Airworthiness Directives; Airbus Model A320-111 Airplanes, and Model A320-200 Series Airplanes, 76973-76974 [05-24525]
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sroberts on PROD1PC70 with RULES
Federal Register / Vol. 70, No. 249 / Thursday, December 29, 2005 / Rules and Regulations
Therefore, the Executive
Subcommittee and committee agreed
that $0.65 per ton of salable dried
prunes is an acceptable assessment rate.
The committee is authorized to use
excess assessment funds from the 2004–
05 crop year (currently estimated at
$13,000) for up to 5 months beyond the
end of the crop year to meet 2003–04
crop year expenses. At the end of the 5
months, the committee either refunds or
credits excess funds to handlers
(§ 993.81(c)).
This action continues in effect the
action that decreased the assessment
obligation imposed on handlers.
Assessments are applied uniformly on
all handlers, and some of the costs may
be passed on to producers. However,
decreasing the assessment rate reduces
the burden on handlers, and may reduce
the burden on producers. In addition,
the committee’s meeting was widely
publicized throughout the California
dried prune industry and all interested
persons were invited to attend the
meeting and participate in committee
deliberations on all issues. Like all
committee meetings, the June 30, 2005,
meeting was a public meeting and all
entities, both large and small, were
encouraged to express views on this
issue.
This action imposes no additional
reporting or recordkeeping requirements
on either small or large California dried
prune handlers. As with all Federal
marketing order programs, reports and
forms are periodically reviewed to
reduce information requirements and
duplication by industry and public
sector agencies.
USDA has not identified any relevant
Federal rules that duplicate, overlap, or
conflict with this rule.
An interim final rule concerning this
action was published in the Federal
Register on September 15, 2005. The
committee staff mailed copies of the
rule to all committee members,
alternates, and prune handlers. In
addition, the rule was made available
through the Internet by the Office of the
Federal Register and USDA. That rule
provided for a 60-day comment period
which ended November 14, 2005. Three
comments were received. Two
comments were not relevant to the
rulemaking action, and one comment
supported the reduced assessment rate
for prunes.
A small business guide on complying
with fruit, vegetable, and specialty crop
marketing agreements and orders may
be viewed at: https://www.ams.usda.gov/
fv/moab/html. Any questions about the
compliance guide should be sent to Jay
Guerber at the previously mentioned
VerDate Aug<31>2005
19:06 Dec 28, 2005
Jkt 208001
address in the FOR FURTHER INFORMATION
CONTACT section.
After consideration of all relevant
material presented, including the
information and recommendation
submitted by the committee and other
available information, it is hereby found
that this rule, as hereinafter set forth,
will tend to effectuate the declared
policy of the Act.
List of Subjects in 7 CFR Part 993
Marketing agreements, Plums, Prunes,
Reporting and recordkeeping
requirements.
For the reasons set forth in the
preamble, 7 CFR part 993 is amended as
follows:
I
PART 993—DRIED PRUNES
PRODUCED IN CALIFORNIA
Accordingly, the interim final rule
amending 7 CFR part 993 which was
published at 70 FR 54469 on September
15, 2005, is adopted as a final rule
without change.
I
Dated: December 22, 2005.
Lloyd C. Day,
Administrator, Agricultural Marketing
Service.
[FR Doc. 05–24544 Filed 12–28–05; 8:45 am]
BILLING CODE 3410–02–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2002–NM–298–AD; Amendment
39–14354; AD 2005–22–10 R1]
RIN 2120–AA64
Airworthiness Directives; Airbus Model
A320–111 Airplanes, and Model A320–
200 Series Airplanes
Federal Aviation
Administration, DOT.
ACTION: Final rule; correction.
AGENCY:
SUMMARY: This document corrects
information in an existing airworthiness
directive (AD) that applies to certain
Airbus Model A320–111 airplanes, and
Model A320–200 series airplanes. That
AD currently requires a detailed
inspection of the tail cone triangle to
determine its position, and corrective
actions if necessary. This document
corrects the applicability by specifying
that the AD affects only airplanes
identified in Airbus Service Bulletin
A320–27–1132, Revision 01, dated June
19, 2002. This correction is necessary to
ensure that only affected airplanes are
subject to the requirements of the AD.
PO 00000
Frm 00003
Fmt 4700
Sfmt 4700
76973
Effective December 5, 2005.
The incorporation by reference of a
certain publication listed in the
regulations was approved previously by
the Director of the Federal Register as of
December 5, 2005 (70 FR 62232, October
31, 2005).
FOR FURTHER INFORMATION CONTACT: Tim
Dulin, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–2141;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION: On
October 20, 2005, the Federal Aviation
Administration (FAA) issued AD 2005–
22–10, amendment 39–14354 (70 FR
62232, October 31, 2005), which applies
to certain Airbus Model A320–111
airplanes, and Model A320–200 series
airplanes. That AD requires a detailed
inspection of the tail cone triangle to
determine its position, and corrective
actions if necessary. That AD was
prompted by a report that the tail cone
triangles were not installed properly on
certain airplanes during production,
resulting in possible mis-rigged elevator
servo-controls. The actions required by
that AD are intended to prevent
excessive vibrations of the elevators,
which could result in reduced structural
integrity and reduced controllability of
the airplane.
DATES:
Need for the Correction
Information obtained recently by the
FAA indicates that we inadvertently
changed the applicability from that
specified in the Notice of Proposed
Rulemaking by omitting from the
statement of applicability of AD 2005–
22–10 that airplanes affected by the AD
are those identified in Airbus Service
Bulletin A320–27–1132, Revision 01,
dated June 19, 2002.
The FAA has determined that a
correction to AD 2005–22–10 is
necessary. The correction will revise the
applicability to include a reference to
Airbus Service Bulletin A320–27–1132,
Revision 01, dated June 19, 2002.
Correction of Publication
This document corrects the error and
correctly adds the AD as an amendment
to section 39.13 of the Federal Aviation
Regulations (14 CFR 39.13).
The AD is reprinted in its entirety for
the convenience of affected operators.
The effective date of the AD remains
December 5, 2005.
Since this action reduces the number
of airplanes affected by revising the
applicability, it has no adverse
economic impact and imposes no
additional burden on any person.
E:\FR\FM\29DER1.SGM
29DER1
76974
Federal Register / Vol. 70, No. 249 / Thursday, December 29, 2005 / Rules and Regulations
Actions Accomplished Per Previous Release
of the Service Bulletin
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
(b) Actions accomplished prior to the
effective date of this AD in accordance with
Airbus Service Bulletin A320–27–1132,
dated March 14, 2001, are considered
acceptable for compliance with the
corresponding actions required by this AD.
Adoption of the Correction
No Reporting Requirement
RIN 2120–AI08
Therefore, the FAA has determined that
notice and public procedures are
unnecessary.
List of Subjects in 14 CFR Part 39
Accordingly, pursuant to the authority
delegated to me by the Administrator,
the Federal Aviation Administration
amends part 39 of the Federal Aviation
Regulations (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
[Corrected]
2. Section 39.13 is amended by
correctly adding the following
airworthiness directive (AD):
I
Detailed Inspection and Corrective Action
sroberts on PROD1PC70 with RULES
(a) Within 800 flight hours after the
effective date of this AD, perform a detailed
inspection to determine the position of each
tail cone triangle in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A320–27–1132, Revision 01,
dated June 19, 2002. If the position of the tail
cone triangle is not within the limits
specified in the service bulletin: Within
3,500 flight hours after the inspection, re-rig
the elevator servo controls to adjust the
elevator neutral setting, and change the
position of the tail cone triangle, in
accordance with the service bulletin.
Note 1: For the purposes of this AD, a
detailed inspection is defined as: ‘‘An
intensive visual examination of a specific
structural area, system, installation, or
assembly to detect damage, failure, or
irregularity. Available lighting is normally
supplemented with a direct source of good
lighting at intensity deemed appropriate by
the inspector. Inspection aids such as mirror,
magnifying lenses, etc., may be used. Surface
cleaning and elaborate access procedures
may be required.’’
19:06 Dec 28, 2005
Jkt 208001
Alternative Methods of Compliance
(d)(1) In accordance with 14 CFR 39.19, the
Manager, International Branch, ANM–116,
Transport Airplane Directorate, FAA, is
authorized to approve alternative methods of
compliance for this AD.
(2) Before using any AMOC approved in
accordance with § 39.19 on any airplane to
which the AMOC applies, notify the
appropriate principal inspector in the FAA
Flight Standards Certificate Holding District
Office.
Incorporation by Reference
2005–22–10 R1 Airbus: Amendment 39–
14354. Docket 2002–NM–298–AD.
Applicability: Model A320–111, –211,
–212, –214, –231, –232, and –233 airplanes,
certificated in any category; as listed in
Airbus Service Bulletin A320–27–1132,
Revision 01, dated June 19, 2002.
Compliance: Required as indicated, unless
accomplished previously.
To prevent excessive vibrations of the
elevators, which could result in reduced
structural integrity and reduced
controllability of the airplane, accomplish
the following:
VerDate Aug<31>2005
(c) Although the service bulletin specifies
to submit certain information to the
manufacturer, this AD does not include such
a requirement.
(e) Unless otherwise specified in this AD,
the actions must be done in accordance with
Airbus Service Bulletin A320–27–1132,
Revision 01, excluding Appendix 01, dated
June 19, 2002. This incorporation by
reference was approved previously by the
Director of the Federal Register as of
December 5, 2005 (70 FR 62232, October 31,
2005). To get copies of this service
information, contact Airbus, 1 Rond Point
Maurice Bellonte, 31707 Blagnac Cedex,
France. To inspect copies of this service
information, go to the FAA, Transport
Airplane Directorate, 1601 Lind Avenue,
SW., Renton, Washington; or to 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.
Note 2: The subject of this AD is addressed
in French airworthiness directive 2002–
514(B) R1, dated November 13, 2002.
Effective Date
(f) The effective date of this amendment
remains December 5, 2005.
Issued in Renton, Washington, on
December 15, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–24525 Filed 12–28–05; 8:45 am]
BILLING CODE 4910–13–P
PO 00000
Frm 00004
Fmt 4700
Sfmt 4700
14 CFR Parts 121, 125, 135, and 145
[Docket No. FAA–2000–7952; Amendment
Nos. 121–319, 125–49, 135–102, and 145–
26]
Service Difficulty Reports
Federal Aviation
Administration, DOT.
ACTION: Final rule and withdrawal of
delayed final rule.
AGENCY:
SUMMARY: The Federal Aviation
Administration (FAA) is withdrawing a
delayed final rule published on
September 15, 2000. That final rule
would have amended the reporting
requirements for certificate holders
concerning failures, malfunctions, and
defects of aircraft, aircraft engines,
systems, and components. We are
withdrawing this rule to allow the FAA
time to re-examine the service difficulty
report (SDR) program and consider the
comments received since the delayed
final rule was published.
In this action we are also adopting
several amendments that improve the
functioning of the SDR program.
DATES: This amendment becomes
effective January 30, 2006.
FOR FURTHER INFORMATION CONTACT:
Emilio Estrada, Flight Standards
Service, Aircraft Maintenance Division
(AFS–300), Federal Aviation
Administration, 800 Independence
Avenue, SW., Washington, DC 20591,
telephone (202) 267–5571, e-mail
emilio.estrada@faa.gov.
SUPPLEMENTARY INFORMATION:
Availability of Rulemaking Documents
You can get an electronic copy of
rulemaking documents using the
Internet by—
(1) Searching the Department of
Transportation’s electronic Docket
Management System (DMS) Web site
(https://dms.dot.gov/search);
(2) Visiting the FAA’s Regulations and
Policies Web page at https://
www.faa.gov/regulations_policies/; or
(3) Accessing the Government
Printing Office’s Web page at https://
www.gpoaccess.gov/fr/.
You can also get a copy by sending a
request to the Federal Aviation
Administration, Office of Rulemaking,
ARM–1, 800 Independence Avenue
SW., Washington, DC 20591, or by
calling (202) 267–9680. Make sure to
identify the amendment number or
docket number of this rulemaking.
E:\FR\FM\29DER1.SGM
29DER1
]]>Agencies
[Federal Register Volume 70, Number 249 (Thursday, December 29, 2005)]
[Rules and Regulations]
[Pages 76973-76974]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-24525]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2002-NM-298-AD; Amendment 39-14354; AD 2005-22-10 R1]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A320-111 Airplanes, and
Model A320-200 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document corrects information in an existing
airworthiness directive (AD) that applies to certain Airbus Model A320-
111 airplanes, and Model A320-200 series airplanes. That AD currently
requires a detailed inspection of the tail cone triangle to determine
its position, and corrective actions if necessary. This document
corrects the applicability by specifying that the AD affects only
airplanes identified in Airbus Service Bulletin A320-27-1132, Revision
01, dated June 19, 2002. This correction is necessary to ensure that
only affected airplanes are subject to the requirements of the AD.
DATES: Effective December 5, 2005.
The incorporation by reference of a certain publication listed in
the regulations was approved previously by the Director of the Federal
Register as of December 5, 2005 (70 FR 62232, October 31, 2005).
FOR FURTHER INFORMATION CONTACT: Tim Dulin, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2141; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: On October 20, 2005, the Federal Aviation
Administration (FAA) issued AD 2005-22-10, amendment 39-14354 (70 FR
62232, October 31, 2005), which applies to certain Airbus Model A320-
111 airplanes, and Model A320-200 series airplanes. That AD requires a
detailed inspection of the tail cone triangle to determine its
position, and corrective actions if necessary. That AD was prompted by
a report that the tail cone triangles were not installed properly on
certain airplanes during production, resulting in possible mis-rigged
elevator servo-controls. The actions required by that AD are intended
to prevent excessive vibrations of the elevators, which could result in
reduced structural integrity and reduced controllability of the
airplane.
Need for the Correction
Information obtained recently by the FAA indicates that we
inadvertently changed the applicability from that specified in the
Notice of Proposed Rulemaking by omitting from the statement of
applicability of AD 2005-22-10 that airplanes affected by the AD are
those identified in Airbus Service Bulletin A320-27-1132, Revision 01,
dated June 19, 2002.
The FAA has determined that a correction to AD 2005-22-10 is
necessary. The correction will revise the applicability to include a
reference to Airbus Service Bulletin A320-27-1132, Revision 01, dated
June 19, 2002.
Correction of Publication
This document corrects the error and correctly adds the AD as an
amendment to section 39.13 of the Federal Aviation Regulations (14 CFR
39.13).
The AD is reprinted in its entirety for the convenience of affected
operators. The effective date of the AD remains December 5, 2005.
Since this action reduces the number of airplanes affected by
revising the applicability, it has no adverse economic impact and
imposes no additional burden on any person.
[[Page 76974]]
Therefore, the FAA has determined that notice and public procedures are
unnecessary.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Correction
0
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends part 39 of
the Federal Aviation Regulations (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 [Corrected]
0
2. Section 39.13 is amended by correctly adding the following
airworthiness directive (AD):
2005-22-10 R1 Airbus: Amendment 39-14354. Docket 2002-NM-298-AD.
Applicability: Model A320-111, -211, -212, -214, -231, -232, and
-233 airplanes, certificated in any category; as listed in Airbus
Service Bulletin A320-27-1132, Revision 01, dated June 19, 2002.
Compliance: Required as indicated, unless accomplished
previously.
To prevent excessive vibrations of the elevators, which could
result in reduced structural integrity and reduced controllability
of the airplane, accomplish the following:
Detailed Inspection and Corrective Action
(a) Within 800 flight hours after the effective date of this AD,
perform a detailed inspection to determine the position of each tail
cone triangle in accordance with the Accomplishment Instructions of
Airbus Service Bulletin A320-27-1132, Revision 01, dated June 19,
2002. If the position of the tail cone triangle is not within the
limits specified in the service bulletin: Within 3,500 flight hours
after the inspection, re-rig the elevator servo controls to adjust
the elevator neutral setting, and change the position of the tail
cone triangle, in accordance with the service bulletin.
Note 1: For the purposes of this AD, a detailed inspection is
defined as: ``An intensive visual examination of a specific
structural area, system, installation, or assembly to detect damage,
failure, or irregularity. Available lighting is normally
supplemented with a direct source of good lighting at intensity
deemed appropriate by the inspector. Inspection aids such as mirror,
magnifying lenses, etc., may be used. Surface cleaning and elaborate
access procedures may be required.''
Actions Accomplished Per Previous Release of the Service Bulletin
(b) Actions accomplished prior to the effective date of this AD
in accordance with Airbus Service Bulletin A320-27-1132, dated March
14, 2001, are considered acceptable for compliance with the
corresponding actions required by this AD.
No Reporting Requirement
(c) Although the service bulletin specifies to submit certain
information to the manufacturer, this AD does not include such a
requirement.
Alternative Methods of Compliance
(d)(1) In accordance with 14 CFR 39.19, the Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
is authorized to approve alternative methods of compliance for this
AD.
(2) Before using any AMOC approved in accordance with Sec.
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Incorporation by Reference
(e) Unless otherwise specified in this AD, the actions must be
done in accordance with Airbus Service Bulletin A320-27-1132,
Revision 01, excluding Appendix 01, dated June 19, 2002. This
incorporation by reference was approved previously by the Director
of the Federal Register as of December 5, 2005 (70 FR 62232, October
31, 2005). To get copies of this service information, contact
Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France.
To inspect copies of this service information, go to the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington; or to 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.
Note 2: The subject of this AD is addressed in French
airworthiness directive 2002-514(B) R1, dated November 13, 2002.
Effective Date
(f) The effective date of this amendment remains December 5,
2005.
Issued in Renton, Washington, on December 15, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-24525 Filed 12-28-05; 8:45 am]
BILLING CODE 4910-13-P
