Airworthiness Directives; Dassault Aviation Airplanes, 11640-11641 [2019-05890]
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11640
Federal Register / Vol. 84, No. 60 / Thursday, March 28, 2019 / Rules and Regulations
(b) Affected ADs
This AD replaces AD 2016–22–05,
Amendment 39–18694 (81 FR 75686,
November 1, 2016).
(c) Applicability
This AD applies to Pratt & Whitney
Division (PW):
(1) PW4164, PW4168, and PW4168A
model turbofan engines that have fuel
nozzles, part number (P/N) 51J345, installed,
and that have any of the following installed:
Talon IIB combustion chamber per Pratt &
Whitney Service Bulletin (SB) PW4G–100–
72–214, dated December 15, 2011; ring case
configuration (RCC) high-pressure
compressor (HPC) per Pratt & Whitney SB
PW4G–100–72–219, Revision No. 1, dated
October 5, 2011, or original issue; or the
outer combustion chamber assembly
waspaloy nuts per Pratt & Whitney SB
PW4G–100–72–253, dated November 24,
2014;
(2) PW4168A model engines with Talon
IIA outer combustion chamber assembly,
P/N 51J100 or 51J382, and fuel nozzles, P/N
51J345, installed;
(3) PW4168A–1D and PW4170 model
engines with engine serial numbers P735001
through P735190, inclusive, and fuel nozzles,
P/N 51J345, installed;
(4) PW4164–1D, PW4168–1D, PW4168A–
1D, and PW4170 model turbofan engines that
have installed the RCC HPC per Pratt &
Whitney SB PW4G–100–72–220, Revision
No. 4, dated September 30, 2011, or earlier
revision, and have fuel nozzles, P/N 51J345,
installed; and
(5) PW4164, PW4164–1D, PW4168,
PW4168–1D, PW4168A, PW4168A–1D, and
PW4170 model turbofan engines with fuel
nozzle, P/N 51J398, installed, that have not
installed the replacement fuel nozzle supply
manifold assemblies, and new brackets and
clamps on the fuel nozzle supply manifold
assemblies per Pratt & Whitney SB PW4G–
100–73–48, Revision No. 1, dated April 24,
2018.
(d) Subject
Joint Aircraft System Component (JASC)
Code 7310, Engine Fuel Distribution.
(e) Unsafe Condition
This AD was prompted by several
instances of fuel leaks on PW engines with
the Talon IIB combustion chamber
configuration installed. We are issuing this
AD to prevent failure of the fuel nozzles. The
unsafe condition, if not addressed, could
result in engine fire and damage to the
airplane.
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(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
(1) Within 800 flight hours (FHs) after
December 6, 2016 (the effective date of AD
2016–22–05), or before further flight,
whichever occurs later, and after that within
every 800 FHs accumulated on the fuel
nozzles, perform the following:
(i) Inspect all fuel nozzles, P/N 51J345, in
accordance with Part A of Pratt & Whitney
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16:25 Mar 27, 2019
Jkt 247001
Alert Service Bulletin (ASB) PW4G–100–
A73–45, dated February 16, 2016.
(ii) For any fuel nozzle that fails the
inspection, before further flight, remove and
replace with a part that is eligible for
installation.
(2) At the next shop visit or within 24
months after the effective date of this AD,
whichever occurs first, remove all fuel
nozzles, P/N 51J345, in accordance with Part
A, of Pratt & Whitney ASB PW4G–100–A73–
47, dated March 10, 2017, and replace with
parts eligible for installation.
(3) At the next shop visit or within 60
months after the effective date of this AD,
whichever comes first, replace the fuel
nozzle supply manifold assemblies and
install the new brackets and clamps on the
fuel nozzle supply manifold assembly in
accordance with Accomplishment
Instructions, ‘‘For Engines Installed on
Aircraft’’ or ‘‘For Engines Not Installed on
Aircraft,’’ of Pratt & Whitney SB PW4G–100–
73–48, Revision No. 1, dated April 24, 2018.
(h) Definitions
(1) For the purpose of this AD, an ‘‘engine
shop visit’’ is the induction of an engine into
the shop for maintenance involving the
separation of pairs of major mating engine
case flanges, except for the following
situations, which do not constitute an engine
shop visit:
(i) Separation of engine flanges solely for
the purposes of transportation of the engine
without subsequent maintenance.
(ii) Separation of engine flanges solely for
the purpose of replacing the fan or propulsor
without subsequent engine maintenance.
(2) For the purpose of this AD, a part that
is ‘‘eligible for installation’’ is a fuel nozzle
with a P/N other than 51J345 that is FAAapproved for installation.
(i) Terminating Action
Installation of the eligible fuel nozzles
constitutes terminating action for the
repetitive inspection requirements of
paragraph (g)(1) of this AD.
(j) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, ECO 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 manager of the certification office,
send it to the attention of the person
identified in paragraph (k) of this AD. You
may email your request to: ANE-AD-AMOC@
faa.gov.
(2) 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.
(k) Related Information
For more information about this AD,
contact Scott Hopper, Aerospace Engineer,
ECO Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone: 781–238–
7154; fax: 781–238–7199; email:
scott.hopper@faa.gov.
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(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 the AD specifies otherwise.
(3) The following service information was
approved for IBR on May 2, 2019.
(i) Pratt & Whitney Alert Service Bulletin
(ASB) PW4G–100–A73–47, dated March 10,
2017; and
(ii) Pratt & Whitney Service Bulletin
PW4G–100–73–48, Revision No. 1, dated
April 24, 2018.
(4) The following service information was
approved for IBR on December 6, 2016.
(i) Pratt & Whitney ASB PW4G–100–A73–
45, dated February 16, 2016.
(ii) [Reserved]
(5) For Pratt & Whitney service information
identified in this AD, contact Pratt & Whitney
Division, 400 Main St., East Hartford, CT
06108; phone: 860–565–8770; fax: 860–565–
4503.
(6) You may view this service information
at FAA, Engine and Propeller Standards
Branch, 1200 District Avenue, Burlington,
MA 01803. For information on the
availability of this material at the FAA, call
781–238–7759.
(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, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Burlington, Massachusetts, on
March 22, 2019.
Karen M. Grant,
Acting Manager, Engine and Propeller
Standards Branch, Aircraft Certification
Service.
[FR Doc. 2019–05905 Filed 3–27–19; 8:45 am]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2018–1010; Product
Identifier 2018–NM–148–AD; Amendment
39–19596; AD 2019–05–14]
RIN 2120–AA64
Airworthiness Directives; Dassault
Aviation Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; removal of
Airworthiness Directive (AD).
AGENCY:
We are removing AD 2012–
02–18, which applied to all Dassault
SUMMARY:
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Federal Register / Vol. 84, No. 60 / Thursday, March 28, 2019 / Rules and Regulations
Aviation Model MYSTERE–FALCON 50
airplanes. AD 2012–02–18 required
revising the maintenance program to
include revised airworthiness
limitations. We issued AD 2012–02–18
to address cracking of the flap tracks,
which could lead to flap asymmetry and
loss of control of the airplane. Since we
issued AD 2012–02–18, we have issued
AD 2017–09–03 to address the unsafe
condition. Accordingly, AD 2012–02–18
is removed.
DATES: This AD becomes effective
March 28, 2019.
ADDRESSES:
on the determination of the cost to the
public.
Examining the AD Docket
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.
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.
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2018–
1010; 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
regulatory evaluation, any comments
received, and other information. The
address for Docket Operations
(telephone 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:
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Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by removing AD 2012–02–18,
Amendment 39–16941 (77 FR 12175,
February 29, 2012) (‘‘AD 2012–02–18’’).
AD 2012–02–18 applied to all Dassault
Aviation Model MYSTERE–FALCON 50
airplanes. The NPRM published in the
Federal Register on December 28, 2018
(83 FR 67155). The NPRM was
prompted by a determination that AD
2012–02–18 is no longer necessary
because we have since issued AD 2017–
09–03, Amendment 39–18865 (82 FR
21467, May 9, 2017) to address the
unsafe condition. The NPRM proposed
to remove AD 2012–02–18. We are
issuing this AD to remove AD 2012–02–
18.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM or
VerDate Sep<11>2014
16:25 Mar 27, 2019
Jkt 247001
Conclusion
We reviewed the relevant data and
determined that air safety and the
public interest require adopting this AD
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.
Regulatory Findings
We determined that this AD will not
have federalism implications under
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the national government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979);
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11641
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
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
removing Airworthiness Directive (AD)
2012–02–18, Amendment 39–16941 (77
FR 12175, February 29, 2012), and
adding the following new AD:
■
2019–05–14 Dassault Aviation:
Amendment 39–19596; Docket No.
FAA–2018–1010; Product Identifier
2018–NM–148–AD.
(a) Effective Date
This AD becomes effective March 28, 2019.
(b) Affected ADs
This AD removes AD 2012–02–18,
Amendment 39–16941 (77 FR 12175,
February 29, 2012).
(c) Applicability
This AD applies to Dassault Aviation
Model MYSTERE–FALCON 50 airplanes, all
serial numbers, certificated in any category.
(d) Related Information
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.
Issued in Des Moines, Washington, on
March 18, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2019–05890 Filed 3–27–19; 8:45 am]
BILLING CODE 4910–13–P
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Agencies
[Federal Register Volume 84, Number 60 (Thursday, March 28, 2019)]
[Rules and Regulations]
[Pages 11640-11641]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-05890]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2018-1010; Product Identifier 2018-NM-148-AD; Amendment
39-19596; AD 2019-05-14]
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; removal of Airworthiness Directive (AD).
-----------------------------------------------------------------------
SUMMARY: We are removing AD 2012-02-18, which applied to all Dassault
[[Page 11641]]
Aviation Model MYSTERE-FALCON 50 airplanes. AD 2012-02-18 required
revising the maintenance program to include revised airworthiness
limitations. We issued AD 2012-02-18 to address cracking of the flap
tracks, which could lead to flap asymmetry and loss of control of the
airplane. Since we issued AD 2012-02-18, we have issued AD 2017-09-03
to address the unsafe condition. Accordingly, AD 2012-02-18 is removed.
DATES: This AD becomes effective March 28, 2019.
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-2018-
1010; 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 regulatory evaluation, any comments received, and other
information. The address for Docket Operations (telephone 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 removing AD 2012-02-18, Amendment 39-16941 (77 FR 12175,
February 29, 2012) (``AD 2012-02-18''). AD 2012-02-18 applied to all
Dassault Aviation Model MYSTERE-FALCON 50 airplanes. The NPRM published
in the Federal Register on December 28, 2018 (83 FR 67155). The NPRM
was prompted by a determination that AD 2012-02-18 is no longer
necessary because we have since issued AD 2017-09-03, Amendment 39-
18865 (82 FR 21467, May 9, 2017) to address the unsafe condition. The
NPRM proposed to remove AD 2012-02-18. We are issuing this AD to remove
AD 2012-02-18.
Comments
We gave the public the opportunity to participate in developing
this AD. 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 AD 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.
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.
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
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. 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 removing Airworthiness Directive (AD)
2012-02-18, Amendment 39-16941 (77 FR 12175, February 29, 2012), and
adding the following new AD:
2019-05-14 Dassault Aviation: Amendment 39-19596; Docket No. FAA-
2018-1010; Product Identifier 2018-NM-148-AD.
(a) Effective Date
This AD becomes effective March 28, 2019.
(b) Affected ADs
This AD removes AD 2012-02-18, Amendment 39-16941 (77 FR 12175,
February 29, 2012).
(c) Applicability
This AD applies to Dassault Aviation Model MYSTERE-FALCON 50
airplanes, all serial numbers, certificated in any category.
(d) Related Information
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.
Issued in Des Moines, Washington, on March 18, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-05890 Filed 3-27-19; 8:45 am]
BILLING CODE 4910-13-P