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2017-19-04 DASSAULT AVIATION: Amendment 39-19034; Docket No. FAA-2017-0524; Product Identifier 2016-NM-122-AD.
(a) EFFECTIVE DATE

    This AD is effective October 19, 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/Maint-
    enance Checks.

(e) REASON

    This AD was prompted by a determination that new  or  more restrictive
    maintenance requirements  and/or  airworthiness limitations are neces-
    sary.  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 al-
    ready 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 ser-
    vice 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 the actions required  by paragraph (g) of this AD termi-
    nates all the 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
    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 (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
    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.

(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.regulation
    s.gov by searching for and locating Docket No. FAA-2017-0524.

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

(l) 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.

(i) Chapter 5-40, Airworthiness Limitations, Revision 14,  dated  November
    2015, of the FALCON 900EX Maintenance Manual.

(ii) Reserved.

(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.

(4) You may view this service information at the FAA,  Transport Standards
    Branch, 1601 Lind Avenue SW, Renton, WA. For information on the avail-
    ability of this material at the FAA, call 425-227-1221.

(5) 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, call
    202-741-6030,  or go to: http://www.archives.gov/federal-register/cfr/
    ibr-locations.html.

Issued in Renton, Washington, on  August 31, 2017.  Dionne Palermo, Acting
Director, System Oversight Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, Inter-
national Section, Transport Standards Branch,  FAA,  1601 Lind Avenue SW.,
Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0524; Product Identifier 2016-NM-122-AD; Amendment
39-19034; AD 2017-19-04]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Dassault Aviation Model FALCON 900EX airplanes. This AD was prompted by
a determination that new or more restrictive maintenance requirements
and/or airworthiness limitations are necessary. This AD requires
revising the maintenance or inspection program, as applicable, to
incorporate new or more restrictive maintenance requirements and/or
airworthiness limitations. We are issuing this AD to address the unsafe
condition on these products.

DATES: This AD is effective October 19, 2017.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 19,
2017.

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
http://www.dassaultfalcon.com. You may view this referenced service
information at the FAA, Transport Standards Branch, 1601 Lind Avenue
SW., Renton, WA. For information on the availability of this material
at the FAA, call 425-227-1221. It is also available on the Internet at
http://www.regulations.gov by searching for and locating Docket No.
FAA-2017-0524.

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 AD, the regulatory evaluation, any comments received, and
other information. The street address for the Docket Office (telephone
800-647-5527) is Docket Management Facility, 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, 1601 Lind
Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-
1149.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Dassault Aviation
Model FALCON 900EX airplanes. The NPRM published in the Federal
Register on June 6, 2017 (82 FR 25986) (``the NPRM'').
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.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.

Conclusion

We reviewed the relevant data and determined that air safety and
the public interest require adopting this AD as proposed except for
minor editorial changes. We have determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM for correcting 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, 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.

Costs of Compliance

We estimate that this AD affects 70 airplanes of U.S. registry.
We estimate the following costs to comply with this 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.
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 to
the Director of the System Oversight Division.

Regulatory Findings

We 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. 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.

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 adding the following new airworthiness
directive (AD):