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2020-02-21 DASSAULT AVIATION: Amendment 39-19833; Docket No. FAA-2019-0700; Product Identifier 2019-NM-105-AD.
(a) EFFECTIVE DATE

    This AD is effective March 18, 2020.

(b) AFFECTED ADS

(1) This AD replaces AD 2014-03-12, Amendment 39-17749 (79 FR 11693, March
    3, 2014) ("AD 2014-03-12");  and AD 2018-19-25, Amendment 39-19426 (83
    FR 48924, September 28, 2018) ("AD 2018-19-25").

(2) This  AD  affects  AD  2010-26-05,  Amendment  39-16544  (75 FR 79952,
    December 21, 2010) ("AD 2010-26-05").

(c) APPLICABILITY

    This AD applies to all  Dassault Aviation Model FALCON 2000 airplanes,
    certificated in any category.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 05,  Time limits/main-
    tenance checks.

(e) REASON

    This AD was prompted by a determination that new  or  more restrictive
    airworthiness limitations are necessary. The FAA is issuing this AD to
    address reduced controllability of the airplane.

(f) COMPLIANCE

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

(g) RETAINED REVISION, WITH NO CHANGES

    This paragraph restates the requirements  of paragraph (g) of AD  2018
    -19-25, with no  changes. Within 90  days after November  2, 2018 (the
    effective date of AD  2018-19-25), revise the existing  maintenance or
    inspection  program,  as applicable,  to  incorporate the  information
    specified  in  Chapter 5-40,  Airworthiness  Limitations, DGT  113876,
    Revision  19,  dated  November  2017,  of  the  Dassault  Falcon  2000
    Maintenance Manual. The initial  compliance times for doing  the tasks
    are at the time specified in Chapter 5-40, Airworthiness  Limitations,
    DGT 113876, Revision 19, dated  November 2017, of the Dassault  Falcon
    2000 Maintenance Manual, or within 90 days after November 2, 2018 (the
    effective date of  AD 2018-19-25), whichever  occurs later; except  as
    required by paragraphs (g)(1) through  (3) of this AD. The  term "LDG"
    in  the  "First  Inspection"  column of  any  table  in  Chapter 5-40,
    Airworthiness  Limitations, DGT  113876, Revision  19, dated  November
    2017,  of the  Dassault Falcon  2000 Maintenance  Manual, means  total
    airplane landings. The term "FH"  in the "First Inspection" column  of
    any  table  in  Chapter 5-40,  Airworthiness Limitations,  DGT 113876,
    Revision  19,  dated  November  2017,  of  the  Dassault  Falcon  2000
    Maintenance Manual,  means total  flight hours.  The term  "FC" in the
    "First Inspection" column of any table in Chapter 5-40,  Airworthiness
    Limitations,  DGT 113876,  Revision 19,  dated November  2017, of  the
    Dassault Falcon 2000 Maintenance Manual, means total flight cycles.

(1) For Task 30-11-09-350-801 identified in the service information speci-
    fied in the introductory text of paragraph (g) of this AD, the initial
    compliance time  is the  later of  the times  specified in  paragraphs
    (g)(1)(i) and (ii) of this AD.

(i) At the earlier of the times specified  in paragraphs (g)(1)(i)(A)  and
    (B) of this AD.

(A) Prior to the accumulation of 2,400 total flight hours  or  2,000 total
    flight cycles, whichever occurs first.

(B) Within 2,400 flight hours  or 2,000 flight cycles  after April 7, 2014
    (the effective date of AD 2014-03-12), whichever occurs first.

(ii) Within 30 days after April 7, 2014 (the effective date of AD 2014-03-
     12).

(2) For  Task 52-20-00-610-801-01  identified  in the  service information
    specified  in the introductory text of paragraph (g)  of this AD,  the
    initial compliance time is within 24 months  after April 7, 2014  (the
    effective date of AD 2014-03-12).

(3) The limited service life  of part number F2MA721512100  is 3,750 total
    flight cycles on the part  or  6 years since the manufacturing date of
    the part, whichever occurs first.

(h) RETAINED NO ALTERNATIVE ACTIONS OR INTERVALS WITH A NEW EXCEPTION

    This paragraph restates  the requirements of paragraph (h) of AD 2018-
    19-25, with a  new exception. Except  as required by  paragraph (i) of
    this AD: After the existing maintenance or inspection program has been
    revised  as  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 (l)(1) of this AD.

(i) NEW REQUIREMENT OF THIS AD: MAINTENANCE OR INSPECTION PROGRAM REVISION

    Within 90 days after the effective date of this AD,  revise the exist-
    ing maintenance or inspection  program, as applicable, to  incorporate
    the information specified in Chapter 5-40, Airworthiness  Limitations,
    Revision 20, dated November 2018, of the Dassault Aviation Falcon 2000
    Maintenance Manual. The initial compliance time for doing the tasks is
    at  the time  specified  in  Chapter 5-40,  Airworthiness Limitations,
    Revision 20, dated November 2018, of the Dassault Aviation Falcon 2000
    Maintenance Manual, or within 90 days after the effective date of this
    AD, whichever occurs  later, except as  required by paragraphs  (i)(1)
    through  (3) of  this AD.  The term  "LDG" in  the "First  Inspection"
    column  of  any  table in  the service  information specified  in this
    paragraph means total airplane landings.  The term "FH" in the  "First
    Inspection" column of any  table in the service  information specified
    in  this paragraph  means total  flight hours.  The term  "FC" in  the
    "First  Inspection" column  of any  table in  the service  information
    specified in this paragraph means total flight cycles. The term "M" in
    the "First Inspection" column of any table in the service  information
    specified in this paragraph means months since date of issuance of the
    original airworthiness certificate  or original export  certificate of
    airworthiness. Accomplishing  the actions  required by  this paragraph
    terminates all requirements of paragraph (g) of this AD.

(1) For Task 30-11-09-350-801 identified in the service information speci-
    fied in the introductory text of paragraph (i) of this AD, the initial
    compliance time is the later of the times specified  in paragraphs (i)
    (1)(i) and (ii) of this AD.

(i) At the earlier of the times specified  in paragraphs (i)(1)(i)(A)  and
    (B) of this AD.

(A) Prior to the accumulation of 2,400 total flight hours  or  2,000 total
    flight cycles, whichever occurs first.

(B) Within 2,400 flight hours  or 2,000 flight cycles  after April 7, 2014
    (the effective date of AD 2014-03-12), whichever occurs first.

(ii) Within  30  days  after  April 7, 2014  (the  effective  date  of  AD
     2014-03-12).

(2) For  Task  52-20-00-610-801-01  identified  in the service information
    specified  in the introductory text  of paragraph (i) of this AD,  the
    initial compliance time is within 24 months  after April 7, 2014  (the
    effective date of AD 2014-03-12).

(3) The limited service life of  part number F2MA721512100  is 3,750 total
    flight cycles on the part or  6 years since the manufacturing date  of
    the part, whichever occurs first.

(j) NEW NO ALTERNATIVE ACTIONS OR INTERVALS

    After the existing maintenance  or inspection program has been revised
    as required by paragraph (i) of this AD, no alternative actions (e.g.,
    inspections) or intervals may be used unless the actions or  intervals
    are approved as an AMOC in accordance with the procedures specified in
    paragraph (l)(1) of this AD.

(k) TERMINATING ACTION FOR CERTAIN ACTIONS IN AD 2010-26-05

    Accomplishing  the  actions  required  by  paragraph (g) of this AD or
    paragraph (i) of this AD terminates the requirements  of paragraph (g)
    of AD 2010-26-05 for all Dassault Aviation Model FALCON 2000 airplanes

(l) OTHER FAA AD PROVISIONS

(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  para-
    graph (m)(2) of this AD. Information may be emailed to 9-ANM-116-AMOC-
    REQUESTS@faa.gov.

(i) Before using any approved AMOC,  notify your appropriate principal in-
    spector,  or  lacking a principal inspector,  the manager of the local
    flight standards district office/certificate holding district office.

(ii) AMOCs approved previously  for AD 2018-19-25,  Amendment 39-19426 (83
     FR 48924,  September 28, 2018),  are approved as AMOCs for the corre-
     sponding provisions of this AD.

(2) Contacting the Manufacturer:  As of the effective date of this AD, 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 Union 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.

(m) RELATED INFORMATION

(1) Refer  to  Mandatory Continuing Airworthiness Information (MCAI)  EASA
    Airworthiness Directive 2019-0131,  dated  June 11, 2019,  for related
    information. This MCAI may be found  in the AD docket  on the internet
    at https://www.regulations.gov  by searching for  and  locating Docket
    No. FAA-2019-0700.

(2) For more information about this AD,  contact Tom Rodriguez,  Aerospace
    Engineer, International Section, Transport Standards Branch, FAA, 2200
    South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3226;
    email tom.rodriguez@faa.gov.

(n) 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.

(3) The following service information was approved  for  IBR  on March 18,
    2020.

(i) Chapter 5-40, Airworthiness Limitations,  Revision 20,  dated November
    2018, of the Dassault Aviation Falcon 2000 Maintenance Manual.

(ii) [Reserved]

(4) The following service information was approved  for IBR on November 2,
    2018 (83 FR 48924, September 28, 2018).

(i) Chapter 5-40, Airworthiness Limitations, DGT 113876 Revision 19, dated
    November 2017, of the Dassault Falcon 2000 Maintenance Manual.

(ii) [Reserved]

(5) For service information identified in this AD, contact Dassault Falcon
    Jet Corporation, Teterboro Airport,  PO Box 2000, South Hackensack, NJ
    07606; telephone 201-440-6700; internet https://www.dassaultfalcon.com

(6) You may view this service information at the FAA,  Transport Standards
    Branch,  2200 South 216th St., Des Moines, WA.  For information on the
    availability of this material at the FAA, call 206-231-3195.

(7) 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,  email
    fedreg.legal@nara.gov,  or  go  to:  https://www.archives.gov/federal-
    register/cfr/ibr-locations.html.

Issued  on  January 28, 2020.  Gaetano A. Sciortino,  Deputy  Director for
Strategic  Initiatives,  Compliance  &  Airworthiness  Division,  Aircraft
Certification Service.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, Inter-
national Section, Transport Standards Branch,  FAA,  2200 South 216th St.,
Des Moines, WA 98198; telephone and fax 206-231-3226; email tom.rodriguez@
faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0700; Product Identifier 2019-NM-105-AD; Amendment
39-19833; AD 2020-02-21]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

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

ACTION: Final rule.

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

SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2018-19-25
and AD 2014-03-12, which applied to all Dassault Aviation Model FALCON
2000 airplanes. Those ADs required revising the existing maintenance or
inspection program, as applicable, to incorporate new maintenance
requirements and airworthiness limitations. Since the FAA issued AD
2018-19-25, the FAA has determined that new or more restrictive
airworthiness limitations are necessary. This AD continues to require
those maintenance or inspection program revisions, and also requires
revising the existing maintenance or inspection program, as applicable,
to incorporate new or more restrictive airworthiness limitations. This
AD was prompted by a determination that new or more restrictive
airworthiness limitations are necessary. The FAA is issuing this AD to
address the unsafe condition on these products.

DATES: This AD is effective March 18, 2020.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of March 18,
2020.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of
November 2, 2018 (83 FR 48924, September 28, 2018).

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
https://www.dassaultfalcon.com. You may view this referenced service
information at the FAA, Transport Standards Branch, 2200 South 216th
St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195. It is also available on the
internet at https://www.regulations.gov by searching for and locating
Docket No. FAA-2019-0700.

Examining the AD Docket

You may examine the AD docket on the internet at https://www.regulations.gov
by searching for and locating Docket No. FAA-2019-0700;
or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, the regulatory evaluation, any comments received, and
other information. The address for Docket Operations is 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, 2200 South
216th St., Des Moines, WA 98198; telephone and fax 206-231-3226; email
tom.rodriguez@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2019-0131, dated June 11, 2019 (``EASA AD 2019-0131'') (also
referred to as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for all Dassault Aviation
Model FALCON 2000 airplanes. You may examine the MCAI in the AD docket
on the internet at https://www.regulations.gov by searching for and
locating Docket No. FAA-2019-0700.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2018-19-25, Amendment 39-19426 (83 FR
48924, September 28, 2018) (``AD 2018-19-25'') and AD 2014-03-12,
Amendment 39-17749 (79 FR 11693, March 3, 2014) (``AD 2014-03-12''). AD
2018-19-25 applied to all Dassault Aviation Model FALCON 2000
airplanes. The NPRM published in the Federal Register on September 25,
2019 (84 FR 50336). The NPRM resulted from a determination
that new or more restrictive airworthiness limitations are necessary.
The NPRM proposed to require revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. The FAA is issuing this AD to
address reduced controllability of the airplane. See the MCAI for
additional background information.

Comments

The FAA gave the public the opportunity to participate in
developing this final rule. The following presents the comment received
on the NPRM and the FAA's response to that comment.

Request To List New Requirements

NetJets Aviation (NJA) requested that the additional required
inspection items or changes from Chapter 5-40, Airworthiness
Limitations, Revision 20, dated November 2018, of the Dassault Aviation
Falcon 2000 Maintenance Manual be listed in paragraph (i) of the
proposed AD to ensure operators are meeting the requirements.
The FAA disagrees with the commenter's request because the required
action is for the operators to incorporate the entirety of the
information specified in Chapter 5-40, Airworthiness Limitations,
Revision 20, dated November 2018, of the Dassault Aviation Falcon 2000
Maintenance Manual into their maintenance or inspection program, as
applicable, and not just the changes that are made in Revision 20 (the
changes are described in the ``Information to Operators'' section of
Revision 20). The AD has not been changed in this regard.

Conclusion

The FAA reviewed the relevant data, considered the comment
received, and determined that air safety and the public interest
require adopting this final rule as proposed, except for minor
editorial changes. The FAA has determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM for addressing 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 20, dated November 2018, of the Dassault Aviation
Falcon 2000 Maintenance Manual. This service information describes
airworthiness limitations for safe life limits.
This AD also requires Chapter 5-40, Airworthiness Limitations, DGT
113876, Revision 19, dated November 2017, of the Dassault Falcon 2000
Maintenance Manual, which the Director of the Federal Register approved
for incorporation by reference as of November 2, 2018 (83 FR 48924,
September 28, 2018).
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

The FAA estimates that this AD affects 200 airplanes of U.S.
registry.
The FAA estimates the following costs to comply with this AD:
The FAA estimates the total cost per operator for the retained
actions from AD 2018-19-25 to be $7,650 (90 work-hours x $85 per work-
hour).
The FAA has determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although the
FAA recognizes that this number may vary from operator to operator. In
the past, the FAA has estimated that this action takes 1 work-hour per
airplane. Since operators incorporate maintenance or inspection program
changes for their affected fleet(s), the FAA has determined that a per-
operator estimate is more accurate than a per-airplane estimate.
The FAA estimates the total cost per operator for the new actions
to be $7,650 (90 work-hours x $85 per work-hour).

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.
The FAA is 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) Will not affect intrastate aviation in Alaska, and
(3) 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:

a. removing Airworthiness Directive (AD) 2014-03-12, Amendment 39-17749
(79 FR 11693, March 3, 2014); and AD 2018-19-25, Amendment 39-19426 (83
FR 48924, September 28, 2018); and

b. adding the following new AD: