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2017-13-02 DASSAULT AVIATION: Amendment 39-18932; Docket No. FAA-2016-9504; Directorate Identifier 2016-NM-107-AD.
(a) EFFECTIVE DATE

    This AD is effective July 27, 2017.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies to Dassault Aviation Model FALCON 7X airplanes, cer-
    tificated in any category,  serial numbers  (S/Ns) 2, 5, and 8 through
    182  inclusive;  except  S/Ns  141, 148, 149, 157, 159, 166, 170, 171,
    174, 175, and 177 through 180 inclusive.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 53, Fuselage.

(e) REASON

    This AD was prompted by reports that during the assembly of structural
    elements on some airplanes,  lack of established procedures  and tools
    caused boring and torqueing defects to be present at some locations on
    the foot of frame (FR) 36 and  FR39. We are issuing this AD to  detect
    and correct  defects in  the bore  holes at  FR36 and  FR39 that could
    adversely affect the structural integrity of the airplane.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) INSPECTION OF BORE HOLES

    At the applicable  time identified in  paragraphs (g)(1) or  (g)(2) of
    this AD, remove the sheer bolts at FR36 and FR39, left hand and  right
    hand,  as  identified  in  Dassault  Service  Bulletin  7X-379,  dated
    February 29,  2016, and  do a  detailed visual  inspection of the bore
    holes for  defects,  in  accordance with  Dassault Service Bulletin 7X
    -379, dated February 29, 2016.

(1) For airplanes with S/Ns 2 and 5:  Before exceeding 4,100 flight cycles
    after the date of release to service after the first C-Check or within
    3 months from the effective date of this AD, whichever occurs later.

(2) For airplanes  other than those identified in paragraph (g)(1) of this
    AD: Before exceeding 4,100 flight cycles since the date of issuance of
    the  original  certificate  of airworthiness  or  the  original export
    certificate of  airworthiness or  within 3 months  from  the effective
    date of this AD, whichever occurs later.

(h) REPAIR OF BORE HOLES AND BOLT REPLACEMENT

(1) If,  during  any inspection required by paragraph (g) of this AD,  any
    defect is found, before further flight, repair the affected areas, and
    replace  the  bolts at  FR36  and FR39,  in  accordance with  Dassault
    Service  Bulletin  7X-379,  dated  February  29,  2016;  except  where
    Dassault Service Bulletin 7X-379,  dated February 29, 2016,  specifies
    to contact Dassault Aviation for instructions, before further  flight,
    repair 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).

(2) If,  during  any inspection required by paragraph (g)  of this AD,  no
    defect is found,  before further flight, replace the bolts at FR36 and
    FR39,  in  accordance  with  Dassault  Service Bulletin 7X-379,  dated
    February 29, 2016.

(i) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs):  The Manager, International
    Branch, ANM-116, 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 Branch, send it to ATTN: 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. 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  EASA; or
    Dassault Aviation’s  EASA 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
    Airworthiness Directive 2016-0116,  dated June 16, 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-2016-9504.

(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.  Information may be emailed to: 9-ANM-116-AMOC
    REQUESTS@faa.gov.

(k) 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) Dassault Service Bulletin 7X-379, dated February 29, 2016.

(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  Airplane
    Directorate, 1601 Lind Avenue SW., Renton, WA. For information on  the
    availability 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 June 12, 2017.  Dionne Palermo,  Acting
Manager, Transport Airplane Directorate, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, Inter-
national Branch, ANM-116,  Transport Airplane Directorate,  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-2016-9504; Directorate Identifier 2016-NM-107-AD;
Amendment 39-18932; AD 2017-13-02]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

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

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Dassault Aviation Model FALCON 7X airplanes. This AD was prompted by
reports that during the assembly of structural elements on some
airplanes, lack of established procedures and tools caused boring and
torqueing defects to be present at some locations. This AD requires a
detailed visual inspection of bore holes for defects, replacement of
bolts, and repair if necessary. We are issuing this AD to address the
unsafe condition on these products.

DATES: This AD is effective July 27, 2017.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of July 27,
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 Airplane Directorate, 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-2016-9504.

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-2016-
9504; 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 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:

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 7X airplanes. The NPRM published in the Federal Register
on December 21, 2016 (81 FR 93645) (``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 2016-0116, dated June 16, 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 7X airplanes. The MCAI states:

During the assembly of structural elements on some aeroplanes,
lack of established procedures and tools caused boring and torqueing
defects to be present at some locations on the foot of frame (FR) 36
and FR39. Dassault Aviation (DA) identified the individual
aeroplanes that are potentially affected by this production
deficiency. Quality control actions have been implemented to ensure
that new aeroplanes, from s/n 183, cannot be affected by this
defect.
This condition, if not detected and corrected, would adversely
affect the structural integrity of the aeroplane.
For the reasons described above, this [EASA] AD requires [a
detailed visual] inspection of bore holes [for defects] and
replacement of bolts at FR36 and FR39 and, depending on findings,
accomplishment of a repair.
To address this potential unsafe condition, DA published Service
Bulletin (SB) F7X-379 to provide corrective action instructions.

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-2016-9504.

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

We reviewed Dassault Service Bulletin 7X-379, dated February 29,
2016. This service information describes procedures for a detailed
visual inspection of bore holes at FR36 and FR39 for defects,
replacement of bolts at FR36 and FR39, and repair. 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 41 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
Inspection and replacement 6 work-hours x $85 per hour = $510
$26
$536
$21,976

We have received no definitive data that would enable us to provide
cost estimates for the on-condition repair specified in this AD.

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 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):