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2021-09-12 DASSAULT AVIATION: Amendment 39-21526; Docket No. FAA-2020-1169; Project Identifier MCAI-2020-01373-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective June 8, 2021.

(b) AFFECTED ADS

(1) This AD replaces AD 2020-07-16, Amendment 39-19895 (85 FR 20405, April
    13, 2020) (AD 2020-07-16).

(2) This AD affects AD 2014-16-23,  Amendment 39-17947  (79 FR 52545, Sep-
    tember 4, 2014) (AD 2014-16-23).

(c) APPLICABILITY

    This AD applies to Dassault Aviation Model FALCON 7X airplanes certif-
    icated in any category,  with an original airworthiness certificate or
    original export certificate of airworthiness issued  on or before June
    1, 2020.

Note 1 to paragraph (c): Model FALCON 7X airplanes with modification M1000
incorporated are commonly referred to  as "Model FALCON 8X" airplanes as a
marketing designation.

(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 structural integrity  and reduced control of airplanes
    due to the failure of system components.

(f) COMPLIANCE

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

(g) RETAINED MAINTENANCE OR INSPECTION PROGRAM REVISION, WITH NO CHANGES

    This paragraph restates the requirements of paragraph (i)  of AD 2020-
    07-16, with no changes.  For airplanes with an  original airworthiness
    certificate or original export certificate of airworthiness issued  on
    or before June 1, 2019, except  as specified in paragraph (h) of  this
    AD: Comply with  all required actions  and compliance times  specified
    in,  and  in  accordance  with,  European Union Aviation Safety Agency
    (EASA) AD 2019-0257, dated October 17, 2019 (EASA AD 2019-0257).

(h) RETAINED EXCEPTIONS TO EASA AD 2019-0257, WITH NO CHANGES

    This paragraph restates the requirements of paragraph (j)  of AD 2020-
    07-16 with no changes.  For  airplanes  with an original airworthiness
    certificate  or original export certificate of airworthiness issued on
    or before June 1, 2019:

(1) The requirements specified in paragraphs (1) and (2)  of EASA AD 2019-
    0257 do not apply to this AD.

(2) Where paragraph (3)  of EASA AD 2019-0257  specifies a compliance time
    of "Within 12 months" after its effective date to "revise the approved
    AMP [Aircraft  Maintenance Program],"  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 2019-0257 within  90
    days after May 18, 2020 (the effective date of AD 2020-07-16).

(3) The initial compliance time for doing the tasks specified in paragraph
    (3) of EASA AD 2019-0257 is at the applicable  "associated thresholds"
    specified in paragraph (3)  of  EASA AD 2019-0257,  or  within 90 days
    after  May 18, 2020  (the effective date of AD 2020-07-16),  whichever
    occurs later.

(4) The provisions specified  in paragraphs (4) and (5)  of  EASA AD 2019-
    0257 do not apply to this AD.

(5) The "Remarks" section of EASA AD 2019-0257 does not apply to this AD.

(i) RETAINED PROVISIONS FOR ALTERNATIVE ACTIONS,  INTERVALS,  AND CRITICAL
    DESIGN CONFIGURATION CONTROL LIMITATIONS (CDCCLS) WITH A NEW EXCEPTION

    This paragraph restates the requirements of paragraph (k)  of AD 2020-
    07-16,  with  a  new   exception.  For  airplanes  with   an  original
    airworthiness   certificate   or   original   export   certificate  of
    airworthiness issued on or before June 1, 2019, except as required  by
    paragraph (j) of this AD, after the maintenance or inspection  program
    has  been  revised  as  required  by  paragraph  (g)  of  this  AD, no
    alternative  actions  (e.g., inspections),  intervals,  or CDCCLs  are
    allowed unless they are approved as specified in the provisions of the
    "Ref. Publications" section of EASA AD 2019-0257.

(j) NEW MAINTENANCE OR INSPECTION PROGRAM REVISION

    Except as specified in paragraph (k)  of this AD:  Comply with all re-
    quired actions and compliance times specified in,  and  in  accordance
    with,  EASA AD 2020-0214,  dated  October 6, 2020 (EASA AD 2020-0214).
    Accomplishing the maintenance  or inspection program revision required
    by this paragraph terminates the requirements of paragraph (g) of this
    AD.

(k) EXCEPTIONS TO EASA AD 2020-0214

(1) The requirements specified in paragraphs (1) and (2)  of EASA AD 2020-
    0214 do not apply to this AD.

(2) Paragraph (3)  of EASA AD 2020-0214  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
    -0214 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 2020-0214 is at the applicable "associated  thresholds"
    specified in  paragraph (3)  of EASA  AD 2020-0214,  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 2019-
    0257 do not apply to this AD.

(5) The "Remarks" section of EASA AD 2020-0214 does not apply to this AD.

(l) NEW PROVISIONS FOR ALTERNATIVE ACTIONS, INTERVALS, AND CDCCLS

    After the maintenance  or  inspection program has been revised  as re-
    quired by paragraph (j) of this AD,  no alternative actions (e.g., in-
    spections), intervals or CDCCLs are allowed except as specified in the
    provisions of the "Ref. Publications" section of EASA AD 2020-0214.

(m) TERMINATING ACTION FOR CERTAIN REQUIREMENTS IN AD 2014-16-23

    Accomplishing the actions required by paragraphs (g) or (j) of this AD
    terminates the requirements of paragraph (q) of AD 2014-16-23.

(n) 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 (o) of this AD.  Information may be
    emailed to 9-AVS-AIR-730-AMOC@faa.gov. Before using any approved AMOC,
    notify your appropriate principal inspector or lacking a principal in-
    spector, the manager of the responsible Flight Standards Office.

(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.

(o) 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.

(p) 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 June 8,
    2021.

(i) European Union  Aviation  Safety  Agency  (EASA)  AD 2020-0214,  dated
    October 6, 2020.

(ii) [Reserved]

(4) The following service information was approved for IBR on May 18, 2020
    (85 FR 20405, April 13, 2020).

(i) European Union  Aviation  Safety  Agency  (EASA)  AD 2019-0257,  dated
    October 17, 2019.

(ii) [Reserved]

(5) For EASA AD 2020-0214,  contact  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.

(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-2020-1169.

(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 April 21, 2021. Lance T. Gant, Director, Compliance & Airworthi-
ness 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-2020-1169; Project Identifier MCAI-2020-01373-T;
Amendment 39-21526; AD 2021-09-12]
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) 2020-07-
16, which applied to certain Dassault Aviation Model FALCON 7X
airplanes. AD 2020-07-16 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 June 8, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of June 8,
2021.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of May
18, 2020 (85 FR 20405, April 13, 2020).

ADDRESSES: For material incorporated by reference (IBR) in this AD,
contact 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. 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-2020-1169.

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-
1169; 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:

Background

The EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2020-0214, dated October 6, 2020
(EASA AD 2020-0214) (also referred to as the Mandatory Continuing
Airworthiness Information, or the MCAI), to correct an unsafe condition
for all Dassault Aviation Model FALCON 7X airplanes.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2020-07-16 Amendment 39-19895 (85 FR 20405,
April 13, 2020) (AD 2020-07-16). AD 2020-07-16 applied to certain
Dassault Aviation Model FALCON 7X airplanes. The NPRM published in the
Federal Register on January 15, 2021 (86 FR 3879). 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 2020-0214.
The FAA is issuing this AD to address reduced structural integrity
and reduced control of airplanes due to the failure of system
components. See the MCAI for additional background information.

Comments

The FAA gave the public the opportunity to participate in
developing this final rule. The FAA has considered the comment
received. One commenter indicated support for the NPRM.

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 IBR Material Under 1 CFR Part 51

EASA AD 2020-0214 describes new or more restrictive airworthiness
limitations for airplane structures and safe life limits.
This AD also requires EASA AD 2019-0257, dated October 17, 2019,
which the Director of the Federal Register approved for incorporation
by reference as of May 18, 2020 (85 FR 20405, April 13, 2020).
This material 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 122 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 2020-07-16 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

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 2020-07-16, Amendment 39-19895 (85
FR 20405, April 13, 2020); and

b. Adding the following new airworthiness directive: