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2021-03-11 DASSAULT AVIATION: Amendment 39-21414; Docket No. FAA-2020-0980; Product Identifier 2020-NM-094-AD.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective March 31, 2021.

(b) AFFECTED ADS

(1) This AD replaces AD 2020-02-21, Amendment 39-19833 (85 FR 7860, Febru-
    ary 12, 2020) (AD 2020-02-21).

(2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR 79952, Decem-
    ber 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  NEW MAINTENANCE  OR  INSPECTION  PROGRAM  REVISION  WITH  NO
    CHANGES

    This paragraph restates the requirements of paragraph (i)  of AD 2020-
    02-21,  with no  changes.  Within  90 days  after March 18, 2020  (the
    effective date of AD  2020-02-21), revise the existing  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 March 18, 2020,  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  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.

(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, Amendment 39-17749 (79 FR 11693,
    March 3, 2014) (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 (j)  of AD 2020-
    02-21, 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 AMOC in  accordance with the
    procedures specified in paragraph (m)(1) of this AD.

(i) NEW MAINTENANCE OR INSPECTION PROGRAM REVISION

    Except as specified in paragraph (j) of this AD:  Comply with  all re-
    quired actions and compliance times specified in,  and  in  accordance
    with, European Union Aviation Safety Agency (EASA) AD 2020-0113, dated
    May 20, 2020 (EASA AD 2020-0113). Accomplishing the maintenance or in-
    spection program revision required  by  this  paragraph terminates the
    requirements of paragraph (g) of this AD.

(j) EXCEPTIONS TO EASA AD 2020-0113

(1) The requirements specified in paragraphs (1) and (2)  of EASA AD 2020-
    0113 do not apply to this AD.

(2) Paragraph (3) of EASA AD 2020-0113  specifies  revising  "the approved
    AMP" within 12 months after  its effective date, but this  AD requires
    revising   the  existing   maintenance  or   inspection  program,   as
    applicable,  to  incorporate the  "limitations,  tasks and  associated
    thresholds and intervals" specified in  paragraph (3)  of EASA AD 2020
    -0113 within 90 days after the effective date of this AD.

(3) The initial compliance time for doing the tasks specified in paragraph
    (3) of EASA AD 2020-0113 is at the applicable "associated  thresholds"
    specified in  paragraph (3)  of EASA  AD 2020-0113,  or within 90 days
    after the effective date of this AD, whichever occurs later.

(4) The provisions specified  in paragraphs (4) and (5)  of  EASA AD 2020-
    0113 do not apply to this AD.

(5) The "Remarks" section of EASA AD 2020-0113 does not apply to this AD.

(k) NEW PROVISIONS FOR ALTERNATIVE ACTIONS AND INTERVALS

    After the maintenance  or  inspection program  has been revised as re-
    quired by paragraph (i) of this AD,  no alternative actions (e.g., in-
    spections) and intervals are allowed unless they are approved as spec-
    ified in the provisions of the "Ref. Publications" section  of EASA AD
    2020-0113.

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

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

(m) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager, Large Aircraft
    Section,  International Validation 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  Large Aircraft
    Section, International Validation Branch,  send it to the attention of
    the person identified in paragraph (n) of this AD.  Information may be
    emailed to: 9-AVS-AIR-730-AMOC@faa.gov.

(i) Before using any approved AMOC,  notify your appropriate principal in-
    spector, or lacking a principal inspector,  the manager of the respon-
    sible Flight Standards District Office.

(ii) AMOCs approved previously for AD 2020-02-21 are approved as AMOCs for
     the corresponding provisions  of EASA AD 2020-0113  that are required
     by paragraph (i) of this AD.

(2) Contacting the Manufacturer:  For any requirement in this AD to obtain
    instructions   from   a  manufacturer,   the   instructions  must   be
    accomplished using a  method approved by  the Manager, Large  Aircraft
    Section, International  Validation Branch,  FAA; or  EASA; or Dassault
    Aviation's EASA Design Organization Approval (DOA). If approved by the
    DOA, the approval must include the DOA-authorized signature.

(n) RELATED INFORMATION

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

(o) 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 31,
    2021.

(i) European Union Aviation Safety Agency (EASA) AD 2020-0113,  dated  May
    20, 2020.

(ii) [Reserved]

(4) The following service information was approved  for  IBR  on March 18,
    2020 (85 FR 7860, February 12, 2020).

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

(ii) [Reserved]

(5) For EASA AD 2020-0113, contact the EASA, Konrad-Adenauer-Ufer 3, 50668
    Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu
    internet www.easa.europa.eu. You may find this EASA AD on the EASA web
    site  at https://ad.easa.europa.eu.  For  information  about  Dassault
    Aviation material,  contact Dassault Falcon Jet Corporation, Teterboro
    Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201-440-
    6700; internet https://www.dassaultfalcon.com.

(6) You may view this material at the FAA, Airworthiness Products Section,
    Operational Safety Branch, 2200 South  216th St., Des Moines, WA.  For
    information on the availability of this material at the FAA, call  206
    -231-3195. This material may be found in the AD docket on the internet
    at https://www.regulations.gov  by searching  for and  locating Docket
    No. FAA-2020-0980.

(7) You may view this material 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 29, 2021. Lance T Gant, Director, Compliance & Airworth-
iness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez,  Aerospace Engineer, Large
Aircraft Section, International Validation 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-2020-0980; Product Identifier 2020-NM-094-AD; Amendment
39-21414; AD 2021-03-11]
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) 2020-02-
21, which applied to all Dassault Aviation Model FALCON 2000 airplanes.
AD 2020-02-21 required revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive
airworthiness limitations. This AD requires revising the existing
maintenance or inspection program, as applicable to incorporate new or
more restrictive airworthiness limitations, as specified in a European
Union Aviation Safety Agency (EASA) AD, which is incorporated by
reference. 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 31, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 31,
2021.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of March
18, 2020 (85 FR 7860, February 12, 2020).

ADDRESSES: For EASA material incorporated by reference (IBR) in this
AD, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
telephone +49 221 8999 000; email ADs@easa.europa.eu; internet
www.easa.europa.eu. You may find this IBR material on the EASA website
at https://ad.easa.europa.eu. For Dassault Aviation 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 IBR material at the FAA, Airworthiness Products Section,
Operational Safety 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 in the AD docket on the internet at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2020-0980.

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-2020-0980;
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, 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,
Large Aircraft Section, International Validation 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 EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2020-0113, dated May 20, 2020 (EASA
AD 2020-0113) (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.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2020-02-21, Amendment 39-19833 (85 FR 7860,
February 12, 2020) (AD 2020-02-21). AD 2020-02-21 applied to all
Dassault Aviation Model FALCON 2000 airplanes. The NPRM published in
the Federal Register on November 3, 2020 (85 FR 69519). The NPRM was
prompted by 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, as
specified in EASA AD 2020-0113. 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 FAA received no comments on the NPRM or
on the determination of the cost to the public.

Conclusion

The FAA reviewed the relevant data 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

EASA AD 2020-0113 describes new or more restrictive airworthiness
limitations for airplane structures and safe life limits.
This AD also requires Chapter 5-40, Airworthiness Limitations,
Revision 20, dated November 2018, of the Dassault Aviation Falcon 2000
Maintenance Manual, which the Director of the Federal Register approved
for incorporation by reference as of March 18, 2020 (85 FR 7860,
February 12, 2020).
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 168 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 2020-02-21 to be $7,650 (90 work-hours x $85 per work-
hour).
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the agency recognizes that this number may vary from operator
to operator. 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


The FAA 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) 2020-02-21, Amendment 39-19833
(85 FR 7860, February 12, 2020), and

b. Adding the following new AD: