Published 2019-12-09 · Federal Register document 2019-26402
Airworthiness Directives; Dassault Aviation Airplanes
Publication 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.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:01.312311+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2019-66422190cf4fa9dc
- Source row
- results[270]
- Raw source SHA-256
- 66422190cf4fa9dc96bac02b1afe14648e349a1393bef6cf5fbf55644fa2ce43
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2019-23-03
- Effective date printed in this edition
- 2020-01-13
Read 14 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective January 13, 2020.
Exact source excerpt. Text positions 10551–10615, end exclusive, in the original decoded publication. SHA-256: b47c53930e524277f914ce8d09ee30144c6d9e50a3d013865fe1f9e81c038b2a
Affected ADs
(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'').
Exact source excerpt. Text positions 10615–10954, end exclusive, in the original decoded publication. SHA-256: 769b3b9af5a38f90e53fb45e70d676c9c48e9b76adef3bf70f5a76adfe6626fa
Applicability wording · Applicability
(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.
Exact source excerpt. Text positions 10954–11257, end exclusive, in the original decoded publication. SHA-256: 3f864abbb2f1a4fba9ba0da5ba5367039d764255aa1179517a8ff4de10a9c17d
Subject
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.
Exact source excerpt. Text positions 11257–11360, 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, 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.
Exact source excerpt. Text positions 11360–11707, end exclusive, in the original decoded publication. SHA-256: 0c2ee840d134d8a12d74238fbf04aadbbf0735eca40723993e92fada0125994d
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11707–11809, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Retained Revision of Maintenance or Inspection Program, With No Changes
(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.
Exact source excerpt. Text positions 11809–13269, end exclusive, in the original decoded publication. SHA-256: 9f6b57ce6362b5d7f4860cf91d54b72b3ec1946d50508cdb00544441a9991571
Retained Requirement for No Alternative Actions and Intervals, With New Exception
(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.
Exact source excerpt. Text positions 13269–13824, end exclusive, in the original decoded publication. SHA-256: 5807329e7e383ec3ae825afbf8566e9734776011c6573778869898bf8ccf6d04
New Requirement of This AD: Maintenance or Inspection Program Revision
(i) New Requirement of This AD: Maintenance or Inspection Program
Revision
Within 90 days after the effective date of this AD, revise the
existing 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.
Exact source excerpt. Text positions 13824–15277, end exclusive, in the original decoded publication. SHA-256: c13f223941d9480a22d95e3c80d00491382ee2662bba2219564380def5ed170f
No Alternative Actions or Intervals
(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.
Exact source excerpt. Text positions 15277–15639, end exclusive, in the original decoded publication. SHA-256: a701faaf8e510e8c4449c73229836f99bccb0feee562e04a4ddeef7ce142fb3a
Terminating Actions for Certain Actions in AD 2010-26-05
(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.
Exact source excerpt. Text positions 15639–15922, end exclusive, in the original decoded publication. SHA-256: 705d610a3689d118b72a6666fa4def02806db39a5b3ba18c20303602845af0fd
Other FAA AD Provisions
(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 [email protected]. Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal
[[Page 67174]]
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.
Exact source excerpt. Text positions 15922–17229, end exclusive, in the original decoded publication. SHA-256: 2f77815eca68948c50c0e8ccde38b7eed0c4c6ff02236f4f2e65cb43bb8d6ea8
Related Information
(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.
Exact source excerpt. Text positions 17229–17760, end exclusive, in the original decoded publication. SHA-256: fd6f951bb43a1699a9d6ee03d972ff152c9ada486b80f49746bacec7de9ca279
Material Incorporated by Reference
(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, P.O. 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 [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 17760–19451, end exclusive, in the original decoded publication. SHA-256: 16ba449cb5ae6b84ce95346f55531e7c5d2acc6550914930f3401bb694fccb08
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 2019-23-03 · 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: 2966751c30c355c01edf7ffa78ac25fb84638b2cc4cff88830337fde4512e69f. Source manifest: a7a165949515e341bb7baa846b158f4f06bbb1da424ab5103ebac7606a12633e.
Official source · 2019-12-09
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 84, Number 236 (Monday, December 9, 2019)]
[Rules and Regulations]
[Pages 67171-67174]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-26402]
-----------------------------------------------------------------------
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).
[[Page 67172]]
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:
<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 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
[[Page 67173]]
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
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) 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
0
b. Adding the following new AD:
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
existing 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 [email protected]. Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal
[[Page 67174]]
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, P.O. 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 [email protected], 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.
[FR Doc. 2019-26402 Filed 12-6-19; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:05:05.362292+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 8fc5d426548fc73030812c4890e3a6d0c7920999a1f15d36ae2f2650d42329f5
- Text SHA-256
- 2966751c30c355c01edf7ffa78ac25fb84638b2cc4cff88830337fde4512e69f
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.