Airworthiness Directives; Airbus Model A310 Series Airplanes, 24936-24938 [05-9063]
Download as PDF
<![CDATA[
24936
Federal Register / Vol. 70, No. 91 / Thursday, May 12, 2005 / Rules and Regulations
Fairness Act of 1996, Pub. L. 104–121.
Finally, this action is not a rule as
defined by 5 U.S.C. 601 et seq., the
Regulatory Flexibility Act, and thus is
exempt from the provisions of that Act.
Paperwork Reduction Act
This rule contains no information
collections or recordkeeping
requirements under the Paperwork
Reduction Act of 1995 (44 U.S.C. 3501
et seq.).
List of Subjects in 7 CFR Part 1
Administrative practice and
procedure, Agriculture, Antitrust, Blind,
Claims, Concessions, Cooperatives,
Equal access to justice, Federal
buildings and facilities, Freedom of
information, Lawyers, Privacy.
Accordingly, we are amending 7 CFR
part 1 as follows:
I
PART 1—ADMINISTRATIVE
REGULATIONS
1. The authority citation for part 1
continues to read as follows:
I
Authority: 5 U.S.C. 301, unless otherwise
noted.
Subpart H—Rules of Practice
Governing Formal Adjudicatory
Proceedings Instituted by the
Secretary Under Various Statutes
2. In § 1.131, paragraph (b) is amended
as follows:
I a. In paragraph (b)(3), by removing the
word ‘‘and’’.
I b. By redesignating paragraph (b)(4) as
paragraph (b)(5) and by adding a new
paragraph (b)(4) to read as set forth
below.
I
§ 1.131 Scope and applicability of this
subpart.
*
*
*
*
*
(b) * * *
(4) Adjudicatory proceedings under
the regulations promulgated under the
Animal Welfare Act (7 U.S.C. 2131 et
seq.) for the denial of an initial license
application (9 CFR 2.11) or the
termination of a license during the
license renewal process or at any other
time (9 CFR 2.12); and
*
*
*
*
*
Done in Washington, DC, this 5th day of
May, 2005.
Mike Johanns,
Secretary of Agriculture.
[FR Doc. 05–9444 Filed 5–11–05; 8:45 am]
BILLING CODE 3410–34–P
VerDate jul<14>2003
13:22 May 11, 2005
Jkt 205001
NUCLEAR REGULATORY
COMMISSION
10 CFR Part 72
RIN 3150–AH64
List of Approved Spent Fuel Storage
Casks: HI–STORM 100 Revision;
Withdrawal of Direct Final Rule
Nuclear Regulatory
Commission.
ACTION: Direct final rule; withdrawal.
AGENCY:
SUMMARY: The Nuclear Regulatory
Commission (NRC) is withdrawing a
direct final rule that would have revised
the Holtec International HI–STORM 100
cask system listing within the ‘‘List of
Approved Spent Fuel Storage Casks’’ to
include Amendment No. 2 to the
Certificate of Compliance. The NRC is
taking this action because it has
received significant adverse comments
in response to an identical proposed
rule which was concurrently published
with the direct final rule.
FOR FURTHER INFORMATION CONTACT:
Jayne M. McCausland, Office of Nuclear
Material Safety and Safeguards, U.S.
Nuclear Regulatory Commission,
Washington, DC 20555, telephone (301)
415–6219 (e-mail: jmm2@nrc.gov).
SUPPLEMENTARY INFORMATION: On
February 28, 2005 (70 FR 9504), the
NRC published in the Federal Register
a direct final rule amending its
regulations in 10 CFR 72.214 to revise
the Holtec International HI–STORM 100
cask system listing within the ‘‘List of
Approved Spent Fuel Storage Casks’’ to
include Amendment No. 2 to the
Certificate of Compliance. Amendment
No. 2 modifies the present cask system
design to include changes to materials
used in construction, changes to the
types of fuel that can be loaded, changes
to shielding and confinement
methodologies and assumptions,
revisions to various temperature limits,
changes in allowable fuel enrichments,
and other changes to reflect current NRC
staff guidance and use of industry
codes. The direct final rule was to
become effective on May 16, 2005. The
NRC also concurrently published an
identical proposed rule on February 28,
2005 (70 FR 9550).
In the February 28, 2005, direct final
rule, NRC stated that if any significant
adverse comments were received, a
notice of timely withdrawal of the direct
final rule would be published in the
Federal Register. As a result, the direct
final rule would not take effect.
The NRC received significant adverse
comment on the direct final rule;
therefore, the NRC is withdrawing the
PO 00000
Frm 00002
Fmt 4700
Sfmt 4700
direct final rule. As stated in the
February 28, 2005, direct final rule, NRC
will address the comments received on
the February 28, 2005, companion
proposed rule in a subsequent final rule.
The NRC will not initiate a second
comment period on this action.
Dated at Rockville, Maryland, this 5th day
of May, 2005.
For the Nuclear Regulatory Commission.
William Borchardt,
Acting Executive Director for Operations.
[FR Doc. 05–9448 Filed 5–11–05; 8:45 am]
BILLING CODE 7590–01–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–20379; Directorate
Identifier 2004–NM–174–AD; Amendment
39–14078; AD 2005–10–01]
RIN 2120–AA64
Airworthiness Directives; Airbus Model
A310 Series 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
Airbus Model A310 series airplanes.
This AD requires measuring the
clearance between the compensator and
the guide assembly of probe no. 1 on the
outboard fuel tanks, and performing
corrective actions if necessary. This AD
is prompted by the results of fuel system
reviews conducted by the manufacturer.
We are issuing this AD to prevent
interference between the compensator
and the guide assembly of probe no. 1,
which could create an ignition source
that could result in a fire or explosion.
DATES: This AD becomes effective June
16, 2005.
The incorporation by reference of a
certain publication listed in the AD is
approved by the Director of the Federal
Register as of June 16, 2005.
ADDRESSES: For service information
identified in this AD, contact Airbus, 1
Rond Point Maurice Bellonte, 31707
Blagnac Cedex, France.
Docket: The AD docket contains the
proposed AD, comments, and any final
disposition. You can 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
E:\FR\FM\12MYR1.SGM
12MYR1
24937
Federal Register / Vol. 70, No. 91 / Thursday, May 12, 2005 / Rules and Regulations
Docket Management Facility office
(telephone (800) 647–5227) is located on
the plaza level of the Nassif Building at
the U.S. Department of Transportation,
400 Seventh Street, SW., room PL–401,
Washington, DC. This docket number is
FAA–2005–20379; the directorate
identifier for this docket is 2004–NM–
174–AD.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–2125;
fax (425) 227–1149.
The FAA
proposed to amend 14 CFR part 39 with
an AD for all Airbus Model A310 series
airplanes. That action, published in the
Federal Register on February 15, 2005
(70 FR 7700), proposed to require
measuring the clearance between the
compensator and the guide assembly of
probe no. 1 on the outboard fuel tanks,
and performing corrective actions if
necessary.
have been submitted on the proposed
AD or on the determination of the cost
to the public.
Comments
The following table provides the
estimated costs for U.S. operators to
comply with this AD.
SUPPLEMENTARY INFORMATION:
We provided the public the
opportunity to participate in the
development of this AD. No comments
Conclusion
We have carefully reviewed the
available data and determined that air
safety and the public interest require
adopting the AD as proposed.
Costs of Compliance
ESTIMATED COSTS
Action
Work hours
Inspection ........................................................
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.
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
13:22 May 11, 2005
2
$65
Jkt 205001
Cost per airplane
Parts
None ...........................
(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. 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.
$130
Number of
U.S.-registered airplanes
59
Fleet cost
$7,670
Applicability
(c) This AD applies to all Airbus Model
310 series airplanes, certificated in any
category.
Unsafe Condition
(d) This AD was prompted by the results
of fuel system reviews conducted by the
manufacturer. We are issuing this AD to
prevent interference between the
compensator and the guide assembly of probe
no. 1, which could create an ignition source
that could result in a fire or explosion.
Compliance
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
(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.
Measurement
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Regulatory Findings
VerDate jul<14>2003
Average
labor rate
per hour
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
I
2005–10–01 Airbus: Amendment 39–14078.
Docket No. FAA–2005–20379;
Directorate Identifier 2004–NM–174–AD.
Effective Date
(a) This AD becomes effective June 16,
2005.
Affected ADs
(b) None.
PO 00000
Frm 00003
Fmt 4700
Sfmt 4700
(f) Within 4,000 flight hours after the
effective date of this AD, measure the
clearance between the compensator and the
guide assembly of probe no. 1 on the left- and
right-hand outboard fuel tanks, in accordance
with the Accomplishment Instructions of
Airbus Service Bulletin A310–28–2152,
dated January 12, 2004. If the clearance
between the compensator and the guide
assembly is less than 3 mm, before further
flight, modify the guide assembly of probe
no. 1 to provide clearance of 3 mm or more
between the compensator and the guide
assembly, in accordance with the
Accomplishment Instructions of the service
bulletin.
Parts Installation
(g) As of the effective date of this AD, no
person may install probe no. 1 on the left-or
right-hand outboard fuel tank unless the
requirements of paragraph (f) of this AD have
been accomplished.
E:\FR\FM\12MYR1.SGM
12MYR1
24938
Federal Register / Vol. 70, No. 91 / Thursday, May 12, 2005 / Rules and Regulations
Alternative Methods of Compliance
(AMOCs)
DEPARTMENT OF TRANSPORTATION
(h) 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.
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–20345; Directorate
Identifier 2004–NM–101–AD; Amendment
39–14083; AD 2005–10–06]
Related Information
(i) French airworthiness directive F–2004–
125, dated July 21, 2004, also addresses the
subject of this AD.
Material Incorporated by Reference
(j) You must use Airbus Service Bulletin
A310–28–2152, dated January 12, 2004, to
perform the actions that are required by this
AD, unless the AD specifies otherwise. The
Director of the Federal Register approves the
incorporation by reference of this document
in accordance with 5 U.S.C. 552(a) and 1 CFR
part 51. To get copies of the service
information, contact Airbus, 1 Rond Point
Maurice Bellonte, 31707 Blagnac Cedex,
France. To view the AD docket, go to the
Docket Management Facility, U.S.
Department of Transportation, 400 Seventh
Street SW., room PL–401, Nassif Building,
Washington, DC. To review copies of the
service information, contact 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 April 29,
2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–9063 Filed 5–11–05; 8:45 am]
BILLING CODE 4910–13–P
RIN 2120–AA64
Airworthiness Directives; Dornier
Model 328–300 Series Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
Dornier Model 328–300 series airplanes.
This AD requires installing a drain hole
in the lower skin of the left- and righthand elevator horns. This AD is
prompted by reports of water found in
the elevator assembly. We are issuing
this AD to prevent water or ice
accumulating in the elevator assembly,
which could result in possible corrosion
that reduces the structural integrity of
the flight control surface, or in an
unbalanced flight control surface. These
conditions could result in reduced
controllability of the airplane.
DATES: This AD becomes effective June
16, 2005.
The incorporation by reference of a
certain publication listed in the AD is
approved by the Director of the Federal
Register as of June 16, 2005.
ADDRESSES: For service information
identified in this AD, contact AvCraft
Aerospace GmbH, P.O. Box 1103, D–
82230 Wessling, Germany.
Docket: The AD docket contains the
proposed AD, comments, and any final
disposition. You can 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 U.S. Department of Transportation,
400 Seventh Street, SW., room PL–401,
Washington, DC. This docket number is
FAA–2005–20345; the directorate
identifier for this docket is 2004–NM–
101–AD.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–2125;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION: The FAA
proposed to amend 14 CFR part 39 with
an AD for certain Dornier Model 328–
300 series airplanes. That action,
published in the Federal Register on
February 15, 2005 (70 FR 7689),
proposed to require installing a drain
hole in the lower skin of the left- and
right-hand elevator horns.
Comments
We provided the public the
opportunity to participate in the
development of this AD. No comments
have been submitted on the proposed
AD or on the determination of the cost
to the public.
Conclusion
We have carefully reviewed the
available data and determined that air
safety and the public interest require
adopting the AD as proposed.
Costs of Compliance
The following table provides the
estimated costs for U.S. operators to
comply with this AD.
ESTIMATED COSTS
Action
Installing drain hole ..................................
1
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.
VerDate jul<14>2003
13:22 May 11, 2005
Average labor
rate per hour
Work hours
Jkt 205001
$65
Parts
$100
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
PO 00000
Frm 00004
Fmt 4700
Sfmt 4700
Cost per airplane
Number of
U.S.-registered
airplanes
$165
49
Fleet cost
$8,085
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
E:\FR\FM\12MYR1.SGM
12MYR1
]]>Agencies
[Federal Register Volume 70, Number 91 (Thursday, May 12, 2005)]
[Rules and Regulations]
[Pages 24936-24938]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-9063]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-20379; Directorate Identifier 2004-NM-174-AD;
Amendment 39-14078; AD 2005-10-01]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A310 Series 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
Airbus Model A310 series airplanes. This AD requires measuring the
clearance between the compensator and the guide assembly of probe no. 1
on the outboard fuel tanks, and performing corrective actions if
necessary. This AD is prompted by the results of fuel system reviews
conducted by the manufacturer. We are issuing this AD to prevent
interference between the compensator and the guide assembly of probe
no. 1, which could create an ignition source that could result in a
fire or explosion.
DATES: This AD becomes effective June 16, 2005.
The incorporation by reference of a certain publication listed in
the AD is approved by the Director of the Federal Register as of June
16, 2005.
ADDRESSES: For service information identified in this AD, contact
Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France.
Docket: The AD docket contains the proposed AD, comments, and any
final disposition. You can 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
[[Page 24937]]
Docket Management Facility office (telephone (800) 647-5227) is located
on the plaza level of the Nassif Building at the U.S. Department of
Transportation, 400 Seventh Street, SW., room PL-401, Washington, DC.
This docket number is FAA-2005-20379; the directorate identifier for
this docket is 2004-NM-174-AD.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2125; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39
with an AD for all Airbus Model A310 series airplanes. That action,
published in the Federal Register on February 15, 2005 (70 FR 7700),
proposed to require measuring the clearance between the compensator and
the guide assembly of probe no. 1 on the outboard fuel tanks, and
performing corrective actions if necessary.
Comments
We provided the public the opportunity to participate in the
development of this AD. No comments have been submitted on the proposed
AD or on the determination of the cost to the public.
Conclusion
We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD as proposed.
Costs of Compliance
The following table provides the estimated costs for U.S. operators
to comply with this AD.
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Number of
Average Cost per U.S.-
Action Work hours labor rate Parts airplane registered Fleet cost
per hour airplanes
----------------------------------------------------------------------------------------------------------------
Inspection................... 2 $65 None............ $130 59 $7,670
----------------------------------------------------------------------------------------------------------------
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 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. 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 FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2005-10-01 Airbus: Amendment 39-14078. Docket No. FAA-2005-20379;
Directorate Identifier 2004-NM-174-AD.
Effective Date
(a) This AD becomes effective June 16, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Airbus Model 310 series airplanes,
certificated in any category.
Unsafe Condition
(d) This AD was prompted by the results of fuel system reviews
conducted by the manufacturer. We are issuing this AD to prevent
interference between the compensator and the guide assembly of probe
no. 1, which could create an ignition source that could result in a
fire or explosion.
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.
Measurement
(f) Within 4,000 flight hours after the effective date of this
AD, measure the clearance between the compensator and the guide
assembly of probe no. 1 on the left- and right-hand outboard fuel
tanks, in accordance with the Accomplishment Instructions of Airbus
Service Bulletin A310-28-2152, dated January 12, 2004. If the
clearance between the compensator and the guide assembly is less
than 3 mm, before further flight, modify the guide assembly of probe
no. 1 to provide clearance of 3 mm or more between the compensator
and the guide assembly, in accordance with the Accomplishment
Instructions of the service bulletin.
Parts Installation
(g) As of the effective date of this AD, no person may install
probe no. 1 on the left-or right-hand outboard fuel tank unless the
requirements of paragraph (f) of this AD have been accomplished.
[[Page 24938]]
Alternative Methods of Compliance (AMOCs)
(h) 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.
Related Information
(i) French airworthiness directive F-2004-125, dated July 21,
2004, also addresses the subject of this AD.
Material Incorporated by Reference
(j) You must use Airbus Service Bulletin A310-28-2152, dated
January 12, 2004, to perform the actions that are required by this
AD, unless the AD specifies otherwise. The Director of the Federal
Register approves the incorporation by reference of this document in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. To get copies of
the service information, contact Airbus, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France. To view the AD docket, go to
the Docket Management Facility, U.S. Department of Transportation,
400 Seventh Street SW., room PL-401, Nassif Building, Washington,
DC. To review copies of the service information, contact 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 April 29, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-9063 Filed 5-11-05; 8:45 am]
BILLING CODE 4910-13-P
