Airworthiness Directives; Dassault Aviation Airplanes, 82901-82903 [2020-28012]
Download as PDF
Federal Register / Vol. 85, No. 245 / Monday, December 21, 2020 / Rules and Regulations
information on the availability of this
material at the FAA, call (781) 238–7759.
(5) 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 on December 4, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020–27985 Filed 12–18–20; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2020–0778; Product
Identifier 2020–NM–097–AD; Amendment
39–21362; AD 2020–26–07]
RIN 2120–AA64
Airworthiness Directives; Dassault
Aviation Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
Examining the AD Docket
The FAA is superseding
Airworthiness Directive (AD) 2019–23–
05, which applied to all Dassault
Aviation Model MYSTERE–FALCON
900 airplanes. AD 2019–23–05 required
revising the existing maintenance or
inspection program, as applicable, to
incorporate new or more restrictive
airworthiness limitations. This AD
continues to require revising the
existing maintenance or inspection
program, as applicable, to incorporate
those new or more restrictive
airworthiness limitations, and also
requires revising the existing
maintenance or inspection program, as
applicable, to incorporate additional
new or more restrictive airworthiness
limitations; as specified in a European
Union Aviation Safety Agency (EASA)
AD, which is incorporated by reference.
This AD was prompted by a
determination that new or more
restrictive airworthiness limitations are
necessary. The FAA is issuing this AD
to address the unsafe condition on these
products.
DATES: This AD is effective January 25,
2021.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of January 25, 2021.
SUMMARY:
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19:44 Dec 18, 2020
Jkt 253001
The Director of the Federal Register
approved the incorporation by reference
of a certain other publication listed in
this AD as of January 13, 2020 (84 FR
67169, December 9, 2019).
ADDRESSES: For EASA material
incorporated by reference (IBR) in this
AD, contact the EASA, KonradAdenauer-Ufer 3, 50668 Cologne,
Germany; phone: +49 221 8999 000;
email: ADs@easa.europa.eu; internet:
www.easa.europa.eu. You may find this
IBR material on the EASA website at
https://ad.easa.europa.eu. For Dassault
service information identified in this
final rule, contact Dassault Falcon Jet
Corporation, Teterboro Airport, P.O.
Box 2000, South Hackensack, NJ 07606;
phone: 201–440–6700; internet: https://
www.dassaultfalcon.com. You may
view this IBR material at the FAA,
Airworthiness Products Section,
Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
It is also available in the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2020–
0778.
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2020–
0778; or in person at Docket Operations
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this final rule,
any comments received, and other
information. The address for Docket
Operations is U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Tom
Rodriguez, Aerospace Engineer, Large
Aircraft Section, International
Validation Branch, FAA, 2200 South
216th St., Des Moines, WA 98198;
phone and fax: 206–231–3226; email:
tom.rodriguez@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
The EASA, which is the Technical
Agent for the Member States of the
European Union, has issued EASA AD
2020–0115, dated May 20, 2020 (EASA
AD 2020–0115) (also referred to as the
Mandatory Continuing Airworthiness
Information, or the MCAI), to correct an
unsafe condition for all Dassault
Aviation Model MYSTERE–FALCON
900 airplanes.
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82901
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to supersede AD 2019–23–05,
Amendment 39–19799 (84 FR 67169,
December 9, 2019) (AD 2019–23–05).
AD 2019–23–05 applied to all Dassault
Aviation Model MYSTERE–FALCON
900 airplanes. The NPRM published in
the Federal Register on August 19, 2020
(85 FR 50970). The NPRM was
prompted by a determination that new
or more restrictive airworthiness
limitations are necessary. The NPRM
proposed to continue to require revising
the existing maintenance or inspection
program, as applicable, to incorporate
new or more restrictive airworthiness
limitations. The NPRM also proposed to
require revising the existing
maintenance or inspection program, as
applicable, to incorporate additional
new or more restrictive airworthiness
limitations, as specified in a EASA AD.
The FAA is issuing this AD to address
reduced structural integrity of the
airplane. See the MCAI for additional
background information.
Comments
The FAA gave the public the
opportunity to participate in developing
this final rule. The FAA has considered
the comments received.
Support for the NPRM
Ian Reineck indicated support for the
NPRM.
Request To Include Actions in the Cost
Estimate
Ian Reineck requested that the cost
estimate be revised to include structural
upkeep per flight hours, rather than
solely maintenance work hours. The
commenter stated this is what
determines the core functions inside
aviation maintenance schedules. The
commenter also stated this would be
inclusive, regardless of operator, but
still reflect the cost of an average
operator’s inspection through the
quantity of accumulated flight time on
the airplane. The commenter concluded
that, if flight time is not presented in the
inspection cost, it presents another
problem: These aircraft may change
ownership or operator-ship as they age.
The FAA infers that the commenter is
requesting that the FAA include the
costs in this AD for complying with the
actions (e.g., inspections) that are
specified in the airworthiness
limitations document referenced in
EASA AD 2020–0115. The FAA
disagrees because those actions are not
directly required by this AD.
Additionally, the FAA does not
distribute the costs over time because
the cost estimates have been
E:\FR\FM\21DER1.SGM
21DER1
82902
Federal Register / Vol. 85, No. 245 / Monday, December 21, 2020 / Rules and Regulations
standardized to include the larger whole
cost of the requirement, not the more
uniform cost per flight hour, which the
FAA has determined is best to inform
the broadest user base. The cost
information provided in this AD
describes only the direct costs of the
specific actions required by this AD.
This AD requires only revising the
existing maintenance or inspection
program, as applicable, to incorporate
the ‘‘limitations, tasks and associated
thresholds and intervals’’ specified in
paragraph (3) of EASA AD 2020–0115,
and provides a compliance time to
phase in the initial actions. Section
91.403(c) of the Federal Aviation
Regulations (14 CFR 91.403(c)) requires
the actions once the maintenance or
inspection program is changed.
Therefore, we have not changed this
final rule in this regard.
Conclusion
The FAA reviewed the relevant data,
considered the comments received, and
determined that air safety and the
public interest require adopting this
final rule as proposed, except for minor
editorial changes. The FAA has
determined that these minor changes:
• Are consistent with the intent that
was proposed in the NPRM for
addressing the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM.
Related Service Information Under 1
CFR Part 51
EASA AD 2020–0115 describes new
or more restrictive airworthiness
limitations for airplane structures and
safe life limits.
This AD also requires Chapter 5–40,
Airworthiness Limitations, Revision 24,
dated September 2018, of the Dassault
Aviation Falcon 900 Maintenance
Manual, which the Director of the
Federal Register approved for
incorporation by reference as of January
13, 2020 (84 FR 67169, December 9,
2019).
This material is reasonably available
because the interested parties have
access to it through their normal course
of business or by the means identified
in the ADDRESSES section.
Costs of Compliance
The FAA estimates that this AD
affects 105 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this AD.
The FAA estimates the total cost per
operator for the retained actions from
AD 2019–23–05 to be $7,650 (90 workhours × $85 per work-hour).
VerDate Sep<11>2014
19:44 Dec 18, 2020
Jkt 253001
The FAA has determined that revising
the existing maintenance or inspection
program takes an average of 90 workhours per operator, although the agency
recognizes that this number may vary
from operator to operator. In the past,
the agency has estimated that this action
takes 1 work-hour per airplane. Since
operators incorporate maintenance or
inspection program changes for their
affected fleet(s), the FAA has
determined that a per-operator estimate
is more accurate than a per-airplane
estimate.
The FAA estimates the total cost per
operator for the new actions to be
$7,650 (90 work-hours × $85 per workhour).
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.
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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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by:
a. Removing Airworthiness Directive
(AD) 2019–23–05, Amendment 39–
19799 (84 FR 67169, December 9, 2019),
and
■ b. Adding the following new AD:
■
■
2020–26–07 Dassault Aviation:
Amendment 39–21362; Docket No.
FAA–2020–0778; Product Identifier
2020–NM–097–AD.
(a) Effective Date
This airworthiness directive (AD) is
effective January 25, 2021.
(b) Affected ADs
(1) This AD replaces AD 2019–23–05,
Amendment 39–19799 (84 FR 67169,
December 9, 2019) (AD 2019–23–05).
(2) This AD affects AD 2010–26–05,
Amendment 39–16544 (75 FR 79952,
December 21, 2010) (AD 2010–26–05).
(c) Applicability
This AD applies to all Dassault Aviation
Model MYSTERE–FALCON 900 airplanes,
certificated in any category.
(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 Revision of Existing
Maintenance or Inspection Program, With
No Changes
This paragraph restates the requirements of
paragraph (i) of AD 2019–23–05, with no
changes. Within 90 days after January 13,
2020 (the effective date of AD 2019–23–05),
revise the existing maintenance or inspection
program, as applicable, to incorporate the
information specified in Chapter 5–40,
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Federal Register / Vol. 85, No. 245 / Monday, December 21, 2020 / Rules and Regulations
Airworthiness Limitations, Revision 24,
dated September 2018, of the Dassault
Aviation Falcon 900 Maintenance Manual.
The initial compliance times for doing the
tasks are at the times specified in Chapter 5–
40, Airworthiness Limitations, Revision 24,
dated September 2018, of the Dassault
Aviation Falcon 900 Maintenance Manual, or
within 90 days after January 13, 2020,
whichever occurs later. The term ‘‘LDG’’ in
the ‘‘First Inspection’’ column of any table in
the service information specified in this
paragraph means total airplane landings. The
term ‘‘FH’’ in the ‘‘First Inspection’’ column
of any table in the service information
specified in this paragraph means total flight
hours. The term ‘‘FC’’ in the ‘‘First
Inspection’’ column of any table in the
service information specified in this
paragraph means total flight cycles. The term
‘‘M’’ in the ‘‘First Inspection’’ column of any
table in the service information specified in
this paragraph means months since the date
of issuance of the original airworthiness
certificate or the date of issuance of the
original export certificate of airworthiness.
Accomplishing the maintenance or
inspection program revision required by
paragraph (i) of this AD terminates the
requirements of this paragraph.
(h) Retained Restrictions on Alternative
Actions or Intervals, With a New Exception
This paragraph restates the requirements of
paragraph (h) of AD 2019–23–05, with a new
exception. Except as required by paragraph
(i) of this AD, after the existing maintenance
or inspection program has been revised as
required by paragraph (g) of this AD, no
alternative actions (e.g., inspections) or
intervals may be used unless the actions or
intervals are approved as an alternative
method of compliance (AMOC) in
accordance with the procedures specified in
paragraph (m)(1) of this AD.
(i) New Maintenance or Inspection Program
Revision
Except as specified in paragraph (j) of this
AD: Comply with all required actions and
compliance times specified in, and in
accordance with, European Union Aviation
Safety Agency (EASA) AD 2020–0115, dated
May 20, 2020 (EASA AD 2020–0115).
Accomplishing the maintenance or
inspection program revision required by this
paragraph terminates the requirements of
paragraph (g) of this AD.
(j) Exceptions to EASA AD 2020–0115
(1) The requirements specified in
paragraphs (1) and (2) of EASA AD 2020–
0115 do not apply to this AD.
(2) Paragraph (3) of EASA AD 2020–0115
specifies revising ‘‘the approved AMP’’
within 12 months after its effective date, but
this AD requires revising the existing
maintenance or inspection program, as
applicable, to incorporate the ‘‘limitations,
tasks and associated thresholds and
intervals’’ specified in paragraph (3) of EASA
AD 2020–0115 within 90 days after the
effective date of this AD.
(3) The initial compliance time for doing
the tasks specified in paragraph (3) of EASA
AD 2020–0115 is at the applicable
‘‘associated thresholds’’ specified in
VerDate Sep<11>2014
19:44 Dec 18, 2020
Jkt 253001
paragraph (3) of EASA AD 2020–0115, or
within 90 days after the effective date of this
AD, whichever occurs later.
(4) The provisions specified in paragraphs
(4) and (5) of EASA AD 2020–0115 do not
apply to this AD.
(5) The ‘‘Remarks’’ section of EASA AD
2020–0115 does not apply to this AD.
(k) New Provisions for Alternative Actions
or Intervals
After the maintenance or inspection
program has been revised as required by
paragraph (i) of this AD, no alternative
actions (e.g., inspections) or intervals are
allowed unless they are approved as
specified in the provisions of the ‘‘Ref.
Publications’’ section of EASA AD 2020–
0115.
(l) Terminating Actions for Certain
Requirements in AD 2010–26–05
Accomplishing the actions required by
paragraph (g) or (i) of this AD terminates the
requirements of paragraph (g)(1) of AD 2010–
26–05, for Dassault Aviation Model
MYSTERE–FALCON 900 airplanes.
(m) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, Large Aircraft
Section, International Validation Branch,
FAA, has the authority to approve AMOCs
for this AD, if requested using the procedures
found in 14 CFR 39.19. In accordance with
14 CFR 39.19, send your request to your
principal inspector or responsible Flight
Standards Office, as appropriate. If sending
information directly to the Large Aircraft
Section, International Validation Branch,
send it to the attention of the person
identified in paragraph (n) of this AD.
Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov.
(i) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(ii) AMOCs approved previously for AD
2019–23–05 are approved as AMOCs for the
corresponding provisions of EASA AD 2020–
0115 that are required by paragraph (i) of this
AD.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, Large Aircraft Section,
International Validation Branch, FAA; or
EASA; or Dassault Aviation’s EASA Design
Organization Approval (DOA). If approved by
the DOA, the approval must include the
DOA-authorized signature.
(o) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(3) The following service information was
approved for IBR on January 25, 2021.
(i) European Union Aviation Safety Agency
(EASA) AD 2020–0115, dated May 20, 2020.
(ii) [Reserved]
(4) The following service information was
approved for IBR on January 13, 2020 (84 FR
67169, December 9, 2019).
(i) Chapter 5–40, Airworthiness
Limitations, Revision 24, dated September
2018, of the Dassault Aviation Falcon 900
Maintenance Manual.
(ii) [Reserved]
(5) For EASA AD 2020–0115, contact the
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; Internet
www.easa.europa.eu. You may find this
EASA AD on the EASA website at https://
ad.easa.europa.eu.
(6) For Dassault service information,
contact Dassault Falcon Jet Corporation,
Teterboro Airport, P.O. Box 2000, South
Hackensack, NJ 07606; phone: 201–440–
6700; internet: https://
www.dassaultfalcon.com.
(7) You may view this material at the FAA,
Airworthiness Products Section, Operational
Safety Branch, 2200 South 216th St., Des
Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195. This material may be found
in the AD docket on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2020–0778.
(7) You may view this material that is
incorporated by reference at the National
Archives and Records Administration
(NARA). For information on the availability
of this material at NARA, email fedreg.legal@
nara.gov, or go to: https://www.archives.gov/
federal-register/cfr/ibr-locations.html.
Issued on December 8, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives,
Compliance & Airworthiness Division,
Aircraft Certification Service.
[FR Doc. 2020–28012 Filed 12–18–20; 8:45 am]
BILLING CODE 4910–13–P
(n) Related Information
For more information about this AD,
contact Tom Rodriguez, Aerospace Engineer,
Large Aircraft Section, International
Validation Branch, FAA, 2200 South 216th
St., Des Moines, WA 98198; phone and fax:
206–231–3226; email: tom.rodriguez@
faa.gov.
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Agencies
[Federal Register Volume 85, Number 245 (Monday, December 21, 2020)]
[Rules and Regulations]
[Pages 82901-82903]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-28012]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0778; Product Identifier 2020-NM-097-AD; Amendment
39-21362; AD 2020-26-07]
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2019-23-
05, which applied to all Dassault Aviation Model MYSTERE-FALCON 900
airplanes. AD 2019-23-05 required revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. This AD continues to require
revising the existing maintenance or inspection program, as applicable,
to incorporate those new or more restrictive airworthiness limitations,
and also requires revising the existing maintenance or inspection
program, as applicable, to incorporate additional new or more
restrictive airworthiness limitations; as specified in a European Union
Aviation Safety Agency (EASA) AD, which is incorporated by reference.
This AD was prompted by a determination that new or more restrictive
airworthiness limitations are necessary. The FAA is issuing this AD to
address the unsafe condition on these products.
DATES: This AD is effective January 25, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 25,
2021.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of
January 13, 2020 (84 FR 67169, December 9, 2019).
ADDRESSES: For EASA material incorporated by reference (IBR) in this
AD, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
phone: +49 221 8999 000; email: [email protected]; internet:
www.easa.europa.eu. You may find this IBR material on the EASA website
at https://ad.easa.europa.eu. For Dassault service information
identified in this final rule, contact Dassault Falcon Jet Corporation,
Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; phone:
201-440-6700; internet: https://www.dassaultfalcon.com. You may view
this IBR material at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call 206-
231-3195. It is also available in the AD docket on the internet at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2020-0778.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-
0778; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
Large Aircraft Section, International Validation Branch, FAA, 2200
South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3226;
email: [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
The EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2020-0115, dated May 20, 2020 (EASA
AD 2020-0115) (also referred to as the Mandatory Continuing
Airworthiness Information, or the MCAI), to correct an unsafe condition
for all Dassault Aviation Model MYSTERE-FALCON 900 airplanes.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2019-23-05, Amendment 39-19799 (84 FR
67169, December 9, 2019) (AD 2019-23-05). AD 2019-23-05 applied to all
Dassault Aviation Model MYSTERE-FALCON 900 airplanes. The NPRM
published in the Federal Register on August 19, 2020 (85 FR 50970). The
NPRM was prompted by a determination that new or more restrictive
airworthiness limitations are necessary. The NPRM proposed to continue
to require revising the existing maintenance or inspection program, as
applicable, to incorporate new or more restrictive airworthiness
limitations. The NPRM also proposed to require revising the existing
maintenance or inspection program, as applicable, to incorporate
additional new or more restrictive airworthiness limitations, as
specified in a EASA AD.
The FAA is issuing this AD to address reduced structural integrity
of the airplane. See the MCAI for additional background information.
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The FAA has considered the comments
received.
Support for the NPRM
Ian Reineck indicated support for the NPRM.
Request To Include Actions in the Cost Estimate
Ian Reineck requested that the cost estimate be revised to include
structural upkeep per flight hours, rather than solely maintenance work
hours. The commenter stated this is what determines the core functions
inside aviation maintenance schedules. The commenter also stated this
would be inclusive, regardless of operator, but still reflect the cost
of an average operator's inspection through the quantity of accumulated
flight time on the airplane. The commenter concluded that, if flight
time is not presented in the inspection cost, it presents another
problem: These aircraft may change ownership or operator-ship as they
age.
The FAA infers that the commenter is requesting that the FAA
include the costs in this AD for complying with the actions (e.g.,
inspections) that are specified in the airworthiness limitations
document referenced in EASA AD 2020-0115. The FAA disagrees because
those actions are not directly required by this AD. Additionally, the
FAA does not distribute the costs over time because the cost estimates
have been
[[Page 82902]]
standardized to include the larger whole cost of the requirement, not
the more uniform cost per flight hour, which the FAA has determined is
best to inform the broadest user base. The cost information provided in
this AD describes only the direct costs of the specific actions
required by this AD. This AD requires only revising the existing
maintenance or inspection program, as applicable, to incorporate the
``limitations, tasks and associated thresholds and intervals''
specified in paragraph (3) of EASA AD 2020-0115, and provides a
compliance time to phase in the initial actions. Section 91.403(c) of
the Federal Aviation Regulations (14 CFR 91.403(c)) requires the
actions once the maintenance or inspection program is changed.
Therefore, we have not changed this final rule in this regard.
Conclusion
The FAA reviewed the relevant data, considered the comments
received, and determined that air safety and the public interest
require adopting this final rule as proposed, except for minor
editorial changes. The FAA has determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.
Related Service Information Under 1 CFR Part 51
EASA AD 2020-0115 describes new or more restrictive airworthiness
limitations for airplane structures and safe life limits.
This AD also requires Chapter 5-40, Airworthiness Limitations,
Revision 24, dated September 2018, of the Dassault Aviation Falcon 900
Maintenance Manual, which the Director of the Federal Register approved
for incorporation by reference as of January 13, 2020 (84 FR 67169,
December 9, 2019).
This material is reasonably available because the interested
parties have access to it through their normal course of business or by
the means identified in the ADDRESSES section.
Costs of Compliance
The FAA estimates that this AD affects 105 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD.
The FAA estimates the total cost per operator for the retained
actions from AD 2019-23-05 to be $7,650 (90 work-hours x $85 per work-
hour).
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the agency recognizes that this number may vary from operator
to operator. In the past, the agency has estimated that this action
takes 1 work-hour per airplane. Since operators incorporate maintenance
or inspection program changes for their affected fleet(s), the FAA has
determined that a per-operator estimate is more accurate than a per-
airplane estimate.
The FAA estimates the total cost per operator for the new actions
to be $7,650 (90 work-hours x $85 per work-hour).
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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) 2019-23-05, Amendment 39-19799
(84 FR 67169, December 9, 2019), and
0
b. Adding the following new AD:
2020-26-07 Dassault Aviation: Amendment 39-21362; Docket No. FAA-
2020-0778; Product Identifier 2020-NM-097-AD.
(a) Effective Date
This airworthiness directive (AD) is effective January 25, 2021.
(b) Affected ADs
(1) This AD replaces AD 2019-23-05, Amendment 39-19799 (84 FR
67169, December 9, 2019) (AD 2019-23-05).
(2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR
79952, December 21, 2010) (AD 2010-26-05).
(c) Applicability
This AD applies to all Dassault Aviation Model MYSTERE-FALCON
900 airplanes, certificated in any category.
(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 Revision of Existing Maintenance or Inspection Program,
With No Changes
This paragraph restates the requirements of paragraph (i) of AD
2019-23-05, with no changes. Within 90 days after January 13, 2020
(the effective date of AD 2019-23-05), revise the existing
maintenance or inspection program, as applicable, to incorporate the
information specified in Chapter 5-40,
[[Page 82903]]
Airworthiness Limitations, Revision 24, dated September 2018, of the
Dassault Aviation Falcon 900 Maintenance Manual. The initial
compliance times for doing the tasks are at the times specified in
Chapter 5-40, Airworthiness Limitations, Revision 24, dated
September 2018, of the Dassault Aviation Falcon 900 Maintenance
Manual, or within 90 days after January 13, 2020, whichever occurs
later. The term ``LDG'' in the ``First Inspection'' column of any
table in the service information specified in this paragraph means
total airplane landings. The term ``FH'' in the ``First Inspection''
column of any table in the service information specified in this
paragraph means total flight hours. The term ``FC'' in the ``First
Inspection'' column of any table in the service information
specified in this paragraph means total flight cycles. The term
``M'' in the ``First Inspection'' column of any table in the service
information specified in this paragraph means months since the date
of issuance of the original airworthiness certificate or the date of
issuance of the original export certificate of airworthiness.
Accomplishing the maintenance or inspection program revision
required by paragraph (i) of this AD terminates the requirements of
this paragraph.
(h) Retained Restrictions on Alternative Actions or Intervals, With a
New Exception
This paragraph restates the requirements of paragraph (h) of AD
2019-23-05, with a new exception. Except as required by paragraph
(i) of this AD, after the existing maintenance or inspection program
has been revised as required by paragraph (g) of this AD, no
alternative actions (e.g., inspections) or intervals may be used
unless the actions or intervals are approved as an alternative
method of compliance (AMOC) in accordance with the procedures
specified in paragraph (m)(1) of this AD.
(i) New Maintenance or Inspection Program Revision
Except as specified in paragraph (j) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, European Union Aviation Safety Agency (EASA) AD
2020-0115, dated May 20, 2020 (EASA AD 2020-0115). Accomplishing the
maintenance or inspection program revision required by this
paragraph terminates the requirements of paragraph (g) of this AD.
(j) Exceptions to EASA AD 2020-0115
(1) The requirements specified in paragraphs (1) and (2) of EASA
AD 2020-0115 do not apply to this AD.
(2) Paragraph (3) of EASA AD 2020-0115 specifies revising ``the
approved AMP'' within 12 months after its effective date, but this
AD requires revising the existing maintenance or inspection program,
as applicable, to incorporate the ``limitations, tasks and
associated thresholds and intervals'' specified in paragraph (3) of
EASA AD 2020-0115 within 90 days after the effective date of this
AD.
(3) The initial compliance time for doing the tasks specified in
paragraph (3) of EASA AD 2020-0115 is at the applicable ``associated
thresholds'' specified in paragraph (3) of EASA AD 2020-0115, or
within 90 days after the effective date of this AD, whichever occurs
later.
(4) The provisions specified in paragraphs (4) and (5) of EASA
AD 2020-0115 do not apply to this AD.
(5) The ``Remarks'' section of EASA AD 2020-0115 does not apply
to this AD.
(k) New Provisions for Alternative Actions or Intervals
After the maintenance or inspection program has been revised as
required by paragraph (i) of this AD, no alternative actions (e.g.,
inspections) or intervals are allowed unless they are approved as
specified in the provisions of the ``Ref. Publications'' section of
EASA AD 2020-0115.
(l) Terminating Actions for Certain Requirements in AD 2010-26-05
Accomplishing the actions required by paragraph (g) or (i) of
this AD terminates the requirements of paragraph (g)(1) of AD 2010-
26-05, for Dassault Aviation Model MYSTERE-FALCON 900 airplanes.
(m) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Large Aircraft Section, International Validation Branch, FAA, has
the authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or responsible Flight
Standards Office, as appropriate. If sending information directly to
the Large Aircraft Section, International Validation Branch, send it
to the attention of the person identified in paragraph (n) of this
AD. Information may be emailed to: [email protected].
(i) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(ii) AMOCs approved previously for AD 2019-23-05 are approved as
AMOCs for the corresponding provisions of EASA AD 2020-0115 that are
required by paragraph (i) of this AD.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, Large Aircraft
Section, International Validation Branch, FAA; or EASA; or Dassault
Aviation's EASA Design Organization Approval (DOA). If approved by
the DOA, the approval must include the DOA-authorized signature.
(n) Related Information
For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, Large Aircraft Section, International Validation
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone and
fax: 206-231-3226; email: [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
January 25, 2021.
(i) European Union Aviation Safety Agency (EASA) AD 2020-0115,
dated May 20, 2020.
(ii) [Reserved]
(4) The following service information was approved for IBR on
January 13, 2020 (84 FR 67169, December 9, 2019).
(i) Chapter 5-40, Airworthiness Limitations, Revision 24, dated
September 2018, of the Dassault Aviation Falcon 900 Maintenance
Manual.
(ii) [Reserved]
(5) For EASA AD 2020-0115, contact the EASA, Konrad-Adenauer-
Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email
[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, contact Dassault Falcon
Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack,
NJ 07606; phone: 201-440-6700; internet: https://www.dassaultfalcon.com.
(7) You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th St.,
Des Moines, WA. For information on the availability of this material
at the FAA, call 206-231-3195. This material may be found in the AD
docket on the internet at https://www.regulations.gov by searching
for and locating Docket No. FAA-2020-0778.
(7) 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 December 8, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020-28012 Filed 12-18-20; 8:45 am]
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