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PROPOSED AD DASSAULT AVIATION: Docket No. FAA-2017-0524; Directorate Identifier 2016-NM-122-AD.
(a) COMMENTS DUE DATE

    We must receive comments by July 21, 2017.

(b) AFFECTED ADS

    This AD affects AD 2014-16-26, Amendment 39-17950 (79 FR 51077, August
    27, 2014) ("AD 2014-16-26").

(c) APPLICABILITY

    This AD  applies to  Dassault Aviation  Model FALCON  900EX airplanes,
    certificated in any category,  serial numbers 1 through  96 inclusive,
    and  serial  numbers 98  through  119 inclusive,  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
    maintenance   requirements   and/or   airworthiness   limitations  are
    necessary.  We  are  issuing this  AD  to  prevent reduced  structural
    integrity of the airplane.

(f) COMPLIANCE

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

(g) REVISION OF MAINTENANCE OR INSPECTION PROGRAM

    Within  90  days after  the  effective date  of  this AD,  revise  the
    maintenance or inspection program,  as applicable, to incorporate  the
    information  specified  in  Chapter  5-40,  Airworthiness Limitations,
    Revision  14, dated  November 2015,  of the  Falcon 900EX  Maintenance
    Manual.  The initial  compliance time  for accomplishing  the  actions
    specified  in Chapter  5-40, Airworthiness  Limitations, Revision  14,
    dated November 2015, of the Falcon 900EX Maintenance Manual, is within
    the applicable times specified in  the maintenance manual, or 90  days
    after the effective date of this AD, whichever occurs later, except as
    provided by paragraphs (g)(1) through (g)(4) of this AD.

(1) The term "LDG"  in the "First Inspection"  column of any table  in the
    service information means total airplane landings.

(2) The term  "FH" in the  "First Inspection" column  of any table  in the
    service information means total flight hours.

(3) The term  "FC" in the  "First Inspection" column  of any table  in the
    service information means total flight cycles.

(4) The  term "M"  in the  "First Inspection"  column of  any table in the
    service information means months.

(h) NO ALTERNATIVE ACTIONS AND INTERVALS

    After accomplishing the revision 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

    Accomplishing paragraph (g) of this AD terminates all requirements  of
    AD 2014-16-26.

(j) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS): The Manager,  International
    Branch,  ANM-116,  Transport   Airplane  Directorate,  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  manager of the  International Branch, 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
    corrective  actions   from  a   manufacturer,  the   action  must   be
    accomplished using  a method  approved by  the Manager,  International
    Branch, ANM-116, Transport Airplane Directorate, 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.

(k) RELATED INFORMATION

(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD
    2016-0128, dated June 23, 2016, 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-2017-0524.

(2) For more information about  this AD, contact Tom Rodriguez,  Aerospace
    Engineer,   International   Branch,   ANM-116,   Transport    Airplane
    Directorate,  FAA,  1601  Lind Avenue  SW.,  Renton,  WA 98057-  3356;
    telephone 425-227-1137; fax 425-227-1149.

(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
    Airplane  Directorate,   1601  Lind   Avenue  SW.,   Renton,  WA.  For
    information on the availability of this material at the FAA, call  425
    -227-1221.

Issued in Renton,  Washington, on May  23, 2017. Michael  Kaszycki, Acting
Manager, Transport Airplane Directorate, Aircraft Certification Service.

DATES: We must receive comments on this proposed AD by July 21, 2017.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


14 CFR Part 39

[Docket No. FAA-2017-0524; Directorate Identifier 2016-NM-122-AD]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for
certain Dassault Aviation Model FALCON 900EX airplanes. This proposed
AD was prompted by a determination that new or more restrictive
maintenance requirements and/or 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/or 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 July 21, 2017.

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 Airplane Directorate, 1601 Lind
Avenue SW., Renton, WA. For information on the availability of this
material at the FAA, call 425-227-1221.

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-2017-0524; 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 proposed AD, 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 Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137;
fax 425-227-1149.

SUPPLEMENTARY INFORMATION:

Comments Invited


We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include "Docket No. FAA-2017-0524;
Directorate Identifier 2016-NM-122-AD" at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD 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 proposed AD.

Discussion

The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA
Airworthiness Directive 2016-0128, dated June 23, 2016 (referred to
after this as the Mandatory Continuing Airworthiness Information, or
"the MCAI"), to correct an unsafe condition for certain Dassault
Aviation Model FALCON 900EX airplanes. The MCAI states:

The airworthiness limitations and maintenance requirements for
the DA [Dassault Aviation] Falcon 900EX type design are included in
Aircraft Maintenance Manual (AMM) chapter 5-40 and are approved by
the European Aviation Safety Agency (EASA). These instructions have
been identified as mandatory for continued airworthiness.

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

Consequently, EASA issued AD 2013-0051 [which corresponds to AD
2014-16-26, Amendment 39-17950 (79 FR 51077, August 27, 2014)
("2014-16-26")] to require accomplishment of the maintenance
tasks, and implementation of the airworthiness limitations, as
specified in DA Falcon 900EX AMM chapter 5-40 (DGT 113874) at
revision 12.

Since that [EASA] AD was issued, DA issued revision 14 of Falcon
900EX AMM chapter 5-40 (DGT 113874) (hereafter referred to as "the
ALS" in this AD), which contains new or more restrictive
maintenance requirements and/or airworthiness limitations. The ALS
introduces, among others, the following new tasks:

--Task 53-50-00-220-803 "Detailed inspection of the baggage compartment";

--Task 53-50-00-220-807 "Detailed inspection of the upper part of frame 30."

For the reason described above, this [EASA] AD retains the
requirements of EASA AD 2013-0051, which is superseded, 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-2017-0524.

Related Service Information Under 1 CFR Part 51


Dassault issued Chapter 5-40, Airworthiness Limitations, Revision
14, dated November 2015, of the Falcon 900EX Maintenance Manual. The
service information describes procedures, maintenance tasks, and
airworthiness limitations specified in the Airworthiness Limitations
section of the AMM. 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 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
(j)(1) of this proposed AD. The request should include a description of
changes to the required actions that will ensure the continued
operational safety of the airplane.

This proposed AD would not supersede AD 2014-16-26. Rather, we have
determined that a stand-alone AD would be more appropriate to address
the changes in the MCAI. This proposed AD would require revising the
maintenance or inspection program, as applicable, to incorporate new or
more restrictive maintenance requirements and/or airworthiness
limitations than those required by AD 2014-16-26. Accomplishment of the
proposed actions would then terminate all requirements of AD 2014-16-
26.

Costs of Compliance


We estimate that this proposed AD affects 70 airplanes of U.S. registry.

We estimate the following costs to comply with this proposed AD:

Estimated Costs

ACTION
LABOR COST
PARTS COST
COST PER
PRODUCT
COST ON U.S.
OPERATORS
Maintenance or inspection program revision......
1 work-hour x $85 per hour = $85
$0
$85
$5,950

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.

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):