Airworthiness Directives; Bombardier, Inc. Airplanes, 3184-3185 [2012-1197]
Download as PDF
3184
Federal Register / Vol. 77, No. 14 / Monday, January 23, 2012 / Proposed Rules
entities during the reporting period and
the results of such vote.
*
*
*
*
*
Dated: January 12, 2012.
Dale L. Aultman,
Secretary, Farm Credit Administration Board.
[FR Doc. 2012–901 Filed 1–20–12; 8:45 am]
BILLING CODE 6705–01–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2012–0034; Directorate
Identifier 2011–NM–153–AD]
RIN 2120–AA64
Airworthiness Directives; Bombardier,
Inc. Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
We propose to adopt a new
airworthiness directive (AD) for certain
Bombardier, Inc. Model CL–600–2B19
(Regional Jet Series 100 & 440)
airplanes. This proposed AD was
prompted by a report of a fire which
started in the vicinity of an electrical
panel that was fed by oxygen escaping
from a damaged third crew person
oxygen line that occurred while the
airplane was on the ground. This
proposed AD would require replacing
and changing the routing of the flexible
oxygen hose of the third crew person
oxygen line and modifying the entrance
compartment assembly. We are
proposing this AD to prevent the
possibility of damage to the third crew
person oxygen line and an oxygen-fed
fire in the airplane.
DATES: We must receive comments on
this proposed AD by March 8, 2012.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: (202) 493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE.,
Washington, DC 20590.
• Hand Delivery: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE.,
Washington, DC, between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays.
srobinson on DSK4SPTVN1PROD with PROPOSALS
SUMMARY:
VerDate Mar<15>2010
16:33 Jan 20, 2012
Jkt 226001
For service information identified in
this proposed AD, contact Bombardier,
ˆ
Inc., 400 Cote-Vertu Road West, Dorval,
´
Quebec H4S 1Y9, Canada; telephone
(514) 855–5000; fax (514) 855–7401;
email thd.crj@aero.bombardier.com;
Internet https://www.bombardier.com.
You may review copies of the
referenced service information at the
FAA, Transport Airplane Directorate,
1601 Lind Avenue SW., Renton,
Washington. For information on the
availability of this material at the FAA,
call (425) 227–1221.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov; or in person at the
Docket Operations office between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket
contains this proposed AD, the
regulatory evaluation, any comments
received, and other information. The
street address for the Docket Operations
office (telephone (800) 647–5527) is in
the ADDRESSES section. Comments will
be available in the AD docket shortly
after receipt.
FOR FURTHER INFORMATION CONTACT:
Cesar Gomez, Aerospace Engineer,
Airframe and Mechanical Systems
Branch, ANE–171, FAA, New York
Aircraft Certification Office, 1600
Stewart Avenue, Suite 410, Westbury,
New York 11590; telephone (516) 228–
7318; fax (516) 794–5531.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written
relevant data, views, or arguments about
this proposed AD. Send your comments
to an address listed under the
ADDRESSES section. Include ‘‘Docket No.
FAA–2012–0034; Directorate Identifier
2011–NM–153–AD’’ at the beginning of
your comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of this proposed AD. We will
consider all comments received by the
closing date and may amend this
proposed AD based on those comments.
We will post all comments we
receive, without change, to https://
www.regulations.gov, including any
personal information you provide. We
will also post a report summarizing each
substantive verbal contact we receive
about this proposed AD.
Discussion
Transport Canada Civil Aviation
(TCCA), which is the aviation authority
for Canada, has issued Canadian
Airworthiness Directive CF–2011–23,
dated July 14, 2011 (referred to after this
PO 00000
Frm 00026
Fmt 4702
Sfmt 4702
as ‘‘the MCAI’’), to correct an unsafe
condition for the specified products.
The MCAI states:
An operator has reported a ground fire in
the CL–600–2B19 aeroplane. The fire burnt
an 18 inch hole through the left upper
fuselage skin panel in the cockpit area. The
fire started in the vicinity of the Junction Box
1 (JB1) electrical panel, and was fed by
oxygen escaping from a damaged third
crewman oxygen line.
This [TCCA] Airworthiness Directive (AD)
was issued to prevent the possibility of
damage to the third crewman oxygen line
and an oxygen fed fire in the aeroplane.
The required actions include
replacing and changing the routing of
the flexible oxygen hose of the third
crew person oxygen line and modifying
the entrance compartment assembly.
You may obtain further information by
examining the MCAI in the AD docket.
Relevant Service Information
Bombardier has issued Service
Bulletin 601R–35–017, Revision A,
dated June 9, 2011. The actions
described in this service information are
intended to correct the unsafe condition
identified in the MCAI.
FAA’s Determination and Requirements
of This Proposed AD
This product has been approved by
the aviation authority of another
country, and is approved for operation
in the United States. Pursuant to our
bilateral agreement with the State of
Design Authority, we have been notified
of the unsafe condition described in the
MCAI and service information
referenced above. We are proposing this
AD because we evaluated all pertinent
information and determined an unsafe
condition exists and is likely to exist or
develop on other products of the same
type design.
Costs of Compliance
Based on the service information, we
estimate that this proposed AD would
affect about 588 products of U.S.
registry. We also estimate that it would
take about 13 work-hours per product to
comply with the basic requirements of
this proposed AD. The average labor
rate is $85 per work-hour. Required
parts would cost about $108 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 the
proposed AD on U.S. operators to be
$713,244, or $1,213 per product.
E:\FR\FM\23JAP1.SGM
23JAP1
Federal Register / Vol. 77, No. 14 / Monday, January 23, 2012 / Proposed Rules
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 determined that this proposed AD
would not have federalism implications
under Executive Order 13132. This
proposed AD would 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 this proposed 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);
3. Will not affect intrastate aviation in
Alaska; and
4. 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 proposed AD and placed it in the
AD docket.
srobinson on DSK4SPTVN1PROD with PROPOSALS
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
VerDate Mar<15>2010
16:33 Jan 20, 2012
Jkt 226001
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
Bombardier, Inc.: Docket No. FAA–2012–
0034; Directorate Identifier 2011–NM–
153–AD.
(a) Comments Due Date
We must receive comments by March 8,
2012.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc. Model
CL–600–2B19 (Regional Jet Series 100 & 440)
airplanes, certificated in any category,
equipped with entrance compartment
assembly having part numbers that begin
with A281001, A282001, A283001, A284001,
4591001, 4592001, 4593001, or 4594001.
(d) Subject
Air Transport Association (ATA) of
America Code 35: Oxygen.
(e) Reason
This AD was prompted by a report of a fire
which started in the vicinity of an electrical
panel that was fed by oxygen escaping from
a damaged third crew person oxygen line that
occurred while the airplane was on the
ground. We are issuing this AD to prevent the
possibility of damage to the third crew
person oxygen line and an oxygen-fed fire in
the airplane.
(f) Compliance
You are responsible for having the actions
required by this AD performed within the
compliance times specified, unless the
actions have already been done.
(g) Actions
Within 4,000 flight hours after the effective
date of this AD, replace and change the
routing of the flexible oxygen hose of the
third crew person oxygen line and modify
the entrance compartment assembly, in
accordance with the Accomplishment
Instructions of Bombardier Service Bulletin
601R–35–017, Revision A, dated June 9,
2011.
(h) Parts Installation
As of the effective date of this AD, no
person may install an entrance compartment
assembly with a part number that begins with
A281001, A282001, A283001, A284001,
4591001, 4592001, 4593001, or 4594001, or
a flexible oxygen hose with part number
38027–0260, on any airplane, unless that
entrance compartment assembly or flexible
oxygen hose has been modified, in
accordance with the Accomplishment
Instructions of Bombardier Service Bulletin
601R–35–017, Revision A, dated June 9,
2011.
PO 00000
Frm 00027
Fmt 4702
Sfmt 4702
3185
(i) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, New York Aircraft
Certification Office (ACO), ANE–170, FAA,
has the authority to approve AMOCs for this
AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR
39.19, send your request to your principal
inspector or local Flight Standards District
Office, as appropriate. If sending information
directly to the ACO, send it to ATTN:
Program Manager, Continuing Operational
Safety, FAA, New York ACO, 1600 Stewart
Avenue, Suite 410, Westbury, New York
11590; telephone (516) 228–7300; fax (516)
794–5531. Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office. The AMOC
approval letter must specifically reference
this AD.
(2) Airworthy Product: For any requirement
in this AD to obtain corrective actions from
a manufacturer or other source, use these
actions if they are FAA-approved. Corrective
actions are considered FAA-approved if they
are approved by the State of Design Authority
(or their delegated agent). You are required
to assure the product is airworthy before it
is returned to service.
(j) Related Information
Refer to MCAI Canadian Airworthiness
Directive CF–2011–23, dated July 14, 2011;
and Bombardier Service Bulletin 601R–35–
017, Revision A, dated June 9, 2011; for
related information.
Issued in Renton, Washington on
January 13, 2012.
John Piccola,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2012–1197 Filed 1–20–12; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2011–1340; Airspace
Docket No. 11–AEA–22]
Proposed Establishment of Class E
Airspace; Grasonville, MD
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
This action proposes to
establish Class E Airspace at
Grasonville, MD, to accommodate a new
Area Navigation (RNAV) Global
Positioning System (GPS) special
Standard Instrument Approach
Procedure (SIAP) serving Queen Anne
E.R. Heliport. This action would
SUMMARY:
E:\FR\FM\23JAP1.SGM
23JAP1
Agencies
[Federal Register Volume 77, Number 14 (Monday, January 23, 2012)]
[Proposed Rules]
[Pages 3184-3185]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2012-1197]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0034; Directorate Identifier 2011-NM-153-AD]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: We propose to adopt a new airworthiness directive (AD) for
certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 &
440) airplanes. This proposed AD was prompted by a report of a fire
which started in the vicinity of an electrical panel that was fed by
oxygen escaping from a damaged third crew person oxygen line that
occurred while the airplane was on the ground. This proposed AD would
require replacing and changing the routing of the flexible oxygen hose
of the third crew person oxygen line and modifying the entrance
compartment assembly. We are proposing this AD to prevent the
possibility of damage to the third crew person oxygen line and an
oxygen-fed fire in the airplane.
DATES: We must receive comments on this proposed AD by March 8, 2012.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
Fax: (202) 493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
For service information identified in this proposed AD, contact
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec
H4S 1Y9, Canada; telephone (514) 855-5000; fax (514) 855-7401; email
thd.crj@aero.bombardier.com; Internet https://www.bombardier.com. You
may review copies of the referenced service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton,
Washington. For information on the availability of this material at the
FAA, call (425) 227-1221.
Examining the AD Docket
You may examine the AD docket on the Internet at https://www.regulations.gov; or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this proposed AD, the regulatory
evaluation, any comments received, and other information. The street
address for the Docket Operations office (telephone (800) 647-5527) is
in the ADDRESSES section. Comments will be available in the AD docket
shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Cesar Gomez, Aerospace Engineer,
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft
Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New
York 11590; telephone (516) 228-7318; fax (516) 794-5531.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2012-0034;
Directorate Identifier 2011-NM-153-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD based on those comments.
We will post all comments we receive, without change, to https://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.
Discussion
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian Airworthiness Directive CF-
2011-23, dated July 14, 2011 (referred to after this as ``the MCAI''),
to correct an unsafe condition for the specified products. The MCAI
states:
An operator has reported a ground fire in the CL-600-2B19
aeroplane. The fire burnt an 18 inch hole through the left upper
fuselage skin panel in the cockpit area. The fire started in the
vicinity of the Junction Box 1 (JB1) electrical panel, and was fed
by oxygen escaping from a damaged third crewman oxygen line.
This [TCCA] Airworthiness Directive (AD) was issued to prevent
the possibility of damage to the third crewman oxygen line and an
oxygen fed fire in the aeroplane.
The required actions include replacing and changing the routing of
the flexible oxygen hose of the third crew person oxygen line and
modifying the entrance compartment assembly. You may obtain further
information by examining the MCAI in the AD docket.
Relevant Service Information
Bombardier has issued Service Bulletin 601R-35-017, Revision A,
dated June 9, 2011. The actions described in this service information
are intended to correct the unsafe condition identified in the MCAI.
FAA's Determination and Requirements of This Proposed AD
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are proposing this AD because we
evaluated all pertinent information and determined an unsafe condition
exists and is likely to exist or develop on other products of the same
type design.
Costs of Compliance
Based on the service information, we estimate that this proposed AD
would affect about 588 products of U.S. registry. We also estimate that
it would take about 13 work-hours per product to comply with the basic
requirements of this proposed AD. The average labor rate is $85 per
work-hour. Required parts would cost about $108 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 the proposed AD on U.S. operators to
be $713,244, or $1,213 per product.
[[Page 3185]]
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 determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed
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);
3. Will not affect intrastate aviation in Alaska; and
4. 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 proposed AD and placed it in the AD docket.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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]
2. The FAA amends Sec. 39.13 by adding the following new AD:
Bombardier, Inc.: Docket No. FAA-2012-0034; Directorate Identifier
2011-NM-153-AD.
(a) Comments Due Date
We must receive comments by March 8, 2012.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc. Model CL-600-2B19 (Regional
Jet Series 100 & 440) airplanes, certificated in any category,
equipped with entrance compartment assembly having part numbers that
begin with A281001, A282001, A283001, A284001, 4591001, 4592001,
4593001, or 4594001.
(d) Subject
Air Transport Association (ATA) of America Code 35: Oxygen.
(e) Reason
This AD was prompted by a report of a fire which started in the
vicinity of an electrical panel that was fed by oxygen escaping from
a damaged third crew person oxygen line that occurred while the
airplane was on the ground. We are issuing this AD to prevent the
possibility of damage to the third crew person oxygen line and an
oxygen-fed fire in the airplane.
(f) Compliance
You are responsible for having the actions required by this AD
performed within the compliance times specified, unless the actions
have already been done.
(g) Actions
Within 4,000 flight hours after the effective date of this AD,
replace and change the routing of the flexible oxygen hose of the
third crew person oxygen line and modify the entrance compartment
assembly, in accordance with the Accomplishment Instructions of
Bombardier Service Bulletin 601R-35-017, Revision A, dated June 9,
2011.
(h) Parts Installation
As of the effective date of this AD, no person may install an
entrance compartment assembly with a part number that begins with
A281001, A282001, A283001, A284001, 4591001, 4592001, 4593001, or
4594001, or a flexible oxygen hose with part number 38027-0260, on
any airplane, unless that entrance compartment assembly or flexible
oxygen hose has been modified, in accordance with the Accomplishment
Instructions of Bombardier Service Bulletin 601R-35-017, Revision A,
dated June 9, 2011.
(i) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York Aircraft Certification Office (ACO), ANE-170, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the ACO, send it to ATTN: Program Manager, Continuing
Operational Safety, FAA, New York ACO, 1600 Stewart Avenue, Suite
410, Westbury, New York 11590; telephone (516) 228-7300; fax (516)
794-5531. Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office. The AMOC approval letter must specifically
reference this AD.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
(j) Related Information
Refer to MCAI Canadian Airworthiness Directive CF-2011-23, dated
July 14, 2011; and Bombardier Service Bulletin 601R-35-017, Revision
A, dated June 9, 2011; for related information.
Issued in Renton, Washington on January 13, 2012.
John Piccola,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-1197 Filed 1-20-12; 8:45 am]
BILLING CODE 4910-13-P