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PROPOSED AD DASSAULT AVIATION: Docket No. FAA-2020-0976; Product Identifier 2020-NM-095-AD.
(a) COMMENTS DUE DATE

    The FAA must receive comments by December 18, 2020.

(b) AFFECTED ADS

(1) This AD replaces AD 2020-04-22, Amendment 39-19858 (85 FR 17489, March
    20, 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
    already 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  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 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)(4) 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  local  flight  standards
    district office/certificate holding district 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

(1) For information about 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 website at https://ad.easa.europa.eu.

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

(3) 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.

(4) 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.

Issued on October 26, 2020. Lance T Gant, Director, Compliance & Airworth-
iness Division, Aircraft Certification Service.

DATES: The FAA must receive comments  on this proposed AD  by December 18,
2020.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0976; Product Identifier 2020-NM-095-AD]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2020-04-22, which applies to certain Dassault Aviation Model FALCON
2000EX airplanes. AD 2020-04-22 requires revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive airworthiness limitations. Since the FAA issued AD
2020-04-22, the FAA has determined that new or more restrictive
airworthiness limitations are necessary. This proposed AD would require
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
will be incorporated by reference. The FAA is proposing this AD to
address the unsafe condition on these products.

DATES: The FAA must receive comments on this proposed AD by December
18, 2020.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:

Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the
instructions for submitting comments.

Fax: 202-493-2251.

Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.

Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.

For EASA material that will be 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 proposed AD, 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 NPRM, any comments
received, and other information. The street address for Docket Operations
is listed above. Comments will be available in the AD docket shortly after
receipt.

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:

Comments Invited

The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include "Docket No. FAA-2020-0976; Product Identifier
2020-NM-095-AD" at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
the proposal because of those comments.

Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
https://www.regulations.gov, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this proposed AD.

Confidential Business Information


CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as "PROPIN." The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to 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. Any
commentary that the FAA receives which is not specifically designated
as CBI will be placed in the public docket for this rulemaking.

Discussion

The FAA issued AD 2020-04-22, Amendment 39-19858 (85 FR 17487,
March 30, 2020) ("AD 2020-04-22"), for certain Dassault Aviation
Model FALCON 2000EX airplanes. AD 2020-04-22 requires revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations. The FAA
issued AD 2020-04-22 to address reduced structural integrity of the
airplane. AD 2020-04-22 specifies that accomplishing the revision
required by paragraph (g) or (i) of that AD terminates the requirements
of paragraph (g)(1) of AD 2010-26-05, Amendment 39-16544 (75 FR 79952,
December 21, 2010), for Dassault Aviation Model FALCON 2000EX
airplanes.

Actions Since AD 2020-04-22 Was Issued

Since the FAA issued AD 2020-04-22, the FAA has determined that new
or more restrictive airworthiness limitations are necessary.

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 for all Dassault Aviation Model FALCON 2000EX airplanes.

Airplanes with an original airworthiness certificate or original
export certificate of airworthiness issued after February 15, 2020,
must comply with the airworthiness limitations specified as part of the
approved type design and referenced on the type certificate data sheet
for those airplanes; this AD therefore does not include these airplanes
in the applicability.

This proposed AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
proposing this AD to address reduced structural integrity of the
airplane. See the MCAI for additional background information.

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 proposed AD would also require 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.

FAA's Determination and Requirements of This Proposed AD

This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to the FAA's bilateral agreement with the State of Design Authority,
the FAA has been notified of the unsafe condition described in the MCAI
and service information referenced above. The FAA is proposing this AD
because the FAA has evaluated all pertinent information and determined
an unsafe condition exists and is likely to exist or develop on other
products of the same type design.

Proposed AD Requirements


This proposed AD would retain the requirements of AD 2020-04-22.
This proposed AD would also require revising the existing maintenance
or inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations, which are specified in EASA AD
2020-0114 described previously, as incorporated by reference. Any
differences with EASA AD 2020-0114 are identified as exceptions in the
regulatory text of this AD.

This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections).
Compliance with these actions is required by 14 CFR 91.403(c). For
airplanes that have been previously modified, altered, or repaired in
the areas addressed by this proposed AD, the operator may not be able
to accomplish the actions described in the revisions. In this
situation, to comply with 14 CFR 91.403(c), the operator must request
approval for an alternative method of compliance according to paragraph
(m)(1) of this proposed AD.

Explanation of Required Compliance Information

In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA initially worked with Airbus and EASA to develop a
process to use certain EASA ADs as the primary source of information
for compliance with requirements for corresponding FAA ADs. The FAA has
since coordinated with other manufacturers and civil aviation
authorities (CAAs) to use this process. As a result, EASA AD 2020-0114
will be incorporated by reference in the FAA final rule. This proposed
AD would, therefore, require compliance with EASA AD 2020-0114 in its
entirety, through that incorporation, except for any differences
identified as exceptions in the regulatory text of this proposed AD.
Using common terms that are the same as the heading of a particular
section in the EASA AD does not mean that operators need comply only
with that section. For example, where the AD requirement refers to
"all required actions and compliance times," compliance with this AD
requirement is not limited to the section titled "Required Action(s)
and Compliance Time(s)" in the EASA AD.

Service information specified in EASA AD 2020-0114 that is required
for compliance with EASA AD 2020-0114 will be available on the internet
at https://www.regulations.gov by searching for and locating Docket No.
FAA-2020-0976 after the FAA final rule is published.

Airworthiness Limitation ADs Using the New Process

The FAA's process of incorporating by reference MCAI ADs as the
primary source of information for compliance with corresponding FAA ADs
has been limited to certain MCAI ADs (primarily those with service
bulletins as the primary source of information for accomplishing the
actions required by the FAA AD). However, the FAA is now expanding the
process to include MCAI ADs that require a change to airworthiness
limitation documents, such as airworthiness limitation sections.

For these ADs that incorporate by reference an MCAI AD that changes
airworthiness limitations, the FAA requirements are unchanged.
Operators must revise the existing maintenance or inspection program,
as applicable, to incorporate the information specified in the new
airworthiness limitation document. The airworthiness limitations must
be followed according to 14 CFR 91.403(c) and 91.409(e).

The previous format of the airworthiness limitation ADs included a
paragraph that specified that 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 the AMOCs paragraph under
"Other FAA Provisions." This new format includes a "New Provisions
for Alternative Actions and Intervals" paragraph that does not
specifically refer to AMOCs, but operators may still request an AMOC to
use an alternative action or interval.

Costs of Compliance

The FAA estimates that this proposed AD affects 17 airplanes of
U.S. registry. The FAA estimates the following costs to comply with
this proposed 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. 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 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

The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed
regulation:

(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.

The Proposed Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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: