preamble attached >>>
ADs updated daily at www.Tdata.com
PROPOSED AD DASSAULT AVIATION: Docket No. FAA-2020-0778; Product Identifier 2020-NM-097-AD.
(a) COMMENTS DUE DATE

    The FAA must receive comments by October 5, 2020.

(b) AFFECTED ADS

(1) This  AD  replaces  AD 2019-23-05,  Amendment  39-19799  (84 FR 67169,
    December 9, 2019) ("AD 2019-23-05").

(2) This  AD  affects  AD  2010-26-05,  Amendment  39-16544  (75 FR 79952,
    December 21, 2010) ("AD 2010-26-05").

(c) APPLICABILITY

    This AD applies to all Dassault Aviation Model MYSTERE-FALCON 900 air-
    planes, certificated in any category.

(d) SUBJECT

    Air   Transport   Association   (ATA)  of   America   Code   05,  Time
    Limits/Maintenance 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 REVISION OF EXISTING MAINTENANCE OR INSPECTION PROGRAM,  WITH
    NO CHANGES

    This paragraph restates the requirements of paragraph (i)  of AD 2019-
    23-05, with  no changes.  Within 90  days after  January 13, 2020 (the
    effective date of AD  2019-23-05), revise the existing  maintenance or
    inspection  program,  as applicable,  to  incorporate the  information
    specified  in Chapter  5-40, Airworthiness  Limitations, Revision  24,
    dated September 2018, of the Dassault Aviation Falcon 900  Maintenance
    Manual. The initial  compliance times for  doing the tasks  are at the
    times specified in  Chapter 5-40, Airworthiness  Limitations, Revision
    24,  dated  September  2018,  of  the  Dassault  Aviation  Falcon  900
    Maintenance  Manual,  or  within  90  days  after  January  13,  2020,
    whichever  occurs  later. 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 the date of issuance of
    the original airworthiness certificate or the date of issuance of  the
    original  export  certificate  of  airworthiness.  Accomplishing   the
    maintenance or inspection program  revision required  by paragraph (i)
    of this AD terminates the requirements of this paragraph.

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

    This paragraph restates the requirements of paragraph (h)  of AD 2019-
    23-05, 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 re-
    quired actions and compliance times specified in,  and  in  accordance
    with, European Union Aviation Safety Agency (EASA) AD 2020-0115, dated
    May 20, 2020  ("EASA AD 2020-0115").  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 2020-0115

(1) The requirements specified  in paragraphs (1) and (2) of EASA AD 2020-
    0115 do not apply to this AD.

(2) Paragraph (3) of EASA AD 2020-0115  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 2020-0115  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 2020-0115 is at the applicable  "associated thresholds"
    specified in paragraph (3) of EASA AD 2020-0115,  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-
    0115 do not apply to this AD.

(5) The "Remarks" section of EASA AD 2020-0115 does not apply to this AD.

(k) NEW PROVISIONS FOR ALTERNATIVE ACTIONS OR 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 unless they are approved as speci-
    fied in the provisions  of the "Ref. Publications" section  of EASA AD
    2020-0115.

(l) TERMINATING ACTIONS FOR CERTAIN REQUIREMENTS 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 MYSTERE-FALCON 900 airplanes.

(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 2019-23-05 are approved as AMOCs for
     the corresponding provisions  of EASA AD 2020-0115  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 information about EASA AD 2020-0115,  contact  the  EASA,  Konrad-
    Adenauer-Ufer 3,  50668 Cologne, Germany;  phone: +49 221 8999 000; e-
    mail: 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 proposed AD,  con-
    tact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000
    South Hackensack, NJ 07606; phone: 201-440-6700; internet: http://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-2020-0778.

(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; phone and fax: 206-231-3226
    email: tom.rodriguez@faa.gov.

Issued on August 13, 2020. Lance T Gant, Director, Compliance & Airworthi-
ness Division, Aircraft Certification Service.

DATES: The FAA must receive comments  on this  proposed  AD  by October 5,
2020.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0778; Product Identifier 2020-NM-097-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)
2019-23-05, which applies to all Dassault Aviation Model MYSTERE-FALCON
900 airplanes. AD 2019-23-05 requires revising the existing maintenance
or inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. Since the FAA issued AD 2019-23-
05, the agency 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 October 5,
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: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590, 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; phone: +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 service information
identified in this proposed AD, contact Dassault Falcon Jet
Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ
07606; phone: 201-440-6700; internet: http://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-2020-0778.

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-2020-0778;
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; phone 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 the ADDRESSES section. Include "Docket No. FAA-2020-0778;
Product Identifier 2020-NM-097-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 this NPRM based on 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 that are received, without
change, to https://www.regulations.gov, including any personal
information you provide.

The FAA will also post a report summarizing each substantive verbal
contact the FAA receives about this NPRM.

Confidential Business Information

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 the person identified in the FOR FURTHER
INFORMATION CONTACT section. 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 2019-23-05, Amendment 39-19799 (84 FR 67169,
December 9, 2019) ("AD 2019-23-05"), for all Dassault Aviation Model
MYSTERE-FALCON 900 airplanes. AD 2019-23-05 requires revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations. The FAA
issued AD 2019-23-05 to address reduced structural integrity of the
airplane. AD 2019-23-05 specifies that accomplishing 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 MYSTERE-FALCON 900 airplanes.

Actions Since AD 2019-23-05 Was Issued

Since the FAA issued AD 2019-23-05, 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 2020-0115, dated May 20, 2020
("EASA AD 2020-0115") (also referred to as the Mandatory Continuing
Airworthiness Information, or "the MCAI"), to correct an unsafe
condition for all Dassault Aviation Model MYSTERE-FALCON 900 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 structural integrity of the
airplane. See the MCAI for additional background information.

Related IBR Material Under 1 CFR Part 51

EASA AD 2020-0115, dated May 20, 2020, 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 24, dated September 2018, of the Dassault
Aviation Falcon 900 Maintenance Manual, which the Director of the
Federal Register approved for incorporation by reference as of January
13, 2020 (84 FR 67169, December 9, 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.

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 2019-23-05.
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
2020-0115 described previously, as incorporated by reference. Any
differences with EASA AD 2020-0115 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 [and CDCCLs] 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 2020-0115
will be incorporated by reference in the FAA final rule. This proposed
AD would, therefore, require compliance with EASA AD 2020-0115 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 2020-0115 that is required
for compliance with EASA AD 2020-0115 will be available on the internet
at https://www.regulations.gov by searching for and locating Docket No.
FAA-2020-0778 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).

Costs of Compliance

The FAA estimates that this proposed AD affects 105 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 2019-23-05 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) 2019-23-05, Amendment 39-19799
(84 FR 67169, December 9, 2019), and

b. Adding the following new AD: