preamble attached >>>
ADs updated daily at www.Tdata.com
2021-04-02 DASSAULT AVIATION: Amendment 39-21423; Docket No. FAA-2020-0976; Product Identifier 2020-NM-095-AD.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective March 30, 2021.

(b) AFFECTED ADS

(1) This AD replaces AD 2020-04-22, Amendment 39-19858 (85 FR 17487, March
    30, 2020) (AD 2020-04-22).

(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 Dassault Aviation  Model FALCON 2000EX  airplanes,
    certificated  in   any  category,   with  an   original  airworthiness
    certificate or original export certificate of airworthiness issued  on
    or before February 15, 2020.

(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 of the airplane.

(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-
    04-22, with no changes.  For airplanes with an  original airworthiness
    certificate or original export certificate of airworthiness issued  on
    or  before  January 15, 2019:  Within  90 days  after May 4, 2020 (the
    effective date of AD  2020-04-22), revise the existing  maintenance or
    inspection  program,  as applicable,  to  incorporate the  information
    specified  in  Chapter 5-40,  Airworthiness  Limitations, DGT  113877,
    Revision  12,  dated  November 2018,  of  the  Dassault Falcon  2000EX
    Maintenance Manual. The initial  compliance times for doing  the tasks
    are at the time specified in Chapter 5-40, Airworthiness  Limitations,
    DGT 113877, Revision 12, dated  November 2018, of the Dassault  Falcon
    2000EX  Maintenance  Manual, or  within  90 days  after  May 4,  2020,
    whichever occurs  later; except  for task  number 52-20-00-610-801-01,
    the initial compliance time is within 24 months after October 8,  2014
    (the effective date of AD 2014-16-12, Amendment 39-17936 (79 FR 52187,
    September 3, 2014)). 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.  Accomplishing  the
    maintenance or inspection program  revision required  by paragraph (i)
    of this AD terminates the requirements of this paragraph.

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

    This paragraph  restates the requirements of paragraph (j) of AD 2020-
    04-22, with a  new exception. Except  as required by  paragraph (k) 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 2020-0114, dated
    May 20, 2020  (EASA  AD 2020-0114).  Accomplishing the  maintenance or
    inspection program revision required by this paragraph terminates  the
    requirements of paragraph (g) of this AD.

(j) EXCEPTIONS TO EASA AD 2020-0114

(1) The requirements specified in paragraphs (1) and (2)  of EASA AD 2020-
    0114 do not apply to this AD.

(2) Paragraph (3) of EASA AD 2020-0114  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
    -0114 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 2020-0114 is at the applicable  "associated thresholds"
    specified in paragraph (3)  of EASA AD 2020-0114,  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-
    0114 do not apply to this AD.

(5) The "Remarks" section of EASA AD 2020-0114 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
    specified in the provisions of the "Ref. Publications" section of EASA
    AD 2020-0114.

(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)(1) of AD 2010-26-05,  for
    Dassault Aviation Model FALCON 2000EX 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  responsible Flight  Standards 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.  Before  using  any approved
    AMOC,  notify  your  appropriate  principal  inspector,  or  lacking a
    principal inspector, 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.

(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 30,
    2021.

(i) European Union Aviation Safety Agency (EASA)  AD 2020-0114,  dated May
    20, 2020.

(ii) [Reserved]

(4) The following service information was approved  for IBR on May 4, 2020
    (85 FR 17487, March 30, 2020).

(i) Chapter 5-40, Airworthiness Limitations, DGT 113877 Revision 12, dated
    November 2018, of the Dassault Falcon 2000EX Maintenance Manual.

(ii) [Reserved]

(5) For EASA AD 2020-0114, 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  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-2020-0976.

(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 February 1, 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-2020-0976; Product Identifier 2020-NM-095-AD; Amendment
39-21423; AD 2021-04-02]
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) 2020-04-
22, which applied to certain Dassault Aviation Model FALCON 2000EX
airplanes. AD 2020-04-22 required revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. This AD continues to require the
actions in AD 2020-04-22 and also requires revising the existing
maintenance or inspection program, as applicable, to incorporate
additional 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 30, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 30,
2021.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of May 4,
2020 (85 FR 17487, March 30, 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-2020-0976.

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-
0976; 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 2020-0114, dated May 20, 2020 (EASA
AD 2020-0114) (also referred to as the Mandatory Continuing
Airworthiness Information, or the MCAI), to correct an unsafe condition
all Dassault Aviation Model FALCON 2000EX airplanes.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2020-04-22, Amendment 39-19858 (85 FR
17487, March 30, 2020) (AD 2020-04-22). AD 2020-04-22 applied to
certain Dassault Aviation Model FALCON 2000EX airplanes. The NPRM
published in the Federal Register on November 3, 2020 (85 FR 69522).
The NPRM was prompted by a determination that new or more restrictive
airworthiness limitations are necessary. The NPRM proposed to continue
to require the actions in AD 2020-04-22 and also require revising the
existing maintenance or inspection program, as applicable, to
incorporate additional new or more restrictive airworthiness
limitations, as specified in EASA AD 2020-0114.
The FAA is issuing this AD to address reduced structural integrity
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 2020-0114 describes new or more restrictive airworthiness
limitations for airplane structures and safe life limits.
This AD also requires Chapter 5-40, Airworthiness Limitations, DGT
113877, Revision 12, dated November 2018, of the Dassault Falcon 2000EX
Maintenance Manual, which the Director of the Federal Register approved
for incorporation by reference as of May 4, 2020 (85 FR 17487, March
30, 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 17 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 2020-04-22 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 revision
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 (AD) 2020-04-22, Amendment 39-19858
(85 FR 17487, March 30, 2020), and

b. Adding the following new AD: