Airworthiness Directives; AvCraft Dornier Model 328-100 Airplanes, 36470-36472 [05-12304]
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<![CDATA[
36470
Federal Register / Vol. 70, No. 121 / Friday, June 24, 2005 / Rules and Regulations
requires no additional forms. The
information will be recorded by the
inspector on the inspection certificate.
In accordance with the Paperwork
Reduction Act of 1995 (44 U.S.C.
Chapter 35), AMS has received OMB
approval for the information collection
requirements for this marketing order
program. These requirements are
approved under the Fruit Crops
collection package, OMB No. 0581–0189
OMB. The reporting modifications made
by this rule are small and will have no
impact on the overall total burden hours
approved by OMB.
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. In addition, USDA has
not identified any relevant Federal rules
that duplicate, overlap or conflict with
this rule.
Further, the Committee’s meetings
were widely publicized throughout the
avocado industry and all interested
persons were invited to attend and
participate in Committee deliberations.
Like all Committee meetings, the
September 8, 2004, and November 10,
2004, meetings were public meetings
and all entities, both large and small,
were able to express their views on
these issues. Finally, interested persons
are invited to submit information on the
regulatory and informational impacts of
this action on small businesses.
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
address in the FOR FURTHER INFORMATION
CONTACT section.
This rule invites comments on
changes to the container and reporting
requirements currently prescribed under
the Florida avocado marketing order.
Any comments received will be
considered prior to finalization of this
rule.
After consideration of all relevant
material presented, including the
Committee’s recommendations, and
other information, it is found that this
interim final rule, as hereinafter set
forth, will tend to effectuate the
declared policy of the Act.
Pursuant to 5 U.S.C. 553, it is also
found and determined upon good cause
that it is impracticable, unnecessary,
and contrary to the public interest to
give preliminary notice prior to putting
this rule into effect and that good cause
exists for not postponing the effective
date of this rule until 30 days after
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16:42 Jun 23, 2005
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publication in the Federal Register
because: (1) The Committee
unanimously recommended these
changes at public meetings and
interested parties had an opportunity to
provide input; (2) growers and handlers
are aware of these changes; (3) the
Florida avocado shipping season started
May 16, 2005; and (4) this rule provides
a 60-day comment period and any
comments received will be considered
prior to finalization of this rule.
DEPARTMENT OF TRANSPORTATION
List of Subjects in 7 CFR Part 915
AGENCY:
Avocados, Marketing agreements,
Reporting and recordkeeping
requirements.
For the reasons set forth in the
preamble, 7 CFR part 915 is amended as
follows:
I
PART 915—AVOCADOS GROWN IN
SOUTH FLORIDA
1. The authority citation for 7 CFR part
915 continues to read as follows:
I
Authority: 7 U.S.C. 601–674.
2. Section 915.150 is amended by
adding paragraph (e) to read as follows:
I
§ 915.150
Reports.
*
*
*
*
*
(e) At the time of inspection, each
handler shall provide to the FederalState Inspection Service the quantity
and size of containers being packed and
inspected for the fresh avocado market.
In addition, each handler shall provide
the number of avocados packed per
container (count per container).
3. Section 915.305 is amended by
adding paragraph (c) to read as follows:
I
§ 915.305 Florida Avocado Container
Regulation 5.
*
*
*
*
*
(c) No handler shall handle any
avocados for the fresh market in 20
bushel plastic field bins to destinations
inside the production area.
Dated: June 20, 2005.
Kenneth C. Clayton,
Acting Administrator, Agricultural Marketing
Service.
[FR Doc. 05–12616 Filed 6–21–05; 3:37 pm]
BILLING CODE 3410–02–P
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Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–21053; Directorate
Identifier 2005–NM–053–AD; Amendment
39–14161; AD 2005–13–24]
RIN 2120–AA64
Airworthiness Directives; AvCraft
Dornier Model 328–100 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all
AvCraft Dornier Model 328–100
airplanes. This AD requires modifying
the electrical wiring of the fuel pumps;
installing insulation at the hand flow
control and shut-off valves, and other
components of the environmental
control system; and installing markings
at fuel wiring harnesses. This AD also
requires revising the Airworthiness
Limitations section of the Instructions
for Continued Airworthiness to
incorporate new inspections of the fuel
tank system. This AD is prompted by
the results of fuel system reviews
conducted by the airplane
manufacturer. We are issuing this AD to
reduce the potential of ignition sources
inside fuel tanks, which, in combination
with flammable fuel vapors, could result
in fuel tank explosions and consequent
loss of the airplane.
DATES: This AD becomes effective July
29, 2005.
The incorporation by reference of
certain publications listed in the AD is
approved by the Director of the Federal
Register as of July 29, 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–2005–21053; the directorate
identifier for this docket is 2005–NM–
053–AD.
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Federal Register / Vol. 70, No. 121 / Friday, June 24, 2005 / Rules and Regulations
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 AvCraft Dornier Model
328–100 airplanes. That action,
published in the Federal Register on
April 26, 2005 (70 FR 21344), proposed
to require modifying the electrical
wiring of the fuel pumps; installing
insulation at the hand flow control and
shut-off valves, and other components
of the environmental control system;
and installing markings at fuel wiring
harnesses. That action also proposed to
require revising the Airworthiness
Limitations section of the Instructions
for Continued Airworthiness to
incorporate new inspections of the fuel
tank system.
FOR FURTHER INFORMATION CONTACT:
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.
Explanation of Changes to Applicability
and Reference Service Bulletin
We have revised the applicability of
the proposed AD to identify model
designations as published in the most
recent type certificate data sheet for the
affected models. We also have revised
the airplane manufacturer’s name of the
referenced service bulletin, Dornier
Service Bulletin SB–328–00–445, dated
August 23, 2004, to ‘‘AvCraft.’’
Conclusion
We have carefully reviewed the
available data 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 will affect about 6 airplanes
of U.S. registry. The required actions
will take about 70 work hours per
airplane, at an average labor rate of $65
per work hour. Required parts will cost
about $14,118 per airplane. Based on
these figures, the estimated cost of the
AD for U.S. operators is $112,008, or
$18,668 per airplane.
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.
36471
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 FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
I
2005–13–24 AvCraft Aerospace GmbH
(Formerly Fairchild Dornier GmbH):
Amendment 39–14161. Docket No.
FAA–2005–21053; Directorate Identifier
2005–NM–053–AD.
Effective Date
(a) This AD becomes effective July 29,
2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all AvCraft Dornier
Model 328–100 airplanes, certificated in any
category.
Unsafe Condition
(d) This AD was prompted by the results
of fuel system reviews conducted by the
airplane manufacturer. We are issuing this
AD to reduce the potential of ignition sources
inside fuel tanks, which, in combination with
flammable fuel vapors, could result in fuel
tank explosions and consequent loss 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.
Modification and Installations
(f) Within 12 months after the effective
date of this AD, do the actions in Table 1 of
this AD in accordance with the
Accomplishment Instructions of AvCraft
Service Bulletin SB–328–00–445, dated
August 23, 2004.
TABLE 1.—REQUIREMENTS
Do the following actions—
By accomplishing all the actions specified in—
(1) Modify the electrical wiring of the left-hand and right-hand fuel pumps ...................................
(2) Install insulation at the left-hand and right-hand flow control and shut-off valves, and other
components of the environmental control system.
(3) Install markings at fuel wiring harnesses ..................................................................................
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Paragraph 2.B(1) of the service bulletin.
Paragraph 2.B(2) of the service bulletin.
Paragraph 2.B(3) of the service bulletin.
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36472
Federal Register / Vol. 70, No. 121 / Friday, June 24, 2005 / Rules and Regulations
Revision to Airworthiness Limitations
(g) Within 12 months after the effective
date of this AD, revise the Airworthiness
Limitations section of the Instructions for
Continued Airworthiness by inserting a copy
of Dornier Temporary Revision ALD–080,
dated October 15, 2003, into the Dornier 328
Airworthiness Limitations Document.
Thereafter, except as provided in paragraph
(h) of this AD, no alternative inspection
intervals may be approved for this fuel tank
system.
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) German airworthiness directive D–
2005–001, dated January 26, 2005, also
addresses the subject of this AD.
Material Incorporated by Reference
(j) You must use the service information
specified in Table 2 of this AD 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 these
documents in accordance with 5 U.S.C.
552(a) and 1 CFR part 51. To get copies of
the service information, contact AvCraft
Aerospace GmbH, P.O. Box 1103, D–82230
Wessling, Germany. 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, go 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.
TABLE 2.—MATERIAL INCORPORATED BY REFERENCE
Service information
Date
AvCraft Service Bulletin SB–328–00–445, including Price Information Sheet ...........................................................................
Dornier Temporary Revision ALD–080 .......................................................................................................................................
Issued in Renton, Washington, on June 15,
2005.
Kevin Mullin,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 05–12304 Filed 6–23–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2002–NM–332–AD; Amendment
39–14158; AD 2005–13–21]
RIN 2120–AA64
Airworthiness Directives; Cessna
Model 650 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: This amendment adopts a
new airworthiness directive (AD),
applicable to all Cessna Model 650
airplanes, that requires inspecting to
determine the part number of the
actuator control unit (ACU) and
replacing the ACU with a new,
improved ACU if necessary. This AD
also requires revising the Limitations
section of the airplane flight manual.
The actions specified by this AD are
intended to prevent uncommanded
movement of the horizontal stabilizer,
which could result in reduced
controllability of the airplane. This
action is intended to address the
identified unsafe condition.
DATES: Effective July 29, 2005.
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16:42 Jun 23, 2005
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The incorporation by reference of
certain publications listed in the
regulations is approved by the Director
of the Federal Register as of July 29,
2005.
The service information
referenced in this AD may be obtained
from Cessna Aircraft Co., P.O. Box 7706,
Wichita, Kansas 67277. This
information may be examined at the
Federal Aviation Administration (FAA),
Transport Airplane Directorate, Rules
Docket, 1601 Lind Avenue, SW.,
Renton, Washington; or at the FAA,
Wichita Aircraft Certification Office,
1801 Airport Road, Room 100, MidContinent Airport, Wichita, Kansas.
ADDRESSES:
FOR FURTHER INFORMATION CONTACT:
Robert P. Busto, Aerospace Engineer,
Systems and Propulsion Branch, ACE–
116W, FAA, Wichita Aircraft
Certification Office, 1801 Airport Road,
Room 100, Mid-Continent Airport,
Wichita, Kansas 67209; telephone (316)
946–4157; fax (316) 946–4107.
A
proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to
include an airworthiness directive (AD)
that is applicable to all Cessna Model
650 airplanes was published as a
supplemental notice of proposed
rulemaking (NPRM) in the Federal
Register on April 22, 2005 (70 FR
20844). That action proposed to require
inspecting to determine the part number
of the actuator control unit (ACU) and
replacing the ACU with a new,
improved ACU if necessary. That action
also proposed to require revising the
Limitations section of the airplane flight
manual.
SUPPLEMENTARY INFORMATION:
PO 00000
Frm 00006
Fmt 4700
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August 23, 2004.
October 15, 2003.
Comments
Interested persons have been afforded
an opportunity to participate in the
making of this amendment. We did not
receive any comments on the proposed
AD.
Conclusion
After careful review of the available
data, the FAA has determined that air
safety and the public interest require the
adoption of the rule as proposed.
Cost Impact
There are approximately 357
airplanes of the affected design in the
worldwide fleet. The FAA estimates that
285 airplanes of U.S. registry will be
affected by this AD.
We estimate that it will take
approximately 2 work hours per
airplane to replace the ACU, and that
the average labor rate is $65 per work
hour. Required parts will cost
approximately $3,000 per airplane, if
the ACU is exchanged. Based on these
figures, the cost impact of the AD on
U.S. operators is estimated to be
$892,050, or $3,130 per airplane.
The cost impact figure discussed
above is based on assumptions that no
operator has yet accomplished any of
the requirements of this AD action, and
that no operator would accomplish
those actions in the future if this AD
were not adopted. The cost impact
figures discussed in AD rulemaking
actions represent only the time
necessary to perform the specific actions
actually required by the AD. These
figures typically do not include
incidental costs, such as the time
required to gain access and close up,
planning time, or time necessitated by
E:\FR\FM\24JNR1.SGM
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]]>Agencies
[Federal Register Volume 70, Number 121 (Friday, June 24, 2005)]
[Rules and Regulations]
[Pages 36470-36472]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-12304]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-21053; Directorate Identifier 2005-NM-053-AD;
Amendment 39-14161; AD 2005-13-24]
RIN 2120-AA64
Airworthiness Directives; AvCraft Dornier Model 328-100 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
AvCraft Dornier Model 328-100 airplanes. This AD requires modifying the
electrical wiring of the fuel pumps; installing insulation at the hand
flow control and shut-off valves, and other components of the
environmental control system; and installing markings at fuel wiring
harnesses. This AD also requires revising the Airworthiness Limitations
section of the Instructions for Continued Airworthiness to incorporate
new inspections of the fuel tank system. This AD is prompted by the
results of fuel system reviews conducted by the airplane manufacturer.
We are issuing this AD to reduce the potential of ignition sources
inside fuel tanks, which, in combination with flammable fuel vapors,
could result in fuel tank explosions and consequent loss of the
airplane.
DATES: This AD becomes effective July 29, 2005.
The incorporation by reference of certain publications listed in
the AD is approved by the Director of the Federal Register as of July
29, 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-2005-21053; the directorate
identifier for this docket is 2005-NM-053-AD.
[[Page 36471]]
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 AvCraft Dornier Model 328-100 airplanes. That
action, published in the Federal Register on April 26, 2005 (70 FR
21344), proposed to require modifying the electrical wiring of the fuel
pumps; installing insulation at the hand flow control and shut-off
valves, and other components of the environmental control system; and
installing markings at fuel wiring harnesses. That action also proposed
to require revising the Airworthiness Limitations section of the
Instructions for Continued Airworthiness to incorporate new inspections
of the fuel tank system.
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.
Explanation of Changes to Applicability and Reference Service Bulletin
We have revised the applicability of the proposed AD to identify
model designations as published in the most recent type certificate
data sheet for the affected models. We also have revised the airplane
manufacturer's name of the referenced service bulletin, Dornier Service
Bulletin SB-328-00-445, dated August 23, 2004, to ``AvCraft.''
Conclusion
We have carefully reviewed the available data 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 will affect about 6 airplanes of U.S. registry. The
required actions will take about 70 work hours per airplane, at an
average labor rate of $65 per work hour. Required parts will cost about
$14,118 per airplane. Based on these figures, the estimated cost of the
AD for U.S. operators is $112,008, or $18,668 per airplane.
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):
2005-13-24 AvCraft Aerospace GmbH (Formerly Fairchild Dornier GmbH):
Amendment 39-14161. Docket No. FAA-2005-21053; Directorate
Identifier 2005-NM-053-AD.
Effective Date
(a) This AD becomes effective July 29, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all AvCraft Dornier Model 328-100
airplanes, certificated in any category.
Unsafe Condition
(d) This AD was prompted by the results of fuel system reviews
conducted by the airplane manufacturer. We are issuing this AD to
reduce the potential of ignition sources inside fuel tanks, which,
in combination with flammable fuel vapors, could result in fuel tank
explosions and consequent loss 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.
Modification and Installations
(f) Within 12 months after the effective date of this AD, do the
actions in Table 1 of this AD in accordance with the Accomplishment
Instructions of AvCraft Service Bulletin SB-328-00-445, dated August
23, 2004.
Table 1.--Requirements
------------------------------------------------------------------------
By accomplishing all the
Do the following actions-- actions specified in--
------------------------------------------------------------------------
(1) Modify the electrical wiring of the left- Paragraph 2.B(1) of the
hand and right-hand fuel pumps. service bulletin.
(2) Install insulation at the left-hand and Paragraph 2.B(2) of the
right-hand flow control and shut-off valves, service bulletin.
and other components of the environmental
control system.
(3) Install markings at fuel wiring harnesses Paragraph 2.B(3) of the
service bulletin.
------------------------------------------------------------------------
[[Page 36472]]
Revision to Airworthiness Limitations
(g) Within 12 months after the effective date of this AD, revise
the Airworthiness Limitations section of the Instructions for
Continued Airworthiness by inserting a copy of Dornier Temporary
Revision ALD-080, dated October 15, 2003, into the Dornier 328
Airworthiness Limitations Document. Thereafter, except as provided
in paragraph (h) of this AD, no alternative inspection intervals may
be approved for this fuel tank system.
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) German airworthiness directive D-2005-001, dated January 26,
2005, also addresses the subject of this AD.
Material Incorporated by Reference
(j) You must use the service information specified in Table 2 of
this AD 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 these documents in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. To get copies of
the service information, contact AvCraft Aerospace GmbH, P.O. Box
1103, D-82230 Wessling, Germany. 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, go 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.
Table 2.--Material Incorporated by Reference
------------------------------------------------------------------------
Service information Date
------------------------------------------------------------------------
AvCraft Service Bulletin SB-328-00-445, August 23, 2004.
including Price Information Sheet.
Dornier Temporary Revision ALD-080......... October 15, 2003.
------------------------------------------------------------------------
Issued in Renton, Washington, on June 15, 2005.
Kevin Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-12304 Filed 6-23-05; 8:45 am]
BILLING CODE 4910-13-P
