Airworthiness Directives; Reims Aviation S.A. Airplanes, 72252-72254 [2012-29395]
Download as PDF
72252
Federal Register / Vol. 77, No. 234 / Wednesday, December 5, 2012 / Proposed Rules
(i) Install the Fuel Return Line Assembly
If you find no evidence of damage of the
fuel return line assembly (Cessna P/N
0516031–1) as a result of the inspection
required by paragraph (g) of this AD, before
further flight, reinstall the fuel return line
assembly (Cessna P/N 0516031–1) following
Cessna Aircraft Company Service Bulletin
SEB–28–01, dated September 21, 2012.
(j) Install Forward and Aft Fuel Return Line
Support Clamps and Brackets
After installing the fuel return line
assembly as required by replacement in
paragraph (h) of this AD or installation in
paragraph (i) of this AD, before further flight,
install the forward and aft fuel return line
support clamps and brackets following
Cessna Aircraft Company Service Bulletin
SEB–28–01, dated September 21, 2012.
(k) Inspect for a Minimum Clearance
Between Certain Parts
After the installation required by paragraph
(j) of this AD, before further flight, inspect for
a minimum clearance between the following
parts throughout the range of copilot pedal
travel. The requirements of this AD take
precedence over the actions required in
Cessna Aircraft Company Service Bulletin
SEB–28–01, dated September 21, 2012:
(1) A minimum clearance of 0.5 inch
between the fuel return line assembly
(Cessna P/N 0516031–1) and the steering
tube assembly (Cessna P/N MC0543022–2C);
and
(2) Visible positive clearance between the
fuel return line assembly (Cessna P/N
0516031–1) and the airplane structure.
(l) Adjust Clearance for Fuel Return Line
Assembly
If you find any clearance less than the
minimum clearance required by paragraph
(k) of this AD, adjust to the minimum
clearance required by paragraph (k) of this
AD.
tkelley on DSK3SPTVN1PROD with
(n) Related Information
(1) For more information about this AD,
contact Jeff Janusz, Aerospace Engineer,
Wichita ACO, FAA, 1801 S. Airport Road,
Room 100, Wichita, Kansas 67209; phone:
(316) 946–4148; fax: (316) 946–4107; email:
jeff.janusz@faa.gov.
(2) For service information identified in
this AD, contact Cessna Aircraft Company,
16:40 Dec 04, 2012
Jkt 229001
Issued in Kansas City, Missouri, on
November 29, 2012.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. 2012–29402 Filed 12–4–12; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
• Hand Delivery: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE.,
Washington, DC 20590, between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays.
For service information identified in
this proposed AD, contact Reims
´
Aviation Industries, Aerodrome de
Reims Prunay, 51360 Prunay, France;
telephone + 33 3 26 48 46 65; fax + 33
3 26 49 18 57; email:
stephan.lapagne@reims-aviation.fr;
Internet: www.geciaviation.com/en/
f406.html. You may review copies of the
referenced service information at the
FAA, Small Airplane Directorate, 901
Locust, Kansas City, Missouri 64106.
For information on the availability of
this material at the FAA, call (816) 329–
4148.
14 CFR Part 39
Examining the AD Docket
[Docket No. FAA–2012–1274; Directorate
Identifier 2012–CE–042–AD]
You may examine the AD docket on
the Internet at https://
www.regulations.gov; 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 proposed AD, the
regulatory evaluation, any comments
received, and other information. The
street address for the Docket Office
(telephone (800) 647–5527) is in the
ADDRESSES section. Comments will be
available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT:
Albert Mercado, Aerospace Engineer,
FAA, Small Airplane Directorate, 901
Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329–
4119; fax: (816) 329–4090; email:
albert.mercado@faa.gov.
RIN 2120–AA64
Airworthiness Directives; Reims
Aviation S.A. Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
We propose to adopt a new
airworthiness directive (AD) for Reims
Aviation S.A. Model F406 airplanes.
This proposed AD results from
mandatory continuing airworthiness
information (MCAI) originated by an
aviation authority of another country to
identify and correct an unsafe condition
on an aviation product. The MCAI
describes the unsafe condition as
improper material used in nose landing
gear (NLG) attachment brackets which
could lead to failure of the NLG bracket
with consequent damage to the airplane
while landing. We are issuing this
proposed AD to require actions to
address the unsafe condition on these
products.
SUMMARY:
(m) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Wichita Aircraft
Certification Office (ACO), 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 ACO, send it to the
attention of the person identified in the
Related Information section of this AD.
(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.
VerDate Mar<15>2010
Customer service, P.O. Box 7706, Wichita, KS
67277; telephone: (316) 517–5800; fax: (316)
517–7271;
customercare@cessna.textron.com; Internet:
https://www.cessnasupport.com. You may
review copies of the referenced service
information at the FAA, Small Airplane
Directorate, 901 Locust, Kansas City, MO
64106. For information on the availability of
this material at the FAA, call (816) 329–4148.
We must receive comments on
this proposed AD by January 22, 2013.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: (202) 493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE.,
Washington, DC 20590.
DATES:
PO 00000
Frm 00008
Fmt 4702
Sfmt 4702
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written
relevant data, views, or arguments about
this proposed AD. Send your comments
to an address listed under the
ADDRESSES section. Include ‘‘Docket No.
FAA–2012–1274; Directorate Identifier
2012–CE–042–AD’’ at the beginning of
your comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of this proposed AD. We will
consider all comments received by the
closing date and may amend this
proposed AD because of those
comments.
We will post all comments we
receive, without change, to https://
regulations.gov, including any personal
information you provide. We will also
post a report summarizing each
E:\FR\FM\05DEP1.SGM
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Federal Register / Vol. 77, No. 234 / Wednesday, December 5, 2012 / Proposed Rules
substantive verbal contact we receive
about this proposed AD.
Discussion
The European Aviation Safety Agency
(EASA), which is the Technical Agent
for the Member States of the European
Community, has issued EASA AD No.:
2012–0202, dated October 1, 2012
(referred to after this as ‘‘the MCAI’’), to
correct an unsafe condition for the
specified products. The MCAI states:
During the manufacturing process, RAI
found that some of the nose landing gear
(NLG) attachment brackets, Part Number (P/
N) 6013119–1, were made of aluminum alloy,
instead of steel. The results of the
investigations showed that some of these
aluminum alloy brackets are likely to be
installed on aeroplanes currently in service.
This condition, if not detected and
corrected, could lead to failure of the NLG
attachment bracket and jamming of the NLG
extension/retraction mechanism, possibly
resulting in a runway excursion and
consequent damage to the aeroplane and
injury to the occupants.
For the reasons described above, this AD
requires inspection of the NLG attachment
bracket P/N 6013119–1 and, depending on
findings, replacement with a serviceable
bracket made of steel.
In addition, as some aluminum alloy P/N
6013119–1 NLG attachment brackets may
have been supplied as spares, this AD also
requires determination that the part is made
of steel, prior to installation.
You may obtain further information by
examining the MCAI in the AD docket.
Relevant Service Information
Reims Aviation S.A. has issued
Service Bulletin No. F406–74, dated
September 26, 2012. The actions
described in this service information are
intended to correct the unsafe condition
identified in the MCAI.
tkelley on DSK3SPTVN1PROD with
FAA’s Determination and Requirements
of the Proposed AD
This product has been approved by
the aviation authority of another
country, and is approved for operation
in the United States. Pursuant to our
bilateral agreement with this State of
Design Authority, they have notified us
of the unsafe condition described in the
MCAI and service information
referenced above. We are proposing this
AD because we evaluated all
information and determined the unsafe
condition exists and is likely to exist or
develop on other products of the same
type design.
Costs of Compliance
We estimate that this proposed AD
will affect 7 products of U.S. registry.
We also estimate that it would take
about .5 work-hour per product to
comply with the basic requirements of
VerDate Mar<15>2010
16:40 Dec 04, 2012
Jkt 229001
72253
this proposed AD. The average labor
rate is $85 per work-hour.
Based on these figures, we estimate
the cost of the proposed AD on U.S.
operators to be $42.50, or $297.50 per
product.
In addition, we estimate that any
necessary follow-on actions would take
about 3 work-hours and require parts
costing $500, for a cost of $755 per
product. We have no way of
determining the number of products
that may need these actions.
List of Subjects in 14 CFR Part 39
Authority for This Rulemaking
1. The authority citation for part 39
continues to read as follows:
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 proposed AD
would not have federalism implications
under Executive Order 13132. This
proposed AD would 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 this proposed regulation:
(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.
PO 00000
Frm 00009
Fmt 4702
Sfmt 4702
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
PART 39—AIRWORTHINESS
DIRECTIVES
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
Reims Aviation S.A.: Docket No. FAA–2012–
1274; Directorate Identifier 2012–CE–
042–AD.
(a) Comments Due Date
We must receive comments by January 22,
2013.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Reims Aviation S.A.
F406 airplanes, all serial numbers,
certificated in any category.
(d) Subject
Air Transport Association of America
(ATA) Code 32: Landing Gear.
(e) Reason
This AD was prompted by reports of
improper material used in nose landing gear
(NLG) attachment brackets which could lead
to failure of the NLG bracket with consequent
damage to the airplane while landing. We are
issuing this proposed AD to ensure the
proper NLG attachment bracket is installed.
(f) Actions and Compliance
Unless already done, do the following
actions following the instructions in Reims
Aviation S.A. Service Bulletin No. F406–74,
dated September 26, 2012:
(1) Within the next 25 hours time-inservice (TIS) after the effective date of this
AD or within the next 30 days after the
effective date of this AD, whichever occurs
first, inspect the nose landing gear (NLG)
attachment brackets, part number (P/N)
6013119–1, to verify if they are made of steel
and not aluminum alloy.
(2) If during the inspection required in
paragraph (f)(1) of this AD, you find that a
NLG attachment bracket made of aluminum
alloy is installed, before further flight,
replace with an airworthy steel NLG
attachment bracket, P/N 6013119–1.
(3) As of the effective date of this AD, do
not install any NLG attachment bracket P/N
6013119–1 that has not been confirmed to be
made of steel.
E:\FR\FM\05DEP1.SGM
05DEP1
72254
Federal Register / Vol. 77, No. 234 / Wednesday, December 5, 2012 / Proposed Rules
(g) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, Standards Office,
FAA, has the authority to approve AMOCs
for this AD, if requested using the procedures
found in 14 CFR 39.19. Send information to
ATTN: Albert Mercado, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4119; fax: (816) 329–
4090; email: albert.mercado@faa.gov. Before
using any approved AMOC on any airplane
to which the AMOC applies, notify your
appropriate principal inspector (PI) in the
FAA Flight Standards District Office (FSDO),
or lacking a PI, your local FSDO.
(2) Airworthy Product: For any requirement
in this AD to obtain corrective actions from
a manufacturer or other source, use these
actions if they are FAA-approved. Corrective
actions are considered FAA-approved if they
are approved by the State of Design Authority
(or their delegated agent). You are required
to assure the product is airworthy before it
is returned to service.
(3) Reporting Requirements: For any
reporting requirement in this AD, a federal
agency may not conduct or sponsor, and a
person is not required to respond to, nor
shall a person be subject to a penalty for
failure to comply with a collection of
information subject to the requirements of
the Paperwork Reduction Act unless that
collection of information displays a current
valid OMB Control Number. The OMB
Control Number for this information
collection is 2120–0056. Public reporting for
this collection of information is estimated to
be approximately 5 minutes per response,
including the time for reviewing instructions,
completing and reviewing the collection of
information. All responses to this collection
of information are mandatory. Comments
concerning the accuracy of this burden and
suggestions for reducing the burden should
be directed to the FAA at: 800 Independence
Ave. SW., Washington, DC 20591, Attn:
Information Collection Clearance Officer,
AES–200.
tkelley on DSK3SPTVN1PROD with
(h) Related Information
Refer to MCAI European Aviation Safety
Agency (EASA) AD No. 2012–0202, dated
October 1, 2012; and Reims Aviation S.A.
Service Bulletin No. F406–74, dated
September 26, 2012, for related information.
For service information related to this AD,
contact Reims Aviation Industries,
´
Aerodrome de Reims Prunay, 51360 Prunay,
France; telephone + 33 3 26 48 46 65; fax +
33 3 26 49 18 57; email:
stephan.lapagne@reims-aviation.fr; Internet:
www.geciaviation.com/en/f406.html. You
may review copies of the referenced service
information at the FAA, Small Airplane
Directorate, 901 Locust, Kansas City,
Missouri 64106. For information on the
availability of this material at the FAA, call
(816) 329–4148.
VerDate Mar<15>2010
16:40 Dec 04, 2012
Jkt 229001
Issued in Kansas City, Missouri, on
November 29, 2012.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. 2012–29395 Filed 12–4–12; 8:45 am]
Minority Business Development Agency.
David Hinson,
National Director.
[FR Doc. 2012–29431 Filed 12–4–12; 8:45 am]
BILLING CODE 3510–21–P
BILLING CODE 4910–13–P
DEPARTMENT OF COMMERCE
Minority Business Development
Agency
15 CFR Part 1400
DEPARTMENT OF HEALTH AND
HUMAN SERVICES
Food and Drug Administration
21 CFR Parts 500, 520, 522, 524, 529,
556, and 558
[Docket No. FDA–2012–N–1067]
[Docket No. 121130667–2667–01]
RIN 0910–AG17
Petition for Inclusion of the ArabAmerican Community in the Groups
Eligible for MBDA Services
Minority Business
Development Agency, Commerce.
ACTION: Notice of proposed rulemaking
and request for comments; amendment.
AGENCY:
The Minority Business
Development Agency (MBDA) publishes
this notice to extend the date on which
it plans to make its decision on a
petition from the American-Arab AntiDiscrimination Committee requesting
formal designation as a group eligible
for MBDA’s services from November 30,
2012 to March 1, 2013.
FOR FURTHER INFORMATION CONTACT: For
further information about this Notice,
contact Josephine Arnold, Minority
Business Development Agency, 1401
Constitution Avenue NW., Room 5053,
Washington, DC 20230, (202) 482–5461.
SUPPLEMENTARY INFORMATION: On May
30, 2012, the Minority Business
Development Agency (MBDA)
published a notice of proposed
rulemaking and request for comments
regarding a petition received on January
11, 2012 from the American-Arab AntiDiscrimination Committee (ADC)
requesting formal designation of ArabAmericans as a minority group that is
socially or economically disadvantaged
pursuant to 15 CFR part 1400. MBDA
has published several notices in the
Federal Register to extend the date for
making a decision on the merits of the
petition. On September 4, 2012, MBDA
published an amendment to extend the
deadline for the decision until
November 30, 2012. The Agency has
determined that an additional ninety
(90) day period for consideration of the
policy implications associated with the
petition is necessary. Therefore, the
Agency has determined that the time in
which it will make its decision on the
petition will be on or before March 1,
2013. This extension will not prejudice
the petitioner.
SUMMARY:
PO 00000
Frm 00010
Fmt 4702
Sfmt 4702
New Animal Drugs; Updating
Tolerances for Residues of New
Animal Drugs in Food
AGENCY:
Food and Drug Administration,
HHS.
ACTION:
Proposed rule.
The Food and Drug
Administration (FDA) is proposing to
revise the animal drug regulations
regarding tolerances for residues of
approved and conditionally approved
new animal drugs in food by
standardizing, simplifying, and
clarifying the determination standards
and codification style. In addition, we
are proposing to add definitions for key
terms. The purpose of the revision is to
enhance understanding of tolerance
determination and improve the
readability of the regulations.
DATES: Submit either electronic or
written comments by March 5, 2013.
See section VI of this document for the
proposed effective date of a final rule
based on this proposed rule.
ADDRESSES: You may submit comments,
identified by Docket No. FDA–2012–N–
1067 and RIN number 0910–AG17, by
any of the following methods:
SUMMARY:
Electronic Submissions
Submit electronic comments in the
following way:
• Federal eRulemaking Portal: https://
www.regulations.gov/. Follow the
instructions for submitting comments.
Written Submissions
Submit written submissions in the
following ways:
• Fax: 301–827–6870.
• Mail/Hand Delivery/Courier (for
paper or CD–ROM submissions):
Division of Dockets Management (HFA–
305), Food and Drug Administration,
5630 Fishers Lane, rm. 1061, Rockville,
MD 20852.
Instructions: All submissions received
must include the Agency name, Docket
E:\FR\FM\05DEP1.SGM
05DEP1
Agencies
[Federal Register Volume 77, Number 234 (Wednesday, December 5, 2012)]
[Proposed Rules]
[Pages 72252-72254]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2012-29395]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-1274; Directorate Identifier 2012-CE-042-AD]
RIN 2120-AA64
Airworthiness Directives; Reims Aviation S.A. Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: We propose to adopt a new airworthiness directive (AD) for
Reims Aviation S.A. Model F406 airplanes. This proposed AD results from
mandatory continuing airworthiness information (MCAI) originated by an
aviation authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe
condition as improper material used in nose landing gear (NLG)
attachment brackets which could lead to failure of the NLG bracket with
consequent damage to the airplane while landing. We are issuing this
proposed AD to require actions to address the unsafe condition on these
products.
DATES: We must receive comments on this proposed AD by January 22,
2013.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
Fax: (202) 493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
For service information identified in this proposed AD, contact
Reims Aviation Industries, A[eacute]rodrome de Reims Prunay, 51360
Prunay, France; telephone + 33 3 26 48 46 65; fax + 33 3 26 49 18 57;
email: stephan.lapagne@reims-aviation.fr; Internet:
www.geciaviation.com/en/f406.html. You may review copies of the
referenced service information at the FAA, Small Airplane Directorate,
901 Locust, Kansas City, Missouri 64106. For information on the
availability of this material at the FAA, call (816) 329-4148.
Examining the AD Docket
You may examine the AD docket on the Internet at https://www.regulations.gov; 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 proposed AD, the regulatory
evaluation, any comments received, and other information. The street
address for the Docket Office (telephone (800) 647-5527) is in the
ADDRESSES section. Comments will be available in the AD docket shortly
after receipt.
FOR FURTHER INFORMATION CONTACT: Albert Mercado, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090; email:
albert.mercado@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2012-1274;
Directorate Identifier 2012-CE-042-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of those comments.
We will post all comments we receive, without change, to https://regulations.gov, including any personal information you provide. We
will also post a report summarizing each
[[Page 72253]]
substantive verbal contact we receive about this proposed AD.
Discussion
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, has issued EASA
AD No.: 2012-0202, dated October 1, 2012 (referred to after this as
``the MCAI''), to correct an unsafe condition for the specified
products. The MCAI states:
During the manufacturing process, RAI found that some of the
nose landing gear (NLG) attachment brackets, Part Number (P/N)
6013119-1, were made of aluminum alloy, instead of steel. The
results of the investigations showed that some of these aluminum
alloy brackets are likely to be installed on aeroplanes currently in
service.
This condition, if not detected and corrected, could lead to
failure of the NLG attachment bracket and jamming of the NLG
extension/retraction mechanism, possibly resulting in a runway
excursion and consequent damage to the aeroplane and injury to the
occupants.
For the reasons described above, this AD requires inspection of
the NLG attachment bracket P/N 6013119-1 and, depending on findings,
replacement with a serviceable bracket made of steel.
In addition, as some aluminum alloy P/N 6013119-1 NLG attachment
brackets may have been supplied as spares, this AD also requires
determination that the part is made of steel, prior to installation.
You may obtain further information by examining the MCAI in the AD
docket.
Relevant Service Information
Reims Aviation S.A. has issued Service Bulletin No. F406-74, dated
September 26, 2012. The actions described in this service information
are intended to correct the unsafe condition identified in the MCAI.
FAA's Determination and Requirements of the Proposed AD
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with this State of Design Authority, they
have notified us of the unsafe condition described in the MCAI and
service information referenced above. We are proposing this AD because
we evaluated all information and determined the unsafe condition exists
and is likely to exist or develop on other products of the same type
design.
Costs of Compliance
We estimate that this proposed AD will affect 7 products of U.S.
registry. We also estimate that it would take about .5 work-hour per
product to comply with the basic requirements of this proposed AD. The
average labor rate is $85 per work-hour.
Based on these figures, we estimate the cost of the proposed AD on
U.S. operators to be $42.50, or $297.50 per product.
In addition, we estimate that any necessary follow-on actions would
take about 3 work-hours and require parts costing $500, for a cost of
$755 per product. We have no way of determining the number of products
that may need these actions.
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 proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed
regulation:
(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.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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.
Sec. 39.13 [Amended]
2. The FAA amends Sec. 39.13 by adding the following new AD:
Reims Aviation S.A.: Docket No. FAA-2012-1274; Directorate
Identifier 2012-CE-042-AD.
(a) Comments Due Date
We must receive comments by January 22, 2013.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Reims Aviation S.A. F406 airplanes, all
serial numbers, certificated in any category.
(d) Subject
Air Transport Association of America (ATA) Code 32: Landing
Gear.
(e) Reason
This AD was prompted by reports of improper material used in
nose landing gear (NLG) attachment brackets which could lead to
failure of the NLG bracket with consequent damage to the airplane
while landing. We are issuing this proposed AD to ensure the proper
NLG attachment bracket is installed.
(f) Actions and Compliance
Unless already done, do the following actions following the
instructions in Reims Aviation S.A. Service Bulletin No. F406-74,
dated September 26, 2012:
(1) Within the next 25 hours time-in-service (TIS) after the
effective date of this AD or within the next 30 days after the
effective date of this AD, whichever occurs first, inspect the nose
landing gear (NLG) attachment brackets, part number (P/N) 6013119-1,
to verify if they are made of steel and not aluminum alloy.
(2) If during the inspection required in paragraph (f)(1) of
this AD, you find that a NLG attachment bracket made of aluminum
alloy is installed, before further flight, replace with an airworthy
steel NLG attachment bracket, P/N 6013119-1.
(3) As of the effective date of this AD, do not install any NLG
attachment bracket P/N 6013119-1 that has not been confirmed to be
made of steel.
[[Page 72254]]
(g) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Office, FAA, has the authority to approve AMOCs for this
AD, if requested using the procedures found in 14 CFR 39.19. Send
information to ATTN: Albert Mercado, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4119; fax: (816) 329-4090; email:
albert.mercado@faa.gov. Before using any approved AMOC on any
airplane to which the AMOC applies, notify your appropriate
principal inspector (PI) in the FAA Flight Standards District Office
(FSDO), or lacking a PI, your local FSDO.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
(3) Reporting Requirements: For any reporting requirement in
this AD, a federal agency may not conduct or sponsor, and a person
is not required to respond to, nor shall a person be subject to a
penalty for failure to comply with a collection of information
subject to the requirements of the Paperwork Reduction Act unless
that collection of information displays a current valid OMB Control
Number. The OMB Control Number for this information collection is
2120-0056. Public reporting for this collection of information is
estimated to be approximately 5 minutes per response, including the
time for reviewing instructions, completing and reviewing the
collection of information. All responses to this collection of
information are mandatory. Comments concerning the accuracy of this
burden and suggestions for reducing the burden should be directed to
the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn:
Information Collection Clearance Officer, AES-200.
(h) Related Information
Refer to MCAI European Aviation Safety Agency (EASA) AD No.
2012-0202, dated October 1, 2012; and Reims Aviation S.A. Service
Bulletin No. F406-74, dated September 26, 2012, for related
information. For service information related to this AD, contact
Reims Aviation Industries, A[eacute]rodrome de Reims Prunay, 51360
Prunay, France; telephone + 33 3 26 48 46 65; fax + 33 3 26 49 18
57; email: stephan.lapagne@reims-aviation.fr; Internet:
www.geciaviation.com/en/f406.html. You may review copies of the
referenced service information at the FAA, Small Airplane
Directorate, 901 Locust, Kansas City, Missouri 64106. For
information on the availability of this material at the FAA, call
(816) 329-4148.
Issued in Kansas City, Missouri, on November 29, 2012.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2012-29395 Filed 12-4-12; 8:45 am]
BILLING CODE 4910-13-P