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2014-25-08 DASSAULT AVIATION: Amendment 39-18050. Docket No. FAA-2014-0566; Directorate Identifier 2014-NM-041-AD.
(a) EFFECTIVE DATE

    This AD becomes effective January 20, 2015.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies to  the  Dassault Aviation  airplanes  identified in
    paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.

(1) Dassault Aviation Model FALCON 2000 airplanes,  having  serial numbers
    (S/Ns) 1 through 231 inclusive.

(2) Dassault Aviation Model FALCON 2000EX airplanes, having S/Ns 1 through
    262 inclusive, and S/Ns 601 through 604 inclusive.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 25, Equipment/Furnish-
    ings.

(e) REASON

    This  AD was  prompted by  a design  review, which  revealed that  the
    forward  servicing  compartment  (FSC)  is  configured  with  tie-down
    points. We  are issuing  this AD  to detect  and correct installed tie
    -down points,  which could  lead to  inadvertent use  of the  FSC as a
    cargo compartment, which  could result in  damage to the  structure of
    the airplane or potential risk of fire.

(f) COMPLIANCE

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

(g) INSPECTION AND REMOVAL

(1) Within 440 flight hours or 9 months after  the  effective date of this
    AD, whichever  occurs first,  inspect the  FSC for  installed tie-down
    points, in accordance with the Accomplishment Instructions of Dassault
    Service Bulletin  F2000-407,  Revision 1,  dated  January 29, 2014; or
    Dassault Service Bulletin F2000EX-289,  Revision 1,  dated January 29,
    2014; as applicable.

(2) If it is determined from  the  inspection required by paragraph (g)(1)
    of this AD that tie-down  points are installed, within the  compliance
    time specified  in paragraph  (g)(1) of  this AD,  remove the tie-down
    points  from   the  FSC,   in  accordance   with  the   Accomplishment
    Instructions of Dassault Service Bulletin F2000-407, Revision 1, dated
    January 29, 2014; or  Dassault Service Bulletin F2000EX-289,  Revision
    1, dated January 29, 2014; as applicable.

(h) CREDIT FOR PREVIOUS ACTIONS

    This  paragraph provides  credit  for  actions required  by paragraphs
    (g)(1) and (g)(2) of this  AD, if those actions were  performed before
    the effective date  of this AD  using Dassault Service  Bulletin F2000
    -407,  dated December 17, 2013; or  Dassault Service Bulletin  F2000EX
    -289, dated December 17, 2013; which are not incorporated by reference
    in this AD.

(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,  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 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. 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. The AMOC  approval letter
    must specifically reference this AD.

(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.

(j) RELATED INFORMATION

(1) Refer  to  Mandatory  Continuing Airworthiness Information (MCAI) EASA
    Airworthiness Directive 2014-0027R1 dated February 5, 2014 for related
    information. This  MCAI  may be found in the AD docket on the Internet
    at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0566-0002.

(2) Service information identified in this AD  that is not incorporated by
    reference is available at the addresses specified in paragraphs (k)(3)
    and (k)(4) of this AD.

(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 F2000-407,  Revision 1,  dated  January 29,
    2014.

(ii) Dassault Service Bulletin F2000EX-289, Revision 1,  dated January 29,
     2014.

(3) For service information identified in this AD, contact Dassault Falcon
    Jet, PO 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  December 5, 2014.  Michael Kaszycki,
Acting  Manager,  Transport Airplane  Directorate,  Aircraft Certification
Service.

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.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0566; Directorate Identifier 2014-NM-041-AD;
Amendment 39-18050; AD 2014-25-08]
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 2000 and FALCON 2000EX airplanes. This
AD was prompted by a design review, which revealed that the forward
servicing compartment (FSC) is configured with tie-down points. This AD
requires inspecting the FSC for installed tie-down points, and removing
those tie-down points. We are issuing this AD to detect and correct
installed tie-down points, which could lead to inadvertent use of the
FSC as a cargo compartment, which could result in damage to the
structure of the airplane or potential risk of fire.

DATES: This AD becomes effective January 20, 2015.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of January 20,
2015.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0566; or in person at
the 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.
For service information identified in this AD, contact Dassault
Falcon Jet, 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.

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 2000 and FALCON 2000EX airplanes. The NPRM published in
the Federal Register on August 14, 2014 (79 FR 47592).
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, has issued EASA
Airworthiness Directive 2014-0027R1, dated February 5, 2014 (referred
to after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for certain Dassault
Aviation Model FALCON 2000 and FALCON 2000EX airplanes. The MCAI
states:

The Forward Servicing Compartment (FSC) of the Falcon 2000 is an
unpressurized service compartment located between fuselage frames 26
and 33. This compartment is accessible from a lockable external door
located in the lower aft fuselage.
A design review has brought to light that the compartment is
configured with tie-down points, which were used by operators to fix
loads (e.g. ski or golf bags) in that compartment. However, the FSC
has not been designed and consequently demonstrated as being
compliant with cargo compartment airworthiness requirements.
This condition, if not corrected, could lead to inadvertent use
of the FSC as [a] cargo compartment, which could result in damage to
the structure of the aeroplane or potential risk of fire.
To address this potential unsafe condition, Dassault Aviation
issued Service Bulletin (SB) F2000-407 and SB F2000EX-289, as
applicable, which provide instructions for removal of the tie-down
points.
For the reasons described above, this [EASA] AD requires removal
of the tie-down points from the FSC.

Note: Operators are also reminded about the intended function of
the FSC.
This [EASA] AD is revised to clarify the AD Applicability and to
correct the [type certificate data sheet] TCDS Number.

Required actions include inspecting for installed tie-down points.
You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0566-0002.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (79 FR 47592, August 14,
2014) 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 (79 FR 47592, August 14, 2014) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM (79 FR 47592, August 14, 2014).

Costs of Compliance

We estimate that this AD affects 247 airplanes of U.S. registry.
We also estimate that it will take about 2 work-hours per product
to comply with the basic requirements of this AD. The average labor
rate is $85 per work-hour. Required parts will cost about $5 per
product. Based on these figures, we estimate the cost of this AD on
U.S. operators to be $43,225, or $175 per product.
According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all costs in our cost
estimate.

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.

Examining the AD Docket

You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0566; 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 Operations office (telephone 800-647-
5527) is in the ADDRESSES section.

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):