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PROPOSED AD DASSAULT AVIATION: Docket No. FAA-2019-0668; Product Identifier 2019-NM-108-AD.
(a) COMMENTS DUE DATE

    We must receive comments by October 28, 2019.

(b) AFFECTED ADS

(1) This  AD  replaces  AD  2016-01-16,  Amendment  39-18376  (81 FR 3320,
    January 21, 2016) ("AD 2016-01-06"); AD 2017-19-03, Amendment 39-19033
    (82 FR 43166, September 14, 2017) ("AD 2017-19-03") and AD 2018-19-05,
    Amendment 39-19405 (83 FR 47813, September 21, 2018) ("AD 2018-19-05")

(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 900 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 reduced structural integrity of the airplane.

(f) COMPLIANCE

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

(g) RETAINED REVISION WITH NO CHANGES

    This paragraph restates the requirements  of paragraph (g) of AD  2018
    -19-05, with no  changes. Within 90  days after October  26, 2018 (the
    effective date of AD 2018-19-05), revise the maintenance or inspection
    program, as  applicable, to  incorporate the  information specified in
    Chapter 5-40, Airworthiness Limitations, Revision 23, dated  September
    2017,  of the  Dassault Aviation  Falcon 900  Maintenance Manual.  The
    initial compliance times for doing the tasks are at the time specified
    in  Chapter  5-40,  Airworthiness  Limitations,  Revision  23,   dated
    September  2017,  of  the  Dassault  Aviation  Falcon  900 Maintenance
    Manual, or  within 90  days after  October 26,  2018, whichever occurs
    later. 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. The term "M" in the "First Inspection" column  of
    any table in the service information specified in this paragraph means
    months.

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

    This paragraph  restates the requirements of paragraph (h) of AD 2018-
    19-05, 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 REQUIREMENT OF THIS AD: REVISION OF MAINTENANCE OR INSPECTION PRO-
    GRAM

    Within  90  days after  the  effective date  of  this AD,  revise  the
    existing  maintenance  or   inspection  program,  as   applicable,  to
    incorporate the information  specified in Chapter  5-40, Airworthiness
    Limitations,  Revision  24,  dated  September  2018,  of  the Dassault
    Aviation Falcon 900 Maintenance  Manual. The initial compliance  times
    for  doing  the tasks  are  at the  time  specified in  Chapter  5-40,
    Airworthiness Limitations, Revision 24,  dated September 2018, of  the
    Dassault Aviation  Falcon 900  Maintenance Manual,  or within  90 days
    after the effective date of this AD, whichever occurs later. 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. The term "M" in the "First Inspection" column of any table  in
    the service information specified in this paragraph means months since
    the date of issuance of the original airworthiness certificate or  the
    date of issuance of the original export certificate of  airworthiness.
    Doing the revision required  by this paragraph terminates  the actions
    required by paragraph (g) of this AD.

(j) 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 ACTIONS 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 900 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 2018-19-05 are approved as AMOCs for
     the corresponding provisions of this AD.

(2) Contacting the Manufacturer:  As of the effective date of this AD, 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
    2019-0132, dated June 11, 2019, 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-2019-0668.

(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,  PO 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 September 3, 2019.  Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification Service

DATES: The FAA must receive comments  on this proposed AD  by  October 28,
2019.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0668; Product Identifier 2019-NM-108-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 Directives (ADs)
2016-01-16, 2017-19-03, and 2018-19-05, which apply to Dassault
Aviation Model MYSTERE-FALCON 900 airplanes. Those ADs require revising
the maintenance or inspection program, as applicable, to incorporate
new or more restrictive maintenance requirements and/or airworthiness
limitations. Since AD 2018-19-05 was 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 October 28,
2019.

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 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 http://www.regulations.
gov by searching for and locating Docket No. FAA-2019-0668;
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; telephone 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-2019-0668;
Product Identifier 2019-NM-108-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 http://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 2018-19-05, Amendment 39-19405 (83 FR 47813,
September 21, 2018) ("AD 2018-19-05"), for all Dassault Aviation
Model MYSTERE-FALCON 900 airplanes. AD 2018-19-05 requires revising the
maintenance or inspection program, as applicable, to incorporate new
and more restrictive maintenance requirements and airworthiness
limitations. AD 2018-19-05 resulted from a determination that more
restrictive maintenance requirements and airworthiness limitations are
necessary. The FAA issued AD 2018-19-05 to address reduced structural
integrity of the airplane. AD 2018-19-05 specified that accomplishing
the actions required by paragraph (g) of that AD would terminate the
requirements of AD 2016-01-16, Amendment 39-18376 (81 FR 3320, January
21, 2016) and AD 2017-19-03, Amendment 39-19033 (82 FR 43166, September
14, 2017). AD 2018-19-05 specifies that accomplishing paragraph (g) of
that AD would terminate the requirements of paragraph (g)(1) of AD
2010-26-05, Amendment 39-16544 (75 FR 79952, December 21, 2010), for
Dassault Aviation Model MYSTERE-FALCON 900 airplanes.

Actions Since AD 2018-19-05 Was Issued

Since AD 2018-19-05 was issued, 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 2019-0132, dated June 11, 2019 (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 900 airplanes. The MCAI states:

The airworthiness limitations for Mystere-Falcon 900
aeroplanes, which are approved by EASA, are currently defined and
published in Dassault Mystere-Falcon 900 [airplane
maintenance manual] AMM, Chapter 5-40. These instructions have been
identified as mandatory for continued airworthiness.

Failure to accomplish these instructions could result in an
unsafe condition [reduced structural integrity of the airplane].

EASA previously issued AD 2018-0027 [which corresponds to FAA AD
2018-19-05], requiring the actions described in Dassault
Mystere-Falcon 900 AMM, Chapter 5-40 (DGT113873) at Revision
23.

Since that [EASA] AD was issued, Dassault published the
[airworthiness limitations section] ALS, as defined in this [EASA]
AD, containing new and/or more restrictive maintenance tasks.

For the reason described above, this [EASA] AD retains the
requirements of EASA AD 2018-0027, which is superseded, and requires
accomplishment of the actions specified in the ALS, as defined in
this [EASA] AD.

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-2019-0668.

Related Service Information Under 1 CFR Part 51

Dassault Aviation has issued Chapter 5-40, Airworthiness
Limitations, Revision 24, dated September 2018, of the Dassault
Aviation Falcon 900 Maintenance Manual. This service information
describes procedures, maintenance tasks, and airworthiness limitations
specified in the Airworthiness Limitations Section (ALS) of the AMM.

This proposed AD would also require Chapter 5-40, Airworthiness
Limitations, Revision 23, dated September 2017, of the Dassault
Aviation Falcon 900 Maintenance Manual, which the Director of the
Federal Register approved for incorporation by reference as of October
26, 2018 (83 FR 47813, September 21, 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, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. The FAA is proposing this AD because the
agency 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 of the requirements of AD 2018-
19-05. 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 134 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 2018-19-05 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 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.

The FAA estimates the total cost per operator for the new proposed
actions 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 has 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) 2016-01-16, Amendment 39-18376
(81 FR 3320, January 21, 2016); AD 2017-19-03, Amendment 39-19033

(82 FR 43166, September 14, 2017); and 2018-19-05, Amendment 39-19405
(83 FR 47813, September 21, 2018); and

b. Adding the following new AD: