Airworthiness Directives; Dassault Model Falcon 2000 Airplanes, 75386-75388 [05-24150]
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75386
Federal Register / Vol. 70, No. 243 / Tuesday, December 20, 2005 / Rules and Regulations
PART 201—EXTENSIONS OF CREDIT
BY FEDERAL RESERVE BANKS
(REGULATION A)
Authority: 12 U.S.C. 248(i)–(j), 343 et seq.,
347a, 347b, 347c, 348 et seq., 357, 374, 374a,
and 461.
1. The authority citation for part 201
continues to read as follows:
I
2. In § 201.51, paragraphs (a) and (b)
are revised to read as follows:
I
§ 201.51 Interest rates applicable to credit
extended by a Federal Reserve Bank.1
(a) Primary credit. The interest rates
for primary credit provided to
depository institutions under § 201.4(a)
are:
Federal Reserve Bank
Rate
Boston ......................................................................................................................................................................
New York .................................................................................................................................................................
Philadelphia .............................................................................................................................................................
Cleveland .................................................................................................................................................................
Richmond .................................................................................................................................................................
Atlanta ......................................................................................................................................................................
Chicago ....................................................................................................................................................................
St. Louis ...................................................................................................................................................................
Minneapolis ..............................................................................................................................................................
Kansas City ..............................................................................................................................................................
Dallas .......................................................................................................................................................................
San Francisco ..........................................................................................................................................................
(b) Secondary credit. The interest
rates for secondary credit provided to
Rate
Boston ......................................................................................................................................................................
New York .................................................................................................................................................................
Philadelphia .............................................................................................................................................................
Cleveland .................................................................................................................................................................
Richmond .................................................................................................................................................................
Atlanta ......................................................................................................................................................................
Chicago ....................................................................................................................................................................
St. Louis ...................................................................................................................................................................
Minneapolis ..............................................................................................................................................................
Kansas City ..............................................................................................................................................................
Dallas .......................................................................................................................................................................
San Francisco ..........................................................................................................................................................
*
*
*
*
ACTION:
By order of the Board of Governors of the
Federal Reserve System, December 14, 2005.
Jennifer J. Johnson,
Secretary of the Board.
[FR Doc. E5–7512 Filed 12–19–05; 8:45 am]
BILLING CODE 6210–01–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–22633; Directorate
Identifier 2005–NM–155–AD; Amendment
39–14422; AD 2005–26–01]
RIN 2120–AA64
Airworthiness Directives; Dassault
Model Falcon 2000 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
AGENCY:
1 The primary, secondary, and seasonal credit
rates described in this section apply to both
VerDate Aug<31>2005
16:09 Dec 19, 2005
Jkt 208001
December
December
December
December
December
December
December
December
December
December
December
December
13,
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13,
14,
13,
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2005.
2005.
2005.
2005.
2005.
2005.
2005.
2005.
2005.
2005.
2005.
2005.
depository institutions under 201.4(b)
are:
Federal Reserve Bank
*
5.25
5.25
5.25
5.25
5.25
5.25
5.25
5.25
5.25
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5.25
Effective
Final rule.
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
Dassault Model Falcon 2000 airplanes.
This AD requires an inspection for the
presence of fail-safe pins, nuts, and
washers on each engine, and
replacement of the fail-safe fastener
assembly with a new assembly if
necessary. This AD results from a report
of a missing pin of a fail-safe fastener.
We are issuing this AD to prevent
reduced structural integrity of an engine
mount due to a missing pin of a fail-safe
fastener, and possible separation of an
engine from the airplane during flight.
DATES: This AD becomes effective
January 24, 2006.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of January 24, 2006.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the Docket
advances and discounts made under the primary,
PO 00000
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5.75
Effective
December
December
December
December
December
December
December
December
December
December
December
December
13,
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2005.
2005.
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2005.
2005.
2005.
2005.
2005.
Management Facility, U.S. Department
of Transportation, 400 Seventh Street
SW., Nassif Building, Room PL–401,
Washington, DC.
Contact Dassault Falcon Jet, P.O. Box
2000, South Hackensack, New Jersey
07606, for service information identified
in this AD.
FOR FURTHER INFORMATION CONTACT: Tom
Rodriguez, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98055–4056; telephone
(425) 227–1137; fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the airworthiness
directive (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
secondary, and seasonal credit programs,
respectively.
E:\FR\FM\20DER1.SGM
20DER1
Federal Register / Vol. 70, No. 243 / Tuesday, December 20, 2005 / Rules and Regulations
the plaza level of the Nassif Building at
the street address stated in the
ADDRESSES section.
Discussion
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to certain Dassault Model Falcon
2000 airplanes. That NPRM was
published in the Federal Register on
October 7, 2005 (70 FR 58634). That
NPRM proposed to require an
inspection for the presence of fail-safe
pins, nuts, and washers on each engine,
and replacement of the fail-safe fastener
assembly with a new assembly if
necessary.
Comments
We provided the public the
opportunity to participate in the
development of this AD. We received no
comments on the NPRM 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.
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
This AD will affect about 149
airplanes of U.S. registry. The required
inspection will take about 1 work hour
per airplane, at an average labor rate of
$65 per work hour. Based on these
figures, the estimated cost of the
inspection required by this AD for U.S.
operators is $9,685, or $65 per airplane.
Authority for This Rulemaking
Jkt 208001
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
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.
16:09 Dec 19, 2005
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 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
Costs of Compliance
VerDate Aug<31>2005
Regulatory Findings
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
I
2005–26–01 Dassault Aviation:
Amendment 39–14422. Docket No.
FAA–2005–22633; Directorate Identifier
2005–NM–155–AD.
Effective Date
(a) This AD becomes effective January 24,
2006.
75387
Unsafe Condition
(d) This AD results from a report of a
missing pin of a fail-safe fastener. We are
issuing this AD to prevent reduced structural
integrity of an engine mount due to a missing
pin of a fail-safe fastener, and possible
separation of an engine from the airplane
during flight.
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.
Inspection and Replacement
(f) Before the accumulation of 3,750 total
landings, or within 2 months after the
effective date of this AD, whichever occurs
later: Do a detailed inspection for the
presence of fail-safe pins, nuts, and washers
on each engine, in accordance with the
Accomplishment Instructions of Dassault
Service Bulletin F2000–301, dated February
2, 2005. If any component is found missing
at an attachment point, before further flight,
replace the fail-safe fastener assembly with a
new assembly, 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.’’
(g) Inspections and replacements done in
accordance with Chapter 54–003, dated
December 2002, of the Dassault Falcon 2000
Maintenance Manual are acceptable for
compliance with the requirements of
paragraph (f) of this AD.
No Reporting
(h) Although the service bulletin
referenced in this AD specifies to submit
certain information to the manufacturer, this
AD does not include that requirement.
Alternative Methods of Compliance
(AMOCs)
(i)(1) 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.
(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.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Dassault Model
Falcon 2000 airplanes, certificated in any
category; up to and including serial number
212, excluding serial number 208.
Related Information
(j) French airworthiness directive F–2005–
018, dated February 2, 2005, also addresses
the subject of this AD.
Material Incorporated by Reference
(k) You must use Dassault Service Bulletin
F2000–301, dated February 2, 2005, to
perform the actions that are required by this
PO 00000
Frm 00009
Fmt 4700
Sfmt 4700
E:\FR\FM\20DER1.SGM
20DER1
75388
Federal Register / Vol. 70, No. 243 / Tuesday, December 20, 2005 / Rules and Regulations
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 Dassault Falcon Jet, P.O. Box
2000, South Hackensack, New Jersey 07606,
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/code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on
December 8, 2005.
Michael Zielinski,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 05–24150 Filed 12–19–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–22527; Directorate
Identifier 2004–NM–04–AD; Amendment 39–
14420; AD 2005–25–27]
RIN 2120–AA64
Airworthiness Directives; Airbus Model
A300 B2 Series Airplanes; A300 B4–
103 and B4–203 Airplanes; and A310–
203 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
Airbus Model A300 B2 series airplanes,
A300 B4–103 and B4–203 airplanes, and
A310–203 airplanes. This AD requires a
one-time inspection for missing or
incorrect rivets in the structural area
affected by conversion from passenger
to freight configuration, and corrective
action if necessary. This AD results from
a report of rivets missing from the
passenger-to-freight converted area. We
are issuing this AD to prevent structural
failure of the main deck and main deck
cargo door areas.
DATES: This AD becomes effective
January 24, 2006.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of January 24, 2006.
ADDRESSES: You may examine the AD
docket on the Internet at https://
VerDate Aug<31>2005
16:09 Dec 19, 2005
Jkt 208001
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street
SW., Nassif Building, room PL–401,
Washington, DC.
Contact EADS Airbus GmbH, Postfach
95 01 09, 21111 Hamburg, Germany, for
service information identified in this
AD.
Jon
Hjelm, Aerospace Engineer, Airframe
and Propulsion Branch, ANE–171, FAA,
New York Aircraft Certification Office,
1600 Stewart Avenue, suite 410,
Westbury, New York 11590; telephone
(516) 228–7323; fax (516) 794–5531.
SUPPLEMENTARY INFORMATION:
FOR FURTHER INFORMATION CONTACT:
Examining the Docket
You may examine the airworthiness
directive (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 street address stated in the
ADDRESSES section.
Discussion
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to certain Airbus Model A300 B2
series airplanes, A300 B4–103 and B4–
203 airplanes, and A310–203 airplanes.
That NPRM was published in the
Federal Register on September 27, 2005
(70 FR 56378). That NPRM proposed to
require a one-time inspection for
missing or incorrect rivets in the entire
structural area affected by conversion
from passenger-to-freight configuration,
and corrective action if necessary.
Comments
We provided the public the
opportunity to participate in the
development of this AD. We received no
comments on the NPRM or on the
determination of the cost to the public.
Clarification of All Operator Telex
(AOT) Reference
We have clarified the reference to the
Airbus AOT, which was cited in the
NPRM as Airbus AOT M113–02–007,
dated June 21, 2002. The reference to
Airbus AOT M113–02–007 parallels the
citation for this AOT that was given in
German airworthiness directive 2002–
200, dated June 27, 2002, which also
addresses the subject of this AD.
However, the service bulletins that are
referenced as the appropriate source of
service information for accomplishing
PO 00000
Frm 00010
Fmt 4700
Sfmt 4700
the required actions refer to this same
AOT with the number BWED/101/02.
Therefore, we have determined that
referring to this AOT as ‘‘Airbus A300
B4, A310–200 All Operator Telex
BWED/101/02 (LBA Approval,
Reference M113–02–007), dated June
21, 2002,’’ will minimize confusion.
Conclusion
We have carefully reviewed the
available data and determined that air
safety and the public interest require
adopting the AD with the change
described previously. We have
determined that this change will neither
increase the economic burden on any
operator nor increase the scope of the
AD.
Costs of Compliance
This AD affects about 6 airplanes of
U.S. registry. The actions take about 80
work hours per airplane, at an average
labor rate of $65 per work hour. Based
on these figures, the estimated cost of
the AD for U.S. operators is $31,200, or
$5,200 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;
E:\FR\FM\20DER1.SGM
20DER1
]]>Agencies
[Federal Register Volume 70, Number 243 (Tuesday, December 20, 2005)]
[Rules and Regulations]
[Pages 75386-75388]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-24150]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22633; Directorate Identifier 2005-NM-155-AD;
Amendment 39-14422; AD 2005-26-01]
RIN 2120-AA64
Airworthiness Directives; Dassault Model Falcon 2000 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Dassault Model Falcon 2000 airplanes. This AD requires an
inspection for the presence of fail-safe pins, nuts, and washers on
each engine, and replacement of the fail-safe fastener assembly with a
new assembly if necessary. This AD results from a report of a missing
pin of a fail-safe fastener. We are issuing this AD to prevent reduced
structural integrity of an engine mount due to a missing pin of a fail-
safe fastener, and possible separation of an engine from the airplane
during flight.
DATES: This AD becomes effective January 24, 2006.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of January 24,
2006.
ADDRESSES: You may examine the AD docket on the Internet at https://
dms.dot.gov or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street SW., Nassif Building,
Room PL-401, Washington, DC.
Contact Dassault Falcon Jet, P.O. Box 2000, South Hackensack, New
Jersey 07606, for service information identified in this AD.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-1137; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the airworthiness directive (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
[[Page 75387]]
the plaza level of the Nassif Building at the street address stated in
the ADDRESSES section.
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to include an AD that would apply to certain Dassault Model
Falcon 2000 airplanes. That NPRM was published in the Federal Register
on October 7, 2005 (70 FR 58634). That NPRM proposed to require an
inspection for the presence of fail-safe pins, nuts, and washers on
each engine, and replacement of the fail-safe fastener assembly with a
new assembly if necessary.
Comments
We provided the public the opportunity to participate in the
development of this AD. We received no comments on the NPRM 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
This AD will affect about 149 airplanes of U.S. registry. The
required inspection will take about 1 work hour per airplane, at an
average labor rate of $65 per work hour. Based on these figures, the
estimated cost of the inspection required by this AD for U.S. operators
is $9,685, or $65 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 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):
2005-26-01 Dassault Aviation: Amendment 39-14422. Docket No. FAA-
2005-22633; Directorate Identifier 2005-NM-155-AD.
Effective Date
(a) This AD becomes effective January 24, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Dassault Model Falcon 2000 airplanes,
certificated in any category; up to and including serial number 212,
excluding serial number 208.
Unsafe Condition
(d) This AD results from a report of a missing pin of a fail-
safe fastener. We are issuing this AD to prevent reduced structural
integrity of an engine mount due to a missing pin of a fail-safe
fastener, and possible separation of an engine from the airplane
during flight.
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.
Inspection and Replacement
(f) Before the accumulation of 3,750 total landings, or within 2
months after the effective date of this AD, whichever occurs later:
Do a detailed inspection for the presence of fail-safe pins, nuts,
and washers on each engine, in accordance with the Accomplishment
Instructions of Dassault Service Bulletin F2000-301, dated February
2, 2005. If any component is found missing at an attachment point,
before further flight, replace the fail-safe fastener assembly with
a new assembly, 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.''
(g) Inspections and replacements done in accordance with Chapter
54-003, dated December 2002, of the Dassault Falcon 2000 Maintenance
Manual are acceptable for compliance with the requirements of
paragraph (f) of this AD.
No Reporting
(h) Although the service bulletin referenced in this AD
specifies to submit certain information to the manufacturer, this AD
does not include that requirement.
Alternative Methods of Compliance (AMOCs)
(i)(1) 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.
(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.
Related Information
(j) French airworthiness directive F-2005-018, dated February 2,
2005, also addresses the subject of this AD.
Material Incorporated by Reference
(k) You must use Dassault Service Bulletin F2000-301, dated
February 2, 2005, to perform the actions that are required by this
[[Page 75388]]
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 Dassault
Falcon Jet, P.O. Box 2000, South Hackensack, New Jersey 07606, 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/code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on December 8, 2005.
Michael Zielinski,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-24150 Filed 12-19-05; 8:45 am]
BILLING CODE 4910-13-P
