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2020-26-07 DASSAULT AVIATION: Amendment 39-21362; Docket No. FAA-2020-0778; Product Identifier 2020-NM-097-AD.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective January 25, 2021.

(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/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 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  alternative  method  of
    compliance  (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  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.

(i) Before using any approved AMOC,  notify your appropriate principal in-
    spector, or lacking a principal inspector,  the manager of the respon-
    sible Flight Standards 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

    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.

(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 January 25,
    2021.

(i) European Union Aviation Safety Agency (EASA) AD 2020-0115,  dated  May
    20, 2020.

(ii) [Reserved]

(4) The following service information was approved  for IBR on January 13,
    2020 (84 FR 67169, December 9, 2019).

(i) Chapter 5-40, Airworthiness Limitations, Revision 24,  dated September
    2018, of the Dassault Aviation Falcon 900 Maintenance Manual.

(ii) [Reserved]

(5) For EASA AD 2020-0115, 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 service information, contact Dassault Falcon Jet Corpora-
    tion,  Teterboro Airport,  P.O. Box 2000,  South Hackensack, NJ 07606;
    phone: 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-2020-0778.

(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  December 8, 2020.  Gaetano A. Sciortino,  Deputy Director  for
Strategic Initiatives,  Compliance & Airworthiness Division, Aircraft Cer-
tification Service.

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.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0778; Product Identifier 2020-NM-097-AD; Amendment
39-21362; AD 2020-26-07]
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) 2019-23-
05, which applied to all Dassault Aviation Model MYSTERE-FALCON 900
airplanes. AD 2019-23-05 required revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. This AD continues to require
revising the existing maintenance or inspection program, as applicable,
to incorporate those new or more restrictive airworthiness limitations,
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 January 25, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 25,
2021.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of
January 13, 2020 (84 FR 67169, December 9, 2019).

ADDRESSES: For EASA material 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 final rule, contact Dassault Falcon Jet Corporation,
Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; phone:
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-2020-0778.

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 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; phone 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 2020-0115, 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.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2019-23-05, Amendment 39-19799 (84 FR
67169, December 9, 2019) (AD 2019-23-05). AD 2019-23-05 applied to all
Dassault Aviation Model MYSTERE-FALCON 900 airplanes. The NPRM
published in the Federal Register on August 19, 2020 (85 FR 50970). The
NPRM was prompted by a determination that new or more restrictive
airworthiness limitations are necessary. The NPRM proposed to continue
to require revising the existing maintenance or inspection program, as
applicable, to incorporate new or more restrictive airworthiness
limitations. The NPRM also proposed to require revising the existing
maintenance or inspection program, as applicable, to incorporate
additional new or more restrictive airworthiness limitations, as
specified in a EASA AD.
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 has considered the comments
received.

Support for the NPRM

Ian Reineck indicated support for the NPRM.

Request To Include Actions in the Cost Estimate

Ian Reineck requested that the cost estimate be revised to include
structural upkeep per flight hours, rather than solely maintenance work
hours. The commenter stated this is what determines the core functions
inside aviation maintenance schedules. The commenter also stated this
would be inclusive, regardless of operator, but still reflect the cost
of an average operator's inspection through the quantity of accumulated
flight time on the airplane. The commenter concluded that, if flight
time is not presented in the inspection cost, it presents another
problem: These aircraft may change ownership or operator-ship as they
age.
The FAA infers that the commenter is requesting that the FAA
include the costs in this AD for complying with the actions (e.g.,
inspections) that are specified in the airworthiness limitations
document referenced in EASA AD 2020-0115. The FAA disagrees because
those actions are not directly required by this AD. Additionally, the
FAA does not distribute the costs over time because the cost estimates
have been standardized to include the larger whole cost of the requirement, not
the more uniform cost per flight hour, which the FAA has determined is
best to inform the broadest user base. The cost information provided in
this AD describes only the direct costs of the specific actions
required by this AD. This AD requires only 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, and provides a
compliance time to phase in the initial actions. Section 91.403(c) of
the Federal Aviation Regulations (14 CFR 91.403(c)) requires the
actions once the maintenance or inspection program is changed.
Therefore, we have not changed this final rule in this regard.

Conclusion

The FAA reviewed the relevant data, considered the comments
received, 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 2020-0115 describes new or more restrictive airworthiness
limitations for airplane structures and safe life limits.
This AD also requires 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.

Costs of Compliance

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

b. Adding the following new AD: