Published 2020-11-02 · Federal Register document 2020-24098
Airworthiness Directives; Dassault Aviation Airplanes
Publication summary
The FAA is superseding Airworthiness Directive (AD) 2019-24- 11, which applied to certain Dassault Aviation Model FALCON 900EX airplanes. AD 2019-24-11 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. This AD continues to require those maintenance or inspection program revisions, 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.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:04.586324+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2020-f01fbc4d7ab3dbaa
- Source row
- results[318]
- Raw source SHA-256
- f01fbc4d7ab3dbaae6a412acd9ff6cece48db77a6a882e46e8f8087200be3837
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2020-21-19
- Effective date printed in this edition
- 2020-12-07
Read 15 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective December 7, 2020.
Exact source excerpt. Text positions 9636–9700, end exclusive, in the original decoded publication. SHA-256: e09d70f0ee5f681800e8b839642dabc3c8e64e2adc5062e1b2dd3087bf9f0ccd
Affected ADs
(b) Affected ADs
(1) This AD replaces AD 2019-24-11, Amendment 39-19814 (84 FR
69997, December 20, 2019) (``AD 2019-24-11'').
(2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR
79952, December 21, 2010) (``AD 2010-26-05'').
Exact source excerpt. Text positions 9700–9946, end exclusive, in the original decoded publication. SHA-256: 1a943bd59b989230e63dfdecda79e38c19d372f8ad8bf60427eb6a015f01b15c
Applicability wording · Applicability
(c) Applicability
This AD applies to Dassault Aviation Model FALCON 900EX
airplanes, certificated in any category, as identified in European
Union Aviation Safety Agency (EASA) AD 2020-0116, dated May 20, 2020
(``EASA AD 2020-0116'').
Exact source excerpt. Text positions 9946–10190, end exclusive, in the original decoded publication. SHA-256: 197caf6e342890a48d85e971cec94d83ecdf7bc3127ab4502730d13d208e9138
Subject
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.
Exact source excerpt. Text positions 10190–10293, end exclusive, in the original decoded publication. SHA-256: b15263823fded4455be00ff56d3a178d819d56a04f0615355cdb43771d1bcef9
Reason
(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.
Exact source excerpt. Text positions 10293–10507, end exclusive, in the original decoded publication. SHA-256: 98888c0375c117bdffc31ce8f1c29a86aa21467f7231d06f297f44341170c50f
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 10507–10609, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Retained Maintenance or Inspection Program Revision, with No Changes
(g) Retained Maintenance or Inspection Program Revision, with No
Changes
This paragraph restates the requirements of paragraph (i) of AD
2019-24-11, with no changes. Within 90 days after January 24, 2020
(the effective date AD 2019-24-11), revise the existing maintenance
or inspection program, as applicable, to incorporate the information
specified in Chapter 5-40, Airworthiness Limitations, Revision 16,
dated September 2018, of the Dassault FALCON 900EX Maintenance
Manual. The initial compliance times for accomplishing the actions
are at the times specified in Chapter 5-40, Airworthiness
Limitations, Revision 16, dated September 2018, or 90 days after
January 24, 2020, whichever occurs later, except as provided by
paragraphs (g)(1) through (4) of this AD. Accomplishing the
maintenance or inspection program revision required by paragraph (i)
of this AD terminates the requirements of this paragraph.
(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.
Exact source excerpt. Text positions 10609–12185, end exclusive, in the original decoded publication. SHA-256: 92cb20256053ff56b826b714ed19a46f2ea744c29c37fa8bf85e29c4b1761afd
Retained Restrictions on Alternative Actions and Intervals, with a New Exception
(h) Retained Restrictions on Alternative Actions and Intervals, with a
New Exception
This paragraph restates the requirements of paragraph (j) of AD
2019-24-11, with a new exception. Except as required by paragraph
(i) of this AD, after the 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.
Exact source excerpt. Text positions 12185–12767, end exclusive, in the original decoded publication. SHA-256: cf5e1d11b50c06d8703f1f99dc4f8b9dabd0854ebb1044757eb9bd973ca57f66
New Maintenance or Inspection Program Revision
(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, EASA AD 2020-0116. Accomplishing the maintenance or
inspection program revision required by this paragraph terminates
the requirements of paragraph (g) of this AD.
Exact source excerpt. Text positions 12767–13133, end exclusive, in the original decoded publication. SHA-256: 57c9d2fc851fa23351d4bbbac30fe93cf49a068cc4b3b34bd86f9cc6d6226c5b
Exceptions to EASA AD 2020-0116
(j) Exceptions to EASA AD 2020-0116
(1) The requirements specified in paragraphs (1) and (2) of EASA
AD 2020-0116 do not apply to this AD.
(2) Paragraph (3) of EASA AD 2020-0116 specifies revising ``the
approved AMP''
[[Page 69144]]
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
2020-0116 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 2020-0116 is at the applicable ``associated
thresholds'' specified in paragraph (3) of EASA AD 2020-0116, 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 2020-0116 do not apply to this AD.
(5) The ``Remarks'' section of EASA AD 2020-0116 does not apply
to this AD.
Exact source excerpt. Text positions 13133–14172, end exclusive, in the original decoded publication. SHA-256: 68f53608c3782e310d1ee05ad87953d72e2fd7df34150737d8612ca1eb075730
New Provisions for Alternative Actions and Intervals
(k) New Provisions for Alternative Actions and Intervals
After the maintenance or inspection program has been revised as
required 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 2020-0116.
Exact source excerpt. Text positions 14172–14525, end exclusive, in the original decoded publication. SHA-256: cc1f13e0c5e3987b633f144800b989072cf0dfd9cf41d60ea67aa294fc2a15ed
Terminating Actions for Certain Actions in AD 2010-26-05
(l) 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 FALCON 900EX airplanes, serial
numbers 1 through 96 inclusive, and serial numbers 98 through 119
inclusive.
Exact source excerpt. Text positions 14525–14868, end exclusive, in the original decoded publication. SHA-256: 036a80d5116225fb48fd0e1d2b2e7fbe75217df3fea69090908ce5267c1e6bbb
Other FAA AD Provisions
(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) of this AD. Information may be emailed to: [email protected].
(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.
Exact source excerpt. Text positions 14868–15962, end exclusive, in the original decoded publication. SHA-256: e742232ed9acf0f795ca5787a25629c53e1500557f98c85f4804e6ac42a2336a
Related Information
(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; telephone
and fax 206-231-3226; email [email protected].
Exact source excerpt. Text positions 15962–16237, end exclusive, in the original decoded publication. SHA-256: 6d34b7c0748da8979bc0088eaa60f508ddee1cd70d277c77448eebc1491a2b1b
Material Incorporated by Reference
(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
December 7, 2020.
(i) European Union Aviation Safety Agency (EASA) AD 2020-0116,
dated May 20, 2020.
(ii) [Reserved]
(4) The following service information was approved for IBR on
January 24, 2020 (84 FR 69997, December 20, 2019).
(i) Chapter 5-40, Airworthiness Limitations, Revision 16, dated
September 2018, of the Dassault FALCON 900EX Maintenance Manual.
(ii) [Reserved]
(5) For EASA AD 2020-0116, contact the EASA, Konrad-Adenauer-
Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email
[email protected]; internet www.easa.europa.eu. You may find this
EASA AD on the EASA website at https://ad.easa.europa.eu.
(6) For Dassault service information identified in this 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.
(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-2020-0678.
(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
[email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 16237–18233, end exclusive, in the original decoded publication. SHA-256: 0049dc3c0ca7dc79cc0b3995efa21c23d302408038a8e5188abcd8912801ad78
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2020-21-19 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 3de67b227bcd6c0818058f6c7bde4d395b68ccad35152ef3fa0d0e195fda0d04. Source manifest: 691b718371f0008dd44b54665330065bad99710767c24336cf7ffe76b1d563d1.
Official source · 2020-11-02
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 85, Number 212 (Monday, November 2, 2020)]
[Rules and Regulations]
[Pages 69142-69144]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-24098]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0678; Product Identifier 2020-NM-098-AD; Amendment
39-21292; AD 2020-21-19]
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) 2019-24-
11, which applied to certain Dassault Aviation Model FALCON 900EX
airplanes. AD 2019-24-11 required revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. This AD continues to require
those maintenance or inspection program revisions, 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 December 7, 2020.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of December 7,
2020.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of
January 24, 2020 (84 FR 69997, December 20, 2019).
ADDRESSES: For the EASA material incorporated by reference (IBR) in
this AD, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne,
Germany; telephone +49 221 8999 000; email [email protected]; internet
www.easa.europa.eu. You may find this IBR material on the EASA website
at https://ad.easa.europa.eu.
For the Dassault service information identified in this 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-2020-0678.
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-
0678; 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; telephone and fax: 206-231-3226;
email: [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
The EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2020-0116, dated May 20, 2020
(``EASA AD 2020-0116'') (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.
EASA AD 2020-0116 superseded EASA AD 2019-0133 (which corresponds to
FAA AD 2019-24-11, Amendment 39-19814 (84 FR 69997, December 20, 2019)
(``AD 2019-24-11'')).
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2019-24-11. AD 2019-24-11 applied to
certain Dassault Aviation Model FALCON 900EX airplanes. The NPRM
published in the Federal Register on August 3, 2020 (85 FR 46563). The
NPRM was prompted by a determination that new or more restrictive
airworthiness limitations are necessary. The NPRM proposed to continue
to require the maintenance or inspection program revisions required by
AD 2019-24-11, and 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 an 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 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 has determined that these
minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM.
Related IBR Material Under 1 CFR Part 51
EASA AD 2020-0116 describes new or more restrictive maintenance
tasks and airworthiness limitations.
This AD also requires Chapter 5-40, Airworthiness Limitations,
Revision 16, dated September 2018, of the Dassault FALCON 900EX
Maintenance Manual, which the Director of the Federal Register approved
for incorporation by reference as of January 24, 2020 (84 FR 69997,
December 20, 2019).
[[Page 69143]]
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 72 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 2019-24-11 to be $7,650 (90 work-hours x $85 per work-
hour).
The FAA has determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although the
FAA 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.
Therefore, 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
0
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]
0
2. The FAA amends Sec. 39.13 by:
0
a. Removing Airworthiness Directive (AD) 2019-24-11, Amendment 39-19814
(84 FR 69997, December 20, 2019), and
0
b. Adding the following new AD:
2020-21-19 Dassault Aviation: Amendment 39-21292; Docket No. FAA-
2020-0678; Product Identifier 2020-NM-098-AD.
(a) Effective Date
This AD is effective December 7, 2020.
(b) Affected ADs
(1) This AD replaces AD 2019-24-11, Amendment 39-19814 (84 FR
69997, December 20, 2019) (``AD 2019-24-11'').
(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, certificated in any category, as identified in European
Union Aviation Safety Agency (EASA) AD 2020-0116, dated May 20, 2020
(``EASA AD 2020-0116'').
(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 already done.
(g) Retained Maintenance or Inspection Program Revision, with No
Changes
This paragraph restates the requirements of paragraph (i) of AD
2019-24-11, with no changes. Within 90 days after January 24, 2020
(the effective date AD 2019-24-11), revise the existing maintenance
or inspection program, as applicable, to incorporate the information
specified in Chapter 5-40, Airworthiness Limitations, Revision 16,
dated September 2018, of the Dassault FALCON 900EX Maintenance
Manual. The initial compliance times for accomplishing the actions
are at the times specified in Chapter 5-40, Airworthiness
Limitations, Revision 16, dated September 2018, or 90 days after
January 24, 2020, whichever occurs later, except as provided by
paragraphs (g)(1) through (4) of this AD. Accomplishing the
maintenance or inspection program revision required by paragraph (i)
of this AD terminates the requirements of this paragraph.
(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.
(h) Retained Restrictions on Alternative Actions and Intervals, with a
New Exception
This paragraph restates the requirements of paragraph (j) of AD
2019-24-11, with a new exception. Except as required by paragraph
(i) of this AD, after the 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
required actions and compliance times specified in, and in
accordance with, EASA AD 2020-0116. 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 2020-0116
(1) The requirements specified in paragraphs (1) and (2) of EASA
AD 2020-0116 do not apply to this AD.
(2) Paragraph (3) of EASA AD 2020-0116 specifies revising ``the
approved AMP''
[[Page 69144]]
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
2020-0116 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 2020-0116 is at the applicable ``associated
thresholds'' specified in paragraph (3) of EASA AD 2020-0116, 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 2020-0116 do not apply to this AD.
(5) The ``Remarks'' section of EASA AD 2020-0116 does not apply
to this AD.
(k) New Provisions for Alternative Actions and Intervals
After the maintenance or inspection program has been revised as
required 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 2020-0116.
(l) 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 FALCON 900EX airplanes, serial
numbers 1 through 96 inclusive, and serial numbers 98 through 119
inclusive.
(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) of this AD. Information may be emailed to: [email protected].
(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; telephone
and fax 206-231-3226; email [email protected].
(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
December 7, 2020.
(i) European Union Aviation Safety Agency (EASA) AD 2020-0116,
dated May 20, 2020.
(ii) [Reserved]
(4) The following service information was approved for IBR on
January 24, 2020 (84 FR 69997, December 20, 2019).
(i) Chapter 5-40, Airworthiness Limitations, Revision 16, dated
September 2018, of the Dassault FALCON 900EX Maintenance Manual.
(ii) [Reserved]
(5) For EASA AD 2020-0116, contact the EASA, Konrad-Adenauer-
Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email
[email protected]; internet www.easa.europa.eu. You may find this
EASA AD on the EASA website at https://ad.easa.europa.eu.
(6) For Dassault service information identified in this 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.
(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-2020-0678.
(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
[email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on October 8, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020-24098 Filed 10-30-20; 8:45 am]
BILLING CODE 4910-13-P
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