Airworthiness Directives; Dassault Aviation Airplanes, 49789-49791 [2018-21343]
Download as PDF
Federal Register / Vol. 83, No. 192 / Wednesday, October 3, 2018 / Rules and Regulations
REQUESTS@faa.gov. Before using any
approved AMOC, notify your appropriate
principal inspector, or lacking a principal
inspector, the manager of the local flight
standards district office/certificate holding
district office.
(2) Contacting the Manufacturer: 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 EASA;
or BAE Systems (Operations) Limited’s EASA
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
2017–0187, dated September 22, 2017, 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–2018–0511.
(2) For more information about this AD,
contact Todd Thompson, Aerospace
Engineer, International Section, Transport
Standards Branch, FAA, 2200 South 216th
St., Des Moines, WA 98198; telephone and
fax 206–231–3228.
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(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.
(i) BAE Systems (Operations) Limited Alert
Service Bulletin J41–A53–058, dated
December 6, 2016.
(ii) BAE Systems (Operations) Limited
Service Bulletin J41–51–001, Revision 4,
dated July 11, 2017.
(3) For service information identified in
this AD, contact BAE Systems (Operations)
Limited, Customer Information Department,
Prestwick International Airport, Ayrshire,
KA9 2RW, Scotland, United Kingdom;
telephone +44 1292 675207; fax +44 1292
675704; email RApublications@
baesystems.com; internet https://
www.baesystems.com/Businesses/
RegionalAircraft/index.htm.
(4) 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.
(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, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Des Moines, Washington, on
September 14, 2018.
John P. Piccola,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2018–21344 Filed 10–2–18; 8:45 am]
BILLING CODE 4910–13–P
VerDate Sep<11>2014
16:40 Oct 02, 2018
Jkt 247001
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2018–0394; Product
Identifier 2018–NM–036–AD; Amendment
39–19441; AD 2018–20–07]
RIN 2120–AA64
Airworthiness Directives; Dassault
Aviation Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for all
Dassault Aviation Model MYSTEREFALCON 50 airplanes. This AD was
prompted by a determination that more
restrictive maintenance requirements
and airworthiness limitations are
necessary. This AD requires revising the
maintenance or inspection program, as
applicable, to incorporate new and more
restrictive maintenance requirements
and airworthiness limitations. We are
issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective November 7,
2018.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of November 7, 2018.
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 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–2018–
0394.
SUMMARY:
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–2018–
0394; 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 (phone: 800–647–5527) is
PO 00000
Frm 00021
Fmt 4700
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49789
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
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to all Dassault Aviation Model
MYSTERE-FALCON 50 airplanes. The
NPRM published in the Federal
Register on May 11, 2018 (83 FR 21953).
The NPRM was prompted by a
determination that more restrictive
maintenance requirements and
airworthiness limitations are necessary.
The NPRM proposed to require revising
the maintenance or inspection program,
as applicable, to incorporate new and
more restrictive maintenance
requirements and airworthiness
limitations.
We are issuing this AD to address
reduced structural integrity of the
airplane.
The European Aviation Safety Agency
(EASA), which is the Technical Agent
for the Member States of the European
Union, has issued EASA Airworthiness
Directive 2018–0026, dated January 30,
2018 (referred to after this as the
Mandatory Continuing Airworthiness
Information, or ‘‘the MCAI’’), to correct
an unsafe condition for all Dassault
Aviation Model MYSTERE-FALCON 50
airplanes. The MCAI states:
The airworthiness limitations and
certification maintenance instructions for the
Dassault Myste`re Falcon 50 aeroplanes,
which are approved by EASA, are currently
defined and published in the Dassault
Myste`re Falcon 50 Aircraft Maintenance
Manual (AMM) chapter 5–40. These
instructions have been identified as
mandatory for continued airworthiness.
Failure to accomplish these instructions
could result in an unsafe condition [i.e,
reduced structural integrity of the airplane].
Consequently, EASA issued [EASA] AD
2016–0067 [which corresponds to FAA AD
2017–09–03, Amendment 39–18865 (82 FR
21467, May 9, 2017)] to require
accomplishment of the maintenance tasks,
and implementation of the airworthiness
limitations, as specified in Dassault Myste`re
Falcon 50 AMM chapter 5–40 Revision 23.
Since that [EASA] AD was issued, Dassault
issued Revision 24 of the Dassault Myste`re
Falcon 50 AMM chapter 5–40, which
introduces new and more restrictive
maintenance requirements and/or
E:\FR\FM\03OCR1.SGM
03OCR1
49790
Federal Register / Vol. 83, No. 192 / Wednesday, October 3, 2018 / Rules and Regulations
airworthiness limitations. For the reason
described above, this [EASA] AD retains the
requirements of EASA AD 2016–0067, which
is superseded, and requires accomplishment
of the actions specified in Revision 24 of the
Dassault Myste`re Falcon 50 AMM chapter 5–
40 * * * .
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–2018–
0394.
Comments
We gave the public the opportunity to
participate in developing this final rule.
We received no comments on the NPRM
or on the determination of the cost to
the public.
Conclusion
We 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. We have 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.
daltland on DSKBBV9HB2PROD with RULES
Related Service Information Under 1
CFR Part 51
Dassault Aviation has issued Chapter
5–40, Airworthiness Limitations, DGT
113872, Revision 24, dated July 2017, of
the Dassault Falcon 50/50EX
Maintenance Manual. This service
information describes instructions
applicable to airworthiness and safe life
limitations. 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
We estimate that this AD affects 250
airplanes of U.S. registry.
We estimate the following costs to
comply with this AD:
We have determined that revising the
maintenance or inspection program
takes an average of 90 work-hours per
operator, although this figure may vary
from operator to operator. In the past,
we have estimated that this action takes
1 work-hour per airplane. Since
operators incorporate maintenance or
inspection program changes for their
affected fleet(s), we have determined
that a per-operator estimate is more
accurate than a per-airplane estimate.
Therefore, we estimate the total cost per
operator to be $7,650 (90 work-hours ×
$85 per work-hour).
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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.
We are issuing this rulemaking under
the authority described in Subtitle VII,
Part A, Subpart III, Section 44701:
‘‘General requirements.’’ Under that
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, methods, and procedures
the Administrator finds necessary for
safety in air commerce. This regulation
is within the scope of that authority
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
This AD is issued in accordance with
authority delegated by the Executive
Director, Aircraft Certification Service,
as authorized by FAA Order 8000.51C.
In accordance with that order, issuance
of ADs is normally a function of the
Compliance and Airworthiness
Division, but during this transition
period, the Executive Director has
delegated the authority to issue ADs
applicable to transport category
airplanes and associated appliances to
the Director of the System Oversight
Division.
Regulatory Findings
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) Is not a ‘‘significant rule’’ under
the DOT Regulatory Policies and
Procedures (44 FR 11034, February 26,
1979),
(3) Will not affect intrastate aviation
in Alaska, and
(4) 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.
PO 00000
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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 adding
the following new airworthiness
directive (AD):
■
2018–20–07 Dassault Aviation:
Amendment 39–19441; Docket No.
FAA–2018–0394; Product Identifier
2018–NM–036–AD.
(a) Effective Date
This AD is effective November 7, 2018.
(b) Affected ADs
This AD affects AD 2010–26–05,
Amendment 39–16544 (75 FR 79952,
December 21, 2010) (‘‘AD 2010–26–05’’); AD
2012–02–18, Amendment 39–16941 (77 FR
12175, February 29, 2012) (‘‘AD 2012–02–
18’’); and AD 2017–09–03, Amendment 39–
18865 (82 FR 21467, May 9, 2017) (‘‘AD
2017–09–03’’).
(c) Applicability
This AD applies to Dassault Aviation
Model MYSTERE-FALCON 50 airplanes,
certificated in any category, all manufacturer
serial numbers.
(d) Subject
Air Transport Association (ATA) of
America Code 05, Time limits/maintenance
checks.
(e) Reason
This AD was prompted by a determination
that more restrictive maintenance
requirements and airworthiness limitations
are necessary. We are 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) Revision of Maintenance or Inspection
Program
Within 90 days after the effective date of
this AD, revise the maintenance or inspection
program, as applicable, to incorporate the
information specified in Chapter 5–40,
Airworthiness Limitations, DGT 113872,
Revision 24, dated July 2017, of the Dassault
Falcon 50/50EX Maintenance Manual. The
initial compliance times for doing the tasks
are at the time specified in Chapter 5–40,
Airworthiness Limitations, DGT 113872,
Revision 24, dated July 2017, of the Dassault
Falcon 50/50EX Maintenance Manual, or
within 90 days after the effective date of this
AD, whichever occurs later.
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Federal Register / Vol. 83, No. 192 / Wednesday, October 3, 2018 / Rules and Regulations
(h) No Alternative Actions or Intervals
After the maintenance or inspection
program has been revised as required by
paragraph (g) of this AD, no alternative
actions (e.g., inspections) or intervals may be
used unless the actions or intervals are
approved as an alternative method of
compliance (AMOC) in accordance with the
procedures specified in paragraph (j)(1) of
this AD.
(i) Terminating Actions for Other ADs
(1) Accomplishing the actions required by
paragraph (g) of this AD terminates all
requirements of AD 2017–09–03.
(2) Accomplishing the actions required by
paragraph (g) of this AD terminates all
requirements of AD 2010–26–05 and AD
2012–02–18 for the Dassault Aviation Model
MYSTERE-FALCON 50 airplanes specified in
those ADs.
daltland on DSKBBV9HB2PROD with RULES
(j) 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 (k)(2) of this AD. Information may
be emailed to: 9-ANM-116-AMOCREQUESTS@faa.gov. Before using any
approved AMOC, notify your appropriate
principal inspector, or lacking a principal
inspector, the manager of the local flight
standards district office/certificate holding
district office.
(2) Contacting the Manufacturer: 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 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.
(k) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA
Airworthiness Directive 2018–0026, dated
January 30, 2018, 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–2018–0394.
(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.
(l) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
VerDate Sep<11>2014
16:40 Oct 02, 2018
Jkt 247001
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.
(i) Chapter 5–40, Airworthiness
Limitations, DGT 113872, Revision 24, dated
July 2017, of the Dassault Falcon 50/50EX
Maintenance Manual.
(ii) Reserved.
(3) 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.
(4) 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.
(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, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Des Moines, Washington, on
September 21, 2018.
John P. Piccola,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2018–21343 Filed 10–2–18; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2018–0517; Product
Identifier 2017–SW–098–AD; Amendment
39–19443; AD 2018–20–09]
RIN 2120–AA64
Airworthiness Directives; Airbus
Helicopters Deutschland GmbH
Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
PO 00000
Frm 00023
Fmt 4700
Sfmt 4700
of certain documents listed in this AD
as of November 7, 2018.
ADDRESSES: For service information
identified in this final rule, contact
Airbus Helicopters, 2701 N Forum
Drive, Grand Prairie, TX 75052;
telephone (972) 641–0000 or (800) 232–
0323; fax (972) 641–3775; or at https://
www.helicopters.airbus.com/website/
en/ref/Technical-Support_73.html. You
may review the referenced service
information at the FAA, Office of the
Regional Counsel, Southwest Region,
10101 Hillwood Pkwy., Room 6N–321,
Fort Worth, TX 76177. It is also
available on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2018–
0517.
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–2018–
0517; 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 AD, the
European Aviation Safety Agency
(EASA) AD, any incorporated-byreference service information, the
economic evaluation, any comments
received, and other information. The
street address for Docket Operations
(phone: 800–647–5527) 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: Matt
Fuller, Senior Aviation Safety Engineer,
Safety Management Section, Rotorcraft
Standards Branch, FAA, 10101
Hillwood Pkwy., Fort Worth, TX 76177;
telephone (817) 222–5110; email
matthew.fuller@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
We are adopting a new
airworthiness directive (AD) for Airbus
Helicopters Deutschland GmbH (Airbus
Helicopters) Model MBB–BK 117 C–2
and MBB–BK 117 D–2 helicopters. This
AD requires altering and re-identifying
the overhead panel shock mount
assembly (shock mount). This AD was
prompted by the manufacturer’s stress
recalculations. The actions of this AD
are intended to correct an unsafe
condition on these products.
DATES: This AD is effective November 7,
2018.
The Director of the Federal Register
approved the incorporation by reference
SUMMARY:
49791
On June 7, 2018, at 83 FR 26387, the
Federal Register published our notice of
proposed rulemaking (NPRM), which
proposed to amend 14 CFR part 39 by
adding an AD that would apply to
Airbus Helicopters Model MBB–BK 117
C–2 and Model MBB–BK 117 D–2
helicopters with an overhead panel
shock mount assembly part number
(P/N) B246M2035102 or P/N
B246M2036101 installed. The NPRM
proposed to require installing a
retaining plate on the shock mount and
re-identifying the shock mount by
changing the last three digits of the P/
N to –966. The NPRM also proposed
prohibiting the installation of shock
E:\FR\FM\03OCR1.SGM
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Agencies
[Federal Register Volume 83, Number 192 (Wednesday, October 3, 2018)]
[Rules and Regulations]
[Pages 49789-49791]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-21343]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2018-0394; Product Identifier 2018-NM-036-AD; Amendment
39-19441; AD 2018-20-07]
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for all
Dassault Aviation Model MYSTERE-FALCON 50 airplanes. This AD was
prompted by a determination that more restrictive maintenance
requirements and airworthiness limitations are necessary. This AD
requires revising the maintenance or inspection program, as applicable,
to incorporate new and more restrictive maintenance requirements and
airworthiness limitations. We are issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective November 7, 2018.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 7,
2018.
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 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-2018-
0394.
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-2018-
0394; 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 (phone: 800-647-
5527) 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
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to all Dassault Aviation Model
MYSTERE-FALCON 50 airplanes. The NPRM published in the Federal Register
on May 11, 2018 (83 FR 21953). The NPRM was prompted by a determination
that more restrictive maintenance requirements and airworthiness
limitations are necessary. The NPRM proposed to require revising the
maintenance or inspection program, as applicable, to incorporate new
and more restrictive maintenance requirements and airworthiness
limitations.
We are issuing this AD to address reduced structural integrity of
the airplane.
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA
Airworthiness Directive 2018-0026, dated January 30, 2018 (referred to
after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for all Dassault Aviation
Model MYSTERE-FALCON 50 airplanes. The MCAI states:
The airworthiness limitations and certification maintenance
instructions for the Dassault Myst[egrave]re Falcon 50 aeroplanes,
which are approved by EASA, are currently defined and published in
the Dassault Myst[egrave]re Falcon 50 Aircraft Maintenance Manual
(AMM) chapter 5-40. These instructions have been identified as
mandatory for continued airworthiness.
Failure to accomplish these instructions could result in an
unsafe condition [i.e, reduced structural integrity of the
airplane].
Consequently, EASA issued [EASA] AD 2016-0067 [which corresponds
to FAA AD 2017-09-03, Amendment 39-18865 (82 FR 21467, May 9, 2017)]
to require accomplishment of the maintenance tasks, and
implementation of the airworthiness limitations, as specified in
Dassault Myst[egrave]re Falcon 50 AMM chapter 5-40 Revision 23.
Since that [EASA] AD was issued, Dassault issued Revision 24 of
the Dassault Myst[egrave]re Falcon 50 AMM chapter 5-40, which
introduces new and more restrictive maintenance requirements and/or
[[Page 49790]]
airworthiness limitations. For the reason described above, this
[EASA] AD retains the requirements of EASA AD 2016-0067, which is
superseded, and requires accomplishment of the actions specified in
Revision 24 of the Dassault Myst[egrave]re Falcon 50 AMM chapter 5-
40 * * * .
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-2018-
0394.
Comments
We gave the public the opportunity to participate in developing
this final rule. We received no comments on the NPRM or on the
determination of the cost to the public.
Conclusion
We 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. We have determined that these minor
changes:
Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.
Related Service Information Under 1 CFR Part 51
Dassault Aviation has issued Chapter 5-40, Airworthiness
Limitations, DGT 113872, Revision 24, dated July 2017, of the Dassault
Falcon 50/50EX Maintenance Manual. This service information describes
instructions applicable to airworthiness and safe life limitations.
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
We estimate that this AD affects 250 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
We have determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although this
figure may vary from operator to operator. In the past, we have
estimated that this action takes 1 work-hour per airplane. Since
operators incorporate maintenance or inspection program changes for
their affected fleet(s), we have determined that a per-operator
estimate is more accurate than a per-airplane estimate. Therefore, we
estimate the total cost per operator 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.
We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the Compliance and Airworthiness Division, but
during this transition period, the Executive Director has delegated the
authority to issue ADs applicable to transport category airplanes and
associated appliances to the Director of the System Oversight Division.
Regulatory Findings
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) Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979),
(3) Will not affect intrastate aviation in Alaska, and
(4) 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 adding the following new airworthiness
directive (AD):
2018-20-07 Dassault Aviation: Amendment 39-19441; Docket No. FAA-
2018-0394; Product Identifier 2018-NM-036-AD.
(a) Effective Date
This AD is effective November 7, 2018.
(b) Affected ADs
This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR 79952,
December 21, 2010) (``AD 2010-26-05''); AD 2012-02-18, Amendment 39-
16941 (77 FR 12175, February 29, 2012) (``AD 2012-02-18''); and AD
2017-09-03, Amendment 39-18865 (82 FR 21467, May 9, 2017) (``AD
2017-09-03'').
(c) Applicability
This AD applies to Dassault Aviation Model MYSTERE-FALCON 50
airplanes, certificated in any category, all manufacturer serial
numbers.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time limits/
maintenance checks.
(e) Reason
This AD was prompted by a determination that more restrictive
maintenance requirements and airworthiness limitations are
necessary. We are 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) Revision of Maintenance or Inspection Program
Within 90 days after the effective date of this AD, revise the
maintenance or inspection program, as applicable, to incorporate the
information specified in Chapter 5-40, Airworthiness Limitations,
DGT 113872, Revision 24, dated July 2017, of the Dassault Falcon 50/
50EX Maintenance Manual. The initial compliance times for doing the
tasks are at the time specified in Chapter 5-40, Airworthiness
Limitations, DGT 113872, Revision 24, dated July 2017, of the
Dassault Falcon 50/50EX Maintenance Manual, or within 90 days after
the effective date of this AD, whichever occurs later.
[[Page 49791]]
(h) No Alternative Actions or Intervals
After the maintenance or inspection program has been revised as
required by paragraph (g) of this AD, no alternative actions (e.g.,
inspections) or intervals may be used unless the actions or
intervals are approved as an alternative method of compliance (AMOC)
in accordance with the procedures specified in paragraph (j)(1) of
this AD.
(i) Terminating Actions for Other ADs
(1) Accomplishing the actions required by paragraph (g) of this
AD terminates all requirements of AD 2017-09-03.
(2) Accomplishing the actions required by paragraph (g) of this
AD terminates all requirements of AD 2010-26-05 and AD 2012-02-18
for the Dassault Aviation Model MYSTERE-FALCON 50 airplanes
specified in those ADs.
(j) 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 (k)(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 inspector, the manager of the local flight
standards district office/certificate holding district office.
(2) Contacting the Manufacturer: 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 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.
(k) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2018-0026, dated January 30,
2018, 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-2018-0394.
(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.
(l) 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.
(i) Chapter 5-40, Airworthiness Limitations, DGT 113872,
Revision 24, dated July 2017, of the Dassault Falcon 50/50EX
Maintenance Manual.
(ii) Reserved.
(3) 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.
(4) 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.
(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, call 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Des Moines, Washington, on September 21, 2018.
John P. Piccola,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2018-21343 Filed 10-2-18; 8:45 am]
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