Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 Airplanes, 54247-54248 [05-18058]
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Federal Register / Vol. 70, No. 177 / Wednesday, September 14, 2005 / Rules and Regulations
P.O. Box 343—CEP 12.225, Sao Jose dos
Campos—SP, Brazil, for a copy of this service
information. You may review copies at the
Docket Management Facility, U.S.
Department of Transportation, 400 Seventh
Street, SW., Room PL–401, Nassif Building,
Washington, DC; on the Internet at https://
dms.dot.gov; or at the National Archives and
Records Administration (NARA).
For information on the availability of this
material at the NARA, call (202) 741–6030,
or go to https://www.archives.gov/
federal_register/code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on
September 6, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 05–18057 Filed 9–13–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–21345; Directorate
Identifier 2005–NM–005–AD; Amendment
39–14266; AD 2005–19–01]
RIN 2120–AA64
Airworthiness Directives; Empresa
Brasileira de Aeronautica S.A.
(EMBRAER) Model ERJ 170 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all
EMBRAER Model ERJ 170 airplanes.
This AD requires inspecting the
hydraulic pressure tubes at the outlet of
the engine-driven hydraulic pumps to
determine the part and serial numbers;
and replacing hydraulic pressure tubes
having certain serial numbers with new
hydraulic pressure tubes. This AD
results from failure of a hydraulic
system due to leakage of hydraulic fluid
from a crack in the pipe coming from
the pressure side of the engine-driven
pump. We are issuing this AD to
prevent cracking of the hydraulic
pressure pipes, which could result in
failure of hydraulic system 1 or 2 or
both, and consequent reduced
controllability of the airplane.
DATES: This AD becomes effective
October 19, 2005.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of October 19, 2005.
ADDRESSES: You may examine the AD
docket on the Internet at https://
VerDate Aug<18>2005
15:56 Sep 13, 2005
Jkt 205001
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street
SW., Nassif Building, Room PL–401,
Washington, DC.
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 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:
Examining the Docket
You may examine the airworthiness
directive (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 street address stated in the
ADDRESSES section.
Discussion
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to all EMBRAER Model ERJ 170
airplanes. That NPRM was published in
the Federal Register on June 3, 2005 (70
FR 32544). That NPRM proposed to
require inspecting the hydraulic
pressure tubes at the outlet of the
engine-driven hydraulic pumps to
determine the part and serial numbers;
and replacing hydraulic pressure tubes
having certain serial numbers with new
hydraulic pressure tubes.
Comments
We provided the public the
opportunity to participate in the
development of this AD. We have
considered the comments received.
Request To Withdraw NPRM
One commenter, the airplane
manufacturer, asserts that hydraulic
pressure tubes having the affected serial
numbers have been removed from all
EMBRAER Model ERJ 170 airplanes.
The commenter states that, since
issuance of Brazilian airworthiness
directive 2004–11–06, dated November
29, 2004, the affected hydraulic pressure
tubes have not been installed in
production on EMBRAER Model ERJ
170 airplanes. The commenter also
states that, as of December 2004,
EMBRAER Service Bulletin 170–29–
PO 00000
Frm 00013
Fmt 4700
Sfmt 4700
54247
0001, dated August 9, 2004, has been
accomplished on the entire worldwide
fleet of Model ERJ 170 airplanes. We
infer the commenter requests that we
withdraw the NPRM.
We do not agree. Even if the
worldwide fleet is in compliance with
the requirements of the AD, the issuance
of the rule is still necessary to ensure
that an affected spare part is not
installed on any airplane in the future.
The manufacturer has advised us that
there are about five affected hydraulic
pressure tubes that have not been
destroyed or returned to the
manufacturer. Issuance of this AD will
ensure that an affected spare part is not
installed on an airplane at some future
time. Therefore, we cannot withdraw
the NPRM.
Change to Applicability
We have revised the applicability of
this AD to identify model designations
as published in the most recent type
certificate data sheet for the affected
models.
Change to Service Bulletin Reference
We have revised the note in paragraph
(f) of this AD to reference the correct
service bulletin name of the secondary
source of service information to
EMBRAER Service Bulletin 170–29–
0001.
Conclusion
We have carefully reviewed the
available data, including the comment
received, and determined that air safety
and the public interest require adopting
the AD with the changes described
previously. We have determined that
these changes will neither increase the
economic burden on any operator nor
increase the scope of the AD.
Costs of Compliance
This AD affects about 27 airplanes of
U.S. registry. The inspection takes about
1 work hour per airplane, at an average
labor rate of $65 per work hour. Based
on these figures, the estimated cost of
the inspection for U.S. operators is
$1,755, or $65 per airplane.
The replacement, if necessary, takes
about 3 work hours per airplane, at an
average labor rate of $65 per work hour.
Required parts are $0 per airplane.
Based on these figures, the estimated
cost of the replacement is $195 per
airplane, if necessary.
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,
E:\FR\FM\14SER1.SGM
14SER1
54248
Federal Register / Vol. 70, No. 177 / Wednesday, September 14, 2005 / Rules and Regulations
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 AD will
not have federalism implications under
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the National Government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
(2) Is not a ‘‘significant rule’’ under
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.
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, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
I
VerDate Aug<18>2005
15:56 Sep 13, 2005
Jkt 205001
2005–19–01 Empresa Brasileira de
Aeronautica S.A. (EMBRAER):
Amendment 39–14266. Docket No.
FAA–2005–21345; Directorate Identifier
2005–NM–005–AD.
pressure tube as applicable. Macchi-Hurel
Dubois (MHD) Service Bulletin CF34–8E
MHD 71–00–011 is included in EMBRAER
Service Bulletin 170–29–0001.
Effective Date
(a) This AD becomes effective October 19,
2005.
No Reporting Requirement
Affected ADs
(b) None.
Applicability
(c) This AD applies to all EMBRAER Model
ERJ 170–100LR, –100 STD, –100SE, and –100
SU airplanes, certificated in any category.
Unsafe Condition
(d) This AD was prompted by failure of a
hydraulic system due to leakage of hydraulic
fluid from a crack in the pipe coming from
the pressure side of the engine-driven pump.
We are issuing this AD to prevent cracking
of the hydraulic pressure pipes, which could
result in failure of hydraulic system 1 or 2
or both, and consequent reduced
controllability of the airplane.
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.
Inspection and Replacement if Necessary
(f) Within 100 flight hours or 14 days after
the effective date of this AD, whichever is
first: Inspect the left and right hydraulic
pressure tubes at the outlet of the enginedriven hydraulic pumps to determine the
part and serial numbers, in accordance with
Part I of the Accomplishment Instructions of
EMBRAER Service Bulletin 170–29–0001,
dated August 9, 2004.
(1) If neither hydraulic pressure tube has
a serial number as identified in Part I of the
service bulletin, then no further action is
required by this paragraph.
(2) If only one hydraulic pressure tube has
a serial number as identified in Part I of the
service bulletin: Within 600 flight hours after
the inspection, replace the affected hydraulic
pressure tube with a new hydraulic pressure
tube, in accordance with Part III or Part IV,
as applicable, of the service bulletin.
(3) If both hydraulic pressure tubes have
serial numbers as identified in Part I of the
service bulletin: Before further flight, replace
one of the affected hydraulic pressure tubes
with a new hydraulic pressure tube, in
accordance with Part III or Part IV, as
applicable, of the service bulletin. Within
600 flight hours after the inspection, replace
the other affected hydraulic pressure tube
with a new hydraulic pressure tube, in
accordance with Part III or Part IV, as
applicable, of the service bulletin.
Note 1: EMBRAER Service Bulletin 170–
29–0001 refers to Macchi-Hurel Dubois
(MHD) Service Bulletin CF34–8E MHD 71–
00–011, dated August 3, 2004, as an
additional source of service information for
inspecting the hydraulic pressure tubes to
determine the part and serial numbers; and
replacing hydraulic pressure tubes having
certain serial numbers with new hydraulic
PO 00000
Frm 00014
Fmt 4700
Sfmt 4700
(g) Although the service bulletin referenced
in this AD specifies to submit certain
information to the manufacturer, this AD
does not include that requirement.
Parts Installation
(h) As of the effective date of this AD, no
person may install a hydraulic pressure pipe
having any part and serial numbers identified
in Part I of the Accomplishment Instructions
of EMBRAER Service Bulletin 170–29–0001,
dated August 9, 2004, on any airplane.
Alternative Methods of Compliance
(AMOCs)
(i) 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.
Material Incorporated by Reference
(j) You must use EMBRAER Service
Bulletin 170–29–0001, dated August 9, 2004,
to perform the actions that are required by
this AD, unless the AD specifies otherwise.
The Director of the Federal Register approved
the incorporation by reference of this
document in accordance with 5 U.S.C. 552(a)
and 1 CFR part 51. Contact Empresa
Brasileira de Aeronautica S.A. (EMBRAER),
P.O. Box 343—CEP 12.225, Sao Jose dos
Campos—SP, Brazil, for a copy of this service
information. You may review copies at the
Docket Management Facility, U.S.
Department of Transportation, 400 Seventh
Street SW., room PL–401, Nassif Building,
Washington, DC; on the Internet at https://
dms.dot.gov; or at the National Archives and
Records Administration (NARA). For
information on the availability of this
material at the NARA, call (202) 741–6030,
or go to https://www.archives.gov/federalregister/cfr/ibr-locations.html.
Issued in Renton, Washington, on
September 6, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 05–18058 Filed 9–13–05; 8:45 am]
BILLING CODE 4910–13–P
E:\FR\FM\14SER1.SGM
14SER1
]]>Agencies
[Federal Register Volume 70, Number 177 (Wednesday, September 14, 2005)]
[Rules and Regulations]
[Pages 54247-54248]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-18058]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-21345; Directorate Identifier 2005-NM-005-AD;
Amendment 39-14266; AD 2005-19-01]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model ERJ 170 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
EMBRAER Model ERJ 170 airplanes. This AD requires inspecting the
hydraulic pressure tubes at the outlet of the engine-driven hydraulic
pumps to determine the part and serial numbers; and replacing hydraulic
pressure tubes having certain serial numbers with new hydraulic
pressure tubes. This AD results from failure of a hydraulic system due
to leakage of hydraulic fluid from a crack in the pipe coming from the
pressure side of the engine-driven pump. We are issuing this AD to
prevent cracking of the hydraulic pressure pipes, which could result in
failure of hydraulic system 1 or 2 or both, and consequent reduced
controllability of the airplane.
DATES: This AD becomes effective October 19, 2005.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of October 19,
2005.
ADDRESSES: You may examine the AD docket on the Internet at https://
dms.dot.gov or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street SW., Nassif Building,
Room PL-401, Washington, DC.
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 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:
Examining the Docket
You may examine the airworthiness directive (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 street address stated in the ADDRESSES section.
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to include an AD that would apply to all EMBRAER Model ERJ
170 airplanes. That NPRM was published in the Federal Register on June
3, 2005 (70 FR 32544). That NPRM proposed to require inspecting the
hydraulic pressure tubes at the outlet of the engine-driven hydraulic
pumps to determine the part and serial numbers; and replacing hydraulic
pressure tubes having certain serial numbers with new hydraulic
pressure tubes.
Comments
We provided the public the opportunity to participate in the
development of this AD. We have considered the comments received.
Request To Withdraw NPRM
One commenter, the airplane manufacturer, asserts that hydraulic
pressure tubes having the affected serial numbers have been removed
from all EMBRAER Model ERJ 170 airplanes. The commenter states that,
since issuance of Brazilian airworthiness directive 2004-11-06, dated
November 29, 2004, the affected hydraulic pressure tubes have not been
installed in production on EMBRAER Model ERJ 170 airplanes. The
commenter also states that, as of December 2004, EMBRAER Service
Bulletin 170-29-0001, dated August 9, 2004, has been accomplished on
the entire worldwide fleet of Model ERJ 170 airplanes. We infer the
commenter requests that we withdraw the NPRM.
We do not agree. Even if the worldwide fleet is in compliance with
the requirements of the AD, the issuance of the rule is still necessary
to ensure that an affected spare part is not installed on any airplane
in the future. The manufacturer has advised us that there are about
five affected hydraulic pressure tubes that have not been destroyed or
returned to the manufacturer. Issuance of this AD will ensure that an
affected spare part is not installed on an airplane at some future
time. Therefore, we cannot withdraw the NPRM.
Change to Applicability
We have revised the applicability of this AD to identify model
designations as published in the most recent type certificate data
sheet for the affected models.
Change to Service Bulletin Reference
We have revised the note in paragraph (f) of this AD to reference
the correct service bulletin name of the secondary source of service
information to EMBRAER Service Bulletin 170-29-0001.
Conclusion
We have carefully reviewed the available data, including the
comment received, and determined that air safety and the public
interest require adopting the AD with the changes described previously.
We have determined that these changes will neither increase the
economic burden on any operator nor increase the scope of the AD.
Costs of Compliance
This AD affects about 27 airplanes of U.S. registry. The inspection
takes about 1 work hour per airplane, at an average labor rate of $65
per work hour. Based on these figures, the estimated cost of the
inspection for U.S. operators is $1,755, or $65 per airplane.
The replacement, if necessary, takes about 3 work hours per
airplane, at an average labor rate of $65 per work hour. Required parts
are $0 per airplane. Based on these figures, the estimated cost of the
replacement is $195 per airplane, if necessary.
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,
[[Page 54248]]
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 AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the National Government and the States, or on the distribution of power
and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866;
(2) Is not a ``significant rule'' under 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. 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, 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 Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2005-19-01 Empresa Brasileira de Aeronautica S.A. (EMBRAER):
Amendment 39-14266. Docket No. FAA-2005-21345; Directorate
Identifier 2005-NM-005-AD.
Effective Date
(a) This AD becomes effective October 19, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all EMBRAER Model ERJ 170-100LR, -100
STD, -100SE, and -100 SU airplanes, certificated in any category.
Unsafe Condition
(d) This AD was prompted by failure of a hydraulic system due to
leakage of hydraulic fluid from a crack in the pipe coming from the
pressure side of the engine-driven pump. We are issuing this AD to
prevent cracking of the hydraulic pressure pipes, which could result
in failure of hydraulic system 1 or 2 or both, and consequent
reduced controllability of the airplane.
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.
Inspection and Replacement if Necessary
(f) Within 100 flight hours or 14 days after the effective date
of this AD, whichever is first: Inspect the left and right hydraulic
pressure tubes at the outlet of the engine-driven hydraulic pumps to
determine the part and serial numbers, in accordance with Part I of
the Accomplishment Instructions of EMBRAER Service Bulletin 170-29-
0001, dated August 9, 2004.
(1) If neither hydraulic pressure tube has a serial number as
identified in Part I of the service bulletin, then no further action
is required by this paragraph.
(2) If only one hydraulic pressure tube has a serial number as
identified in Part I of the service bulletin: Within 600 flight
hours after the inspection, replace the affected hydraulic pressure
tube with a new hydraulic pressure tube, in accordance with Part III
or Part IV, as applicable, of the service bulletin.
(3) If both hydraulic pressure tubes have serial numbers as
identified in Part I of the service bulletin: Before further flight,
replace one of the affected hydraulic pressure tubes with a new
hydraulic pressure tube, in accordance with Part III or Part IV, as
applicable, of the service bulletin. Within 600 flight hours after
the inspection, replace the other affected hydraulic pressure tube
with a new hydraulic pressure tube, in accordance with Part III or
Part IV, as applicable, of the service bulletin.
Note 1: EMBRAER Service Bulletin 170-29-0001 refers to Macchi-
Hurel Dubois (MHD) Service Bulletin CF34-8E MHD 71-00-011, dated
August 3, 2004, as an additional source of service information for
inspecting the hydraulic pressure tubes to determine the part and
serial numbers; and replacing hydraulic pressure tubes having
certain serial numbers with new hydraulic pressure tube as
applicable. Macchi-Hurel Dubois (MHD) Service Bulletin CF34-8E MHD
71-00-011 is included in EMBRAER Service Bulletin 170-29-0001.
No Reporting Requirement
(g) Although the service bulletin referenced in this AD
specifies to submit certain information to the manufacturer, this AD
does not include that requirement.
Parts Installation
(h) As of the effective date of this AD, no person may install a
hydraulic pressure pipe having any part and serial numbers
identified in Part I of the Accomplishment Instructions of EMBRAER
Service Bulletin 170-29-0001, dated August 9, 2004, on any airplane.
Alternative Methods of Compliance (AMOCs)
(i) 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.
Material Incorporated by Reference
(j) You must use EMBRAER Service Bulletin 170-29-0001, dated
August 9, 2004, to perform the actions that are required by this AD,
unless the AD specifies otherwise. The Director of the Federal
Register approved the incorporation by reference of this document in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Empresa
Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box 343--CEP 12.225,
Sao Jose dos Campos--SP, Brazil, for a copy of this service
information. You may review copies at the Docket Management
Facility, U.S. Department of Transportation, 400 Seventh Street SW.,
room PL-401, Nassif Building, Washington, DC; on the Internet at
https://dms.dot.gov; or at the National Archives and Records
Administration (NARA). For information on the availability of this
material at the NARA, call (202) 741-6030, or go to https://
www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on September 6, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-18058 Filed 9-13-05; 8:45 am]
BILLING CODE 4910-13-P
