Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes, 5626-5627 [E6-1420]
Download as PDF
5626
Federal Register / Vol. 71, No. 22 / Thursday, February 2, 2006 / Proposed Rules
(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 an
Authorized Representative for the Boeing
Commercial Airplanes Delegation Option
Authorization Organization who 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.
p.m., Monday through Friday, except
Federal holidays. The Docket
Management Facility office (telephone
(800) 647–5227) is located on the plaza
level of the Nassif Building at the DOT
street address stated in the ADDRESSES
section. Comments will be available in
the AD docket shortly after the Docket
Management System receives them.
[Docket No. FAA–2006–23739; Directorate
Identifier 2005–NM–240–AD]
and follow the instructions for sending
your comments electronically.
• Mail: Docket Management Facility,
U.S. Department of Transportation, 400
Seventh Street SW., Nassif Building,
room PL–401, Washington, DC 20590.
• Fax: (202) 493–2251.
• Hand Delivery: Room PL–401 on
the plaza level of the Nassif Building,
400 Seventh Street, SW., Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
Contact Empresa Brasileira de
Aeronautica S.A. (EMBRAER), P.O. Box
343—CEP 12.225, Sao Jose dos
Campos—SP, Brazil, for service
information identified in this proposed
AD.
FOR FURTHER INFORMATION CONTACT:
Todd Thompson, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–1175;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
RIN 2120–AA64
Comments Invited
Airworthiness Directives; Empresa
Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB–145, –145ER,
–145MR, –145LR, –145XR, –145MP, and
–145EP Airplanes
We invite you to submit any relevant
written data, views, or arguments
regarding this proposed AD. Send your
comments to an address listed in the
ADDRESSES section. Include the docket
number ‘‘FAA–2006–23739; Directorate
Identifier 2005–NM–240–AD’’ at the
beginning of your comments. We
specifically invite comments on the
overall regulatory, economic,
environmental, and energy aspects of
the proposed AD. We will consider all
comments received by the closing date
and may amend the proposed AD in
light of those comments.
We will post all comments we
receive, without change, to https://
dms.dot.gov, including any personal
information you provide. We will also
post a report summarizing each
substantive verbal contact with FAA
personnel concerning this proposed AD.
Using the search function of that web
site, anyone can find and read the
comments in any of our dockets,
including the name of the individual
who sent the comment (or signed the
comment on behalf of an association,
business, labor union, etc.). You may
review the DOT’s complete Privacy Act
Statement in the Federal Register
published on April 11, 2000 (65 FR
19477–78), or you may visit https://
dms.dot.gov.
EMBRAER has issued Service Bulletin
145–71–0008, Change 01, dated July 24,
2001. The service bulletin describes
procedures for modifying the routing of
wire harness W407 near the fire
extinguishing tube in the rear part of the
left-hand and right-hand engines, and
installing new supports for derivations
of wire harness W407 that lead to
certain connectors. Accomplishing the
actions specified in the service
information is intended to adequately
address the unsafe condition. The DAC
mandated the service information and
issued Brazilian airworthiness directive
2005–10–05, dated November 17, 2005,
to ensure the continued airworthiness of
these airplanes in Brazil.
Issued in Renton, Washington, on January
26, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E6–1419 Filed 2–1–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM).
hsrobinson on PROD1PC71 with PROPOSALS
AGENCY:
SUMMARY: The FAA proposes to adopt a
new airworthiness directive (AD) for
certain EMBRAER Model EMB–145,
–145ER, –145MR, –145LR, –145XR,
–145MP, and –145EP airplanes. This
proposed AD would require modifying
the routing of wire harness W407 near
the fire extinguishing tube in the area of
each engine, and installing new
supports for related wiring. This
proposed AD results from reports of
chafing of wire harness W407 against
the supports and nacelle structure in the
engine area. We are proposing this AD
to prevent such chafing, which could
result in an engine shutting down
during flight.
DATES: We must receive comments on
this proposed AD by March 6, 2006.
ADDRESSES: Use one of the following
addresses to submit comments on this
proposed AD.
• DOT Docket Web site: Go to
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
• Government-wide rulemaking Web
site: Go to https://www.regulations.gov
VerDate Aug<31>2005
15:25 Feb 01, 2006
Jkt 208001
Examining the Docket
You may examine the AD docket on
the Internet at https://dms.dot.gov, or in
person at the Docket Management
Facility office between 9 a.m. and 5
PO 00000
Frm 00007
Fmt 4702
Sfmt 4702
Discussion
The Departmento de Aviacao Civil
(DAC), which is the airworthiness
authority for Brazil, notified us that an
unsafe condition may exist on certain
EMBRAER Model EMB–145, –145ER,
–145MR, –145LR, –145XR, –145MP, and
–145EP airplanes. The DAC advises that
it has received reports of chafing of wire
harness W407 against the supports and
nacelle structure in the engine area.
This condition, if not corrected, could
result in an engine shutting down
during flight.
Relevant Service Information
FAA’s Determination and Requirements
of the Proposed AD
These airplane models are
manufactured in Brazil and are type
certificated for operation in the United
States under the provisions of § 21.29 of
the Federal Aviation Regulations (14
CFR 21.29) and the applicable bilateral
airworthiness agreement. Pursuant to
this bilateral airworthiness agreement,
the DAC has kept the FAA informed of
the situation described above. We have
examined the DAC’s findings, evaluated
all pertinent information, and
determined that we need to issue an AD
for airplanes of this type design that are
certificated for operation in the United
States.
Therefore, we are proposing this AD,
which would require accomplishing the
actions specified in the service
information described previously.
E:\FR\FM\02FEP1.SGM
02FEP1
Federal Register / Vol. 71, No. 22 / Thursday, February 2, 2006 / Proposed Rules
Costs of Compliance
This proposed AD would affect about
126 airplanes of U.S. registry. The
proposed actions would take up to 3
work hours per airplane, at an average
labor rate of $65 per work hour.
Required parts would be provided at no
charge. Based on these figures, the
estimated cost of the proposed AD for
U.S. operators is $24,570, or $195 per
airplane.
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.
hsrobinson on PROD1PC71 with PROPOSALS
Regulatory Findings
We have 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 that the 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); 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 proposed AD and placed it in the
AD docket. See the ADDRESSES section
for a location to examine the regulatory
evaluation.
VerDate Aug<31>2005
15:25 Feb 01, 2006
Jkt 208001
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, 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.
§ 39.13
[Amended]
5627
Alternative Methods of Compliance
(AMOCs)
(h)(1) The Manager, International Branch,
ANM–116, Transport Airplane Directorate,
FAA, has the authority to approve AMOCs
for this AD, if requested in accordance with
the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in
accordance with § 39.19 on any airplane to
which the AMOC applies, notify the
appropriate principal inspector in the FAA
Flight Standards Certificate Holding District
Office.
Related Information
(i) Brazilian airworthiness directive 2005–
10–05, dated November 17, 2005, also
addresses the subject of this AD.
2. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
Empresa Brasileira de Aeronautica S.A.
(EMBRAER): Docket No. FAA–2006–
23739; Directorate Identifier 2005–NM–
240–AD.
Issued in Renton, Washington, on January
25, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E6–1420 Filed 2–1–06; 8:45 am]
BILLING CODE 4910–13–P
Comments Due Date
(a) The FAA must receive comments on
this AD action by March 6, 2006.
DEPARTMENT OF STATE
Affected ADs
(b) None.
[Public Notice 5292]
RIN 1400–AC16
Applicability
(c) This AD applies to EMBRAER Model
EMB–145, –145ER, –145MR, –145LR,
–145XR, –145MP, and –145EP airplanes,
certificated in any category; serial numbers
145004 through 145129 inclusive.
Unsafe Condition
(d) This AD results from reports of chafing
of wire harness W407 against the supports
and nacelle structure in the engine area. We
are issuing this AD to prevent such chafing,
which could result in an engine shutting
down during flight.
Compliance
(e) You are responsible for having the
actions required by this AD performed within
the compliance times specified, unless the
actions have already been done.
Modifying Wire Harness Routing and
Installing Supports
(f) Within 5,000 flight hours after the
effective date of this AD, modify the routing
of wire harness W407 near the fire
extinguishing tube in the rear part of the lefthand and right-hand engines, and install new
supports for derivations of wire harness
W407 that lead to applicable connectors, in
accordance with the Accomplishment
Instructions of EMBRAER Service Bulletin
145–71–0008, Change 01, dated July 24,
2001.
Actions Accomplished Previously
(g) Actions done before the effective date
of this AD in accordance with EMBRAER
Service Bulletin 145–71–0008, dated April
23, 1999, are acceptable for compliance with
the requirements of paragraph (f) of this AD.
PO 00000
Frm 00008
22 CFR Part 62
Fmt 4702
Sfmt 4702
Au Pair Exchange Programs
Department of State.
Proposed rule with request for
comment.
AGENCY:
ACTION:
SUMMARY: The Department of State
(Department) is proposing the
amendment of its existing au pair
regulations under the Exchange Visitor
Program (J–1 visa) to permit designated
au pair sponsors to request a one-time
extension of six, nine or 12 months
beyond an au pair participant’s original
12-month program (the maximum
duration of program participation).
DATES: Comment Dates: The Department
will accept comments from the public
up to 60 days from February 2, 2006.
ADDRESSES: You may submit comments,
identified by any of the following
methods:
E-mail: jexchanges@state.gov. You
must include the RIN in the subject line
of your message.
Mail (paper, disk, or CD–ROM
submissions): U.S. Department of State,
Office of Exchange Coordination and
Designation, SA–44, 301 4th Street,
SW., Room 734, Washington, DC 20547.
Please include RIN.
Fax: 202–203–5087. Please include
RIN.
Persons with access to the Internet
may also view this notice and provide
comments by going to the
E:\FR\FM\02FEP1.SGM
02FEP1
Agencies
[Federal Register Volume 71, Number 22 (Thursday, February 2, 2006)]
[Proposed Rules]
[Pages 5626-5627]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E6-1420]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-23739; Directorate Identifier 2005-NM-240-AD]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -
145EP Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain EMBRAER Model EMB-145, -145ER, -145MR, -145LR, -145XR, -
145MP, and -145EP airplanes. This proposed AD would require modifying
the routing of wire harness W407 near the fire extinguishing tube in
the area of each engine, and installing new supports for related
wiring. This proposed AD results from reports of chafing of wire
harness W407 against the supports and nacelle structure in the engine
area. We are proposing this AD to prevent such chafing, which could
result in an engine shutting down during flight.
DATES: We must receive comments on this proposed AD by March 6, 2006.
ADDRESSES: Use one of the following addresses to submit comments on
this proposed AD.
DOT Docket Web site: Go to https://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking Web site: Go to https://
www.regulations.gov and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility, U.S. Department of
Transportation, 400 Seventh Street SW., Nassif Building, room PL-401,
Washington, DC 20590.
Fax: (202) 493-2251.
Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street, SW., Washington, DC, between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
Contact Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box
343--CEP 12.225, Sao Jose dos Campos--SP, Brazil, for service
information identified in this proposed AD.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-1175; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to submit any relevant written data, views, or
arguments regarding this proposed AD. Send your comments to an address
listed in the ADDRESSES section. Include the docket number ``FAA-2006-
23739; Directorate Identifier 2005-NM-240-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of the proposed AD. We will
consider all comments received by the closing date and may amend the
proposed AD in light of those comments.
We will post all comments we receive, without change, to https://
dms.dot.gov, including any personal information you provide. We will
also post a report summarizing each substantive verbal contact with FAA
personnel concerning this proposed AD. Using the search function of
that web site, anyone can find and read the comments in any of our
dockets, including the name of the individual who sent the comment (or
signed the comment on behalf of an association, business, labor union,
etc.). You may review the DOT's complete Privacy Act Statement in the
Federal Register published on April 11, 2000 (65 FR 19477-78), or you
may visit https://dms.dot.gov.
Examining the Docket
You may examine the AD docket on the Internet at https://
dms.dot.gov, or in person at the Docket Management Facility office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the DOT
street address stated in the ADDRESSES section. Comments will be
available in the AD docket shortly after the Docket Management System
receives them.
Discussion
The Departmento de Aviacao Civil (DAC), which is the airworthiness
authority for Brazil, notified us that an unsafe condition may exist on
certain EMBRAER Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP,
and -145EP airplanes. The DAC advises that it has received reports of
chafing of wire harness W407 against the supports and nacelle structure
in the engine area. This condition, if not corrected, could result in
an engine shutting down during flight.
Relevant Service Information
EMBRAER has issued Service Bulletin 145-71-0008, Change 01, dated
July 24, 2001. The service bulletin describes procedures for modifying
the routing of wire harness W407 near the fire extinguishing tube in
the rear part of the left-hand and right-hand engines, and installing
new supports for derivations of wire harness W407 that lead to certain
connectors. Accomplishing the actions specified in the service
information is intended to adequately address the unsafe condition. The
DAC mandated the service information and issued Brazilian airworthiness
directive 2005-10-05, dated November 17, 2005, to ensure the continued
airworthiness of these airplanes in Brazil.
FAA's Determination and Requirements of the Proposed AD
These airplane models are manufactured in Brazil and are type
certificated for operation in the United States under the provisions of
Sec. 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and the
applicable bilateral airworthiness agreement. Pursuant to this
bilateral airworthiness agreement, the DAC has kept the FAA informed of
the situation described above. We have examined the DAC's findings,
evaluated all pertinent information, and determined that we need to
issue an AD for airplanes of this type design that are certificated for
operation in the United States.
Therefore, we are proposing this AD, which would require
accomplishing the actions specified in the service information
described previously.
[[Page 5627]]
Costs of Compliance
This proposed AD would affect about 126 airplanes of U.S. registry.
The proposed actions would take up to 3 work hours per airplane, at an
average labor rate of $65 per work hour. Required parts would be
provided at no charge. Based on these figures, the estimated cost of
the proposed AD for U.S. operators is $24,570, or $195 per airplane.
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 have 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 that the 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); 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 proposed AD and placed it in the AD docket. See the
ADDRESSES section for a location to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, 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 Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
Empresa Brasileira de Aeronautica S.A. (EMBRAER): Docket No. FAA-
2006-23739; Directorate Identifier 2005-NM-240-AD.
Comments Due Date
(a) The FAA must receive comments on this AD action by March 6,
2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to EMBRAER Model EMB-145, -145ER, -145MR, -
145LR, -145XR, -145MP, and -145EP airplanes, certificated in any
category; serial numbers 145004 through 145129 inclusive.
Unsafe Condition
(d) This AD results from reports of chafing of wire harness W407
against the supports and nacelle structure in the engine area. We
are issuing this AD to prevent such chafing, which could result in
an engine shutting down during flight.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Modifying Wire Harness Routing and Installing Supports
(f) Within 5,000 flight hours after the effective date of this
AD, modify the routing of wire harness W407 near the fire
extinguishing tube in the rear part of the left-hand and right-hand
engines, and install new supports for derivations of wire harness
W407 that lead to applicable connectors, in accordance with the
Accomplishment Instructions of EMBRAER Service Bulletin 145-71-0008,
Change 01, dated July 24, 2001.
Actions Accomplished Previously
(g) Actions done before the effective date of this AD in
accordance with EMBRAER Service Bulletin 145-71-0008, dated April
23, 1999, are acceptable for compliance with the requirements of
paragraph (f) of this AD.
Alternative Methods of Compliance (AMOCs)
(h)(1) The Manager, International Branch, ANM-116, Transport
Airplane Directorate, FAA, has the authority to approve AMOCs for
this AD, if requested in accordance with the procedures found in 14
CFR 39.19.
(2) Before using any AMOC approved in accordance with Sec.
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Related Information
(i) Brazilian airworthiness directive 2005-10-05, dated November
17, 2005, also addresses the subject of this AD.
Issued in Renton, Washington, on January 25, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E6-1420 Filed 2-1-06; 8:45 am]
BILLING CODE 4910-13-P