Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-500 Airplanes, 444-446 [2010-32809]
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444
Federal Register / Vol. 76, No. 3 / Wednesday, January 5, 2011 / Rules and Regulations
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.
Related Information
(i) Refer to MCAI European Aviation Safety
Agency Emergency Airworthiness Directive
2010–0239–E, dated November 19, 2010
[Corrected November 23, 2010]; and Airbus
A300–600 AOT 27A6068, Revision 01, dated
November 18, 2010; for related information.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2010–1023 Directorate
Identifier 2010–CE–055–AD; Amendment
39–16557; AD 2011–01–04]
RIN 2120–AA64
Airworthiness Directives; Empresa
Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB–500 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for the
products listed above. This AD results
from mandatory continuing
airworthiness information (MCAI)
issued 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:
fax: ++55 12 3927–2610; E-mail:
reliability.executive@embraer.com.br;
Internet: https://www.embraer.com.br.
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.
FOR FURTHER INFORMATION CONTACT: Jim
Rutherford, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4165; fax: (816)
329–4090.
SUPPLEMENTARY INFORMATION:
Discussion
Material Incorporated by Reference
SUMMARY:
(j) You must use Airbus A300–600 All
Operators Telex 27A6068, Revision 01, dated
November 18, 2010, to do the actions
required by this AD, unless the AD specifies
otherwise.
(1) The Director of the Federal Register
approved the incorporation by reference of
this service information under 5 U.S.C.
552(a) and 1 CFR part 51.
(2) For service information identified in
this AD, contact Airbus SAS—EAW
(Airworthiness Office), 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France;
telephone +33 5 61 93 36 96; fax +33 5 61
93 44 51; e-mail: account.airwortheas@airbus.com; Internet https://
www.airbus.com.
(3) You may review copies of the service
information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the
availability of this material at the FAA, call
425–227–1221.
(4) You may also review copies of the
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/
code_of_federal_regulations/
ibr_locations.html.
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to the specified products. That
NPRM was published in the Federal
Register on October 15, 2010 (75 FR
63422). That NPRM proposed to correct
an unsafe condition for the specified
products. The MCAI states:
It has been detected a short circuit in
harness W101 due to its interference with the
main door mechanism. Further analysis of
the affected region has also revealed the
possibility of chafing between the same
harness and the oxygen tubing. The chafing
of the wiring harness against the oxygen
tubing could lead to a short circuit of the
wiring harness and a subsequent fire in the
airplane.
Since this condition may occur in other
airplanes of the same type and affects flight
safety, a corrective action is required. Thus,
sufficient reason exists to request compliance
with this AD in the indicated time limit.
It has been detected a short circuit in
harness W101 due to its interference with the
main door mechanism. Further analysis of
the affected region has also revealed the
possibility of chafing between the same
harness and the oxygen tubing. The chafing
of the wiring harness against the oxygen
tubing could lead to a short circuit of the
wiring harness and a subsequent fire in the
airplane.
Since this condition may occur in other
airplanes of the same type and affects flight
safety, a corrective action is required. Thus,
sufficient reason exists to request compliance
with this AD in the indicated time limit.
We are issuing this AD to require
actions to correct the unsafe condition
on these products.
DATES: This AD becomes effective
February 9, 2011.
On February 9, 2011, the Director of
the Federal Register approved the
incorporation by reference of certain
publications listed in this AD.
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov or in person at
Document 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 20590.
For service information identified in
this AD, contact EMBRAER Empresa
´
Brasileira de Aeronautica S.A., Phenom
Maintenance Support, Av. Brig. Farina
Lima, 2170, Sao Jose dos Campos—SP,
CEP: 12227–901—PO Box: 38/2,
BRASIL, telephone: ++55 12 3927–5383;
The MCAI requires installing clamps to
the W101 wiring harness.
Issued in Renton, Washington, on
December 22, 2010.
Jeffrey E. Duven,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2010–32995 Filed 1–4–11; 8:45 am]
WReier-Aviles on DSKGBLS3C1PROD with RULES
BILLING CODE 4910–13–P
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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 available data and
determined that air safety and the
public interest require adopting the AD
as proposed.
Differences Between This AD and the
MCAI or Service Information
We have reviewed the MCAI and
related service information and, in
general, agree with their substance. But
we might have found it necessary to use
different words from those in the MCAI
to ensure the AD is clear for U.S.
operators and is enforceable. In making
these changes, we do not intend to differ
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05JAR1
Federal Register / Vol. 76, No. 3 / Wednesday, January 5, 2011 / Rules and Regulations
substantively from the information
provided in the MCAI and related
service information.
We might also have required different
actions in this AD from those in the
MCAI in order to follow FAA policies.
Any such differences are highlighted in
a Note within the AD.
Costs of Compliance
We estimate that this AD will affect
83 products of U.S. registry. We also
estimate that it will take about 12 workhours 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 $13 per
product.
Based on these figures, we estimate
the cost of this AD to the U.S. operators
to be $85,739 or $1,033 per product.
Authority for This Rulemaking
WReier-Aviles on DSKGBLS3C1PROD with RULES
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 this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
(2) Is not a ‘‘significant rule’’ under
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
(3) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
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15:20 Jan 04, 2011
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We prepared a regulatory evaluation
of the estimated costs to comply with
this AD and placed it in the AD Docket.
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 the NPRM, 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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
445
harness and the oxygen tubing. The chafing
of the wiring harness against the oxygen
tubing could lead to a short circuit of the
wiring harness and a subsequent fire in the
airplane.
Since this condition may occur in other
airplanes of the same type and affects flight
safety, a corrective action is required. Thus,
sufficient reason exists to request compliance
with this AD in the indicated time limit.
The MCAI requires installing clamps to the
W101 wiring harness.
Actions and Compliance
(f) Unless already done, within 600 hours
time-in-service (TIS) after February 9, 2011
(the effective date of this AD) or within 12
months after February 9, 2011 (the effective
date of this AD), whichever comes first,
install clamps and protection sleeves to
harness W101 within the cockpit area and
rework structures to eliminate the fretting
spots of the harness with the main door
locking mechanism and with the oxygen
tube. Do the installation following Empresa
´
Brasileira de Aeronautica S.A. (EMBRAER)
Service Bulletin No. SB 500–24–0002, dated
March 8, 2010.
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
FAA AD Differences
PART 39—AIRWORTHINESS
DIRECTIVES
Other FAA AD Provisions
(g) 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: Jim Rutherford, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4165; fax: (816) 329–
4090. 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 FAAapproved 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,
■
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 AD:
■
2011–01–04 Empresa Brasileira de
Aeronautica S.A. (EMBRAER):
Amendment 39–16557; Docket No.
FAA–2010–1023; Directorate Identifier
2010–CE–055–AD.
Effective Date
(a) This airworthiness directive (AD)
becomes effective February 9, 2011.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Empresa Brasileira
de Aeronautica S.A. (EMBRAER) Model
EMB–500 airplanes, serial numbers 50000005
thru 50000105, certificated in any category.
Subject
(d) Air Transport Association of America
(ATA) Code 92: Wiring Elements.
Reason
(e) The mandatory continuing
airworthiness information (MCAI) states:
It has been detected a short circuit in
harness W101 due to its interference with the
main door mechanism. Further analysis of
the affected region has also revealed the
possibility of chafing between the same
PO 00000
Frm 00027
Fmt 4700
Sfmt 4700
Note: This AD differs from the MCAI
and/or service information as follows: No
differences.
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05JAR1
446
Federal Register / Vol. 76, No. 3 / Wednesday, January 5, 2011 / Rules and Regulations
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.
Related Information
ˆ
(h) Refer to MCAI AGENCIA NACIONAL
DE AVIACAO CIVIL—BRAZIL (ANAC), AD
¸˜
No.: 2010–09–02, dated October 17, 2010;
´
and Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Service Bulletin No. SB 500–24–
0002, dated March 8, 2010, for related
information.
Material Incorporated by Reference
(i) You must use Empresa Brasileira de
´
Aeronautica S.A. (EMBRAER) Service
Bulletin No. SB 500–24–0002, dated March 8,
2010, to do the actions required by this AD,
unless the AD specifies otherwise.
(1) The Director of the Federal Register
approved the incorporation by reference of
this service information under 5 U.S.C.
552(a) and 1 CFR part 51.
(2) For service information identified in
this AD, contact EMBRAER Empresa
´
Brasileira de Aeronautica S.A., Phenom
Maintenance Support, Av. Brig. Farina Lima,
2170, Sao Jose dos Campos—SP, CEP: 12227–
901—PO Box: 38/2, BRASIL, telephone: ++55
12 3927–5383; fax: ++55 12 3927–2610; Email: reliability.executive@embraer.com.br;
Internet: https://www.embraer.com.br.
(3) 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.
(4) You may also review copies of the
service information incorporated by reference
for this AD 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/
code_of_federal_regulations/
ibr_locations.html.
Issued in Kansas City, Missouri, on
December 21, 2010.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. 2010–32809 Filed 1–4–11; 8:45 am]
WReier-Aviles on DSKGBLS3C1PROD with RULES
BILLING CODE 4910–13–P
SOCIAL SECURITY ADMINISTRATION
20 CFR Part 416
[Docket No. SSA–2008–0050]
RIN 0960–AE59
Supplemental Security Income (SSI)
for the Aged, Blind, and Disabled;
Dedicated Accounts and Installment
Payments for Certain Past-Due SSI
Benefits
AGENCY:
Social Security Administration
(SSA).
ACTION:
Final rules.
These final rules adopt, with
some minor changes, the interim final
rules with request for comment we
published in the Federal Register on
December 20, 1996. 61 FR 67203. The
interim final rules concerned dedicated
accounts and installment payments for
certain past-due SSI benefits and
reflected amendments to the Social
Security Act (Act) made by sections 213
and 221 of the Personal Responsibility
and Work Opportunity Reconciliation
Act of 1996 (PRWORA). These final
rules reflect these provisions, as well as
subsequent changes to these provisions
made by the Balanced Budget Act of
1997 (BBA), the Social Security
Protection Act of 2004 (SSPA), and the
Deficit Reduction Act of 2005 (DRA).
The changes we are making in these
final rules will ensure that our rules
accurately reflect the statutory
provisions on which they are based.
DATES: These final rules are effective
February 4, 2011.
FOR FURTHER INFORMATION CONTACT:
Brian Rudick, Office of Regulations,
Social Security Administration, 6401
Security Boulevard, Baltimore, MD
21235–6401, (410) 965–7102. For
information on eligibility or filing for
benefits, call our national toll-free
number, 1–800–772–1213 or TTY
1–800–325–0778, or visit our Internet
site, Social Security Online, at https://
www.socialsecurity.gov.
SUPPLEMENTARY INFORMATION:
SUMMARY:
Electronic Version
The electronic file of this document is
available on the date of publication in
the Federal Register at https://
www.gpoaccess.gov/fr/.
Background
The interim final rules reflected the
dedicated account requirements that
were added by section 213 of the
PRWORA. Public Law 104–193.
Congress enacted the PRWORA on
August 22, 1996. Section 213 of the
PRWORA added a new section
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15:20 Jan 04, 2011
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1631(a)(2)(F) of the Act for payments
made after August 22, 1996. Under
section 1631(a)(2)(F) of the Act, the
representative payee of an eligible
person under age 18 must establish in
certain situations ‘‘an account in a
financial institution,’’ which we refer to
as a ‘‘dedicated account.’’ Specifically,
the representative payee must establish
a dedicated account if the person is
eligible for past-due monthly SSI
benefits, including any federally
administered State supplementary
payments, that exceed 6 times the
maximum ‘‘monthly benefit payable’’
under title XVI, which we call the
Federal benefit rate (FBR), after any
withholding for interim assistance
reimbursement (IAR) to a State(s) and
after payment of attorney fees. Under
section 1631(a)(2)(F) of the Act, the
past-due benefits in a dedicated account
may only be used for certain allowable
expenses.
Sections 213(b) and (c) of the
PRWORA also amended sections
1613(a) and 1612(b) of the Act,
respectively, to provide that funds in a
dedicated account, established and
maintained in accordance with section
1631(a)(2)(F) of the Act, including
accrued interest or other earnings, are
excluded from resources and from
income.
Since we published the interim final
rules, Congress has enacted three other
laws that made additional changes to
the dedicated account requirements. We
are including these statutory changes in
the final rules without requesting public
comment because the changes are
required by statute and we are making
no discretionary policy changes.
The BBA made one clarification and
one revision to section 1631(a)(2)(F) of
the Act. Public Law 105–33. Section
5522(b)(2) of the BBA amended section
1631(a)(2)(F)(iii) of the Act by clarifying
which subsequent past-due benefits a
representative payee may deposit in an
established dedicated account. Congress
made this technical change to the
statute because the PRWORA used the
two different terms ‘‘underpayment’’ and
‘‘past-due benefits’’ to describe funds
that could be deposited in these
accounts. This terminology caused
confusion. Section 5522(b)(2) of the
BBA corrected this technical issue, and
we are including this change in these
final rules. As amended by section
5522(b)(2) of the BBA, section
1631(a)(2)(F)(iii) of the Act states that
the representative payee may deposit
into an established dedicated account
any other funds representing past-due
benefits under title XVI of the Act
which equal or exceed the maximum
monthly FBR, including any federally
E:\FR\FM\05JAR1.SGM
05JAR1
Agencies
[Federal Register Volume 76, Number 3 (Wednesday, January 5, 2011)]
[Rules and Regulations]
[Pages 444-446]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-32809]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-1023 Directorate Identifier 2010-CE-055-AD;
Amendment 39-16557; AD 2011-01-04]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB-500 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. This AD results from mandatory continuing
airworthiness information (MCAI) issued 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:
It has been detected a short circuit in harness W101 due to its
interference with the main door mechanism. Further analysis of the
affected region has also revealed the possibility of chafing between
the same harness and the oxygen tubing. The chafing of the wiring
harness against the oxygen tubing could lead to a short circuit of
the wiring harness and a subsequent fire in the airplane.
Since this condition may occur in other airplanes of the same
type and affects flight safety, a corrective action is required.
Thus, sufficient reason exists to request compliance with this AD in
the indicated time limit.
We are issuing this AD to require actions to correct the unsafe
condition on these products.
DATES: This AD becomes effective February 9, 2011.
On February 9, 2011, the Director of the Federal Register approved
the incorporation by reference of certain publications listed in this
AD.
ADDRESSES: You may examine the AD docket on the Internet at https://www.regulations.gov or in person at Document 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
20590.
For service information identified in this AD, contact EMBRAER
Empresa Brasileira de Aeron[aacute]utica S.A., Phenom Maintenance
Support, Av. Brig. Farina Lima, 2170, Sao Jose dos Campos--SP, CEP:
12227-901--PO Box: 38/2, BRASIL, telephone: ++55 12 3927-5383; fax:
++55 12 3927-2610; E-mail: reliability.executive@embraer.com.br;
Internet: https://www.embraer.com.br. 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.
FOR FURTHER INFORMATION CONTACT: Jim Rutherford, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4165; fax: (816) 329-4090.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on October 15, 2010 (75
FR 63422). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
It has been detected a short circuit in harness W101 due to its
interference with the main door mechanism. Further analysis of the
affected region has also revealed the possibility of chafing between
the same harness and the oxygen tubing. The chafing of the wiring
harness against the oxygen tubing could lead to a short circuit of
the wiring harness and a subsequent fire in the airplane.
Since this condition may occur in other airplanes of the same
type and affects flight safety, a corrective action is required.
Thus, sufficient reason exists to request compliance with this AD in
the indicated time limit.
The MCAI requires installing clamps to the W101 wiring harness.
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 available data and determined that air safety and
the public interest require adopting the AD as proposed.
Differences Between This AD and the MCAI or Service Information
We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable. In making these
changes, we do not intend to differ
[[Page 445]]
substantively from the information provided in the MCAI and related
service information.
We might also have required different actions in this AD from those
in the MCAI in order to follow FAA policies. Any such differences are
highlighted in a Note within the AD.
Costs of Compliance
We estimate that this AD will affect 83 products of U.S. registry.
We also estimate that it will take about 12 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 $13 per product.
Based on these figures, we estimate the cost of this AD to the U.S.
operators to be $85,739 or $1,033 per product.
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 this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866;
(2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD Docket.
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 the NPRM, 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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
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 AD:
2011-01-04 Empresa Brasileira de Aeronautica S.A. (EMBRAER):
Amendment 39-16557; Docket No. FAA-2010-1023; Directorate Identifier
2010-CE-055-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective February
9, 2011.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB-500 airplanes, serial numbers 50000005 thru
50000105, certificated in any category.
Subject
(d) Air Transport Association of America (ATA) Code 92: Wiring
Elements.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
It has been detected a short circuit in harness W101 due to its
interference with the main door mechanism. Further analysis of the
affected region has also revealed the possibility of chafing between
the same harness and the oxygen tubing. The chafing of the wiring
harness against the oxygen tubing could lead to a short circuit of
the wiring harness and a subsequent fire in the airplane.
Since this condition may occur in other airplanes of the same
type and affects flight safety, a corrective action is required.
Thus, sufficient reason exists to request compliance with this AD in
the indicated time limit.
The MCAI requires installing clamps to the W101 wiring harness.
Actions and Compliance
(f) Unless already done, within 600 hours time-in-service (TIS)
after February 9, 2011 (the effective date of this AD) or within 12
months after February 9, 2011 (the effective date of this AD),
whichever comes first, install clamps and protection sleeves to
harness W101 within the cockpit area and rework structures to
eliminate the fretting spots of the harness with the main door
locking mechanism and with the oxygen tube. Do the installation
following Empresa Brasileira de Aeron[aacute]utica S.A. (EMBRAER)
Service Bulletin No. SB 500-24-0002, dated March 8, 2010.
FAA AD Differences
Note: This AD differs from the MCAI and/or service information
as follows: No differences.
Other FAA AD Provisions
(g) 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: Jim Rutherford, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4165; fax: (816) 329-4090. 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,
[[Page 446]]
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.
Related Information
(h) Refer to MCAI AG[Ecirc]NCIA NACIONAL DE
AVIA[Ccedil][Atilde]O CIVIL--BRAZIL (ANAC), AD No.: 2010-09-02,
dated October 17, 2010; and Empresa Brasileira de Aeron[aacute]utica
S.A. (EMBRAER) Service Bulletin No. SB 500-24-0002, dated March 8,
2010, for related information.
Material Incorporated by Reference
(i) You must use Empresa Brasileira de Aeron[aacute]utica S.A.
(EMBRAER) Service Bulletin No. SB 500-24-0002, dated March 8, 2010,
to do the actions required by this AD, unless the AD specifies
otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact
EMBRAER Empresa Brasileira de Aeron[aacute]utica S.A., Phenom
Maintenance Support, Av. Brig. Farina Lima, 2170, Sao Jose dos
Campos--SP, CEP: 12227-901--PO Box: 38/2, BRASIL, telephone: ++55 12
3927-5383; fax: ++55 12 3927-2610; E-mail:
reliability.executive@embraer.com.br; Internet: https://www.embraer.com.br.
(3) 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.
(4) You may also review copies of the service information
incorporated by reference for this AD 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/code_of_federal_regulations/ibr_locations.html.
Issued in Kansas City, Missouri, on December 21, 2010.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2010-32809 Filed 1-4-11; 8:45 am]
BILLING CODE 4910-13-P