preamble attached >>>
ADs updated daily at www.Tdata.com
PROPOSED AD DASSAULT AVIATION: Docket No. FAA-2019-0870; Product Identifier 2019-NM-125-AD.
(a) COMMENTS DUE DATE

    The FAA must receive comments by January 3, 2020.

(b) AFFECTED ADS

(1) This  AD  replaces  AD 2018-19-27,  Amendment  39-19428  (83 FR 50479,
    October 9, 2018) ("AD 2018-19-27");  and AD 2014-16-12,  Amendment 39-
    17936 (79 FR 52187, September 3, 2014) ("AD 2014-16-12").

(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  Dassault Aviation Model FALCON 2000EX airplanes,
    certificated in any category,  with an original airworthiness certifi-
    cate or  original export certificate of airworthiness issued on or be-
    fore January 15, 2019.

(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 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-
    19-27, with no  changes. Within 90  days after November  13, 2018 (the
    effective date of AD  2018-19-27), revise the existing  maintenance or
    inspection  program,  as applicable,  to  incorporate the  information
    specified  in  Chapter 5-40,  Airworthiness  Limitations, DGT  113877,
    Revision  11,  dated  November 2017,  of  the  Dassault Falcon  2000EX
    Maintenance Manual. The initial  compliance times for doing  the tasks
    are at the time specified in Chapter 5-40, Airworthiness  Limitations,
    DGT 113877, Revision 11, dated  November 2017, of the Dassault  Falcon
    2000EX Maintenance Manual, or within 90 days after November 13,  2018,
    whichever occurs  later; except  for task  number 52-20-00-610-801-01,
    the initial compliance time is within 24 months after October 8,  2014
    (the effective date  of AD 2014-16-12).  The term "LDG"  in the "First
    Inspection"  column  of  any  table  in  Chapter  5-40,  Airworthiness
    Limitations, DGT 113877, Revision 11, dated November 2017, means total
    airplane landings. The term "FH"  in the "First Inspection" column  of
    any  table  in  Chapter 5-40,  Airworthiness Limitations,  DGT 113877,
    Revision 11, dated November 2017,  means total flight hours. The  term
    "FC" in the  "First Inspection" column  of any table  in Chapter 5-40,
    Airworthiness  Limitations, DGT  113877, Revision  11, dated  November
    2017, means total flight cycles.

(h) RETAINED PROVISION: NO ALTERNATIVE ACTIONS OR INTERVALS,  WITH  A  NEW
    EXCEPTION

    This paragraph restates the requirements of paragraph (h)  of AD 2018-
    19-27, with a  new exception. Except  as required by  paragraph (i) of
    this AD, 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 (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, Airworthiness  Limitations,
    DGT 113877, Revision 12, dated  November 2018, of the Dassault  Falcon
    2000EX Maintenance Manual. The initial compliance times for doing  the
    tasks  are  at  the  time  specified  in  Chapter  5-40, Airworthiness
    Limitations,  DGT 113877,  Revision 12,  dated November  2018, of  the
    Dassault Falcon 2000EX Maintenance Manual, or within 90 days after the
    effective date  of this  AD, whichever  occurs later;  except for task
    number 52-20-00-610-801-01, the initial  compliance time is within  24
    months after October  8, 2014 (the  effective date of  AD 2014-16-12).
    The term "LDG" in  the "First Inspection" column  of any table in  the
    service information specified in  this paragraph means total  airplane
    landings. The term "FH" in the "First Inspection" column of any  table
    in the  service information  specified in  this paragraph  means total
    flight hours. The  term "FC" in  the "First Inspection"  column of any
    table in  the service  information specified  in this  paragraph means
    total flight  cycles. Doing  the revision  required by  this paragraph
    terminates the actions required by paragraph (g) of this AD.

(j) NEW PROVISION: 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 FALCON 2000EX airplanes.

(l) OTHER FAA AD PROVISIONS

(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 (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 2018-19-27 are not approved as AMOCs
     for this AD.

(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.

(m) RELATED INFORMATION

(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD
    2019-0154, 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-2019-0870.

(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; phone and fax: 206-231-3226.

(3) For service information identified in this AD, contact Dassault Falcon
    Jet Corporation, Teterboro Airport,  PO Box 2000, South Hackensack, NJ
    07606;  phone: 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 November 7, 2019.  Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification Service

DATES: The FAA must receive comments  on  this  proposed AD  by January 3,
2020.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0870; Product Identifier 2019-NM-125-AD]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2018-19-27 and AD 2014-16-12, which apply to certain Dassault Aviation
Model FALCON 2000EX airplanes. Those ADs require revising the
maintenance or inspection program, as applicable, to incorporate new
maintenance requirements and airworthiness limitations. Since AD 2018-
19-27 and AD 2014-16-12 were issued, the FAA has determined that new or
more restrictive airworthiness limitations are necessary. This proposed
AD would require revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive
airworthiness limitations. The FAA is proposing this AD to address the
unsafe condition on these products.

DATES: The FAA must receive comments on this proposed AD by January 3,
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: 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; phone: 201-440-6700; internet: http://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.

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-2019-0870;
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 NPRM, 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; phone and fax: 206-231-3226.

SUPPLEMENTARY INFORMATION:

Comments Invited

The FAA invites 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-2019-0870;
Product Identifier 2019-NM-125-AD" at the beginning of your comments.
The FAA specifically invites comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. The
FAA will consider all comments received by the closing date and may
amend this proposed 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 proposed AD.

Discussion

The FAA issued AD 2018-19-27, Amendment 39-19428 (83 FR 50479,
October 9, 2018) ("AD 2018-19-27"), for certain Dassault Aviation
Model FALCON 2000EX airplanes. AD 2018-19-27 requires revising the
maintenance or inspection program, as applicable, to incorporate new
maintenance requirements and airworthiness limitations. AD 2018-19-27
resulted from a determination that new or more restrictive maintenance
requirements and airworthiness limitations are necessary. AD 2018-19-27
specifies that accomplishing the actions required by paragraph (g) of
that AD terminates the requirements of AD 2014-16-12,
Amendment 39-17936 (79 FR 52187, September 3, 2014) ("AD 2014-16-
12"), but it does not supersede AD 2014-16-12. In addition, AD 2018-
19-27 specifies that accomplishing paragraph (g) of that AD terminates
the requirements of paragraph (g)(1) of AD 2010-26-05, Amendment 39-
16544 (75 FR 79952, December 21, 2010) ("AD 2010-26-05"), for
Dassault Aviation Model FALCON 2000EX airplanes. This terminating
provision of certain requirements of AD 2010-26-05 is included in this
proposed AD.

This AD proposes to supersede AD 2018-19-27 and AD 2014-16-12, but
does not propose to supersede AD 2010-26-05.

Actions Since AD 2018-19-27 Was Issued

Since the FAA issued AD 2018-19-27, the FAA has determined that new
or more restrictive airworthiness limitations are necessary.

The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2019-0154, dated July 3, 2019 (referred to after this as the
Mandatory Continuing Airworthiness Information, or "the MCAI"), to
correct an unsafe condition for all Dassault Aviation Model FALCON
2000EX 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-2019-0870.

This proposed AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
proposing this AD to address reduced structural integrity of the
airplane. See the MCAI for additional background information.

Related Service Information Under 1 CFR Part 51

Dassault has issued Chapter 5-40, Airworthiness Limitations, DGT
113877, Revision 12, dated November 2018, of the Dassault Falcon 2000EX
Maintenance Manual. This service information describes instructions
applicable to airworthiness and safe life limitations.

This proposed AD would also require Chapter 5-40, Airworthiness
Limitations, DGT 113877, Revision 11, dated November 2017, of the
Dassault Falcon 2000EX Maintenance Manual, which the Director of the
Federal Register approved for incorporation by reference as of November
13, 2018 (83 FR 50479, October 9, 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.

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 our bilateral agreement with the State of Design Authority, The FAA
has been notified of the unsafe condition described in the MCAI and
service information referenced above. The FAA is proposing this AD
because the FAA evaluated all the relevant information and determined
the unsafe condition described previously is likely to exist or develop
on other products of the same type design.

Proposed Requirements of This NPRM

This proposed AD would retain all requirements of AD 2018-19-27.
This proposed AD would also require revising the existing maintenance
or inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations.

This proposed AD would require 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
(l)(1) of this proposed AD.

Costs of Compliance

The FAA estimates that this proposed AD affects 173 airplanes of
U.S. registry. The FAA estimates the following costs to comply with
this proposed AD:

The FAA estimates the total cost per operator for the retained
actions from AD 2018-19-27 to be $7,650 (90 work-hours x $85 per work-
hour).

The FAA has determined that the new revision of 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 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 and associated appliances to the
Director of the System Oversight Division.

Regulatory Findings

The FAA 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) 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.

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:

a. Removing Airworthiness Directive (AD) 2018-19-27, Amendment 39-19428
(83 FR 50479, October 9, 2018); and AD 2014-16-12, Amendment 39-17936
(79 FR 52187, September 3, 2014); and

b. Adding the following new AD: