Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 Airplanes, 71537-71538 [E8-27170]
Download as PDF
Federal Register / Vol. 73, No. 228 / Tuesday, November 25, 2008 / Rules and Regulations
FAA, Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington; or 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 Renton, Washington, on October
24, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–27168 Filed 11–24–08; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
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 August 21, 2008 (73 FR
49362). That NPRM proposed to correct
an unsafe condition for the specified
products. The MCAI states:
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2008–0889; Directorate
Identifier 2008–NM–092–AD; Amendment
39–15738; AD 2008–23–17]
RIN 2120–AA64
Airworthiness Directives; Empresa
Brasileira de Aeronautica S.A.
(EMBRAER) Model ERJ 170 and ERJ
190 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: We are adopting a new
airworthiness directive (AD) for the
products listed above. This 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:
erowe on PROD1PC63 with RULES
[E]scape slide system installation [was
found with] * * * tie-down straps which are
used for escape slide packing [having not
been removed]. The non-removal of the tiedown straps does not allow the aircraft door
to reach the fully open position and the
consequent deployment of the escape slide
system in a * * * emergency evacuation,
affecting the occupying safety.
The unsafe condition is failure of an
evacuation system, which could impede
an emergency evacuation and increase
the chance of injury to passengers and
flightcrew during the evacuation. We
are issuing this AD to require actions to
correct the unsafe condition on these
products.
This AD becomes effective
December 30, 2008.
The Director of the Federal Register
approved the incorporation by reference
DATES:
VerDate Aug<31>2005
14:39 Nov 24, 2008
Jkt 217001
of certain publications listed in this AD
as of December 30, 2008.
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov or in person at the
U.S. Department of Transportation,
Docket Operations, M–30, West
Building Ground Floor, Room W12–140,
1200 New Jersey Avenue, SE.,
Washington, DC.
FOR FURTHER INFORMATION CONTACT:
Kenny Kaulia, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone
(425) 227–2848; fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
[E]scape slide system installation [was
found with] * * * tie-down straps which are
used for escape slide packing [having not
been removed]. The non-removal of the tiedown straps does not allow the aircraft door
to reach the fully open position and the
consequent deployment of the escape slide
system in a * * * emergency evacuation,
affecting the occupying safety.
The unsafe condition is failure of an
evacuation system, which could impede
an emergency evacuation and increase
the chance of injury to passengers and
flightcrew during the evacuation. The
corrective action involves inspection of
the forward and rearward doors’
emergency evacuation slide packs for
the presence of tie-down straps, and, if
applicable, removal of the tie-down
straps. You may obtain further
information by examining the MCAI in
the AD docket.
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
PO 00000
Frm 00017
Fmt 4700
Sfmt 4700
71537
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 required different
actions in this AD from those in the
MCAI in order to follow our FAA
policies. Any such differences are
highlighted in a NOTE within the AD.
Costs of Compliance
We estimate that this AD will affect
about 144 products of U.S. registry. We
also estimate that it will take about 2
work-hours per product to comply with
the basic requirements of this AD. The
average labor rate is $80 per work-hour.
Based on these figures, we estimate the
cost of this AD to the U.S. operators to
be $23,040, or $160 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 the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
E:\FR\FM\25NOR1.SGM
25NOR1
71538
Federal Register / Vol. 73, No. 228 / Tuesday, November 25, 2008 / Rules and Regulations
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 Operations office 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 Operations 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
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 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]
2. The FAA amends § 39.13 by adding
the following new AD:
■
2008–23–17 Empresa Brasileira de
Aeronautica S.A. (EMBRAER):
Amendment 39–15738. Docket No.
FAA–2008–0889; Directorate Identifier
2008–NM–092–AD.
Effective Date
(a) This airworthiness directive (AD)
becomes effective December 30, 2008.
erowe on PROD1PC63 with RULES
Affected ADs
(b) None.
Subject
(d) Air Transport Association (ATA) of
America Code 25: Equipment/Furnishings.
Reason
(e) The mandatory continuing
airworthiness information (MCAI) states:
[E]scape slide system installation [was
found with] * * * tie-down straps which are
used for escape slide packing [having not
been removed]. The non-removal of the tiedown straps does not allow the aircraft door
to reach the fully open position and the
consequent deployment of the escape slide
system in a * * * emergency evacuation,
affecting the occupying safety.
The unsafe condition is failure of an
evacuation system, which could impede an
emergency evacuation and increase the
chance of injury to passengers and flightcrew
during the evacuation. The corrective action
involves inspection of the forward and
rearward doors’ emergency evacuation slide
packs for the presence of tie-down straps,
and, if applicable, removal of the tie-down
straps.
Actions and Compliance
(f) Unless already done: Within 600 flight
hours after the effective date of this AD, carry
out a general visual inspection (GVI) of the
emergency evacuation slide packs installed
on the forward and rearward doors, in
accordance with the Accomplishment
Instructions of EMBRAER Service Bulletin
170–25–0088, dated December 21, 2007; or
190–25–0062, dated December 21, 2007; as
applicable. If tie-down straps are found, they
must be cut and removed from the slide pack
before further flight.
Note 1: For the purposes of this AD, a
general visual inspection (GVI) is: ‘‘A visual
examination of an interior or exterior area,
installation, or assembly to detect obvious
damage, failure, or irregularity. This level of
inspection is made from within touching
distance unless otherwise specified. A mirror
may be necessary to ensure visual access to
all exposed surfaces in the inspection area.
This level of inspection is made under
normally available lighting conditions such
as daylight, hangar lighting, flashlight, or
droplight and may require removal or
opening of access panels or doors. Stands,
ladders, or platforms may be required to gain
proximity to the area being checked.’’
FAA AD Differences
Applicability
(c) This AD applies to the airplanes
specified in paragraphs (c)(1) and (c)(2) of
this AD.
(1) EMBRAER Model ERJ 170–100 LR,
–100 STD, –100 SE, and –100 SU, –200 LR,
–200 STD, and –200 SU airplanes, serial
numbers 17000002, 17000004 thru 17000013,
and 17000015 thru 17000196, certificated in
any category.
(2) EMBRAER Model ERJ 190–100 STD,
–100 LR, –100 IGW, –100 ECJ, –200 STD,
–200 LR, and –200 IGW airplanes, serial
VerDate Aug<31>2005
numbers 19000002, 19000004 thru 19000132,
and 19000135, certificated in any category.
14:39 Nov 24, 2008
Jkt 217001
Note 2: 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: Kenny Kaulia,
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
Aerospace Engineer, International Branch,
ANM–116, Transport Airplane Directorate,
FAA, 1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone (425)
227–2848; 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 2008–01–03 and 2008–01–04, both
effective March 3, 2008; and EMBRAER
Service Bulletins 170–25–0088 and 190–25–
0062, both dated December 21, 2007; for
related information.
Material Incorporated by Reference
(i) You must use EMBRAER Service
Bulletin 170–25–0088, dated December 21,
2007; or EMBRAER Service Bulletin 190–25–
0062, dated December 21, 2007; as
applicable; 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 Empresa Brasileira de
Aeronautica S.A. (EMBRAER), Technical
Publications Section (PC 060), Av. Brigadeiro
˜
Faria Lima, 2170—Putim—12227–901 Sao
Jose dos Campos—SP—BRASIL; telephone:
+55 12 3927–5852 or +55 12 3309–0732; fax:
+55 12 3927–7546; e-mail:
distrib@embraer.com.br; Internet: https://
www.flyembraer.com.
(3) You may review copies at the FAA,
Transport Airplane Directorate, 1601 Lind
Avenue, SW., Renton, Washington; or 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 Renton, Washington, on
November 6, 2008.
Stephen P. Boyd,
Assistant Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E8–27170 Filed 11–24–08; 8:45 am]
BILLING CODE 4910–13–P
E:\FR\FM\25NOR1.SGM
25NOR1
Agencies
[Federal Register Volume 73, Number 228 (Tuesday, November 25, 2008)]
[Rules and Regulations]
[Pages 71537-71538]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-27170]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-0889; Directorate Identifier 2008-NM-092-AD;
Amendment 39-15738; AD 2008-23-17]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model ERJ 170 and ERJ 190 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) 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:
[E]scape slide system installation [was found with] * * * tie-
down straps which are used for escape slide packing [having not been
removed]. The non-removal of the tie-down straps does not allow the
aircraft door to reach the fully open position and the consequent
deployment of the escape slide system in a * * * emergency
evacuation, affecting the occupying safety.
The unsafe condition is failure of an evacuation system, which could
impede an emergency evacuation and increase the chance of injury to
passengers and flightcrew during the evacuation. We are issuing this AD
to require actions to correct the unsafe condition on these products.
DATES: This AD becomes effective December 30, 2008.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of December 30,
2008.
ADDRESSES: You may examine the AD docket on the Internet at https://
www.regulations.gov or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC.
FOR FURTHER INFORMATION CONTACT: Kenny Kaulia, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
227-2848; fax (425) 227-1149.
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 August 21, 2008 (73
FR 49362). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
[E]scape slide system installation [was found with] * * * tie-
down straps which are used for escape slide packing [having not been
removed]. The non-removal of the tie-down straps does not allow the
aircraft door to reach the fully open position and the consequent
deployment of the escape slide system in a * * * emergency
evacuation, affecting the occupying safety.
The unsafe condition is failure of an evacuation system, which could
impede an emergency evacuation and increase the chance of injury to
passengers and flightcrew during the evacuation. The corrective action
involves inspection of the forward and rearward doors' emergency
evacuation slide packs for the presence of tie-down straps, and, if
applicable, removal of the tie-down straps. You may obtain further
information by examining the MCAI in the AD docket.
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 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 our FAA policies. Any such differences
are highlighted in a NOTE within the AD.
Costs of Compliance
We estimate that this AD will affect about 144 products of U.S.
registry. We also estimate that it will take about 2 work-hours per
product to comply with the basic requirements of this AD. The average
labor rate is $80 per work-hour. Based on these figures, we estimate
the cost of this AD to the U.S. operators to be $23,040, or $160 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 the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
[[Page 71538]]
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 Operations office
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 Operations 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:
2008-23-17 Empresa Brasileira de Aeronautica S.A. (EMBRAER):
Amendment 39-15738. Docket No. FAA-2008-0889; Directorate Identifier
2008-NM-092-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective December
30, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to the airplanes specified in paragraphs
(c)(1) and (c)(2) of this AD.
(1) EMBRAER Model ERJ 170-100 LR, -100 STD, -100 SE, and -100
SU, -200 LR, -200 STD, and -200 SU airplanes, serial numbers
17000002, 17000004 thru 17000013, and 17000015 thru 17000196,
certificated in any category.
(2) EMBRAER Model ERJ 190-100 STD, -100 LR, -100 IGW, -100 ECJ,
-200 STD, -200 LR, and -200 IGW airplanes, serial numbers 19000002,
19000004 thru 19000132, and 19000135, certificated in any category.
Subject
(d) Air Transport Association (ATA) of America Code 25:
Equipment/Furnishings.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
[E]scape slide system installation [was found with] * * * tie-
down straps which are used for escape slide packing [having not been
removed]. The non-removal of the tie-down straps does not allow the
aircraft door to reach the fully open position and the consequent
deployment of the escape slide system in a * * * emergency
evacuation, affecting the occupying safety.
The unsafe condition is failure of an evacuation system, which could
impede an emergency evacuation and increase the chance of injury to
passengers and flightcrew during the evacuation. The corrective
action involves inspection of the forward and rearward doors'
emergency evacuation slide packs for the presence of tie-down
straps, and, if applicable, removal of the tie-down straps.
Actions and Compliance
(f) Unless already done: Within 600 flight hours after the
effective date of this AD, carry out a general visual inspection
(GVI) of the emergency evacuation slide packs installed on the
forward and rearward doors, in accordance with the Accomplishment
Instructions of EMBRAER Service Bulletin 170-25-0088, dated December
21, 2007; or 190-25-0062, dated December 21, 2007; as applicable. If
tie-down straps are found, they must be cut and removed from the
slide pack before further flight.
Note 1: For the purposes of this AD, a general visual inspection
(GVI) is: ``A visual examination of an interior or exterior area,
installation, or assembly to detect obvious damage, failure, or
irregularity. This level of inspection is made from within touching
distance unless otherwise specified. A mirror may be necessary to
ensure visual access to all exposed surfaces in the inspection area.
This level of inspection is made under normally available lighting
conditions such as daylight, hangar lighting, flashlight, or
droplight and may require removal or opening of access panels or
doors. Stands, ladders, or platforms may be required to gain
proximity to the area being checked.''
FAA AD Differences
Note 2: 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:
Kenny Kaulia, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone (425) 227-2848; 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 2008-01-03
and 2008-01-04, both effective March 3, 2008; and EMBRAER Service
Bulletins 170-25-0088 and 190-25-0062, both dated December 21, 2007;
for related information.
Material Incorporated by Reference
(i) You must use EMBRAER Service Bulletin 170-25-0088, dated
December 21, 2007; or EMBRAER Service Bulletin 190-25-0062, dated
December 21, 2007; as applicable; 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
Empresa Brasileira de Aeronautica S.A. (EMBRAER), Technical
Publications Section (PC 060), Av. Brigadeiro Faria Lima, 2170--
Putim--12227-901 Sao Jose dos Campos--SP--BRASIL; telephone: +55 12
3927-5852 or +55 12 3309-0732; fax: +55 12 3927-7546; e-mail:
distrib@embraer.com.br; Internet: https://www.flyembraer.com.
(3) You may review copies at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or 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 Renton, Washington, on November 6, 2008.
Stephen P. Boyd,
Assistant Manager, Transport Airplane Directorate, Aircraft
Certification Service.
[FR Doc. E8-27170 Filed 11-24-08; 8:45 am]
BILLING CODE 4910-13-P