Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 Airplanes, 60599-60600 [E7-21005]
Download as PDF
Federal Register / Vol. 72, No. 206 / Thursday, October 25, 2007 / Proposed Rules
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–0082; Directorate
Identifier 2007–NM–219–AD]
RIN 2120–AA64
Airworthiness Directives; Empresa
Brasileira de Aeronautica S.A.
(EMBRAER) Model ERJ 170 and ERJ
190 Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
SUMMARY: We propose to adopt a new
airworthiness directive (AD) for the
products listed above. 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:
It has been found that the implementation
of the Inertial Reference Units (IRU) on the
ERJ–170 [and ERJ–190] may lead, in certain
degraded modes, to an erroneous Flight Path
Angle (FPA) indication on both Primary
Flight Displays, with no alert to the flight
crew. On the ERJ–170 [and ERJ–190], FPA is
considered as important as pitch and bank
angle for piloting purposes.
The unsafe condition is reduced
ability of the flightcrew to control the
flight path of the airplane. The proposed
AD would require actions that are
intended to address the unsafe
condition described in the MCAI.
DATES: We must receive comments on
this proposed AD by November 26,
2007.
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 AD, contact Empresa Brasileira de
Aeronautica S.A. (EMBRAER), P.O. Box
pwalker on PROD1PC71 with PROPOSALS
ADDRESSES:
VerDate Aug<31>2005
17:49 Oct 24, 2007
Jkt 214001
343—CEP 12.225, Sao Jose dos
Campos—SP, Brazil.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov; or in person at the
Docket Operations office 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 Operations
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:
Sanjay Ralhan, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone
(425) 227–1405; fax (425) 227–1149.
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–2007–0082; Directorate Identifier
2007–NM–219–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 based on those comments.
We will post all comments we
receive, without change, to https://
www.regulations.gov, including any
personal information you provide. We
will also post a report summarizing each
substantive verbal contact we receive
about this proposed AD.
Discussion
ˆ
The Agencia Nacional de Aviacao
¸˜
Civil (ANAC), which is the aviation
authority for Brazil, has issued Brazilian
Airworthiness Directives 2007–08–03
and 2007–08–04, both effective August
27, 2007 (referred to after this as ‘‘the
MCAI’’), to correct an unsafe condition
for the specified products. The MCAI
state:
It has been found that the implementation
of the Inertial Reference Units (IRU) on the
ERJ–170 [and ERJ–190] may lead, in certain
degraded modes, to an erroneous Flight Path
Angle (FPA) indication on both Primary
Flight Displays, with no alert to the flight
crew. On the ERJ–170 [and ERJ–190], FPA is
considered as important as pitch and bank
angle for piloting purposes.
PO 00000
Frm 00012
Fmt 4702
Sfmt 4702
60599
The unsafe condition is reduced
ability of the flightcrew to control the
flight path of the airplane. The
corrective action is removal of certain
wiring connections in the electrical
connectors of both IRUs. You may
obtain further information by examining
the MCAI in the AD docket.
Relevant Service Information
Embraer has issued Service Bulletins
170–34–0019 and 190–34–0009, both
dated February 26, 2007. The actions
described in this service information are
intended to correct the unsafe condition
identified in the MCAI.
FAA’s Determination and Requirements
of This 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 the State of
Design Authority, we have been notified
of the unsafe condition described in the
MCAI and service information
referenced above. We are proposing this
AD because we evaluated all pertinent
information and determined an unsafe
condition exists and is likely to exist or
develop on other products of the same
type design.
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
substantively from the information
provided in the MCAI and related
service information.
We might also have proposed
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
proposed AD.
Costs of Compliance
Based on the service information, we
estimate that this proposed AD would
affect about 108 products of U.S.
registry. We also estimate that it would
take about 6 work-hours per product to
comply with the basic requirements of
this proposed AD. The average labor
rate is $80 per work-hour. Required
parts would cost about $62 per product.
Where the service information lists
required parts costs that are covered
under warranty, we have assumed that
there will be no charge for these costs.
As we do not control warranty coverage
E:\FR\FM\25OCP1.SGM
25OCP1
60600
Federal Register / Vol. 72, No. 206 / Thursday, October 25, 2007 / Proposed Rules
for affected parties, some parties may
incur costs higher than estimated here.
Based on these figures, we estimate the
cost of the proposed AD on U.S.
operators to be $58,536, or $542 per
product.
PART 39—AIRWORTHINESS
DIRECTIVES
Authority for This Rulemaking
§ 39.13
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.
2. The FAA amends § 39.13 by adding
the following new AD:
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); 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.
pwalker on PROD1PC71 with PROPOSALS
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Safety.
1. The authority citation for part 39
continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
[Amended]
EMPRESA BRASILEIRA DE
AERONAUTICA S.A. (EMBRAER):
Docket No. FAA–2007–0082; Directorate
Identifier 2007–NM–219–AD.
Comments Due Date
(a) We must receive comments by
November 26, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to EMBRAER Model
ERJ 170–100 LR, –100 STD, –100 SE, –100
SU, –200 LR, –200 STD, and –200 SU
airplanes, certificated in any category, as
identified in Embraer Service Bulletin 170–
34–0019, dated February 26, 2007; and
Model ERJ 190–100 STD, –100 LR, –100 IGW,
–200 STD, –200 LR, and –200 IGW airplanes;
certificated in any category, as identified in
Embraer Service Bulletin 190–34–0009, dated
February 26, 2007.
Subject
(d) Air Transport Association (ATA) of
America Code 34: Navigation.
Reason
(e) The mandatory continuing
airworthiness information (MCAI) states:
It has been found that the implementation
of the Inertial Reference Units (IRU) on the
ERJ–170 [and ERJ–190] may lead, in certain
degraded modes, to an erroneous Flight Path
Angle (FPA) indication on both Primary
Flight Displays, with no alert to the flight
crew. On the ERJ–170 [and ERJ–190], FPA is
considered as important as pitch and bank
angle for piloting purposes.
The unsafe condition is reduced ability of
the flightcrew to control the flight path of the
airplane. The corrective action is removal of
certain wiring connections in the electrical
connectors of both IRUs.
Actions and Compliance
(f) Within 18 months after the effective
date of this AD, unless already done, remove
the wiring connections from pins 51 and 52
in the electrical connectors of both IRUs, in
accordance with the Accomplishment
Instructions of Embraer Service Bulletin 170–
34–0019 or 190–34–0009, as applicable, both
dated February 26, 2007.
FAA AD Differences
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
Other FAA AD Provisions
(g) The following provisions also apply to
this AD:
17:49 Oct 24, 2007
Jkt 214001
PO 00000
Frm 00013
Fmt 4702
Related Information
(h) Refer to MCAI Brazilian Airworthiness
Directives 2007–08–03 and 2007–08–04, both
effective August 27, 2007, and to Embraer
Service Bulletins 170–34–0019 and 190–34–
0009, both dated February 26, 2007, for
related information.
Issued in Renton, Washington, on October
12, 2007.
Stephen P. Boyd,
Assistant Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E7–21005 Filed 10–24–07; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–0089; Directorate
Identifier 2007–NM–117–AD]
RIN 2120–AA64
Airworthiness Directives; Various
Transport Category Airplanes
Equipped With Auxiliary Fuel Tanks
Installed in Accordance With Certain
Supplemental Type Certificates
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
Note: This AD differs from the MCAI and/
or service information as follows: No
differences.
VerDate Aug<31>2005
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Branch, ANM–116, Transport Airplane
Directorate, FAA, has the authority to
approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19.
Send information to ATTN: Sanjay Ralhan,
Aerospace Engineer, International Branch,
ANM–116, Transport Airplane Directorate,
FAA, 1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone (425)
227–1405; fax (425) 227–1149. 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, under the
provisions of the Paperwork Reduction Act,
the Office of Management and Budget (OMB)
has approved the information collection
requirements and has assigned OMB Control
Number 2120–0056.
Sfmt 4702
SUMMARY: The FAA proposes to adopt a
new airworthiness directive (AD) for
E:\FR\FM\25OCP1.SGM
25OCP1
Agencies
[Federal Register Volume 72, Number 206 (Thursday, October 25, 2007)]
[Proposed Rules]
[Pages 60599-60600]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-21005]
[[Page 60599]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-0082; Directorate Identifier 2007-NM-219-AD]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model ERJ 170 and ERJ 190 Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: We propose to adopt a new airworthiness directive (AD) for the
products listed above. 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:
It has been found that the implementation of the Inertial
Reference Units (IRU) on the ERJ-170 [and ERJ-190] may lead, in
certain degraded modes, to an erroneous Flight Path Angle (FPA)
indication on both Primary Flight Displays, with no alert to the
flight crew. On the ERJ-170 [and ERJ-190], FPA is considered as
important as pitch and bank angle for piloting purposes.
The unsafe condition is reduced ability of the flightcrew to
control the flight path of the airplane. The proposed AD would require
actions that are intended to address the unsafe condition described in
the MCAI.
DATES: We must receive comments on this proposed AD by November 26,
2007.
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 AD, contact Empresa
Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box 343--CEP 12.225, Sao
Jose dos Campos--SP, Brazil.
Examining the AD Docket
You may examine the AD docket on the Internet at https://
www.regulations.gov; or in person at the Docket Operations office
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 Operations 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: Sanjay Ralhan, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
227-1405; fax (425) 227-1149.
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-2007-0082;
Directorate Identifier 2007-NM-219-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 based on those comments.
We will post all comments we receive, without change, to https://
www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.
Discussion
The Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC),
which is the aviation authority for Brazil, has issued Brazilian
Airworthiness Directives 2007-08-03 and 2007-08-04, both effective
August 27, 2007 (referred to after this as ``the MCAI''), to correct an
unsafe condition for the specified products. The MCAI state:
It has been found that the implementation of the Inertial
Reference Units (IRU) on the ERJ-170 [and ERJ-190] may lead, in
certain degraded modes, to an erroneous Flight Path Angle (FPA)
indication on both Primary Flight Displays, with no alert to the
flight crew. On the ERJ-170 [and ERJ-190], FPA is considered as
important as pitch and bank angle for piloting purposes.
The unsafe condition is reduced ability of the flightcrew to
control the flight path of the airplane. The corrective action is
removal of certain wiring connections in the electrical connectors of
both IRUs. You may obtain further information by examining the MCAI in
the AD docket.
Relevant Service Information
Embraer has issued Service Bulletins 170-34-0019 and 190-34-0009,
both dated February 26, 2007. The actions described in this service
information are intended to correct the unsafe condition identified in
the MCAI.
FAA's Determination and Requirements of This 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 the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are proposing this AD because we
evaluated all pertinent information and determined an unsafe condition
exists and is likely to exist or develop on other products of the same
type design.
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 substantively from the information
provided in the MCAI and related service information.
We might also have proposed 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 proposed AD.
Costs of Compliance
Based on the service information, we estimate that this proposed AD
would affect about 108 products of U.S. registry. We also estimate that
it would take about 6 work-hours per product to comply with the basic
requirements of this proposed AD. The average labor rate is $80 per
work-hour. Required parts would cost about $62 per product. Where the
service information lists required parts costs that are covered under
warranty, we have assumed that there will be no charge for these costs.
As we do not control warranty coverage
[[Page 60600]]
for affected parties, some parties may incur costs higher than
estimated here. Based on these figures, we estimate the cost of the
proposed AD on U.S. operators to be $58,536, or $542 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 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); 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.
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 FAA amends Sec. 39.13 by adding the following new AD:
EMPRESA BRASILEIRA DE AERONAUTICA S.A. (EMBRAER): Docket No. FAA-
2007-0082; Directorate Identifier 2007-NM-219-AD.
Comments Due Date
(a) We must receive comments by November 26, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to EMBRAER Model ERJ 170-100 LR, -100 STD, -
100 SE, -100 SU, -200 LR, -200 STD, and -200 SU airplanes,
certificated in any category, as identified in Embraer Service
Bulletin 170-34-0019, dated February 26, 2007; and Model ERJ 190-100
STD, -100 LR, -100 IGW, -200 STD, -200 LR, and -200 IGW airplanes;
certificated in any category, as identified in Embraer Service
Bulletin 190-34-0009, dated February 26, 2007.
Subject
(d) Air Transport Association (ATA) of America Code 34:
Navigation.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
It has been found that the implementation of the Inertial
Reference Units (IRU) on the ERJ-170 [and ERJ-190] may lead, in
certain degraded modes, to an erroneous Flight Path Angle (FPA)
indication on both Primary Flight Displays, with no alert to the
flight crew. On the ERJ-170 [and ERJ-190], FPA is considered as
important as pitch and bank angle for piloting purposes.
The unsafe condition is reduced ability of the flightcrew to
control the flight path of the airplane. The corrective action is
removal of certain wiring connections in the electrical connectors
of both IRUs.
Actions and Compliance
(f) Within 18 months after the effective date of this AD, unless
already done, remove the wiring connections from pins 51 and 52 in
the electrical connectors of both IRUs, in accordance with the
Accomplishment Instructions of Embraer Service Bulletin 170-34-0019
or 190-34-0009, as applicable, both dated February 26, 2007.
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,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
has the authority to approve AMOCs for this AD, if requested using
the procedures found in 14 CFR 39.19. Send information to ATTN:
Sanjay Ralhan, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone (425) 227-1405; fax (425) 227-1149.
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, under the provisions of the Paperwork Reduction Act, the
Office of Management and Budget (OMB) has approved the information
collection requirements and has assigned OMB Control Number 2120-
0056.
Related Information
(h) Refer to MCAI Brazilian Airworthiness Directives 2007-08-03
and 2007-08-04, both effective August 27, 2007, and to Embraer
Service Bulletins 170-34-0019 and 190-34-0009, both dated February
26, 2007, for related information.
Issued in Renton, Washington, on October 12, 2007.
Stephen P. Boyd,
Assistant Manager, Transport Airplane Directorate, Aircraft
Certification Service.
[FR Doc. E7-21005 Filed 10-24-07; 8:45 am]
BILLING CODE 4910-13-P