Airworthiness Directives; Viking Air Limited Model (Caribou) DHC-4 and (Caribou) DHC-4A Airplanes; and Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes, 8589-8591 [E8-2623]
Download as PDF
<![CDATA[
Federal Register / Vol. 73, No. 31 / Thursday, February 14, 2008 / Rules and Regulations
https://www.nrc.gov/NRC/reading-rm/
adams.html. From this site, the public
can gain entry into the NRC’s
Agencywide Document Access and
Management System (ADAMS), which
provides text and image files of NRC’s
public documents. If you do not have
access to ADAMS or if there are
problems in accessing the documents
located in ADAMS, contact the NRC’s
PDR Reference staff at (800) 397–4209,
(301) 415–4737, or by e-mail to
pdr@nrc.gov.
ebenthall on PRODPC61 with RULES
FOR FURTHER INFORMATION CONTACT:
Stewart Schneider, Office of Nuclear
Reactor Regulation, U.S. Nuclear
Regulatory Commission, Washington,
DC 20555–0001; telephone (301) 415–
4123; e-mail sxs4@nrc.gov.
SUPPLEMENTARY INFORMATION: The
Nuclear Regulatory Commission
published a final rule amending
regulations that would become effective
January 3, 2008. The final rule,
published December 4, 2007 (72 FR
68043) related to the reporting of annual
dose to workers, the definition of Total
Effective Dose Equivalent (TEDE), the
labeling of certain containers holding
licensed material, and the determination
of cumulative occupational radiation
dose. This final rule limits the routine
reporting of annual doses to those
workers whose annual dose exceeds a
specific dose threshold or who request
a report. The rule also modifies the
labeling requirements for certain
containers holding licensed material
within posted areas in nuclear power
facilities, and will amend the definition
of TEDE to be consistent with current
Commission policy. Finally, this rule
removes the requirement that licensees
attempt to obtain cumulative exposure
records for workers unless these
individuals are being authorized to
receive a planned special exposure.
These revisions reduce the
administrative and information
collection burdens on NRC and
Agreement State licensees without
affecting the level of protection for
either the health and safety of workers
and the public, or for the environment.
This final rule amends information
collection requirements contained in 10
CFR parts 19, 20, and 50, and NRC Form
4 that are subject to the Paperwork
Reduction Act of 1995 (44 U.S.C. 3501
et seq.). These information collection
requirements were sent for approval to
the Office of Management and Budget
on November 28, 2007. The effective
date of this final rule was deferred to
VerDate Aug<31>2005
15:28 Feb 13, 2008
Jkt 214001
allow sufficient time for OMB to
complete its review of the information
collections requirements imposed in
this rule. Because the rule will reduce
the burden for existing information
collection requirements, the public
burden for the information collections
in 10 CFR parts 19 and NRC Form 4 is
expected to be decreased by 235 and 44
hours per licensee, respectively. This
reduction includes the time required for
reviewing instructions, searching
existing data sources, gathering and
maintaining the data needed and
completing and reviewing the
information collection. The NRC has
received final approval for these
amended requirements by the Office of
Management and Budget, approval
number(s) 3150–0044, 3150–0014,
3150–0011, and 3150–0005.
Dated at Rockville, Maryland, this 8th day
of February, 2008.
For the Nuclear Regulatory Commission.
Michael T. Lesar,
Chief, Rulemaking, Directives and Editing
Branch, Division of Administrative Services,
Office of Administration.
[FR Doc. E8–2801 Filed 2–13–08; 8:45 am]
BILLING CODE 7590–01–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket Nos. FAA–2007–0410, FAA–2007–
0411, and FAA–2007–0412; Directorate
Identifiers 2007–NM–338–AD, 2007–NM–
291–AD, and 2007–NM–290–AD;
Amendments 39–15325, 39–15326, 39–
15327; ADs 2008–01–02, 2004–07–22 R1,
and 90–25–05 R1]
RIN 2120–AA64
Airworthiness Directives; Viking Air
Limited Model (Caribou) DHC–4 and
(Caribou) DHC–4A Airplanes; and
Boeing Model 747–100, 747–100B, 747–
100B SUD, 747–200B, 747–200C, 747–
200F, 747–300, 747–400, 747–400D,
747–400F, 747SR, and 747SP Series
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; corrections.
AGENCY:
SUMMARY: The FAA is correcting
typographical errors in three existing
airworthiness directives (ADs) that were
published in the Federal Register on
January 8, 2008 (73 FR 1269); January 7,
PO 00000
Frm 00003
Fmt 4700
Sfmt 4700
8589
2008 (73 FR 1052); and January 7, 2008
(73 FR 1055). The errors resulted in
incorrect docket numbers. One AD
applies to all Viking Air Limited Model
(Caribou) DHC–4 and (Caribou) DHC–
4A airplanes. The other two ADs apply
to all Boeing Model 747–100, 747–100B,
747–100B SUD, 747–200B, 747–200C,
747–200F, 747–300, 747–400, 747–
400D, 747–400F, 747SR, and 747SP
series airplanes. The Viking Air AD
requires doing a fluorescent penetrant
inspection for cracking of certain upper
engine mount bracket assemblies, and
corrective actions if necessary. One of
the Boeing ADs requires revising the
FAA-approved maintenance inspection
program to include inspections that will
give no less than the required damage
tolerance rating for each structural
significant item, and repair of cracked
structure. The other Boeing AD requires
implementing a corrosion prevention
and control program.
DATES: AD 2008–01–02 is effective
January 23, 2008. ADs 2004–07–22 R1
and 90–25–05 R1 are effective January
22, 2008.
ADDRESSES: You may examine the AD
dockets on the Internet at https://
www.regulations.gov; or in person at the
Docket Management Facility between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The AD
dockets contain this AD, the regulatory
evaluation, any comments received, and
other information. The address for the
Docket Office (telephone 800–647–5527)
is the Document Management Facility,
U.S. Department of Transportation,
Docket Operations, M–30, West
Building Ground Floor, Room W12–140,
1200 New Jersey Avenue, SE.,
Washington, DC 20590.
FOR FURTHER INFORMATION ON AD 2008–01–
02, CONTACT: George Duckett, 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–
7325; fax (516) 794–5531.
FOR FURTHER INFORMATION ON ADS 2004–
07–22 R1 AND 90–25–05 R1, CONTACT: Ivan
Li, Aerospace Engineer, Airframe
Branch, ANM–120S, FAA, Seattle
Aircraft Certification Office, 1601 Lind
Avenue, SW., Renton, Washington
98057–3356; telephone (425) 917–6437;
fax (425) 917–6590.
SUPPLEMENTARY INFORMATION: We have
issued the ADs identified in the
following table.
E:\FR\FM\14FER1.SGM
14FER1
8590
Federal Register / Vol. 73, No. 31 / Thursday, February 14, 2008 / Rules and Regulations
AFFECTED ADS
AD—
Affects—
And requires—
2008–01–02, amendment 39–15325 (73 FR
1269, January 8, 2008), issued December
20, 2007.
All Viking Air Limited Model (Caribou) DHC–4
and (Caribou) DHC–4A airplanes.
2004–07–22 R1, amendment 39–15326 (73 FR
1052, January 7, 2008), issued December
26, 2007.
All Boeing Model 747–100, 747–100B, 747–
100B SUD, 747–200B, 747–200C, 747–
200F, 747–300, 747–400, 747–400D, 747–
400F, 747SR, and 747SP series airplanes.
90–25–05 R1, amendment 39–15327 (73 FR
1055, January 7, 2008), issued December
26, 2007.
All Boeing Model 747–100, 747–100B, 747–
100B SUD, 747–200B, 747–200C, 747–
200F, 747–300, 747–400, 747–400D, 747–
400F, 747SR, and 747SP series airplanes.
A fluorescent penetrant inspection (FPI) for
cracking of certain upper engine mount
bracket assemblies, and corrective actions
if necessary.
Revising the FAA-approved maintenance inspection program to include inspections that
will give no less than the required damage
tolerance rating for each structural significant item, and repair of cracked structure.
Implementing a corrosion prevention and control program. (That AD revised an earlier
AD by removing future type-certificated
models from the applicability.)
As published, those ADs specify
incorrect docket numbers throughout
the preamble and regulatory text. Docket
numbers are assigned by the Federal
Document Management System. We
have been informed that incorrect
docket numbers were assigned. The
correct docket information is provided
in the following table.
CORRECTED AD DOCKET NUMBERS
AD No.
Original Docket No.
AD 2008–01–02 ................................................................
2004–07–22 R1 ................................................................
AD 90–25–05 R1 ..............................................................
FAA–2008–0410 .............................................................
FAA–2008–0411 .............................................................
FAA–2008–0412 .............................................................
Any commenter who submitted
comments to an original, incorrect
docket number should check Docket No.
FAA–2007–0410, FAA–2007–0411, or
FAA 2007–0412 on
www.regulations.gov to determine
whether the comments have been
received and filed in the appropriate
docket. If not, or if it is not possible to
determine whether comments have been
posted to the correct docket, the
comments should be resubmitted using
the correct docket number.
No other part of the preamble or
regulatory information has been
changed; therefore, the final rule is not
republished in the Federal Register.
The effective date of AD 2008–01–02
remains January 23, 2008. The effective
date of AD 2004–07–22 R1 remains
January 22, 2008. The effective date of
AD 90–25–05 R1 remains January 22,
2008.
ebenthall on PRODPC61 with RULES
Correction
In the Federal Register of January 8,
2008, on page 1269, in the third column,
the headings section of AD 2008–01–02
is corrected to read as follows:
‘‘[Docket No. FAA–2007–0410;
Directorate Identifier 2007–NM–338–
AD; Amendment 39–15325; AD 2008–
01–02]’’
In the Federal Register of January 7,
2008, on page 1052, in the first column,
the headings section of AD 2004–07–22
R1 is corrected to read as follows:
VerDate Aug<31>2005
15:28 Feb 13, 2008
Jkt 214001
‘‘[Docket No. FAA–2007–0411;
Directorate Identifier 2007–NM–291–
AD; Amendment 39–15326; AD 2004–
07–22 R1]’’
In the Federal Register of January 7,
2008, on page 1055, in the second
column, the headings section of AD 90–
25–05 R1 is corrected to read as follows:
‘‘[Docket No. FAA–2007–0412;
Directorate Identifier 2007–NM–290–
AD; Amendment 39–15327; AD 90–25–
05 R1]’’
In the Federal Register of January 8,
2008, on page 1270, in the second and
third columns, the Supplemental
Information section of Docket No. FAA–
2008–0410, Directorate Identifier 2007–
NM–338–AD, is corrected to read as
follows:
‘‘* * * Include ‘‘Docket No. FAA–
2007–0410; Directorate Identifier 2007–
NM–338–AD’’ at the beginning of your
comments. * * *
In the Federal Register of January 7,
2008, on page 1053, in the second
column, the Supplemental Information
section of Docket No. FAA–2008–0411,
Directorate Identifier 2007–NM–291–
AD, is corrected to read as follows:
‘‘* * * Include ‘‘Docket No. FAA–
2007–0411; Directorate Identifier 2007–
NM–291–AD’’ at the beginning of your
comments. * * *
In the Federal Register of January 7,
2008, on page 1056, in the third column,
the Supplemental Information section of
Docket No. FAA–2008–0412, Directorate
PO 00000
Frm 00004
Fmt 4700
Sfmt 4700
Corrected Docket No.
FAA–2007–0410
FAA–2007–0411
FAA–2007–0412
Identifier 2007–NM–290–AD, is
corrected to read as follows:
‘‘* * * Include ‘‘Docket No. FAA–
2007–0412; Directorate Identifier 2007–
NM–290–AD’’ at the beginning of your
comments. * * *
§ 39.13
[Corrected]
I In the Federal Register of January 8,
2008, on page 1271, in the first column,
paragraph 2. of PART 39—
AIRWORTHINESS DIRECTIVES of AD
2008–01–02 is corrected to read as
follows:
*
*
*
*
*
2008–01–02 Viking Air Limited (Formerly
Bombardier, Inc.): Amendment 39–
15325. Docket No. FAA–2007–0410;
Directorate Identifier 2007–NM–338–AD.
*
*
*
*
*
In the Federal Register of January 7,
2008, on page 1053, in the third column,
paragraph 2. of PART 39–
AIRWORTHINESS DIRECTIVES of AD
2004–07–22 R1 is corrected to read as
follows:
*
*
*
*
*
2004–07–22 R1 Boeing: Amendment 39–
15326. Docket No. FAA–2007–0411;
Directorate Identifier 2007–NM–291–AD.
*
*
*
*
*
In the Federal Register of January 7,
2008, on page 1057, in the first column,
paragraph 2. of PART 39–
AIRWORTHINESS DIRECTIVES of AD
90–25–05 R1 is corrected to read as
follows:
*
*
*
*
*
I
E:\FR\FM\14FER1.SGM
14FER1
Federal Register / Vol. 73, No. 31 / Thursday, February 14, 2008 / Rules and Regulations
90–25–05 R1 Boeing: Amendment 39–
15327. Docket No. FAA–2007–0412;
Directorate Identifier 2007–NM–290–AD.
*
*
*
*
*
Issued in Renton, Washington, on February
7, 2008.
Kevin Hull,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E8–2623 Filed 2–13–08; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
14 CFR Part 39
[Docket No. FAA–2007–0183; Directorate
Identifier 2007–NM–146–AD; Amendment
39–15376; AD 2008–04–04]
RIN 2120–AA64
Airworthiness Directives; Bombardier
Model DHC–8–400 Series Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: We are adopting a new
airworthiness directive (AD) for the
products listed above. This AD results
from mandatory continuing
airworthiness information (MCAI)
originated by an aviation authority of
another country to identify and correct
an unsafe condition on an aviation
product. The MCAI describes the unsafe
condition as:
ebenthall on PRODPC61 with RULES
There has been a reported case of failure
of a bracket (P/N 85217732–108) of the overcentering spring assembly inside the
translating door of the forward baggage
compartment. * * * Failure of the bracket
caused the eyebolt at the bottom of the spring
assembly to become loose, resulted in
damage of the support beam during normal
door handle movement. Damage of the
support beam, which is dormant, in
combination with failure of a doorstop
attached to any remaining undamaged
support beam will degrade the structural
integrity of the door, resulting in possible
depressurization or loss of the door.
We are issuing this AD to require
actions to correct the unsafe condition
on these products.
DATES: This AD becomes effective
March 20, 2008.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of March 20, 2008.
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov or in person at the
U.S. Department of Transportation,
15:28 Feb 13, 2008
Jkt 214001
FOR FURTHER INFORMATION CONTACT:
Pong K. Lee, 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) 228–7324; fax
(516) 794–5531.
SUPPLEMENTARY INFORMATION:
Discussion
Federal Aviation Administration
VerDate Aug<31>2005
Docket Operations, M–30, West
Building Ground Floor, Room W12–140,
1200 New Jersey Avenue, SE.,
Washington, DC.
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to the specified products. That
NPRM was published in the Federal
Register on November 13, 2007 (72 FR
63827). That NPRM proposed to correct
an unsafe condition for the specified
products. The MCAI states:
There has been a reported case of failure
of a bracket (P/N 85217732–108) of the overcentering spring assembly inside the
translating door of the forward baggage
compartment. This condition can exist on
other translating doors on the aircraft.
Investigation concluded that an insufficient
gap between the bottom eyebolt and the
barrel of the spring assembly caused an
increase of tension load on the bracket and
resulted in subsequent failure of the bracket.
Failure of the bracket caused the eyebolt at
the bottom of the spring assembly to become
loose, resulted in damage of the support
beam during normal door handle movement.
Damage of the support beam, which is
dormant, in combination with failure of a
doorstop attached to any remaining
undamaged support beam will degrade the
structural integrity of the door, resulting in
possible depressurization or loss of the door.
Corrective actions include a one-time
inspection for damage of the spring
support bracket and support beam of the
forward baggage door, aft service door,
and aft passenger door; repetitive
inspections for integrity (corrosion,
damage, cracking, and looseness or
misalignment) of the doorstops of
support beams found to be within
damage limits; repair of support beams,
or replacement of damaged brackets,
support beams, or doorstops, as
applicable; and removal of certain
washers and nuts. You may obtain
further information by examining the
MCAI in the AD docket.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM or
on the determination of the cost to the
public.
PO 00000
Frm 00005
Fmt 4700
Sfmt 4700
8591
Conclusion
We reviewed the available data and
determined that air safety and the
public interest require adopting the AD
as proposed.
Differences Between This AD and the
MCAI or Service Information
We have reviewed the MCAI and
related service information and, in
general, agree with their substance. But
we might have found it necessary to use
different words from those in the MCAI
to ensure the AD is clear for U.S.
operators and is enforceable. In making
these changes, we do not intend to differ
substantively from the information
provided in the MCAI and related
service information.
We might also have required different
actions in this AD from those in the
MCAI in order to follow our FAA
policies. Any such differences are
highlighted in a NOTE within the AD.
Costs of Compliance
We estimate that this AD will affect
about 29 products of U.S. registry. We
also estimate that it will take about 5
work-hours per product to comply with
the basic requirements of this AD. The
average labor rate is $80 per work-hour.
Required parts will cost about $0 per
product. Where the service information
lists required parts costs that are
covered under warranty, we have
assumed that there will be no charge for
these parts. As we do not control
warranty coverage for affected parties,
some parties may incur costs higher
than estimated here. Based on these
figures, we estimate the cost of this AD
to the U.S. operators to be $11,600, or
$400 per product.
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.
E:\FR\FM\14FER1.SGM
14FER1
]]>Agencies
[Federal Register Volume 73, Number 31 (Thursday, February 14, 2008)]
[Rules and Regulations]
[Pages 8589-8591]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-2623]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket Nos. FAA-2007-0410, FAA-2007-0411, and FAA-2007-0412;
Directorate Identifiers 2007-NM-338-AD, 2007-NM-291-AD, and 2007-NM-
290-AD; Amendments 39-15325, 39-15326, 39-15327; ADs 2008-01-02, 2004-
07-22 R1, and 90-25-05 R1]
RIN 2120-AA64
Airworthiness Directives; Viking Air Limited Model (Caribou) DHC-
4 and (Caribou) DHC-4A Airplanes; and Boeing Model 747-100, 747-100B,
747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D,
747-400F, 747SR, and 747SP Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; corrections.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting typographical errors in three existing
airworthiness directives (ADs) that were published in the Federal
Register on January 8, 2008 (73 FR 1269); January 7, 2008 (73 FR 1052);
and January 7, 2008 (73 FR 1055). The errors resulted in incorrect
docket numbers. One AD applies to all Viking Air Limited Model
(Caribou) DHC-4 and (Caribou) DHC-4A airplanes. The other two ADs apply
to all Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP
series airplanes. The Viking Air AD requires doing a fluorescent
penetrant inspection for cracking of certain upper engine mount bracket
assemblies, and corrective actions if necessary. One of the Boeing ADs
requires revising the FAA-approved maintenance inspection program to
include inspections that will give no less than the required damage
tolerance rating for each structural significant item, and repair of
cracked structure. The other Boeing AD requires implementing a
corrosion prevention and control program.
DATES: AD 2008-01-02 is effective January 23, 2008. ADs 2004-07-22 R1
and 90-25-05 R1 are effective January 22, 2008.
ADDRESSES: You may examine the AD dockets on the Internet at https://
www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD dockets contain this AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (telephone 800-647-5527) is the Document Management
Facility, U.S. Department of Transportation, Docket Operations, M-30,
West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590.
FOR FURTHER INFORMATION ON AD 2008-01-02, CONTACT: George Duckett,
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) 228-7325; fax (516) 794-5531.
FOR FURTHER INFORMATION ON ADs 2004-07-22 R1 and 90-25-05 R1, CONTACT:
Ivan Li, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle
Aircraft Certification Office, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone (425) 917-6437; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION: We have issued the ADs identified in the
following table.
[[Page 8590]]
Affected ADs
------------------------------------------------------------------------
AD-- Affects-- And requires--
------------------------------------------------------------------------
2008-01-02, amendment 39- All Viking Air A fluorescent
15325 (73 FR 1269, January Limited Model penetrant
8, 2008), issued December (Caribou) DHC-4 and inspection (FPI)
20, 2007. (Caribou) DHC-4A for cracking of
airplanes. certain upper
engine mount
bracket assemblies,
and corrective
actions if
necessary.
2004-07-22 R1, amendment 39- All Boeing Model 747- Revising the FAA-
15326 (73 FR 1052, January 100, 747-100B, 747- approved
7, 2008), issued December 100B SUD, 747-200B, maintenance
26, 2007. 747-200C, 747-200F, inspection program
747-300, 747-400, to include
747-400D, 747-400F, inspections that
747SR, and 747SP will give no less
series airplanes. than the required
damage tolerance
rating for each
structural
significant item,
and repair of
cracked structure.
90-25-05 R1, amendment 39- All Boeing Model 747- Implementing a
15327 (73 FR 1055, January 100, 747-100B, 747- corrosion
7, 2008), issued December 100B SUD, 747-200B, prevention and
26, 2007. 747-200C, 747-200F, control program.
747-300, 747-400, (That AD revised an
747-400D, 747-400F, earlier AD by
747SR, and 747SP removing future
series airplanes. type-certificated
models from the
applicability.)
------------------------------------------------------------------------
As published, those ADs specify incorrect docket numbers throughout
the preamble and regulatory text. Docket numbers are assigned by the
Federal Document Management System. We have been informed that
incorrect docket numbers were assigned. The correct docket information
is provided in the following table.
Corrected AD Docket Numbers
----------------------------------------------------------------------------------------------------------------
AD No. Original Docket No. Corrected Docket No.
----------------------------------------------------------------------------------------------------------------
AD 2008-01-02........................ FAA-2008-0410................ FAA-2007-0410
2004-07-22 R1........................ FAA-2008-0411................ FAA-2007-0411
AD 90-25-05 R1....................... FAA-2008-0412................ FAA-2007-0412
----------------------------------------------------------------------------------------------------------------
Any commenter who submitted comments to an original, incorrect
docket number should check Docket No. FAA-2007-0410, FAA-2007-0411, or
FAA 2007-0412 on www.regulations.gov to determine whether the comments
have been received and filed in the appropriate docket. If not, or if
it is not possible to determine whether comments have been posted to
the correct docket, the comments should be resubmitted using the
correct docket number.
No other part of the preamble or regulatory information has been
changed; therefore, the final rule is not republished in the Federal
Register.
The effective date of AD 2008-01-02 remains January 23, 2008. The
effective date of AD 2004-07-22 R1 remains January 22, 2008. The
effective date of AD 90-25-05 R1 remains January 22, 2008.
Correction
In the Federal Register of January 8, 2008, on page 1269, in the
third column, the headings section of AD 2008-01-02 is corrected to
read as follows:
``[Docket No. FAA-2007-0410; Directorate Identifier 2007-NM-338-AD;
Amendment 39-15325; AD 2008-01-02]''
In the Federal Register of January 7, 2008, on page 1052, in the
first column, the headings section of AD 2004-07-22 R1 is corrected to
read as follows:
``[Docket No. FAA-2007-0411; Directorate Identifier 2007-NM-291-AD;
Amendment 39-15326; AD 2004-07-22 R1]''
In the Federal Register of January 7, 2008, on page 1055, in the
second column, the headings section of AD 90-25-05 R1 is corrected to
read as follows:
``[Docket No. FAA-2007-0412; Directorate Identifier 2007-NM-290-AD;
Amendment 39-15327; AD 90-25-05 R1]''
In the Federal Register of January 8, 2008, on page 1270, in the
second and third columns, the Supplemental Information section of
Docket No. FAA-2008-0410, Directorate Identifier 2007-NM-338-AD, is
corrected to read as follows:
``* * * Include ``Docket No. FAA-2007-0410; Directorate Identifier
2007-NM-338-AD'' at the beginning of your comments. * * *
In the Federal Register of January 7, 2008, on page 1053, in the
second column, the Supplemental Information section of Docket No. FAA-
2008-0411, Directorate Identifier 2007-NM-291-AD, is corrected to read
as follows:
``* * * Include ``Docket No. FAA-2007-0411; Directorate Identifier
2007-NM-291-AD'' at the beginning of your comments. * * *
In the Federal Register of January 7, 2008, on page 1056, in the
third column, the Supplemental Information section of Docket No. FAA-
2008-0412, Directorate Identifier 2007-NM-290-AD, is corrected to read
as follows:
``* * * Include ``Docket No. FAA-2007-0412; Directorate Identifier
2007-NM-290-AD'' at the beginning of your comments. * * *
Sec. 39.13 [Corrected]
0
In the Federal Register of January 8, 2008, on page 1271, in the first
column, paragraph 2. of PART 39--AIRWORTHINESS DIRECTIVES of AD 2008-
01-02 is corrected to read as follows:
* * * * *
2008-01-02 Viking Air Limited (Formerly Bombardier, Inc.): Amendment
39-15325. Docket No. FAA-2007-0410; Directorate Identifier 2007-NM-
338-AD.
* * * * *
In the Federal Register of January 7, 2008, on page 1053, in the
third column, paragraph 2. of PART 39-AIRWORTHINESS DIRECTIVES of AD
2004-07-22 R1 is corrected to read as follows:
* * * * *
2004-07-22 R1 Boeing: Amendment 39-15326. Docket No. FAA-2007-0411;
Directorate Identifier 2007-NM-291-AD.
* * * * *
0
In the Federal Register of January 7, 2008, on page 1057, in the first
column, paragraph 2. of PART 39-AIRWORTHINESS DIRECTIVES of AD 90-25-05
R1 is corrected to read as follows:
* * * * *
[[Page 8591]]
90-25-05 R1 Boeing: Amendment 39-15327. Docket No. FAA-2007-0412;
Directorate Identifier 2007-NM-290-AD.
* * * * *
Issued in Renton, Washington, on February 7, 2008.
Kevin Hull,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-2623 Filed 2-13-08; 8:45 am]
BILLING CODE 4910-13-P
