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PROPOSED AD DASSAULT AVIATION: Docket No. FAA-2020-0980; Product Identifier 2020-NM-094-AD.
(a) COMMENTS DUE DATE

    The FAA must receive comments by December 18, 2020.

(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
    already 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)), 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
    required 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
    inspection 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.,
    inspections) and  intervals are  allowed unless  they are  approved as
    specified 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)(4) 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 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

(1) 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
    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-2020-0980.

(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 27, 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-2020-0980; Product Identifier 2020-NM-094-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)
2020-02-21, which applies to all Dassault Aviation Model FALCON 2000
airplanes. AD 2020-02-21 requires revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive and airworthiness limitations. Since the FAA issued AD
2020-02-21, 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-2020-0980.

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 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-2020-0980; Product Identifier
2020-NM-094-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 2020-02-21, Amendment 39-19833 (85 FR 7860,
February 12, 2020) ("AD 2020-02-21"), for all Dassault Aviation Model
FALCON 2000 airplanes. AD 2020-02-21 requires revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive airworthiness limitations. The FAA issued AD 2020-02-
21 to address reduced controllability of the airplane. AD 2020-02-21
specifies that accomplishing the revision required by paragraph (g) or
(i) of that AD terminates the requirements of paragraph (g) of AD 2010-
26-05, Amendment 39-16544 (75 FR 79952, December 21, 2010), for Model
FALCON 2000 airplanes.

Actions Since AD 2020-02-21 Was Issued

Since the FAA issued AD 2020-02-21, 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 2020-0113, 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.

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 controllability of the airplane.
See the MCAI for additional background information.

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 proposed AD would also require 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 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 2020-02-21.
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
2020-0113 described previously, as incorporated by reference. Any
differences with EASA AD 2020-0113 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 2020-0113
will be incorporated by reference in the FAA final rule. This proposed
AD would, therefore, require compliance with EASA AD 2020-0113 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 2020-0113 that is required
for compliance with EASA AD 2020-0113 will be available on the internet
at https://www.regulations.gov by searching for and locating Docket No.
FAA-2020-0980 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 168 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 2020-02-21 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. 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

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

b. Adding the following new AD: