Airworthiness Directives; BAE Systems (Operations) Limited Model ATP Airplanes, 58293-58295 [05-19833]
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Federal Register / Vol. 70, No. 193 / Thursday, October 6, 2005 / Rules and Regulations
Authority: 7 U.S.C. 8301–8317; 7 CFR 2.22,
2.80, and 371.4.
2. In § 77.7, paragraph (b) is revised to
read as follows:
I
§ 77.7
Accredited-free States or zones.
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*
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(b) The following are accredited-free
zones:
(1) A zone in Michigan known as the
Upper Peninsula that comprises Alger,
Baraga, Chippewa, Delta, Dickinson,
Gogebic, Houghton, Iron, Keweenaw,
Luce, Mackinac, Marquette,
Menominee, Ontonagon, and
Schoolcraft Counties.
(2) All of the State of New Mexico
except for the zone that comprises those
portions of Curry and Roosevelt
Counties, NM, described in § 77.9(b)(2).
*
*
*
*
*
I 3. In § 77.9, paragraph (b)(1) is revised
to read as follows.
§ 77.9 Modified accredited advanced
States or zones.
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*
*
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(b) * * *
(1) The following are modified
accredited advanced zones: All of the
State of Michigan except for the zones
that comprise those counties or portions
of counties in Michigan described in
§ 77.7(b)(1) and § 77.11(b).
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Done in Washington, DC, this 30th day of
September 2005.
W. Ron DeHaven,
Administrator, Animal and Plant Health
Inspection Service.
[FR Doc. 05–20098 Filed 10–5–05; 8:45 am]
653, 654, and 655 on July 14, 2005 (70
FR 40635). This final rule ensures that
the Federal Agricultural Mortgage
Corporation (Farmer Mac) continues to
hold high-quality, liquid investments to
maintain a sufficient liquidity reserve,
invest surplus funds, and manage
interest-rate risk, while maintaining
non-program investments at appropriate
levels considering Farmer Mac’s status
as a Government-sponsored enterprise.
In accordance with 12 U.S.C. 2252, the
effective date of the final rule is 30 days
from the date of publication in the
Federal Register during which either or
both Houses of Congress are in session.
Based on the records of the sessions of
Congress, the effective date of the
regulation is September 30, 2005.
EFFECTIVE DATE: The regulation
amending 12 CFR parts 620, 621, 650,
651, 652, 653, 654, and 655 published
on July 14, 2005 (70 FR 40635) is
effective September 30, 2005.
FOR FURTHER INFORMATION CONTACT:
Joseph T. Connor, Associate Director for
Policy and Analysis Office of Secondary
Market Oversight, Farm Credit
Administration, McLean, VA 22102–
5090, (703) 883–4364, TTY (703) 883–
4434; or Jennifer A. Cohn, Senior
Attorney, Office of General Counsel,
Farm Credit Administration, McLean,
VA 22102–5090, (703) 883–4020, TTY
(703) 883–4020.
(12 U.S.C. 2252(a)(9) and (10))
Dated: September 30, 2005.
Jeanette C. Brinkley,
Secretary, Farm Credit Administration Board.
[FR Doc. 05–20036 Filed 10–5–05; 8:45 am]
BILLING CODE 3410–34–P
BILLING CODE 6705–01–P
FARM CREDIT ADMINISTRATION
DEPARTMENT OF TRANSPORTATION
12 CFR Parts 620, 621, 650, 651, 652,
653, 654, and 655
Federal Aviation Administration
14 CFR Part 39
RIN 3052–AC18
Disclosure to Shareholders;
Accounting and Reporting
Requirements; Federal Agricultural
Mortgage Corporation General
Provisions; Federal Agricultural
Mortgage Corporation Governance;
Federal Agricultural Mortgage
Corporation Funding and Fiscal
Affairs; Federal Agricultural Mortgage
Corporation Disclosure and Reporting
Requirements; Effective Date
Farm Credit Administration.
Notice of effective date.
AGENCY:
ACTION:
The Farm Credit
Administration (FCA) published a final
rule under parts 620, 621, 650, 651, 652,
SUMMARY:
VerDate Aug<31>2005
15:31 Oct 05, 2005
Jkt 208001
[Docket No. FAA–2005–22583; Directorate
Identifier 2002–NM–303–AD; Amendment
39–14318; AD 2005–20–22]
RIN 2120–AA64
Airworthiness Directives; BAE
Systems (Operations) Limited Model
ATP Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all BAE
Systems (Operations) Limited Model
ATP airplanes. This AD requires
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58293
repetitive inspections for environmental
damage, including corrosion, of the
fuselage and wing structure, and
corrective actions if necessary. This AD
results from information indicating the
potential for environmental damage of
the fuselage and wing structure. We are
issuing this AD to detect and correct
such damage, including corrosion, in
the fuselage and wing structure, which
could result in cracking and consequent
reduced structural integrity of the
fuselage and wing structure.
DATES: This AD becomes effective
October 21, 2005.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of October 21, 2005.
We must receive comments on this
AD by December 5, 2005.
ADDRESSES: Use one of the following
addresses to submit comments on this
AD.
• DOT Docket Web Site: Go to
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
• Government-Wide Rulemaking Web
Site: Go to https://www.regulations.gov
and follow the instructions for sending
your comments electronically.
• Mail: Docket Management Facility;
U.S. Department of Transportation, 400
Seventh Street SW., Nassif Building,
Room PL–401, Washington, DC 20590.
• Fax: (202) 493–2251.
• Hand Delivery: Room PL–401 on
the plaza level of the Nassif Building,
400 Seventh Street SW., Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
Contact British Aerospace Regional
Aircraft American Support, 13850
Mclearen Road, Herndon, Virginia
20171, for service information identified
in this AD.
FOR FURTHER INFORMATION CONTACT:
Todd Thompson, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–1175;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Discussion
The Civil Aviation Authority (CAA),
which is the airworthiness authority for
the United Kingdom, notified us that an
unsafe condition may exist on all BAE
Systems (Operations) Limited Model
ATP airplanes. The CAA advises that
there is a potential for environmental
damage of the fuselage and wing
structure. New inspections for
environmental damage were added to
the ATP Maintenance Review Board
E:\FR\FM\06OCR1.SGM
06OCR1
58294
Federal Register / Vol. 70, No. 193 / Thursday, October 6, 2005 / Rules and Regulations
(MRB) Report and the Maintenance
Planning Document (MPD). However,
no compliance statements were
included in these documents to advise
operators when the first inspections
must be performed. Environmental
damage such as corrosion, if not
corrected, could result in cracking and
consequent reduced structural integrity
of the fuselage and wing structure.
Relevant Service Information
BAE Systems (Operations) Limited
has issued Service Bulletin ATP–51–
001, dated August 14, 2002. The service
bulletin describes procedures for
repetitive detailed visual inspections for
environmental damage, including but
not limited to corrosion, of the fuselage
and wing structure, and corrective
actions if necessary. If damage is found,
the service bulletin specifies to refer to
the structural repair manual (SRM) for
corrective action (repair). If the damage
is outside the limits specified in the
SRM, the service bulletin specifies to
contact the manufacturer for repair
instructions. The service bulletin also
specifies reporting the inspection results
to the manufacturer. The service
bulletin specifies that the repetitive
interval for the inspections in the
service bulletin is stated in the MRB
Report and the MPD. This repetitive
interval is 8 years.
Accomplishing the actions specified
in the service information is intended to
adequately address the unsafe
condition. The CAA mandated BAE
Systems (Operations) Limited Service
Bulletin ATP–51–001 to ensure the
continued airworthiness of these
airplanes in the United Kingdom.
FAA’s Determination and Requirements
of This AD
This airplane model is manufactured
in the United Kingdom and is type
certificated for operation in the United
States under the provisions of section
21.29 of the Federal Aviation
Regulations (14 CFR 21.29) and the
applicable bilateral airworthiness
agreement. Pursuant to this bilateral
airworthiness agreement, the CAA has
kept the FAA informed of the situation
described above. We have examined the
CAA’s findings, evaluated all pertinent
information, and determined that we
need to issue an AD for products of this
type design that are certificated for
operation in the United States.
Therefore, we are issuing this AD to
detect and correct environmental
damage, including corrosion, of the
fuselage and wing structure, which
could result in cracking and consequent
reduced structural integrity of the
fuselage and wing structure. This AD
VerDate Aug<31>2005
15:31 Oct 05, 2005
Jkt 208001
requires accomplishing the actions
specified in BAE Systems (Operations)
Limited Service Bulletin ATP–51–001,
described previously, except as
discussed under ‘‘Differences Between
the AD and Service Information.’’
Clarification of Inspection Terminology
In this AD, the ‘‘detailed visual
inspections’’ specified in BAE Systems
(Operations) Limited Service Bulletin
ATP–51–001 are referred to as ‘‘detailed
inspections.’’ We have included the
definition for a detailed inspection in a
note in the AD.
Differences Between the AD and
Service Information
If damage is found that is outside the
limits specified in the SRM, BAE
Systems (Operations) Limited Service
Bulletin ATP–51–001 specifies
reporting the details of the damage to InService Engineering and asking for
repair instructions. This AD requires
repairing any damage that is outside the
limits specified in the SRM in
accordance with a method that we or
the CAA (or its delegated agent)
approve. In light of the type of repair
that would be required to address the
unsafe condition, and consistent with
existing bilateral airworthiness
agreements, we have determined that,
for this AD, a repair we or the CAA
approve would be acceptable for
compliance with this AD.
BAE Systems (Operations) Limited
Service Bulletin ATP–51–001 specifies
reporting the inspection results to the
manufacturer. This AD does not require
that action.
Costs of Compliance
None of the airplanes affected by this
action are on the U.S. Register. All
airplanes affected by this AD are
currently operated by non-U.S.
operators under foreign registry;
therefore, they are not directly affected
by this AD action. However, we
consider this AD necessary to ensure
that the unsafe condition is addressed if
any affected airplane is imported and
placed on the U.S. Register in the future.
If an affected airplane is imported and
placed on the U.S. Register in the future,
the required actions would take about
44 work hours per airplane, at an
average labor rate of $65 per work hour.
Based on these figures, the estimated
cost of the AD would be $2,860 per
airplane, per inspection cycle.
FAA’s Determination of the Effective
Date
No airplane affected by this AD is
currently on the U.S. Register.
Therefore, providing notice and
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Fmt 4700
Sfmt 4700
opportunity for public comment is
unnecessary before this AD is issued,
and this AD may be made effective in
less than 30 days after it is published in
the Federal Register.
Comments Invited
This AD is a final rule that involves
requirements that affect flight safety and
was not preceded by notice and an
opportunity for public comment;
however, we invite you to submit any
relevant written data, views, or
arguments regarding this AD. Send your
comments to an address listed in the
ADDRESSES section. Include ‘‘Docket No.
FAA–2005–22583; Directorate Identifier
2002–NM–303–AD’’ at the beginning of
your comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of the AD that might suggest a
need to modify it.
We will post all comments we
receive, without change, to https://
dms.dot.gov, including any personal
information you provide. We will also
post a report summarizing each
substantive verbal contact with FAA
personnel concerning this AD. Using the
search function of that web site, anyone
can find and read the comments in any
of our dockets, including the name of
the individual who sent the comment
(or signed the comment on behalf of an
association, business, labor union, etc.).
You may review the DOT’s complete
Privacy Act Statement in the Federal
Register published on April 11, 2000
(65 FR 19477–78), or you may visit
https://dms.dot.gov.
Examining the Docket
You may 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 DOT
street address stated in the ADDRESSES
section. Comments will be available in
the AD docket shortly after the Docket
Management System receives them.
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,
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Federal Register / Vol. 70, No. 193 / Thursday, October 6, 2005 / Rules and Regulations
‘‘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 the regulation:
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
3. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a regulatory evaluation
of the estimated costs to comply with
this AD and placed it in the AD docket.
See the ADDRESSES section for a location
to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
I
2005–20–22 BAE Systems (Operations)
Limited (Formerly British Aerospace
Regional Aircraft): Amendment 39–
14318. Docket No. FAA–2005–22583;
Directorate Identifier 2002–NM–303–AD.
VerDate Aug<31>2005
15:31 Oct 05, 2005
Jkt 208001
(a) This AD becomes effective October 21,
2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all BAE Systems
(Operations) Limited Model ATP airplanes,
certificated in any category.
Unsafe Condition
(d) This AD results from information
indicating the potential for environmental
damage of the fuselage and wing structure.
We are issuing this AD to detect and correct
such damage, including corrosion, in the
fuselage and wing structure, which could
result in cracking and consequent reduced
structural integrity of the fuselage and wing
structure.
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.
Repetitive Inspections and Corrective
Actions
(f) Within 18 months after the effective
date of this AD, perform detailed inspections
for environmental damage, including but not
limited to corrosion, of the fuselage and wing
structure and any applicable corrective
action in accordance with the
Accomplishment Instructions of BAE
Systems (Operations) Limited Service
Bulletin ATP–51–001, dated August 14,
2002, except as provided by paragraph (g) of
this AD. Any applicable corrective actions
must be accomplished before further flight.
Thereafter, repeat these inspections at
intervals not to exceed those specified in the
ATP Maintenance Review Board Report and
the Maintenance Planning Document, as
applicable, in accordance with the service
bulletin.
Note 1: For the purposes of this AD, a
detailed inspection is: ‘‘An intensive
examination of a specific item, installation,
or assembly to detect damage, failure, or
irregularity. Available lighting is normally
supplemented with a direct source of good
lighting at an intensity deemed appropriate.
Inspection aids such as mirror, magnifying
lenses, etc., may be necessary. Surface
cleaning and elaborate procedures may be
required.’’
No Reporting
(h) Although British Aerospace ATP
Service Bulletin ATP–51–001, dated August
14, 2002, specifies reporting inspection
results to the manufacturer, this AD does not
require that action.
Alternative Methods of Compliance
(AMOCs)
(i)(1) The Manager, International Branch,
ANM–116, has the authority to approve
AMOCs for this AD, if requested in
accordance with the procedures found in 14
CFR 39.19.
(2) Before using any AMOC approved in
accordance with 14 CFR 39.19 on any
airplane to which the AMOC applies, notify
the appropriate principal inspector in the
FAA Flight Standards Certificate Holding
District Office.
Related Information
(j) None.
Material Incorporated by Reference
(k) You must use BAE Systems
(Operations) Limited Service Bulletin ATP–
51–001, dated August 14, 2002, to perform
the actions that are required by this AD,
unless the AD specifies otherwise. The
Director of the Federal Register approved the
incorporation by reference of this document
in accordance with 5 U.S.C. 552(a) and 1 CFR
part 51. Contact British Aerospace Regional
Aircraft American Support, 13850 Mclearen
Road, Herndon, Virginia 20171, for a copy of
this service information. You may review
copies at the Docket Management Facility,
U.S. Department of Transportation, 400
Seventh Street SW., room PL–401, Nassif
Building, Washington, DC; on the Internet at
https://dms.dot.gov; or at the National
Archives and Records Administration
(NARA). For information on the availability
of this material at the NARA, call (202) 741–
6030, or go to https://www.archives.gov/
federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on
September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–19833 Filed 10–5–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Exception to Service Bulletin Instructions
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
Effective Date
58295
14 CFR Part 39
(g) If damage is found that is outside the
limits specified in the structural repair
manual, as referenced in BAE Systems
(Operations) Limited Service Bulletin ATP–
51–001, dated August 14, 2002, and the
service bulletin specifies reporting the details
of the damage to In-Service Engineering and
asking for repair instructions: Before further
flight, repair the damage in accordance with
a method approved by either the Manager,
International Branch, ANM–116, Transport
Airplane Directorate, FAA; or the Civil
Aviation Authority (or its delegated agent).
[Docket No. FAA–2005–22586; Directorate
Identifier 2002–NM–258–AD; Amendment
39–14315; AD 2005–20–19]
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RIN 2120–AA64
Airworthiness Directives; BAE
Systems (Operations) Limited Model
ATP Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
AGENCY:
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06OCR1
]]>Agencies
[Federal Register Volume 70, Number 193 (Thursday, October 6, 2005)]
[Rules and Regulations]
[Pages 58293-58295]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-19833]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22583; Directorate Identifier 2002-NM-303-AD;
Amendment 39-14318; AD 2005-20-22]
RIN 2120-AA64
Airworthiness Directives; BAE Systems (Operations) Limited Model
ATP Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
BAE Systems (Operations) Limited Model ATP airplanes. This AD requires
repetitive inspections for environmental damage, including corrosion,
of the fuselage and wing structure, and corrective actions if
necessary. This AD results from information indicating the potential
for environmental damage of the fuselage and wing structure. We are
issuing this AD to detect and correct such damage, including corrosion,
in the fuselage and wing structure, which could result in cracking and
consequent reduced structural integrity of the fuselage and wing
structure.
DATES: This AD becomes effective October 21, 2005.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of October 21,
2005.
We must receive comments on this AD by December 5, 2005.
ADDRESSES: Use one of the following addresses to submit comments on
this AD.
DOT Docket Web Site: Go to https://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-Wide Rulemaking Web Site: Go to https://
www.regulations.gov and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility; U.S. Department of
Transportation, 400 Seventh Street SW., Nassif Building, Room PL-401,
Washington, DC 20590.
Fax: (202) 493-2251.
Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street SW., Washington, DC, between 9 a.m.
and 5 p.m., Monday through Friday, except Federal holidays.
Contact British Aerospace Regional Aircraft American Support, 13850
Mclearen Road, Herndon, Virginia 20171, for service information
identified in this AD.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-1175; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
The Civil Aviation Authority (CAA), which is the airworthiness
authority for the United Kingdom, notified us that an unsafe condition
may exist on all BAE Systems (Operations) Limited Model ATP airplanes.
The CAA advises that there is a potential for environmental damage of
the fuselage and wing structure. New inspections for environmental
damage were added to the ATP Maintenance Review Board
[[Page 58294]]
(MRB) Report and the Maintenance Planning Document (MPD). However, no
compliance statements were included in these documents to advise
operators when the first inspections must be performed. Environmental
damage such as corrosion, if not corrected, could result in cracking
and consequent reduced structural integrity of the fuselage and wing
structure.
Relevant Service Information
BAE Systems (Operations) Limited has issued Service Bulletin ATP-
51-001, dated August 14, 2002. The service bulletin describes
procedures for repetitive detailed visual inspections for environmental
damage, including but not limited to corrosion, of the fuselage and
wing structure, and corrective actions if necessary. If damage is
found, the service bulletin specifies to refer to the structural repair
manual (SRM) for corrective action (repair). If the damage is outside
the limits specified in the SRM, the service bulletin specifies to
contact the manufacturer for repair instructions. The service bulletin
also specifies reporting the inspection results to the manufacturer.
The service bulletin specifies that the repetitive interval for the
inspections in the service bulletin is stated in the MRB Report and the
MPD. This repetitive interval is 8 years.
Accomplishing the actions specified in the service information is
intended to adequately address the unsafe condition. The CAA mandated
BAE Systems (Operations) Limited Service Bulletin ATP-51-001 to ensure
the continued airworthiness of these airplanes in the United Kingdom.
FAA's Determination and Requirements of This AD
This airplane model is manufactured in the United Kingdom and is
type certificated for operation in the United States under the
provisions of section 21.29 of the Federal Aviation Regulations (14 CFR
21.29) and the applicable bilateral airworthiness agreement. Pursuant
to this bilateral airworthiness agreement, the CAA has kept the FAA
informed of the situation described above. We have examined the CAA's
findings, evaluated all pertinent information, and determined that we
need to issue an AD for products of this type design that are
certificated for operation in the United States.
Therefore, we are issuing this AD to detect and correct
environmental damage, including corrosion, of the fuselage and wing
structure, which could result in cracking and consequent reduced
structural integrity of the fuselage and wing structure. This AD
requires accomplishing the actions specified in BAE Systems
(Operations) Limited Service Bulletin ATP-51-001, described previously,
except as discussed under ``Differences Between the AD and Service
Information.''
Clarification of Inspection Terminology
In this AD, the ``detailed visual inspections'' specified in BAE
Systems (Operations) Limited Service Bulletin ATP-51-001 are referred
to as ``detailed inspections.'' We have included the definition for a
detailed inspection in a note in the AD.
Differences Between the AD and Service Information
If damage is found that is outside the limits specified in the SRM,
BAE Systems (Operations) Limited Service Bulletin ATP-51-001 specifies
reporting the details of the damage to In-Service Engineering and
asking for repair instructions. This AD requires repairing any damage
that is outside the limits specified in the SRM in accordance with a
method that we or the CAA (or its delegated agent) approve. In light of
the type of repair that would be required to address the unsafe
condition, and consistent with existing bilateral airworthiness
agreements, we have determined that, for this AD, a repair we or the
CAA approve would be acceptable for compliance with this AD.
BAE Systems (Operations) Limited Service Bulletin ATP-51-001
specifies reporting the inspection results to the manufacturer. This AD
does not require that action.
Costs of Compliance
None of the airplanes affected by this action are on the U.S.
Register. All airplanes affected by this AD are currently operated by
non-U.S. operators under foreign registry; therefore, they are not
directly affected by this AD action. However, we consider this AD
necessary to ensure that the unsafe condition is addressed if any
affected airplane is imported and placed on the U.S. Register in the
future.
If an affected airplane is imported and placed on the U.S. Register
in the future, the required actions would take about 44 work hours per
airplane, at an average labor rate of $65 per work hour. Based on these
figures, the estimated cost of the AD would be $2,860 per airplane, per
inspection cycle.
FAA's Determination of the Effective Date
No airplane affected by this AD is currently on the U.S. Register.
Therefore, providing notice and opportunity for public comment is
unnecessary before this AD is issued, and this AD may be made effective
in less than 30 days after it is published in the Federal Register.
Comments Invited
This AD is a final rule that involves requirements that affect
flight safety and was not preceded by notice and an opportunity for
public comment; however, we invite you to submit any relevant written
data, views, or arguments regarding this AD. Send your comments to an
address listed in the ADDRESSES section. Include ``Docket No. FAA-2005-
22583; Directorate Identifier 2002-NM-303-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of the AD that might
suggest a need to modify it.
We will post all comments we receive, without change, to https://
dms.dot.gov, including any personal information you provide. We will
also post a report summarizing each substantive verbal contact with FAA
personnel concerning this AD. Using the search function of that web
site, anyone can find and read the comments in any of our dockets,
including the name of the individual who sent the comment (or signed
the comment on behalf of an association, business, labor union, etc.).
You may review the DOT's complete Privacy Act Statement in the Federal
Register published on April 11, 2000 (65 FR 19477-78), or you may visit
https://dms.dot.gov.
Examining the Docket
You may 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 DOT
street address stated in the ADDRESSES section. Comments will be
available in the AD docket shortly after the Docket Management System
receives them.
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,
[[Page 58295]]
``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 the regulation:
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
3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket. See the ADDRESSES
section for a location to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2005-20-22 BAE Systems (Operations) Limited (Formerly British
Aerospace Regional Aircraft): Amendment 39-14318. Docket No. FAA-
2005-22583; Directorate Identifier 2002-NM-303-AD.
Effective Date
(a) This AD becomes effective October 21, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all BAE Systems (Operations) Limited
Model ATP airplanes, certificated in any category.
Unsafe Condition
(d) This AD results from information indicating the potential
for environmental damage of the fuselage and wing structure. We are
issuing this AD to detect and correct such damage, including
corrosion, in the fuselage and wing structure, which could result in
cracking and consequent reduced structural integrity of the fuselage
and wing structure.
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.
Repetitive Inspections and Corrective Actions
(f) Within 18 months after the effective date of this AD,
perform detailed inspections for environmental damage, including but
not limited to corrosion, of the fuselage and wing structure and any
applicable corrective action in accordance with the Accomplishment
Instructions of BAE Systems (Operations) Limited Service Bulletin
ATP-51-001, dated August 14, 2002, except as provided by paragraph
(g) of this AD. Any applicable corrective actions must be
accomplished before further flight. Thereafter, repeat these
inspections at intervals not to exceed those specified in the ATP
Maintenance Review Board Report and the Maintenance Planning
Document, as applicable, in accordance with the service bulletin.
Note 1: For the purposes of this AD, a detailed inspection is:
``An intensive examination of a specific item, installation, or
assembly to detect damage, failure, or irregularity. Available
lighting is normally supplemented with a direct source of good
lighting at an intensity deemed appropriate. Inspection aids such as
mirror, magnifying lenses, etc., may be necessary. Surface cleaning
and elaborate procedures may be required.''
Exception to Service Bulletin Instructions
(g) If damage is found that is outside the limits specified in
the structural repair manual, as referenced in BAE Systems
(Operations) Limited Service Bulletin ATP-51-001, dated August 14,
2002, and the service bulletin specifies reporting the details of
the damage to In-Service Engineering and asking for repair
instructions: Before further flight, repair the damage in accordance
with a method approved by either the Manager, International Branch,
ANM-116, Transport Airplane Directorate, FAA; or the Civil Aviation
Authority (or its delegated agent).
No Reporting
(h) Although British Aerospace ATP Service Bulletin ATP-51-001,
dated August 14, 2002, specifies reporting inspection results to the
manufacturer, this AD does not require that action.
Alternative Methods of Compliance (AMOCs)
(i)(1) The Manager, International Branch, ANM-116, has the
authority to approve AMOCs for this AD, if requested in accordance
with the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in accordance with 14 CFR
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Related Information
(j) None.
Material Incorporated by Reference
(k) You must use BAE Systems (Operations) Limited Service
Bulletin ATP-51-001, dated August 14, 2002, to perform the actions
that are required by this AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the incorporation by
reference of this document in accordance with 5 U.S.C. 552(a) and 1
CFR part 51. Contact British Aerospace Regional Aircraft American
Support, 13850 Mclearen Road, Herndon, Virginia 20171, for a copy of
this service information. You may review copies at the Docket
Management Facility, U.S. Department of Transportation, 400 Seventh
Street SW., room PL-401, Nassif Building, Washington, DC; on the
Internet at https://dms.dot.gov; or at the National Archives and
Records Administration (NARA). For information on the availability
of this material at the NARA, call (202) 741-6030, or go to https://
www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-19833 Filed 10-5-05; 8:45 am]
BILLING CODE 4910-13-P
