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2020-23-10 DASSAULT AVIATION: Amendment 39-21326; Docket No. FAA-2020-0582; Product Identifier 2020-NM-059-AD.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective December 23, 2020.

(b) AFFECTED ADS

    This AD replaces AD 2014-26-07,Amendment 39-18058 (80 FR 2815, January
    21, 2015) ("AD 2014-26-07"); and AD 2019-07-01, Amendment 39-19612 (84
    FR 16390, April 19, 2019) ("AD 2019-07-01").

(c) APPLICABILITY

    This AD applies to the Dassault Aviation airplanes  specified in para-
    graphs (c)(1) and (2) of this AD,  certificated  in  any  category, as
    identified  in  European Union Aviation Safety Agency  (EASA) AD 2019-
    0141, dated June 17, 2019 ("EASA AD 2019-0141").

(1) Model FAN JET FALCON airplanes.

(2) Model FAN JET FALCON SERIES C, D, E, F, and G airplanes.

(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, among other things, fatigue cracking and damage in  principal
    structural elements; such fatigue cracking and damage could result  in
    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 (g)  of AD 2019-
    07-01 with no changes. Within 12 months after May 24, 2019 (the effec-
    tive date of AD 2019-07-01) revise the existing maintenance or inspec-
    tion program, as applicable,  to incorporate the airworthiness limita-
    tions and maintenance requirements  specified  in  Chapter 5-40,  Air-
    worthiness Limitations, DGT 131028, Revision 17, dated September 2017,
    of  the  Dassault Aviation Falcon 20 Maintenance Manual.  The  initial
    compliance time  for  accomplishing  the  actions is at the applicable
    time specified in Chapter 5-40, Airworthiness Limitations, DGT 131028,
    Revision 17, dated September 2017,  of the Dassault Aviation Falcon 20
    Maintenance Manual or within 12 months  after May 24, 2019,  whichever
    occurs later.  Where the threshold column in the table in paragraph B,
    Mandatory Maintenance Operations, of Chapter 5-40, Airworthiness Limi-
    tations, DGT 131028 Revision 17, dated September 2017, of the Dassault
    Aviation Falcon 20 Maintenance Manual  specifies  a compliance time in
    years,  those  compliance  times are since the date of issuance of the
    original French or EASA airworthiness certificate  or date of issuance
    of the original French  or  EASA export certificate  of airworthiness.
    Accomplishing the maintenance  or inspection program revision required
    by paragraph (i) of this AD terminates the requirements  of this para-
    graph.

(h) RETAINED RESTRICTIONS ON ALTERNATIVE ACTIONS AND INTERVALS  WITH A NEW
    EXCEPTION

    This paragraph restates the requirements of paragraph (h)  of AD 2019-
    07-01,  with a new exception.  Except as required  by paragraph (i) of
    this AD, after accomplishing the revision 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 speci-
    fied in paragraph (l)(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,  EASA AD 2019-0141.  Accomplishing the maintenance or inspection
    program revision required  by  this  paragraph terminates the require-
    ments of paragraph (g) of this AD.

(j) EXCEPTIONS TO EASA AD 2019-0141

(1) The requirements specified in paragraphs (1), (2), (4) and (5) of EASA
    AD 2019-0141 do not apply to this AD.

(2) Paragraph (3) of EASA AD 2019-0141  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 2019-0141  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 2019-0141 is at the applicable  "associated thresholds"
    specified in paragraph (3)  of EASA AD 2019-0141,  or  within  90 days
    after the effective date of this AD, whichever occurs later.

(4) The "Remarks" section of EASA AD 2019-0141 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)  or intervals are allowed except as specified in the provi-
    sions of the "Ref. Publications" section of EASA AD 2019-0141.

(l) 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 (m) 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 local
    flight standards district office/certificate holding district office.

(ii) AMOCs approved previously for AD 2019-07-01 are approved as AMOCs for
     the corresponding provisions  of  EASA AD 2019-0141 that are required
     by paragraph (g) 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.

(m) 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.

(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 December 23,
    2020.

(i) European Union Aviation Safety Agency (EASA) AD 2019-0141,  dated June
    17, 2019.

(ii) [Reserved]

(4) The following service information was approved for IBR on May 24, 2019
    (84 FR 16390, April 19, 2019).

(i) Chapter 5-40, Airworthiness Limitations, DGT 131028 Revision 17, dated
    September 2017, of the Dassault Aviation Falcon 20 Maintenance Manual.

(ii) [Reserved]

(5) For EASA AD 2019-0141, 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.

(6) For Dassault Aviation material,  contact  Dassault Falcon Jet Corpora-
    tion,  Teterboro Airport,  P.O. Box 2000,  South Hackensack, NJ 07606;
    telephone 201-440-6700; internet https://www.dassaultfalcon.com.

(7) 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-2020-0582.

(8) 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 November 4, 2020. 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-2020-0582; Product Identifier 2020-NM-059-AD; Amendment
39-21326; AD 2020-23-10]
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) 2014-26-07
and AD 2019-07-01 which apply to Dassault Aviation Model FAN JET FALCON
and FAN JET FALCON SERIES C, D, E, F, and G airplanes. AD 2019-07-01
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 December 23, 2020.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of December 23,
2020.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of May
24, 2019 (84 FR 16390, April 19, 2019).

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 the Dassault Aviation material
identified in this AD that continues to be IBR, 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-2020-0582.

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-
0582; 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 2019-0141, dated June 17, 2019
(``EASA AD 2019-0141'') (also referred to as the Mandatory Continuing
Airworthiness Information, or ``the MCAI''), to correct an unsafe
condition for certain Dassault Aviation Model FAN JET FALCON and FAN
JET FALCON SERIES C, D, E, F, and G airplanes.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2019-07-01, Amendment 39-19612 (84 FR
16390, April 19, 2019) (``AD 2019-07-01'') and AD 2014-26-07, Amendment
39-18058 (80 FR 2815, January 21, 2015) (``AD 2014-26-07''). AD 2019-
07-01 applied to certain Dassault Aviation Model FAN JET FALCON and FAN
JET FALCON SERIES C, D, E, F, and G airplanes. The NPRM published in
the Federal Register on July 15, 2020 (85 FR 42746). 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 an EASA AD.
The FAA is issuing this AD to address, among other things, fatigue
cracking and damage in principal structural elements; such fatigue
cracking and damage could result in 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 IBR Material Under 1 CFR Part 51

EASA AD 2019-0141 describes new or more restrictive airworthiness
limitations for airplane structures and safe life limits.
This AD also requires Chapter 5-40, Airworthiness Limitations, DGT
131028, Revision 17, dated September 2017, of the Dassault Aviation
Falcon 20 Maintenance Manual, which the Director of the Federal
Register approved for incorporation by reference as of May 24, 2019 (84
FR 16390, April 19, 2019).
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 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 2019-07-01 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. In the past, the agency 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 proposed 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 (AD) 2014-26-07, Amendment 39-18058
(80 FR 2815, January 21, 2015); and AD 2019-07-01, Amendment 39-19612
(84 FR 16390, April 19, 2019); and

b. Adding the following new AD: