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2019-23-03 DASSAULT AVIATION: Amendment 39-19796; Docket No. FAA-2019-0697; Product Identifier 2019-NM-110-AD.
(a) EFFECTIVE DATE

    This AD is effective January 13, 2020.

(b) AFFECTED ADS

(1) This AD replaces AD 2014-16-27,Amendment 39-17951 (79 FR 51071, August
    27, 2014) ("AD 2014-16-27"); and AD 2017-19-14, Amendment 39-19044 (82
    FR 43674, September 19, 2017) ("AD 2017-19-14").

(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  Dassault Aviation Model FALCON 900EX airplanes,
    serial number (S/N) 97 and S/Ns 120 and higher,  certificated  in  any
    category,  with  an  original  airworthiness  certificate  or original
    export certificate of airworthiness  issued on or before  September 1,
    2018.

(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, among other things, fatigue cracking and damage in  principal
    structural elements; such fatigue cracking and damage could result  in
    reduced structural integrity of the airplane.

(f) COMPLIANCE

    Comply  with this  AD within  the compliance  times specified,  unless
    already done.

(g) RETAINED REVISION OF MAINTENANCE OR INSPECTION PROGRAM WITH NO CHANGES

    This paragraph restates the requirements of paragraph (g)  of AD 2017-
    19-14, with  no changes.  Within 90  days after  October 24, 2017 (the
    effective date of AD  2017-19-14), revise the existing  maintenance or
    inspection  program,  as applicable,  to  incorporate the  information
    specified  in  Chapter 5-40,  Airworthiness  Limitations,  Revision 9,
    dated November 2015, of the Dassault Falcon 900EX EASy, Falcon  900LX,
    and Falcon 900DX Maintenance Manual. The initial compliance times  for
    accomplishing  the actions  specified in  Chapter 5-40,  Airworthiness
    Limitations, Revision 9, dated  November 2015, of the  Dassault Falcon
    900EX  EASy, Falcon  900LX, and  Falcon 900DX  Maintenance Manual,  is
    within the applicable times specified in the maintenance manual or  90
    days  after  October  24,  2017,  whichever  occurs  later,  except as
    provided by paragraphs (g)(1) through (4) of this AD.

(1) The term "LDG"  in  the  "First Inspection" column of any table in the
    service information means total airplane landings.

(2) The term "FH"  in  the  "First Inspection" column of any table  in the
    service information means total flight hours.

(3) The term "FC"  in  the  "First Inspection" column of any table  in the
    service information means total flight cycles.

(4) The term "M"  in  the  "First Inspection" column of any table  in  the
    service information means months.

(h) RETAINED REQUIREMENT FOR NO ALTERNATIVE ACTIONS AND INTERVALS WITH NEW
    EXCEPTION

    This paragraph restates the requirements specified in paragraph (h) of
    AD 2017-19-14, with a new  exception. Except as required by  paragraph
    (i) of this AD, after accomplishing the revision required by paragraph
    (g) of this AD, no alternative actions (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 (l)(1) of this AD.

(i) NEW REQUIREMENT OF THIS AD: MAINTENANCE OR INSPECTION PROGRAM REVISION

    Within 90 days after the effective date of this AD,  revise the exist-
    ing maintenance or inspection  program, as applicable, to  incorporate
    the information specified in Chapter 5-40, Airworthiness  Limitations,
    Revision 11, dated September 2018, of the Dassault Falcon 900EX  EASy,
    Falcon  900LX,  and  Falcon  900DX  Maintenance  Manual.  The  initial
    compliance  times  for  accomplishing the  actions  are  at the  times
    specified  in Chapter  5-40, Airworthiness  Limitations, Revision  11,
    dated September 2018, of the Dassault Falcon 900EX EASy, Falcon 900LX,
    and Falcon 900DX  Maintenance Manual, or  90 days after  the effective
    date  of  this  AD,  whichever occurs  later,  except  as  provided by
    paragraphs (i)(1) through (4) of this AD.

(1) The term "LDG"  in  the  "First Inspection" column of any table in the
    service information means total airplane landings.

(2) The term "FH"  in  the  "First Inspection" column of any table  in the
    service information means total flight hours.

(3) The term "FC"  in  the  "First Inspection" column of any table  in the
    service information means total flight cycles.

(4) The term "M"  in  the  "First Inspection" column of any table  in  the
    service information  means months  since the  date of  issuance of the
    original  airworthiness certificate  or the  date of  issuance of  the
    original export certificate of airworthiness.

(j) NO ALTERNATIVE ACTIONS OR INTERVALS

    After the existing maintenance  or inspection program has been revised
    as required by paragraph (i) of this AD, no alternative actions (e.g.,
    inspections) or intervals may be used unless the actions and intervals
    are approved as an AMOC in accordance with the procedures specified in
    paragraph (l)(1) of this AD.

(k) TERMINATING ACTIONS 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  900EX  airplanes,  S/N 97 and S/Ns 120  and
    higher.

(l) OTHER FAA AD PROVISIONS

(1) Alternative Methods of Compliance (AMOCs):  The Manager, International
    Section, Transport Standards 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  International
    Section,  send  it  to  the  attention  of  the  person  identified in
    paragraph (m)(2) of this AD.  Information may be emailed to  9-ANM-116
    -AMOC-REQUESTS@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:  As of the effective date of this AD, for
    any  requirement  in  this  AD to  obtain  corrective  actions  from a
    manufacturer, the action must be accomplished using a method  approved
    by  the Manager,  International Section,  Transport Standards  Branch,
    FAA; or the European Union Aviation Safety Agency (EASA); or  Dassault
    Aviation's EASA Design Organization Approval (DOA). If approved by the
    DOA, the approval must include the DOA-authorized signature.

(m) RELATED INFORMATION

(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD
    2019-0134, dated June 11, 2019, for related information. This MCAI may
    be found in the AD docket on the internet  at https://www.regulations.
    gov by searching for and locating Docket No. FAA-2019-0697.

(2) For more information about this AD,  contact Tom Rodriguez,  Aerospace
    Engineer, International Section, Transport Standards Branch, FAA, 2200
    South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3226.

(n) MATERIAL INCORPORATED BY REFERENCE

(1) The Director of the Federal Register  approved  the  incorporation  by
    reference (IBR) of  the service information  listed in this  paragraph
    under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use  this service information as applicable to do the actions
    required by this AD, unless this AD specifies otherwise.

(3) The following service information was approved for IBR  on January 13,
    2020.

(i) Chapter 5-40, Airworthiness Limitations, Revision 11,  dated September
    2018, of the Dassault Falcon 900EX EASy, Falcon 900LX and Falcon 900DX
    Maintenance Manual.

(ii) [Reserved]

(4) The following service information was approved for IBR  on October 24,
    2017 (82 FR 43674, September 19, 2017).

(i) Chapter 5-40, Airworthiness Limitations,  Revision 9,  dated  November
    2015, of the Dassault Falcon 900EX EASy, Falcon 900LX and Falcon 900DX
    Maintenance Manual.

(ii) [Reserved]

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

(6) You may view this service information at the FAA,  Transport Standards
    Branch,  2200 South 216th St., Des Moines, WA.  For information on the
    availability of this material at the FAA, call 206-231-3195.

(7) You  may  view  this  service  information  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 in Des Moines, Washington, on November 14, 2019.  Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification Service

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, Inter-
national Section,  Transport Standards Branch,  FAA, 2200 South 216th St.,
Des Moines, WA 98198; telephone and fax 206-231-3226.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0697; Product Identifier 2019-NM-110-AD; Amendment
39-19796; AD 2019-23-03]
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 Directives (AD) 2017-19-
14 and AD 2014-16-27, which apply to certain Dassault Aviation Model
FALCON 900EX airplanes. Those ADs require revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive maintenance requirements and/or airworthiness
limitations. Since the FAA issued AD 2017-19-14 and AD 2014-16-27, the
FAA determined that new or more restrictive airworthiness limitations
are necessary. This AD requires revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. The FAA is issuing this AD to
address the unsafe condition on these products.

DATES: This AD is effective January 13, 2020.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 13,
2020.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of
October 24, 2017 (82 FR 43674, September 19, 2017).

ADDRESSES: For service information identified in this final rule,
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 referenced service
information at the FAA, Transport Standards 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 on the
internet at https://www.regulations.gov by searching for and locating
Docket No. FAA-2019-0697.

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-2019-
0697; 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, the regulatory evaluation, 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,
International Section, Transport Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; telephone and fax 206-231-3226.

SUPPLEMENTARY INFORMATION:

Discussion

The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2019-0134, dated June 11, 2019 (``EASA AD 2019-0134'') (also
referred to as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for certain Dassault
Aviation Model FALCON 900EX airplanes. You may examine the MCAI in the
AD docket on the internet at https://www.regulations.gov by searching
for and locating Docket No. FAA-2019-0697.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2017-19-14, Amendment 39-19044 (82 FR
43674, September 19, 2017) (``AD 2017-19-14''); and AD 2014-16-27,
Amendment 39-17951 (79 FR 51071, August 27, 2014) (``AD 2014-16-27'').
AD 2017-19-14 and AD 2014-16-27 applied to certain Dassault Aviation
Model FALCON 900EX airplanes. Further, AD 2014-16-27 terminates
paragraph (g)(1) of AD 2010-26-05, Amendment 39-16544 (75 FR 79952,
December 21, 2010), for certain Dassault Aviation Model FALCON 900EX
airplanes, and this terminating provision is included in this AD. The
NPRM published in the Federal Register on September 13, 2019 (84 FR
48310). The NPRM was prompted by the FAA's determination that new or
more restrictive airworthiness limitations are necessary. The NPRM
proposed to require revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive
airworthiness limitations. The FAA is issuing this AD to address, among
other things, fatigue cracking and damage in principal structural
elements; such fatigue cracking and damage could result in reduced
structural integrity of the airplane. See the MCAI for additional
background information.

Comments

The FAA gave the public the opportunity to participate in
developing this final rule. The FAA received no comments on the NPRM or
on the determination of the cost to the public.

Conclusion

The FAA reviewed the relevant data and determined that air safety
and the public interest require adopting this final rule as proposed,
except for minor editorial changes. The FAA 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

Dassault Aviation has issued Chapter 5-40, Airworthiness
Limitations, Revision 11, dated September 2018, of the Dassault Falcon
900EX EASy, Falcon 900LX, and Falcon 900DX Maintenance Manual. This
service information describes procedures, maintenance tasks, and
airworthiness limitations specified in the Airworthiness Limitations
section of the airplane maintenance manual.
This AD also requires Chapter 5-40, Airworthiness Limitations,
Revision 9, dated November 2015, of the Dassault Falcon 900EX EASy,
Falcon 900LX, and Falcon 900DX Maintenance Manual, which the Director
of the Federal Register approved for incorporation by reference as of
October 24, 2017 (82 FR 43674, September 19, 2017).
This service information 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 79 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 2017-19-14 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 FAA 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.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the Compliance and Airworthiness Division, but
during this transition period, the Executive Director has delegated the
authority to issue ADs applicable to transport category airplanes and
associated appliances to the Director of the System Oversight Division.

Regulatory Findings

The FAA determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the national government and the States, or on the distribution of power
and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39


Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

1. The authority citation for part 39 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec. 39.13 [Amended]

2. The FAA amends Sec. 39.13 by

a. Removing Airworthiness Directive (AD) 2014-16-27, Amendment 39-17951
(79 FR 51071, August 27, 2014); and AD 2017-19-14, Amendment 39-19044
(82 FR 43674, September 19, 2017); and

b. Adding the following new AD: