Airworthiness Directives; Dassault Aviation Airplanes, 67171-67174 [2019-26402]
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Federal Register / Vol. 84, No. 236 / Monday, December 9, 2019 / Rules and Regulations
(h) Retained Requirement for No Alternative
Actions or Intervals, With a New Exception
This paragraph restates the requirements of
paragraph (h) of AD 2018–19–05, 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 (l)(1) of this AD.
(i) New Requirement of This AD: Revision of
Existing Maintenance or Inspection Program
Within 90 days after the effective date of
this AD, revise the existing maintenance or
inspection program, as applicable, to
incorporate the information specified in
Chapter 5–40, Airworthiness Limitations,
Revision 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 the effective
date of this AD, 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. Doing the revision required by
this paragraph terminates the actions
required by paragraph (g) of this AD.
(j) No Alternative Actions or Intervals
After the existing maintenance or
inspection program has been revised as
required by paragraph (i) of this AD, no
alternative actions (e.g., inspections) or
intervals may be used unless the actions or
intervals are approved as an AMOC in
accordance with the procedures specified in
paragraph (l)(1) of this AD.
tkelley on DSKBCP9HB2PROD with RULES
(k) 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.
(l) Other FAA AD Provisions
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Section, Transport Standards Branch, FAA,
has the authority to approve AMOCs for this
AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR
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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 9-ANM-116-AMOC–
REQUESTS@faa.gov.
(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
2018–19–05 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
2019–0132, dated June 11, 2019, for related
information. This MCAI may be found in the
AD docket on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2019–0668.
(2) For more information about this AD,
contact Tom Rodriguez, Aerospace Engineer,
International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des
Moines, WA 98198; telephone and fax 206–
231–3226.
(n) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(3) The following service information was
approved for IBR on January 13, 2020.
(i) Chapter 5–40, Airworthiness
Limitations, Revision 24, dated September
2018, of the Dassault Aviation Falcon 900
Maintenance Manual.
(ii) [Reserved]
(4) The following service information was
approved for IBR on October 26, 2018 (83 FR
47813, September 21, 2018).
(i) Chapter 5–40, Airworthiness
Limitations, Revision 23, dated September
2017, of the Dassault Aviation Falcon 900
Maintenance Manual.
(ii) [Reserved]
(5) For service information identified in
this AD, contact Dassault Falcon Jet
Corporation, Teterboro Airport, P.O. Box
2000, South Hackensack, NJ 07606;
telephone 201–440–6700; internet https://
www.dassaultfalcon.com.
(6) You may view this service information
at the FAA, Transport Standards Branch,
PO 00000
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67171
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 fedreg.legal@nara.gov, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Des Moines, Washington, on
November 15, 2019.
Dionne Palermo,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2019–26450 Filed 12–6–19; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2019–0697; Product
Identifier 2019–NM–110–AD; Amendment
39–19796; AD 2019–23–03]
RIN 2120–AA64
Airworthiness Directives; Dassault
Aviation Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
The FAA is superseding
Airworthiness Directives (AD) 2017–19–
14 and AD 2014–16–27, which apply to
certain Dassault Aviation Model
FALCON 900EX airplanes. Those ADs
require revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive maintenance requirements
and/or airworthiness limitations. Since
the FAA issued AD 2017–19–14 and AD
2014–16–27, the FAA determined that
new or more restrictive airworthiness
limitations are necessary. This AD
requires revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive airworthiness limitations.
The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective January 13,
2020.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of January 13, 2020.
The Director of the Federal Register
approved the incorporation by reference
of a certain other publication listed in
this AD as of October 24, 2017 (82 FR
43674, September 19, 2017).
SUMMARY:
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Federal Register / Vol. 84, No. 236 / Monday, December 9, 2019 / Rules and Regulations
For service information
identified in this final rule, contact
Dassault Falcon Jet Corporation,
Teterboro Airport, P.O. Box 2000, South
Hackensack, NJ 07606; telephone 201–
440–6700; internet https://
www.dassaultfalcon.com. You may
view this referenced service information
at the FAA, Transport Standards
Branch, 2200 South 216th St., Des
Moines, WA. For information on the
availability of this material at the FAA,
call 206–231–3195. It is also available
on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2019–
0697.
ADDRESSES:
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2019–
0697; or in person at Docket Operations
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this final rule,
the regulatory evaluation, any
comments received, and other
information. The address for Docket
Operations is U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Tom
Rodriguez, Aerospace Engineer,
International Section, Transport
Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198;
telephone and fax 206–231–3226.
SUPPLEMENTARY INFORMATION:
tkelley on DSKBCP9HB2PROD with RULES
Discussion
The European Union Aviation Safety
Agency (EASA), which is the Technical
Agent for the Member States of the
European Union, has issued EASA AD
2019–0134, dated June 11, 2019 (‘‘EASA
AD 2019–0134’’) (also referred to as the
Mandatory Continuing Airworthiness
Information, or ‘‘the MCAI’’), to correct
an unsafe condition for certain Dassault
Aviation Model FALCON 900EX
airplanes. You may examine the MCAI
in the AD docket on the internet at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2019–0697.
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to supersede AD 2017–19–14,
Amendment 39–19044 (82 FR 43674,
September 19, 2017) (‘‘AD 2017–19–
14’’); and AD 2014–16–27, Amendment
39–17951 (79 FR 51071, August 27,
2014) (‘‘AD 2014–16–27’’). AD 2017–
19–14 and AD 2014–16–27 applied to
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certain Dassault Aviation Model
FALCON 900EX airplanes. Further, AD
2014–16–27 terminates paragraph (g)(1)
of AD 2010–26–05, Amendment 39–
16544 (75 FR 79952, December 21,
2010), for certain Dassault Aviation
Model FALCON 900EX airplanes, and
this terminating provision is included in
this AD. The NPRM published in the
Federal Register on September 13, 2019
(84 FR 48310). The NPRM was
prompted by the FAA’s determination
that new or more restrictive
airworthiness limitations are necessary.
The NPRM proposed to require revising
the existing maintenance or inspection
program, as applicable, to incorporate
new or more restrictive airworthiness
limitations. The FAA is issuing this AD
to address, among other things, fatigue
cracking and damage in principal
structural elements; such fatigue
cracking and damage could result in
reduced structural integrity of the
airplane. See the MCAI for additional
background information.
Comments
The FAA gave the public the
opportunity to participate in developing
this final rule. The FAA received no
comments on the NPRM or on the
determination of the cost to the public.
Conclusion
The FAA reviewed the relevant data
and determined that air safety and the
public interest require adopting this
final rule as proposed, except for minor
editorial changes. The FAA determined
that these minor changes:
• 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,
Revision 11, dated September 2018, of
the Dassault Falcon 900EX EASy,
Falcon 900LX, and Falcon 900DX
Maintenance Manual. This service
information describes procedures,
maintenance tasks, and airworthiness
limitations specified in the
Airworthiness Limitations section of the
airplane maintenance manual.
This AD also requires Chapter 5–40,
Airworthiness Limitations, Revision 9,
dated November 2015, of the Dassault
Falcon 900EX EASy, Falcon 900LX, and
Falcon 900DX Maintenance Manual,
which the Director of the Federal
Register approved for incorporation by
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reference as of October 24, 2017 (82 FR
43674, September 19, 2017).
This service information is reasonably
available because the interested parties
have access to it through their normal
course of business or by the means
identified in the ADDRESSES section.
Costs of Compliance
The FAA estimates that this AD
affects 79 airplanes of U.S. registry.
The FAA estimates the following
costs to comply with this AD:
The FAA estimates the total cost per
operator for the retained actions from
AD 2017–19–14 to be $7,650 (90 workhours × $85 per work-hour).
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 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 × $85 per
work-hour).
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII:
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
The FAA is issuing this rulemaking
under the authority described in
Subtitle VII, Part A, Subpart III, Section
44701: ‘‘General requirements.’’ Under
that section, Congress charges the FAA
with promoting safe flight of civil
aircraft in air commerce by prescribing
regulations for practices, methods, and
procedures the Administrator finds
necessary for safety in air commerce.
This regulation is within the scope of
that authority because it addresses an
unsafe condition that is likely to exist or
develop on products identified in this
rulemaking action.
This AD is issued in accordance with
authority delegated by the Executive
Director, Aircraft Certification Service,
as authorized by FAA Order 8000.51C.
In accordance with that order, issuance
of ADs is normally a function of the
Compliance and Airworthiness
Division, but during this transition
period, the Executive Director has
delegated the authority to issue ADs
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Federal Register / Vol. 84, No. 236 / Monday, December 9, 2019 / Rules and Regulations
applicable to transport category
airplanes and associated appliances to
the Director of the System Oversight
Division.
Regulatory Findings
The FAA determined that this AD
will not have federalism implications
under Executive Order 13132. This AD
will not have a substantial direct effect
on the States, on the relationship
between the national government and
the States, or on the distribution of
power and responsibilities among the
various levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Will not affect intrastate aviation
in Alaska, and
(3) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
(d) Subject
Air Transport Association (ATA) of
America Code 05, Time Limits/Maintenance
Checks.
(e) Reason
This AD was prompted by a determination
that new or more restrictive airworthiness
limitations are necessary. The FAA is issuing
this AD to address, among other things,
fatigue cracking and damage in principal
structural elements; such fatigue cracking
and damage could result in reduced
structural integrity of the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(a) Effective Date
This AD is effective January 13, 2020.
(g) Retained Revision of Maintenance or
Inspection Program, With No Changes
This paragraph restates the requirements of
paragraph (g) of AD 2017–19–14, with no
changes. Within 90 days after October 24,
2017 (the effective date of AD 2017–19–14),
revise the existing maintenance or inspection
program, as applicable, to incorporate the
information specified in Chapter 5–40,
Airworthiness Limitations, Revision 9, dated
November 2015, of the Dassault Falcon
900EX EASy, Falcon 900LX, and Falcon
900DX Maintenance Manual. The initial
compliance times for accomplishing the
actions specified in Chapter 5–40,
Airworthiness Limitations, Revision 9, dated
November 2015, of the Dassault Falcon
900EX EASy, Falcon 900LX, and Falcon
900DX Maintenance Manual, is within the
applicable times specified in the
maintenance manual or 90 days after October
24, 2017, whichever occurs later, except as
provided by paragraphs (g)(1) through (4) of
this AD.
(1) The term ‘‘LDG’’ in the ‘‘First
Inspection’’ column of any table in the
service information means total airplane
landings.
(2) The term ‘‘FH’’ in the ‘‘First Inspection’’
column of any table in the service
information means total flight hours.
(3) The term ‘‘FC’’ in the ‘‘First Inspection’’
column of any table in the service
information means total flight cycles.
(4) The term ‘‘M’’ in the ‘‘First Inspection’’
column of any table in the service
information means months.
(b) Affected ADs
(1) This AD replaces AD 2014–16–27,
Amendment 39–17951 (79 FR 51071, August
27, 2014) (‘‘AD 2014–16–27’’); and AD 2017–
19–14, Amendment 39–19044 (82 FR 43674,
September 19, 2017) (‘‘AD 2017–19–14’’).
(2) This AD affects AD 2010–26–05,
Amendment 39–16544 (75 FR 79952,
December 21, 2010) (‘‘AD 2010–26–05’’).
(h) Retained Requirement for No Alternative
Actions and Intervals, With New Exception
This paragraph restates the requirements
specified in paragraph (h) of AD 2017–19–14,
with a new exception. Except as required by
paragraph (i) of this AD, after accomplishing
the revision required by paragraph (g) of this
AD, no alternative actions (inspections) or
intervals may be used unless the actions or
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) 2014–16–27, Amendment 39–
17951 (79 FR 51071, August 27, 2014);
and AD 2017–19–14, Amendment 39–
19044 (82 FR 43674, September 19,
2017); and
■ b. Adding the following new AD:
■
■
2019–23–03 Dassault Aviation:
Amendment 39–19796; Docket No.
FAA–2019–0697; Product Identifier
2019–NM–110–AD.
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(c) Applicability
This AD applies to Dassault Aviation
Model FALCON 900EX airplanes, serial
number (S/N) 97 and S/Ns 120 and higher,
certificated in any category, with an original
airworthiness certificate or original export
certificate of airworthiness issued on or
before September 1, 2018.
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67173
intervals are approved as an alternative
method of compliance (AMOC) in
accordance with the procedures specified in
paragraph (l)(1) of this AD.
(i) New Requirement of This AD:
Maintenance or Inspection Program
Revision
Within 90 days after the effective date of
this AD, revise the existing maintenance or
inspection program, as applicable, to
incorporate the information specified in
Chapter 5–40, Airworthiness Limitations,
Revision 11, dated September 2018, of the
Dassault Falcon 900EX EASy, Falcon 900LX,
and Falcon 900DX Maintenance Manual. The
initial compliance times for accomplishing
the actions are at the times specified in
Chapter 5–40, Airworthiness Limitations,
Revision 11, dated September 2018, of the
Dassault Falcon 900EX EASy, Falcon 900LX,
and Falcon 900DX Maintenance Manual, or
90 days after the effective date of this AD,
whichever occurs later, except as provided
by paragraphs (i)(1) through (4) of this AD.
(1) The term ‘‘LDG’’ in the ‘‘First
Inspection’’ column of any table in the
service information means total airplane
landings.
(2) The term ‘‘FH’’ in the ‘‘First Inspection’’
column of any table in the service
information means total flight hours.
(3) The term ‘‘FC’’ in the ‘‘First Inspection’’
column of any table in the service
information means total flight cycles.
(4) The term ‘‘M’’ in the ‘‘First Inspection’’
column of any table in the service
information means months since the date of
issuance of the original airworthiness
certificate or the date of issuance of the
original export certificate of airworthiness.
(j) No Alternative Actions or Intervals
After the existing maintenance or
inspection program has been revised as
required by paragraph (i) of this AD, no
alternative actions (e.g., inspections) or
intervals may be used unless the actions and
intervals are approved as an AMOC in
accordance with the procedures specified in
paragraph (l)(1) of this AD.
(k) Terminating Actions for Certain Actions
in AD 2010–26–05
Accomplishing the actions required by
paragraph (g) or (i) of this AD terminates the
requirements of paragraph (g)(1) of AD 2010–
26–05, for Dassault Aviation Model 900EX
airplanes, S/N 97 and S/Ns 120 and higher.
(l) Other FAA AD Provisions
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Section, Transport Standards Branch, FAA,
has the authority to approve AMOCs for this
AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR
39.19, send your request to your principal
inspector or local Flight Standards District
Office, as appropriate. If sending information
directly to the International Section, send it
to the attention of the person identified in
paragraph (m)(2) of this AD. Information may
be emailed to 9-ANM-116-AMOCREQUESTS@faa.gov. Before using any
approved AMOC, notify your appropriate
principal inspector, or lacking a principal
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Federal Register / Vol. 84, No. 236 / Monday, December 9, 2019 / Rules and Regulations
inspector, the manager of the local flight
standards district office/certificate holding
district office.
(2) Contacting the Manufacturer: As of the
effective date of this AD, for any requirement
in this AD to obtain corrective actions from
a manufacturer, the action must be
accomplished using a method approved by
the Manager, International Section, Transport
Standards Branch, FAA; or the European
Union Aviation Safety Agency (EASA); or
Dassault Aviation’s EASA Design
Organization Approval (DOA). If approved by
the DOA, the approval must include the
DOA-authorized signature.
Issued in Des Moines, Washington, on
November 14, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division,
Aircraft Certification Service.
(m) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA AD
2019–0134, dated June 11, 2019, for related
information. This MCAI may be found in the
AD docket on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2019–0697.
(2) For more information about this AD,
contact Tom Rodriguez, Aerospace Engineer,
International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des
Moines, WA 98198; telephone and fax 206–
231–3226.
[Docket No. FAA–2019–0671; Product
Identifier 2019–NM–080–AD; Amendment
39–19788; AD 2019–22–09]
(n) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(3) The following service information was
approved for IBR on January 13, 2020.
(i) Chapter 5–40, Airworthiness
Limitations, Revision 11, dated September
2018, of the Dassault Falcon 900EX EASy,
Falcon 900LX, and Falcon 900DX
Maintenance Manual.
(ii) [Reserved]
(4) The following service information was
approved for IBR on October 24, 2017 (82 FR
43674, September 19, 2017).
(i) Chapter 5–40, Airworthiness
Limitations, Revision 9, dated November
2015, of the Dassault Falcon 900EX EASy,
Falcon 900LX, and Falcon 900DX
Maintenance Manual.
(ii) [Reserved]
(5) For service information identified in
this AD, contact Dassault Falcon Jet
Corporation, Teterboro Airport, P.O. Box
2000, South Hackensack, NJ 07606;
telephone 201–440–6700; internet https://
www.dassaultfalcon.com.
(6) You may view this service information
at the FAA, Transport Standards Branch,
2200 South 216th St., Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
(7) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
email fedreg.legal@nara.gov, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
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[FR Doc. 2019–26402 Filed 12–6–19; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Airworthiness Directives; The Boeing
Company Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
The FAA is adopting a new
airworthiness directive (AD) for certain
The Boeing Company Model 787–8
airplanes. This AD was prompted by a
report of fatigue cracking in the lug root
radius of a main landing gear (MLG) aft
hanger link lug fitting. This AD requires
repetitive surface high frequency eddy
current (HFEC) inspections of the left
and right side MLG aft hanger link lug
fitting for cracking, and applicable oncondition actions. The FAA is issuing
this AD to address the unsafe condition
on these products.
DATES: This AD is effective January 13,
2020.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of January 13, 2020.
ADDRESSES: For service information
identified in this final rule, contact
Boeing Commercial Airplanes,
Attention: Contractual & Data Services
(C&DS), 2600 Westminster Blvd., MC
110–SK57, Seal Beach, CA 90740–5600;
telephone 562–797–1717; internet
https://www.myboeingfleet.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–2019–0671.
SUMMARY:
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
Fmt 4700
Sfmt 4700
SUPPLEMENTARY INFORMATION:
Discussion
AGENCY:
Frm 00006
Greg
Rutar, Aerospace Engineer, Airframe
Section, FAA, Seattle ACO Branch, 2200
South 216th St., Des Moines, WA 98198;
phone and fax: 206–231–3529; email:
greg.rutar@faa.gov.
FOR FURTHER INFORMATION CONTACT:
RIN 2120–AA64
PO 00000
and locating Docket No. FAA–2019–
0671; 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.
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain The Boeing Company
Model 787–8 airplanes. The NPRM
published in the Federal Register on
September 6, 2019 (84 FR 46898). The
NPRM was prompted by a report of
fatigue cracking in the lug root radius of
an MLG aft hanger link lug fitting. The
NPRM proposed to require repetitive
surface HFEC inspections of the left and
right side MLG aft hanger link lug fitting
for cracking, and applicable oncondition actions.
The FAA is issuing this AD to address
fatigue cracking in the left and right side
MLG aft hanger link lug fittings. This
condition, if not addressed, could result
in undetected fatigue cracks that can
grow and weaken the primary structure
such that it cannot sustain limit load,
which could adversely affect the
structural integrity of the airplane.
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
The Air Line Pilots Association,
International (ALPA), Boeing, and
Austin Russo expressed support for the
NPRM.
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:
C:\TARSHA\09DER1.SGM
09DER1
Agencies
[Federal Register Volume 84, Number 236 (Monday, December 9, 2019)]
[Rules and Regulations]
[Pages 67171-67174]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-26402]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0697; Product Identifier 2019-NM-110-AD; Amendment
39-19796; AD 2019-23-03]
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is superseding Airworthiness Directives (AD) 2017-19-
14 and AD 2014-16-27, which apply to certain Dassault Aviation Model
FALCON 900EX airplanes. Those ADs require revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive maintenance requirements and/or airworthiness
limitations. Since the FAA issued AD 2017-19-14 and AD 2014-16-27, the
FAA determined that new or more restrictive airworthiness limitations
are necessary. This AD requires revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. The FAA is issuing this AD to
address the unsafe condition on these products.
DATES: This AD is effective January 13, 2020.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 13,
2020.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of
October 24, 2017 (82 FR 43674, September 19, 2017).
[[Page 67172]]
ADDRESSES: For service information identified in this final rule,
contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box
2000, South Hackensack, NJ 07606; telephone 201-440-6700; internet
https://www.dassaultfalcon.com. You may view this referenced service
information at the FAA, Transport Standards Branch, 2200 South 216th
St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195. It is also available on the
internet at https://www.regulations.gov by searching for and locating
Docket No. FAA-2019-0697.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0697; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, the regulatory evaluation, any comments received, and
other information. The address for Docket Operations is U.S. Department
of Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
International Section, Transport Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; telephone and fax 206-231-3226.
SUPPLEMENTARY INFORMATION:
Discussion
The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2019-0134, dated June 11, 2019 (``EASA AD 2019-0134'') (also
referred to as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for certain Dassault
Aviation Model FALCON 900EX airplanes. You may examine the MCAI in the
AD docket on the internet at https://www.regulations.gov by searching
for and locating Docket No. FAA-2019-0697.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2017-19-14, Amendment 39-19044 (82 FR
43674, September 19, 2017) (``AD 2017-19-14''); and AD 2014-16-27,
Amendment 39-17951 (79 FR 51071, August 27, 2014) (``AD 2014-16-27'').
AD 2017-19-14 and AD 2014-16-27 applied to certain Dassault Aviation
Model FALCON 900EX airplanes. Further, AD 2014-16-27 terminates
paragraph (g)(1) of AD 2010-26-05, Amendment 39-16544 (75 FR 79952,
December 21, 2010), for certain Dassault Aviation Model FALCON 900EX
airplanes, and this terminating provision is included in this AD. The
NPRM published in the Federal Register on September 13, 2019 (84 FR
48310). The NPRM was prompted by the FAA's determination that new or
more restrictive airworthiness limitations are necessary. The NPRM
proposed to require revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive
airworthiness limitations. The FAA is issuing this AD to address, among
other things, fatigue cracking and damage in principal structural
elements; such fatigue cracking and damage could result in reduced
structural integrity of the airplane. See the MCAI for additional
background information.
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The FAA received no comments on the NPRM or
on the determination of the cost to the public.
Conclusion
The FAA reviewed the relevant data and determined that air safety
and the public interest require adopting this final rule as proposed,
except for minor editorial changes. The FAA determined that these minor
changes:
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, Revision 11, dated September 2018, of the Dassault Falcon
900EX EASy, Falcon 900LX, and Falcon 900DX Maintenance Manual. This
service information describes procedures, maintenance tasks, and
airworthiness limitations specified in the Airworthiness Limitations
section of the airplane maintenance manual.
This AD also requires Chapter 5-40, Airworthiness Limitations,
Revision 9, dated November 2015, of the Dassault Falcon 900EX EASy,
Falcon 900LX, and Falcon 900DX Maintenance Manual, which the Director
of the Federal Register approved for incorporation by reference as of
October 24, 2017 (82 FR 43674, September 19, 2017).
This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.
Costs of Compliance
The FAA estimates that this AD affects 79 airplanes of U.S.
registry.
The FAA estimates the following costs to comply with this AD:
The FAA estimates the total cost per operator for the retained
actions from AD 2017-19-14 to be $7,650 (90 work-hours x $85 per work-
hour).
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the agency recognizes that this number may vary from operator
to operator. In the past, the FAA has estimated that this action takes
1 work-hour per airplane. Since operators incorporate maintenance or
inspection program changes for their affected fleet(s), the FAA has
determined that a per-operator estimate is more accurate than a per-
airplane estimate. The FAA estimates the total cost per operator for
the new actions to be $7,650 (90 work-hours x $85 per work-hour).
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the Compliance and Airworthiness Division, but
during this transition period, the Executive Director has delegated the
authority to issue ADs
[[Page 67173]]
applicable to transport category airplanes and associated appliances to
the Director of the System Oversight Division.
Regulatory Findings
The FAA determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the national government and the States, or on the distribution of power
and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by
0
a. Removing Airworthiness Directive (AD) 2014-16-27, Amendment 39-17951
(79 FR 51071, August 27, 2014); and AD 2017-19-14, Amendment 39-19044
(82 FR 43674, September 19, 2017); and
0
b. Adding the following new AD:
2019-23-03 Dassault Aviation: Amendment 39-19796; Docket No. FAA-
2019-0697; Product Identifier 2019-NM-110-AD.
(a) Effective Date
This AD is effective January 13, 2020.
(b) Affected ADs
(1) This AD replaces AD 2014-16-27, Amendment 39-17951 (79 FR
51071, August 27, 2014) (``AD 2014-16-27''); and AD 2017-19-14,
Amendment 39-19044 (82 FR 43674, September 19, 2017) (``AD 2017-19-
14'').
(2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR
79952, December 21, 2010) (``AD 2010-26-05'').
(c) Applicability
This AD applies to Dassault Aviation Model FALCON 900EX
airplanes, serial number (S/N) 97 and S/Ns 120 and higher,
certificated in any category, with an original airworthiness
certificate or original export certificate of airworthiness issued
on or before September 1, 2018.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.
(e) Reason
This AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
issuing this AD to address, among other things, fatigue cracking and
damage in principal structural elements; such fatigue cracking and
damage could result in reduced structural integrity of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Retained Revision of Maintenance or Inspection Program, With No
Changes
This paragraph restates the requirements of paragraph (g) of AD
2017-19-14, with no changes. Within 90 days after October 24, 2017
(the effective date of AD 2017-19-14), revise the existing
maintenance or inspection program, as applicable, to incorporate the
information specified in Chapter 5-40, Airworthiness Limitations,
Revision 9, dated November 2015, of the Dassault Falcon 900EX EASy,
Falcon 900LX, and Falcon 900DX Maintenance Manual. The initial
compliance times for accomplishing the actions specified in Chapter
5-40, Airworthiness Limitations, Revision 9, dated November 2015, of
the Dassault Falcon 900EX EASy, Falcon 900LX, and Falcon 900DX
Maintenance Manual, is within the applicable times specified in the
maintenance manual or 90 days after October 24, 2017, whichever
occurs later, except as provided by paragraphs (g)(1) through (4) of
this AD.
(1) The term ``LDG'' in the ``First Inspection'' column of any
table in the service information means total airplane landings.
(2) The term ``FH'' in the ``First Inspection'' column of any
table in the service information means total flight hours.
(3) The term ``FC'' in the ``First Inspection'' column of any
table in the service information means total flight cycles.
(4) The term ``M'' in the ``First Inspection'' column of any
table in the service information means months.
(h) Retained Requirement for No Alternative Actions and Intervals, With
New Exception
This paragraph restates the requirements specified in paragraph
(h) of AD 2017-19-14, with a new exception. Except as required by
paragraph (i) of this AD, after accomplishing the revision required
by paragraph (g) of this AD, no alternative actions (inspections) or
intervals may be used unless the actions or intervals are approved
as an alternative method of compliance (AMOC) in accordance with the
procedures specified in paragraph (l)(1) of this AD.
(i) New Requirement of This AD: Maintenance or Inspection Program
Revision
Within 90 days after the effective date of this AD, revise the
existing maintenance or inspection program, as applicable, to
incorporate the information specified in Chapter 5-40, Airworthiness
Limitations, Revision 11, dated September 2018, of the Dassault
Falcon 900EX EASy, Falcon 900LX, and Falcon 900DX Maintenance
Manual. The initial compliance times for accomplishing the actions
are at the times specified in Chapter 5-40, Airworthiness
Limitations, Revision 11, dated September 2018, of the Dassault
Falcon 900EX EASy, Falcon 900LX, and Falcon 900DX Maintenance
Manual, or 90 days after the effective date of this AD, whichever
occurs later, except as provided by paragraphs (i)(1) through (4) of
this AD.
(1) The term ``LDG'' in the ``First Inspection'' column of any
table in the service information means total airplane landings.
(2) The term ``FH'' in the ``First Inspection'' column of any
table in the service information means total flight hours.
(3) The term ``FC'' in the ``First Inspection'' column of any
table in the service information means total flight cycles.
(4) The term ``M'' in the ``First Inspection'' column of any
table in the service information means months since the date of
issuance of the original airworthiness certificate or the date of
issuance of the original export certificate of airworthiness.
(j) No Alternative Actions or Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (i) of this AD, no alternative
actions (e.g., inspections) or intervals may be used unless the
actions and intervals are approved as an AMOC in accordance with the
procedures specified in paragraph (l)(1) of this AD.
(k) Terminating Actions for Certain Actions in AD 2010-26-05
Accomplishing the actions required by paragraph (g) or (i) of
this AD terminates the requirements of paragraph (g)(1) of AD 2010-
26-05, for Dassault Aviation Model 900EX airplanes, S/N 97 and S/Ns
120 and higher.
(l) Other FAA AD Provisions
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Section, Transport Standards Branch, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the International Section, send it to the attention of
the person identified in paragraph (m)(2) of this AD. Information
may be emailed to [email protected]. Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal
[[Page 67174]]
inspector, the manager of the local flight standards district
office/certificate holding district office.
(2) Contacting the Manufacturer: As of the effective date of
this AD, for any requirement in this AD to obtain corrective actions
from a manufacturer, the action must be accomplished using a method
approved by the Manager, International Section, Transport Standards
Branch, FAA; or the European Union Aviation Safety Agency (EASA); or
Dassault Aviation's EASA Design Organization Approval (DOA). If
approved by the DOA, the approval must include the DOA-authorized
signature.
(m) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2019-0134, dated June 11, 2019, for related
information. This MCAI may be found in the AD docket on the internet
at https://www.regulations.gov by searching for and locating Docket
No. FAA-2019-0697.
(2) For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
and fax 206-231-3226.
(n) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(3) The following service information was approved for IBR on
January 13, 2020.
(i) Chapter 5-40, Airworthiness Limitations, Revision 11, dated
September 2018, of the Dassault Falcon 900EX EASy, Falcon 900LX, and
Falcon 900DX Maintenance Manual.
(ii) [Reserved]
(4) The following service information was approved for IBR on
October 24, 2017 (82 FR 43674, September 19, 2017).
(i) Chapter 5-40, Airworthiness Limitations, Revision 9, dated
November 2015, of the Dassault Falcon 900EX EASy, Falcon 900LX, and
Falcon 900DX Maintenance Manual.
(ii) [Reserved]
(5) For service information identified in this AD, contact
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000,
South Hackensack, NJ 07606; telephone 201-440-6700; internet https://www.dassaultfalcon.com.
(6) You may view this service information at the FAA, Transport
Standards Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call
206-231-3195.
(7) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, email [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Des Moines, Washington, on November 14, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-26402 Filed 12-6-19; 8:45 am]
BILLING CODE 4910-13-P