AD 2020-02-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault | Various | Airworthiness Directives; Dassault Aviation Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Dassault Aviation Airplanes |
Unsafe Condition
fatigue cracking and damage in principal structural elements; such fatigue cracking and damage could result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations; revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in Chapter 5-40-01, Airworthiness Limitations, DMD 44729, Revision 9, dated November 29, 2017, of the Dassault Aviation Falcon 20 Maintenance Manual.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 90 days after April 8, 2019
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes, certificated in any category, on which the supplemental structural inspection program (SSIP) has been incorporated into the airplane's maintenance program.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
The FAA is superseding Airworthiness Directive (AD) 2019-03- 14, which applied to certain Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes. AD 2019-03-14 required revising the existing maintenance or inspection program, as applicable, to incorporate new maintenance requirements and airworthiness limitations. This AD continues to require, and adds new requirements for, revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. 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.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to Dassault Aviation Model FAN JET FALCON, FAN
JET FALCON SERIES C, D, E, F, and G airplanes, certificated in any
category, on which the supplemental structural inspection program
(SSIP) has been incorporated into the airplane's maintenance
program.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 85, Number 25 (Thursday, February 6, 2020)]
[Rules and Regulations]
[Pages 6744-6746]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2020-02199]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0860; Product Identifier 2019-NM-123-AD; Amendment
39-19827; AD 2020-02-13]
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) 2019-03-
14, which applied to certain Dassault Aviation Model FAN JET FALCON,
FAN JET FALCON SERIES C, D, E, F, and G airplanes. AD 2019-03-14
required revising the existing maintenance or inspection program, as
applicable, to incorporate new maintenance requirements and
airworthiness limitations. This AD continues to require, and adds new
requirements for, revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive
airworthiness limitations. 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 March 12, 2020.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 12,
2020.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of April
8, 2019 (84 FR 7269, March 4, 2019).
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
<a href="https://www.dassaultfalcon.com">https://www.dassaultfalcon.com</a>. 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 <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating
Docket No. FAA-2019-0860.
Examining the AD Docket
You may examine the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2019-
0860; 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; email
<a href="/cdn-cgi/l/email-protection#3b4f54561549545f49525c4e5e417b5d5a5a155c544d"><span class="__cf_email__" data-cfemail="a4d0cbc98ad6cbc0d6cdc3d1c1dee4c2c5c58ac3cbd2">[email protected]</span></a>.
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 2019-0142, dated June 17, 2019 (``EASA AD 2019-0142'') (also
referred to as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct
[[Page 6745]]
an unsafe condition for certain Dassault Aviation Model FAN JET FALCON,
FAN JET FALCON SERIES C, D, E, F, and G airplanes. You may examine the
MCAI in the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by
searching for and locating Docket No. FAA-2019-0860.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2019-03-14, Amendment 39-19566 (84 FR 7269,
March 4, 2019) (``AD 2019-03-14''). AD 2019-03-14 applied to certain
Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E,
F, and G airplanes. The NPRM published in the Federal Register on
November 4, 2019 (84 FR 59315). The NPRM was prompted by a
determination that new or more restrictive airworthiness limitations
are necessary. The NPRM proposed continue to require, and adds new
requirements for, 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 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 Service Information Under 1 CFR Part 51
Dassault Aviation has issued Chapter 5-40-01, Airworthiness
Limitations, Revision 10, effective January 1, 2019, of the Dassault
Aviation Falcon 20 Maintenance Manual, specifically for aircraft that
have incorporated the supplemental structural inspection program
(SSIP). This service information describes airworthiness limitations
for safe life limits.
This AD also requires Chapter 5-40-01, Airworthiness Limitations,
DMD 44729, Revision 9, dated November 29, 2017, of the Dassault
Aviation Falcon 20 Maintenance Manual, which the Director of the
Federal Register approved for incorporation by reference as of April 8,
2019 (84 FR 7269, March 4, 2019).
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 61 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 2019-03-14 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. 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
We 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 removing Airworthiness Directive (AD)
2019-03-14, Amendment 39-19566 (84 FR 7269, March 4, 2019), and adding
the following new AD:
2020-02-13 Dassault Aviation: Amendment 39-19827; Docket No. FAA-
2019-0860; Product Identifier 2019-NM-123-AD.
(a) Effective Date
This AD is effective March 12, 2020.
(b) Affected ADs
(1) This AD replaces AD 2019-03-14, Amendment 39-19566 (84 FR
7269, March 4, 2019) (``AD 2019-03-14'').
(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 FAN JET FALCON, FAN
JET FALCON SERIES C, D, E, F, and G airplanes, certificated in any
category, on which the supplemental structural inspection program
(SSIP) has been incorporated into the airplane's maintenance
program.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time limits/
maintenance checks.
[[Page 6746]]
(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, With No Changes
This paragraph restates the requirements of paragraph (g) of AD
2019-03-14, with no changes. Within 90 days after April 8, 2019 (the
effective date of AD 2019-03-14), revise the existing maintenance or
inspection program, as applicable, to incorporate the information
specified in Chapter 5-40-01, Airworthiness Limitations, DMD 44729,
Revision 9, dated November 29, 2017, of the Dassault Aviation Falcon
20 Maintenance Manual. The initial compliance time for doing the
tasks is at the time specified in Chapter 5-40-01, Airworthiness
Limitations, DMD 44729, Revision 9, dated November 29, 2017, of the
Dassault Aviation Falcon 20 Maintenance Manual, or within 90 days
after April 8, 2019 (the effective date of AD 2019-03-14), whichever
occurs later. Where the threshold column in the table in paragraph
B, Mandatory Maintenance Operations, of Chapter 5-40-01,
Airworthiness Limitations, DMD 44729, Revision 9, dated November 29,
2017, of the Dassault Aviation Falcon 20 Maintenance Manual
specifies a compliance time in years, those compliance times start
from the date of issuance of the original airworthiness certificate
or date of issuance of the original export certificate of
airworthiness.
(h) Retained Requirement of No Alternative Actions or Intervals, With a
New Exception
This paragraph restates the requirements of paragraph (h) of AD
2019-03-14, 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 (e.g., inspections)
or intervals may be used unless the actions and 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 5-40-01,
Airworthiness Limitations, Revision 10, effective January 1, 2019,
of the Dassault Aviation Falcon 20 Maintenance Manual. The initial
compliance time for doing the tasks is at the time specified in
Chapter 5-40-01, Airworthiness Limitations, Revision 10, effective
January 1, 2019, of the Dassault Aviation Falcon 20 Maintenance
Manual, or within 90 days after the effective date of this AD,
whichever occurs later. Where the threshold column in the table in
paragraph B, Mandatory Maintenance Operations, of Chapter 5-40-01,
Airworthiness Limitations, Revision 10, dated January 1, 2019, of
the Dassault Aviation Falcon 20 Maintenance Manual specifies a
compliance time in years, those compliance times start from the date
of issuance of the original airworthiness certificate or the
original export certificate of airworthiness. Accomplishing the
actions required by this paragraph terminates the actions required
by paragraph (g) of this AD.
(j) New 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 or 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 FAN JET FALCON, FAN JET FALCON
SERIES C, D, E, F, and G airplanes.
(l) Other FAA AD Provisions
The following provisions also apply to this AD:
(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 <a href="/cdn-cgi/l/email-protection#360f1b77787b1b0707001b777b79751b64736763736562657650575718515940"><span class="__cf_email__" data-cfemail="c8f1e5898685e5f9f9fee58985878be59a8d999d8d9b9c9b88aea9a9e6afa7be">[email protected]</span></a>.
(i) 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.
(ii) AMOCs approved previously for AD 2019-03-14 are approved as
AMOCs for the corresponding provisions of this AD.
(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 2019-0142, dated June 17, 2019 (``EASA AD 2019-
0142''), for related information. This MCAI may be found in the AD
docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching
for and locating Docket No. FAA-2019-0860.
(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; email <a href="/cdn-cgi/l/email-protection#41352e2c6f332e2533282634243b012720206f262e37"><span class="__cf_email__" data-cfemail="f0849f9dde829f9482999785958ab0969191de979f86">[email protected]</span></a>.
(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
March 12, 2020.
(i) Chapter 5-40-01, Airworthiness Limitations, Revision 10,
effective January 1, 2019, of the Dassault Aviation Falcon 20
Maintenance Manual.
(ii) [Reserved]
(4) The following service information was approved for IBR on
April 8, 2019 (84 FR 7269, March 4, 2019).
(i) Chapter 5-40-01, Airworthiness Limitations, DMD 44729,
Revision 9, dated November 29, 2017, of the Dassault Aviation Falcon
20 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 <a href="https://www.dassaultfalcon.com">https://www.dassaultfalcon.com</a>.
(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 <a href="/cdn-cgi/l/email-protection#b8dedddccadddf96d4dddfd9d4f8d6d9cad996dfd7ce"><span class="__cf_email__" data-cfemail="f4929190869193da9891939598b49a958695da939b82">[email protected]</span></a>, or go to: <a href="https://www.archives.gov/federal-register/cfr/ibr-locations.html">https://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on January 23, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020-02199 Filed 2-5-20; 8:45 am]
BILLING CODE 4910-13-P
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.