintenance  or  inspection  program,  as  applicable,  to incorporate
    Falcon 200  Maintenance Manual,  Airworthiness Limitations,  Chapter 5
    -40-00, Revision 17, dated  December 20, 2017. The  initial compliance
    time for accomplishing the actions is at the applicable time specified
    in Falcon 200  Maintenance Manual, Airworthiness  Limitations, Chapter
    5-40-00, Revision 17, dated December 20, 2017; or within 90 days after
    the effective date of this AD; whichever occurs later.

(h) NO ALTERNATIVE ACTIONS OR INTERVALS

    After  the  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 (i)(1)  of this
    AD.

(i) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) ALTERNATIVE METHODS OF COMPLIANCE (AMOCs): The  Manager, 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 (j)(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
    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  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.

(j) RELATED INFORMATION

(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD
    2018-0009, dated January 15, 2018, for related information. This  MCAI
    may   be   found   in   the    AD   docket   on   the   internet    at
    http://www.regulations.gov by  searching for  and locating  Docket No.
    FAA-2018-0549.

(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.

(3) 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  http://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.

Issued in  Des Moines,  Washington, on  June 12,  2018. Michael  Kaszycki,
Acting  Director,  System   Oversight  Division,  Aircraft   Certification
Service.

DATES: We must receive comments on this proposed AD by August 6, 2018.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


14 CFR Part 39

[Docket No. FAA-2018-0549; Product Identifier 2018-NM-014-AD]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for all
Dassault Aviation Model MYSTERE-FALCON 200 airplanes. This proposed AD
was prompted by a determination that more restrictive maintenance
requirements and airworthiness limitations are necessary. This proposed
AD would require revising the maintenance or inspection program, as
applicable, to incorporate new or more restrictive maintenance
requirements and airworthiness limitations. We are proposing this AD to
address the unsafe condition on these products.

DATES: We must receive comments on this proposed AD by August 6, 2018.

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 http://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: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.

For service information identified in this NPRM, contact Dassault
Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South
Hackensack, NJ 07606; telephone 201-440-6700; internet
http://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.

Examining the AD Docket

You may examine the AD docket on the internet at http://www.regulations.gov
by searching for and locating Docket No. FAA-2018-
0549; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains this NPRM, the regulatory evaluation, any comments received,
and other information. The street address for the Docket Operations
office (telephone 800-647-5527) is in the ADDRESSES section. 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.

SUPPLEMENTARY INFORMATION:

Comments Invited


We invite you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under the ADDRESSES section. Include "Docket No. FAA-2018-0549;
Product Identifier 2018-NM-014-AD" at the beginning of your comments.
We specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of this NPRM. We will consider all
comments received by the closing date and may amend this NPRM based on
those comments.
We will post all comments we receive, without change, to
http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this NPRM.

Discussion

The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA AD
2018-0009, dated January 15, 2018 (referred to after this as the
Mandatory Continuing Airworthiness Information, or "the MCAI"), to
correct an unsafe condition for all Dassault Aviation Model MYSTERE-
FALCON 200 airplanes. The MCAI states:

The airworthiness limitations for Dassault Mystere Falcon
200 aeroplanes, which are approved by EASA, are currently defined
and published in AMM [aircraft maintenance manual] ALS
[airworthiness limitations section] Chapter 5-40. These instructions
have been identified as mandatory for continued airworthiness.

Failure to accomplish these instructions could result in an
unsafe condition.

EASA previously issued AD 2008-0221 (later corrected), requiring
the actions described in Dassault Mystere Falcon 200 AMM
Chapter 5-40 (DMD 18740A) at Revision 14. Since that [EASA] AD was
issued, Dassault published the ALS, containing new and/or more
restrictive maintenance tasks.

For the reason described above, this [EASA] AD takes over the
requirements for Mystere Falcon 200 aeroplanes from EASA AD
2008-0221 and requires accomplishment of the actions specified in
the ALS.

You may examine the MCAI in the AD docket on the internet at
http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0549.

Related Service Information Under 1 CFR Part 51

Dassault Aviation has issued Falcon 200 Maintenance Manual,
Airworthiness Limitations, Chapter 5-40-00, Revision 17, dated December
20, 2017. The service information describes mandatory maintenance tasks
that operators must perform at specified intervals. 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.

FAA's Determination and Requirements of This Proposed AD

This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are proposing this AD because we
evaluated all pertinent information and determined an unsafe condition
exists and is likely to exist or develop on other products of the same
type design.

This AD requires revisions to certain operator maintenance
documents to include new actions (e.g., inspections). Compliance with
these actions is required by 14 CFR 91.403(c). For airplanes that have
been previously modified, altered, or repaired in the areas addressed
by this proposed AD, the operator may not be able to accomplish the
actions described in the revisions. In this situation, to comply with
14 CFR 91.403(c), the operator must request approval for an alternative
method of compliance according to paragraph (i)(1) of this proposed AD.
The request should include a description of changes to the required
actions that will ensure the continued damage tolerance of the affected
structure.

Difference Between This Proposed AD and the MCAI or Service Information

The MCAI specifies that if there are findings from the
airworthiness limitations section (ALS) inspection tasks, corrective
actions must be accomplished in accordance with Dassault maintenance
documentation. However, this proposed AD does not include that
requirement. Operators of U.S.-registered airplanes are required by
general airworthiness and operational regulations to perform
maintenance using methods that are acceptable to the FAA. We consider
those methods to be adequate to address any corrective actions
necessitated by the findings of ALS inspections required by this
proposed AD.

Costs of Compliance

We estimate that this proposed AD affects 9 airplanes of U.S.
registry. We estimate the following costs to comply with this proposed AD:

We have determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although we
recognize that this number may vary from operator to operator. In the
past, we have estimated that this action takes 1 work-hour per
airplane. Since operators incorporate maintenance or inspection program
changes for their affected fleet(s), we have determined that a per-
operator estimate is more accurate than a per-airplane estimate. Therefore,
we estimate 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.

We are 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 proposed 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 to the Director of the System Oversight
Division.

Regulatory Findings

We determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed regulation:

1. Is not a "significant regulatory action" under Executive Order 12866;

2. Is not a "significant rule" under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);

3. Will not affect intrastate aviation in Alaska; and

4. 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.

The Proposed Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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):