Airworthiness Directives; Dassault Aviation Airplanes, 74603-74605 [2014-29225]
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Federal Register / Vol. 79, No. 241 / Tuesday, December 16, 2014 / Rules and Regulations
(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.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair
required by this AD if it is approved by the
Boeing Commercial Airplanes Organization
Designation Authorization (ODA) that has
been authorized by the Manager, Seattle
ACO, to make those findings. For a repair
method to be approved, the repair must meet
the certification basis of the airplane, and the
approval must specifically refer to this AD.
(r) Related Information
(1) For more information about this AD,
contact Nenita Odesa, Aerospace Engineer,
Airframe Branch, ANM–120L, FAA, Los
Angeles Aircraft Certification Office, 3960
Paramount Boulevard, Lakewood, CA 90712–
4137; phone: (562) 627–5234; fax: (562) 627–
5210; email: nenita.odesa@faa.gov.
(2) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (s)(3) and (s)(4) of this AD.
(s) Material Incorporated by Reference
tkelley on DSK3SPTVN1PROD with RULES
(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.
(i) Boeing Service Bulletin 737–53–1058,
Revision 4, dated January 9, 2014.
(ii) Reserved.
(3) For service information identified in
this AD, contact Boeing Commercial
Airplanes, Attention: Data & Services
Management, P.O. Box 3707, MC 2H–65,
Seattle, WA 98124–2207; telephone 206–
544–5000, extension 1; fax 206–766–5680;
Internet https://www.myboeingfleet.com.
(4) You may view this service information
at FAA, Transport Airplane Directorate, 1601
Lind Avenue SW., Renton, WA. For
information on the availability of this
material at the FAA, call 425–227–1221.
(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 Renton, Washington, on
December 5, 2014.
Michael J. Kaszycki,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2014–29190 Filed 12–15–14; 8:45 am]
BILLING CODE 4910–13–P
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Jkt 235001
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2014–0566; Directorate
Identifier 2014–NM–041–AD; Amendment
39–18050; AD 2014–25–08]
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 certain
Dassault Aviation Model FALCON 2000
and FALCON 2000EX airplanes. This
AD was prompted by a design review,
which revealed that the forward
servicing compartment (FSC) is
configured with tie-down points. This
AD requires inspecting the FSC for
installed tie-down points, and removing
those tie-down points. We are issuing
this AD to detect and correct installed
tie-down points, which could lead to
inadvertent use of the FSC as a cargo
compartment, which could result in
damage to the structure of the airplane
or potential risk of fire.
DATES: This AD becomes effective
January 20, 2015.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of January 20, 2015.
ADDRESSES: You may examine the AD
docket on the Internet at https://www.
regulations.gov/#!docketDetail;D=FAA2014-0566; or in person at the Docket
Management Facility, U.S. Department
of Transportation, Docket Operations,
M–30, West Building Ground Floor,
Room W12–140, 1200 New Jersey
Avenue SE., Washington, DC.
For service information identified in
this AD, contact Dassault Falcon Jet,
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
Airplane Directorate, 1601 Lind Avenue
SW., Renton, WA. For information on
the availability of this material at the
FAA, call 425–227–1221.
FOR FURTHER INFORMATION CONTACT: Tom
Rodriguez, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA
98057–3356; telephone 425–227–1137;
fax 425- 227–1149.
SUMMARY:
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74603
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 certain Dassault Aviation
Model FALCON 2000 and FALCON
2000EX airplanes. The NPRM published
in the Federal Register on August 14,
2014 (79 FR 47592).
The European Aviation Safety Agency
(EASA), which is the Technical Agent
for the Member States of the European
Community, has issued EASA
Airworthiness Directive 2014–0027R1,
dated February 5, 2014 (referred to after
this as the Mandatory Continuing
Airworthiness Information, or ‘‘the
MCAI’’), to correct an unsafe condition
for certain Dassault Aviation Model
FALCON 2000 and FALCON 2000EX
airplanes. The MCAI states:
The Forward Servicing Compartment (FSC)
of the Falcon 2000 is an unpressurized
service compartment located between
fuselage frames 26 and 33. This compartment
is accessible from a lockable external door
located in the lower aft fuselage.
A design review has brought to light that
the compartment is configured with tie-down
points, which were used by operators to fix
loads (e.g. ski or golf bags) in that
compartment. However, the FSC has not been
designed and consequently demonstrated as
being compliant with cargo compartment
airworthiness requirements.
This condition, if not corrected, could lead
to inadvertent use of the FSC as [a] cargo
compartment, which could result in damage
to the structure of the aeroplane or potential
risk of fire.
To address this potential unsafe condition,
Dassault Aviation issued Service Bulletin
(SB) F2000–407 and SB F2000EX–289, as
applicable, which provide instructions for
removal of the tie-down points.
For the reasons described above, this
[EASA] AD requires removal of the tie-down
points from the FSC.
Note: Operators are also reminded about
the intended function of the FSC.
This [EASA] AD is revised to clarify the
AD Applicability and to correct the [type
certificate data sheet] TCDS Number.
Required actions include inspecting
for installed tie-down points. You may
examine the MCAI in the AD docket on
the Internet at https://www.regulations.
gov/#!documentDetail;D=FAA-20140566-0002.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM (79
FR 47592, August 14, 2014) or on the
determination of the cost to the public.
Conclusion
We reviewed the relevant data and
determined that air safety and the
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74604
Federal Register / Vol. 79, No. 241 / Tuesday, December 16, 2014 / Rules and Regulations
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 (79 FR
47592, August 14, 2014) for correcting
the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM (79 FR 47592,
August 14, 2014).
Costs of Compliance
We estimate that this AD affects 247
airplanes of U.S. registry.
We also estimate that it will take
about 2 work-hours per product to
comply with the basic requirements of
this AD. The average labor rate is $85
per work-hour. Required parts will cost
about $5 per product. Based on these
figures, we estimate the cost of this AD
on U.S. operators to be $43,225, or $175
per product.
According to the manufacturer, some
of the costs of this AD may be covered
under warranty, thereby reducing the
cost impact on affected individuals. We
do not control warranty coverage for
affected individuals. As a result, we
have included all costs in our cost
estimate.
tkelley on DSK3SPTVN1PROD with RULES
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.
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.
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16:25 Dec 15, 2014
Jkt 235001
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.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://www.regulations.
gov/#!docketDetail;D=FAA-2014-0566;
or in person at the Docket Management
Facility 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 street address for the
Docket Operations office (telephone
800–647–5527) is in the ADDRESSES
section.
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 adding
the following new airworthiness
directive (AD):
■
2014–25–08 Dassault Aviation:
Amendment 39–18050. Docket No.
FAA–2014–0566; Directorate Identifier
2014–NM–041–AD.
(a) Effective Date
This AD becomes effective January 20,
2015.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the Dassault Aviation
airplanes identified in paragraphs (c)(1) and
(c)(2) of this AD, certificated in any category.
(1) Dassault Aviation Model FALCON 2000
airplanes, having serial numbers (S/Ns) 1
through 231 inclusive.
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(2) Dassault Aviation Model FALCON
2000EX airplanes, having S/Ns 1 through 262
inclusive, and S/Ns 601 through 604
inclusive.
(d) Subject
Air Transport Association (ATA) of
America Code 25, Equipment/Furnishings.
(e) Reason
This AD was prompted by a design review,
which revealed that the forward servicing
compartment (FSC) is configured with tiedown points. We are issuing this AD to
detect and correct installed tie-down points,
which could lead to inadvertent use of the
FSC as a cargo compartment, which could
result in damage to the structure of the
airplane or potential risk of fire.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Inspection and Removal
(1) Within 440 flight hours or 9 months
after the effective date of this AD, whichever
occurs first, inspect the FSC for installed tiedown points, in accordance with the
Accomplishment Instructions of Dassault
Service Bulletin F2000–407, Revision 1,
dated January 29, 2014; or Dassault Service
Bulletin F2000EX–289, Revision 1, dated
January 29, 2014; as applicable.
(2) If it is determined from the inspection
required by paragraph (g)(1) of this AD that
tie-down points are installed, within the
compliance time specified in paragraph (g)(1)
of this AD, remove the tie-down points from
the FSC, in accordance with the
Accomplishment Instructions of Dassault
Service Bulletin F2000–407, Revision 1,
dated January 29, 2014; or Dassault Service
Bulletin F2000EX–289, Revision 1, dated
January 29, 2014; as applicable.
(h) Credit for Previous Actions
This paragraph provides credit for actions
required by paragraphs (g)(1) and (g)(2) of
this AD, if those actions were performed
before the effective date of this AD using
Dassault Service Bulletin F2000–407, dated
December 17, 2013; or Dassault Service
Bulletin F2000EX–289, dated December 17,
2013; which are not incorporated by
reference in this AD.
(i) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Branch, ANM–116, Transport Airplane
Directorate, 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 Branch, send it to ATTN:
Tom Rodriguez, Aerospace Engineer,
International Branch, ANM–116, Transport
Airplane Directorate, FAA, 1601 Lind
Avenue SW., Renton, WA 98057–3356;
telephone 425–227–1137; fax 425–227–1149.
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Federal Register / Vol. 79, No. 241 / Tuesday, December 16, 2014 / Rules and Regulations
Information may be emailed to: 9-ANM-116AMOC-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. The AMOC approval letter
must specifically reference this AD.
(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 Branch, ANM–
116, Transport Airplane Directorate, 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.
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA
Airworthiness Directive 2014–0027R1, dated
February 5, 2014, for related information.
This MCAI may be found in the AD docket
on the Internet at https://www.regulations.
gov/#!documentDetail;D=FAA-2014-05660002.
(2) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (k)(3) and (k)(4) of this AD.
(k) Material Incorporated by Reference
tkelley on DSK3SPTVN1PROD with RULES
(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) Dassault Service Bulletin F2000–407,
Revision 1, dated January 29, 2014.
(ii) Dassault Service Bulletin F2000EX–
289, Revision 1, dated January 29, 2014.
(3) For service information identified in
this AD, contact Dassault Falcon Jet, 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 Airplane Directorate,
1601 Lind Avenue SW., Renton, WA. For
information on the availability of this
material at the FAA, call 425–227–1221.
(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 Renton, Washington, on
December 5, 2014.
Michael Kaszycki,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2014–29225 Filed 12–15–14; 8:45 am]
BILLING CODE 4910–13–P
16:25 Dec 15, 2014
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2014–0448; Directorate
Identifier 2013–NM–055–AD; Amendment
39–18048; AD 2014–25–06]
RIN 2120–AA64
Airworthiness Directives; Airbus
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for all
Airbus Model A300 series airplanes;
Airbus Model A300 B4–600, B4–600R,
and F4–600R series airplanes, and
Model A300 C4–605R Variant F
airplanes (collectively called Model
A300–600 series airplanes); and Airbus
Model A310 series airplanes. This AD
was prompted by a report of early
ruptures on the levers of the nose
landing gear (NLG) sequence valve. This
AD requires a one-time inspection for
damage of the landing gear sequence
valve levers and pin shearing indicating
areas on the NLG and the main landing
gears (MLGs); and depending on
findings, replacing the sequence valve
and lever, or doing a one-time
inspection to detect interference
between control rods and sequence
valves and corrective actions if
necessary. We are issuing this AD to
detect and correct interference between
a landing gear leg and door, which
could result in failure of that landing
gear to extend and could damage the
airplane and injure occupants.
DATES: This AD becomes effective
January 20, 2015.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of January 20, 2015.
ADDRESSES: You may examine the AD
docket on the Internet at https://www.
regulations.gov/#!docketDetail;D=FAA2014-0448; or in person at the Docket
Management Facility, U.S. Department
of Transportation, Docket Operations,
M–30, West Building Ground Floor,
Room W12–140, 1200 New Jersey
Avenue SE., Washington, DC.
For service information identified in
this AD, contact Airbus SAS,
Airworthiness Office—EAW, 1 Rond
Point Maurice Bellonte, 31707 Blagnac
Cedex, France; telephone +33 5 61 93 36
96; fax +33 5 61 93 44 51; email
account.airworth-eas@airbus.com;
SUMMARY:
(j) Related Information
VerDate Sep<11>2014
DEPARTMENT OF TRANSPORTATION
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74605
Internet https://www.airbus.com. You
may view this referenced service
information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue
SW., Renton, WA. For information on
the availability of this material at the
FAA, call 425–227–1221.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA
98057–3356; telephone 425–227–2125;
fax 425–227–1149.
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 Airbus Model A300 series
airplanes; Airbus Model A300 B4–600,
B4–600R, and F4–600R series airplanes,
and Model A300 C4–605R Variant F
airplanes (collectively called Model
A300–600 series airplanes); and Airbus
Model A310 series airplanes. The NPRM
published in the Federal Register on
July 16, 2014 (79 FR 41459).
The European Aviation Safety Agency
(EASA), which is the Technical Agent
for the Member States of the European
Community, has issued EASA
Airworthiness Directive 2013–0058,
dated March 11, 2013 (referred to after
this as the Mandatory Continuing
Airworthiness Information, or ‘‘the
MCAI’’), to correct an unsafe condition
for all Airbus Model A300 series
airplanes; Airbus Model A300 B4–600,
B4–600R, and F4–600R series airplanes,
and Model A300 C4–605R Variant F
airplanes (collectively called Model
A300–600 series airplanes); and Airbus
Model A310 series airplanes. The MCAI
states:
Operators have reported five cases of early
ruptures on levers of the nose landing gear
(NLG) sequence valve.
Analysis showed that these fatigue
ruptures were due to an incorrect adjustment
of the mechanical links. As the design of the
main landing gear (MLG) sequence valve
lever is similar, there is sufficient reason to
assume that these parts are similarly affected
by fatigue.
This condition, if not detected and
corrected, could lead to interference between
landing gear leg and door and consequent
failure of the landing gear to extend, possibly
resulting in damage to the aeroplane and
injury to occupants.
For the reasons described above, this
[EASA] AD requires a one-time inspection of
the sequence valve control lever [for damage,
which could include cracking or
deformation], of the adjustment of the control
rod between doors and landing gear sequence
valve and depending on inspections results,
accomplishment of applicable corrective
actions.
E:\FR\FM\16DER1.SGM
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Agencies
[Federal Register Volume 79, Number 241 (Tuesday, December 16, 2014)]
[Rules and Regulations]
[Pages 74603-74605]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2014-29225]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2014-0566; Directorate Identifier 2014-NM-041-AD;
Amendment 39-18050; AD 2014-25-08]
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 certain
Dassault Aviation Model FALCON 2000 and FALCON 2000EX airplanes. This
AD was prompted by a design review, which revealed that the forward
servicing compartment (FSC) is configured with tie-down points. This AD
requires inspecting the FSC for installed tie-down points, and removing
those tie-down points. We are issuing this AD to detect and correct
installed tie-down points, which could lead to inadvertent use of the
FSC as a cargo compartment, which could result in damage to the
structure of the airplane or potential risk of fire.
DATES: This AD becomes effective January 20, 2015.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of January 20,
2015.
ADDRESSES: You may examine the AD docket on the Internet at https://www.regulations.gov/#!docketDetail;D=FAA-2014-0566; or in person at the
Docket Management Facility, U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC.
For service information identified in this AD, contact Dassault
Falcon Jet, 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 Airplane
Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the
availability of this material at the FAA, call 425-227-1221.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137;
fax 425- 227-1149.
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 certain Dassault Aviation
Model FALCON 2000 and FALCON 2000EX airplanes. The NPRM published in
the Federal Register on August 14, 2014 (79 FR 47592).
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, has issued EASA
Airworthiness Directive 2014-0027R1, dated February 5, 2014 (referred
to after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for certain Dassault
Aviation Model FALCON 2000 and FALCON 2000EX airplanes. The MCAI
states:
The Forward Servicing Compartment (FSC) of the Falcon 2000 is an
unpressurized service compartment located between fuselage frames 26
and 33. This compartment is accessible from a lockable external door
located in the lower aft fuselage.
A design review has brought to light that the compartment is
configured with tie-down points, which were used by operators to fix
loads (e.g. ski or golf bags) in that compartment. However, the FSC
has not been designed and consequently demonstrated as being
compliant with cargo compartment airworthiness requirements.
This condition, if not corrected, could lead to inadvertent use
of the FSC as [a] cargo compartment, which could result in damage to
the structure of the aeroplane or potential risk of fire.
To address this potential unsafe condition, Dassault Aviation
issued Service Bulletin (SB) F2000-407 and SB F2000EX-289, as
applicable, which provide instructions for removal of the tie-down
points.
For the reasons described above, this [EASA] AD requires removal
of the tie-down points from the FSC.
Note: Operators are also reminded about the intended function of
the FSC.
This [EASA] AD is revised to clarify the AD Applicability and to
correct the [type certificate data sheet] TCDS Number.
Required actions include inspecting for installed tie-down points.
You may examine the MCAI in the AD docket on the Internet at https://www.regulations.gov/#!documentDetail;D=FAA-2014-0566-0002.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (79 FR 47592, August 14,
2014) or on the determination of the cost to the public.
Conclusion
We reviewed the relevant data and determined that air safety and
the
[[Page 74604]]
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 (79 FR 47592, August 14, 2014) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM (79 FR 47592, August 14, 2014).
Costs of Compliance
We estimate that this AD affects 247 airplanes of U.S. registry.
We also estimate that it will take about 2 work-hours per product
to comply with the basic requirements of this AD. The average labor
rate is $85 per work-hour. Required parts will cost about $5 per
product. Based on these figures, we estimate the cost of this AD on
U.S. operators to be $43,225, or $175 per product.
According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all costs in our cost
estimate.
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.
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.
Examining the AD Docket
You may examine the AD docket on the Internet at https://www.regulations.gov/#!docketDetail;D=FAA-2014-0566; or in person at the
Docket Management Facility 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 street address for the Docket Operations office (telephone 800-647-
5527) is in the ADDRESSES section.
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):
2014-25-08 Dassault Aviation: Amendment 39-18050. Docket No. FAA-
2014-0566; Directorate Identifier 2014-NM-041-AD.
(a) Effective Date
This AD becomes effective January 20, 2015.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the Dassault Aviation airplanes identified in
paragraphs (c)(1) and (c)(2) of this AD, certificated in any
category.
(1) Dassault Aviation Model FALCON 2000 airplanes, having serial
numbers (S/Ns) 1 through 231 inclusive.
(2) Dassault Aviation Model FALCON 2000EX airplanes, having S/Ns
1 through 262 inclusive, and S/Ns 601 through 604 inclusive.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
Furnishings.
(e) Reason
This AD was prompted by a design review, which revealed that the
forward servicing compartment (FSC) is configured with tie-down
points. We are issuing this AD to detect and correct installed tie-
down points, which could lead to inadvertent use of the FSC as a
cargo compartment, which could result in damage to the structure of
the airplane or potential risk of fire.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Inspection and Removal
(1) Within 440 flight hours or 9 months after the effective date
of this AD, whichever occurs first, inspect the FSC for installed
tie-down points, in accordance with the Accomplishment Instructions
of Dassault Service Bulletin F2000-407, Revision 1, dated January
29, 2014; or Dassault Service Bulletin F2000EX-289, Revision 1,
dated January 29, 2014; as applicable.
(2) If it is determined from the inspection required by
paragraph (g)(1) of this AD that tie-down points are installed,
within the compliance time specified in paragraph (g)(1) of this AD,
remove the tie-down points from the FSC, in accordance with the
Accomplishment Instructions of Dassault Service Bulletin F2000-407,
Revision 1, dated January 29, 2014; or Dassault Service Bulletin
F2000EX-289, Revision 1, dated January 29, 2014; as applicable.
(h) Credit for Previous Actions
This paragraph provides credit for actions required by
paragraphs (g)(1) and (g)(2) of this AD, if those actions were
performed before the effective date of this AD using Dassault
Service Bulletin F2000-407, dated December 17, 2013; or Dassault
Service Bulletin F2000EX-289, dated December 17, 2013; which are not
incorporated by reference in this AD.
(i) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, 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 Branch, send it to ATTN: Tom
Rodriguez, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
WA 98057-3356; telephone 425-227-1137; fax 425-227-1149.
[[Page 74605]]
Information may be emailed to: 9-ANM-116-AMOC-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. The AMOC approval letter must specifically reference this
AD.
(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
Branch, ANM-116, Transport Airplane Directorate, 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.
(j) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2014-0027R1, dated February 5,
2014, for related information. This MCAI may be found in the AD
docket on the Internet at https://www.regulations.gov/#!documentDetail;D=FAA-2014-0566-0002.
(2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (k)(3) and (k)(4) of this AD.
(k) 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) Dassault Service Bulletin F2000-407, Revision 1, dated
January 29, 2014.
(ii) Dassault Service Bulletin F2000EX-289, Revision 1, dated
January 29, 2014.
(3) For service information identified in this AD, contact
Dassault Falcon Jet, 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
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
(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 Renton, Washington, on December 5, 2014.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2014-29225 Filed 12-15-14; 8:45 am]
BILLING CODE 4910-13-P