AD 2017-13-02

[Federal Register Volume 82, Number 119 (Thursday, June 22, 2017)]
[Rules and Regulations]
[Pages 28395-28397]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2017-12808]


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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 
<a href="http://www.dassaultfalcon.com">http://www.dassaultfalcon.com</a>. 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 <a href="http://www.regulations.gov">http://www.regulations.gov</a> 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://

[[Page 28396]]

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 <a href="http://www.regulations.gov">http://www.regulations.gov</a> 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:
    <bullet> Are consistent with the intent that was proposed in the 
NPRM for correcting the unsafe condition; and
    <bullet> 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
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Inspection and replacement............  6 work-hours x $85 per               $26            $536         $21,976
                                         hour = $510.
----------------------------------------------------------------------------------------------------------------

    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:

[[Page 28397]]

PART 39--AIRWORTHINESS DIRECTIVES

0
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]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

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, 
certificated 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 already 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 <a href="http://www.regulations.gov">http://www.regulations.gov</a> 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: <a href="/cdn-cgi/l/email-protection#6a53472b2427475b5b5c472b27252947382f3b3f2f393e392a0c0b0b440d051c"><span class="__cf_email__" data-cfemail="3801157976751509090e157975777b156a7d696d7d6b6c6b785e5959165f574e">[email&#160;protected]</span></a>.

(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 <a href="http://www.dassaultfalcon.com">http://www.dassaultfalcon.com</a>.
    (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: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.

    Issued in Renton, Washington, on June 12, 2017.
Dionne Palermo,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2017-12808 Filed 6-21-17; 8:45 am]
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