[Federal Register Volume 61, Number 130 (Friday, July 5, 1996)]
[Rules and Regulations]
[Pages 35122-35125]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 96-15953]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 94-NM-102-AD; Amendment 39-9679; AD 96-13-11]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A300 B2 and B4 Series
Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
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SUMMARY: This amendment supersedes an existing airworthiness directive
(AD), applicable to all Airbus Model A300 B2, B4-100, and B4-200 series
airplanes, that currently requires supplemental structural inspections
to detect fatigue cracking, and repair of cracked structure. This
amendment requires revising the supplemental structural inspection
(SSID) program by changing some of the inspection techniques, changing
some of the thresholds and intervals for inspections, expanding the
area to be inspected for some of the inspections, and revising the
Fleet Leader Program. This amendment is prompted by a review of recent
service history and reports received from the current SSID program
required by the existing AD. The actions specified by this AD are
intended to prevent reduced structural integrity of these airplanes due
to fatigue cracking.
DATES: Effective August 9, 1996.
The incorporation by reference of Airbus Industrie A300
Supplemental Structural Inspection Document (SSID), Revision 2, dated
June 1994, as listed in the regulations is approved by the Director of
the Federal Register as of August 9, 1996.
The incorporation by reference of Airbus Industrie A300
Supplemental Structural Inspection Document (SSID), dated September
1989, as listed in the regulations, was approved previously by the
Director of the Federal Register as of March 9, 1993 (58 FR 6703,
February 2, 1993).
ADDRESSES: The service information referenced in this AD may be
obtained from Airbus Industrie, 1 Rond Point Maurice Bellonte, 31707
Blagnac Cedex, France. This information may be examined at the Federal
Aviation Administration (FAA), Transport Airplane Directorate, Rules
Docket, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of
the Federal Register, 800 North Capitol Street, NW., suite 700,
Washington, DC.
FOR FURTHER INFORMATION CONTACT: Phil Forde, Aerospace Engineer,
Standardization Branch, ANM-113, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (206)
227-2146; fax (206) 227-1149.
SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) by superseding AD 93-01-24,
amendment 39-8478 (58 FR 6703, February 2, 1993), which is applicable
to all Airbus Model A300 B2, B4-100, and B4-200 series airplanes, was
published in the Federal Register on January 31, 1996 (61 FR 3343). The
action proposed to continue to require supplemental structural
inspections to detect fatigue cracking, and repair of cracked
structure. The action also proposed to require revising the
supplemental structural inspection program, including changing some of
the inspection techniques, changing some of the thresholds and
intervals for certain inspections, expanding the area to be inspected
for some of the inspections, and revising the Fleet Leader Program.
Interested persons have been afforded an opportunity to participate
in the making of this amendment. Due consideration has been given to
the two comments received.
Support for the Proposal
Both commenters support the proposed rule.
Conclusion
After careful review of the available data, including the comment
noted above, the FAA has determined that air safety and the public
interest require the adoption of the rule as proposed.
Cost Impact
The FAA estimates that approximately 26 Model A300 series airplanes
of U.S. registry will be affected by this AD.
The actions that are currently required by AD 93-01-24 take
approximately 564 work hours per airplane to accomplish, at an average
labor rate of $60 per work hour. Based on these figures, the cost
impact on U.S. operators of the actions required by AD 93-01-24 is
estimated to be $879,840, or $33,840 per airplane.
Implementation of the inspections, repairs, and replacements
specified in Revision 2 of the SSID into an operator's maintenance
program is estimated to require approximately 597 work hours (including
removal, inspection, and installation work hours) per airplane per
year, at an average labor rate of $60 per
[[Page 35123]]
work hour. Based on these figures, the cost impact on U.S. operators of
the proposed requirements of this AD is estimated to be $931,320, or
$35,820 per airplane.
The cost impact figures discussed above are based on assumptions
that no operator has yet accomplished any of the requirements of this
AD action, and that no operator would accomplish those actions in the
future if this AD were not adopted.
Regulatory Impact
The regulations adopted herein will not have substantial direct
effects 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. Therefore, in
accordance with Executive Order 12612, it is determined that this final
rule does not have sufficient federalism implications to warrant the
preparation of a Federalism Assessment.
For the reasons discussed above, I certify that this action (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. A final evaluation has been prepared for this action
and it is contained in the Rules Docket. A copy of it may be obtained
from the Rules Docket at the location provided under the caption
ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends part 39 of
the Federal Aviation Regulations (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. Section 39.13 is amended by removing amendment 39-8478 (58 FR
6703, February 2, 1993), and by adding a new airworthiness directive
(AD), amendment 39-9679, to read as follows:
96-13-11 Airbus Industries: Amendment 39-9679. Docket 94-NM-102-AD.
Supersedes AD 93-01-24, Amendment 39-8478.
Applicability: All Model A300 B2-1A, B2-1C, B2K-3C, and B2-203
series airplanes, and Model A300 B4-2C, B4-103, and B4-203 series
airplanes; certificated in any category.
Note 1: This AD applies to each airplane identified in the
preceding applicability provision, regardless of whether it has been
otherwise modified, altered, or repaired in the area subject to the
requirements of this AD. For airplanes that have been modified,
altered, or repaired so that the performance of the requirements of
this AD is affected, the owner/operator must request approval for an
alternative method of compliance in accordance with paragraph (m) of
this AD. The request should include an assessment of the effect of
the modification, alteration, or repair on the unsafe condition
addressed by this AD; and, if the unsafe condition has not been
eliminated, the request should include specific proposed actions to
address it.
Compliance: Required as indicated, unless accomplished
previously.
To prevent reduced structural integrity of these airplanes due
to fatigue cracking, accomplish the following:
(a) Within one year after March 9, 1993 (the effective date of
AD 93-01-24, amendment 39-8478), incorporate a revision into the
FAA-approved maintenance inspection program that provides for
supplemental maintenance inspections, modifications, repair, or
replacement of the significant structural details (SSD) and
significant structural items (SSI) specified in ``Airbus Industrie
A300 Supplemental Structural Inspection Document'' (SSID), dated
September 1989 (hereafter referred to as ``the SSID'').
(b) Within one year after the effective date of this AD, replace
the revision of the FAA-approved maintenance program required by
paragraph (a) of this AD with the inspections, inspection intervals,
repairs, and replacements defined in ``Airbus Industrie A300
Supplemental Structural Inspection Document'' (SSID), Revision 2,
dated June 1994 (hereafter referred to as ``Revision 2 of the
SSID''). Accomplish the actions specified in the service bulletins
identified in Section 6, ``SB Reference List,'' Revision 2 of the
SSID, at the times specified in those service bulletins. The actions
are to be accomplished in accordance with those service bulletins.
(1) For airplanes that have exceeded the threshold specified in
any of the service bulletins identified in Section 6, ``SB Reference
List,'' Revision 2 of the SSID: Accomplish the actions specified in
those service bulletins within the grace period specified in that
service bulletin. The grace period is to be measured from the
effective date of this AD.
(2) For airplanes that have exceeded the threshold specified in
any of the service bulletins identified in Section 6, ``SB Reference
List,'' Revision 2 of the SSID, and a grace period is not specified
in that service bulletin: Accomplish the actions specified in that
service bulletins within 1,500 flight cycles after the effective
date of this AD.
(c) If any cracked structure is detected during the inspections
required by either paragraph (a) or (b) of this AD, prior to further
flight, permanently repair the cracked structure in accordance with
either paragraph (c)(1), (c)(2), or (c)(3) of this AD.
Note 2: A permanent repair is defined as a repair that meets the
certification basis of the airplane, and does not require additional
modification at a later date.
(1) The service bulletins listed in Section 6, ``SB Reference
List,'' of the SSID [for airplanes that are currently being
inspected in accordance with paragraph (a) of this AD]; or in
accordance with a method approved by the Manager, Standardization
Branch, ANM-113, FAA, Transport Airplane Directorate, if a permanent
repair is not specified in any of these service bulletins. Or
(2) The service bulletins listed in Section 6, ``SB Reference
List,'' of Revision 2 of the SSID [for airplanes that are currently
being inspected in accordance with paragraph (b) of this AD]; or in
accordance with a method approved by the Manager, Standardization
Branch, ANM-113, if a permanent repair is not specified in any of
these service bulletins. Or
(3) Other permanent repair data meeting the certification basis
of the airplane which is approved by the Manager, Standardization
Branch, ANM-113, or by the Direction Gonorale de l'Aviation Civile
(DGAC) of France.
(d) For airplanes identified as Fleet Leader Program (FLP) in
Section 5, ``Fleet Leader Program,'' of the SSID or Revision 2 of
the SSID: Inspect according to the instructions and intervals
specified in paragraph 4.4, ``Adjustment of Inspection Requirements
and DSG,'' of Section 4, or Section 9, as applicable, of the SSID
[for airplanes inspected in accordance with paragraph (a) of this
AD], or Revision 2 of the SSID [for airplanes inspected in
accordance with paragraph (b) of this AD], for each SSD.
(e) For the purpose of accomplishing paragraphs (d), (f), (g),
and (i) of this AD, operators shall not use paragraph 6.2,
``Complete RR Method,'' of Section 9 of the SSID to calculate
inspection thresholds and intervals.
(f) For Model A300-B2 and B2K-3C series airplanes: For any SSD
that has exceeded the values of the threshold specified in paragraph
6, ``Inspection Threshold and Intervals,'' Section 9 of the SSID,
inspect at the time specified in either paragraph (f)(1) or (f)(2)
of this AD, as applicable.
(1) For airplanes inspected in accordance with paragraph (a) of
this AD: Inspect within 2,000 landings after March 9, 1993, in
accordance with the SSID. Or
(2) For airplanes inspected in accordance with paragraph (b) of
this AD: Inspect within 2,000 landings after the effective date of
this AD, in accordance with Revision 2 of the SSID.
(g) For Model A300-B4 series airplanes: For any SSD that has
exceeded the values of the threshold specified in paragraph 6,
``Inspection Threshold and Intervals,'' Section 9 of the SSID,
inspect at the time specified in either paragraph (g)(1) or (g)(2)
of this AD, as applicable.
[[Page 35124]]
(1) For airplanes inspected in accordance with paragraph (a) of
this AD: Inspect within 1,500 landings after March 9, 1993 [the
effective date of AD 93-01-24, amendment 39-8478]. Or
(2) For airplanes inspected in accordance with paragraph (b) of
this AD: Inspect within 1,500 landings after the effective date of
this AD.
(h) For airplanes identified as FLP in Section 5, ``Fleet Leader
Program,'' of the SSID or Revision 2 of the SSID: Within one year
after the effective date of this AD, apply the basic requirements
given in Revision 2 of the SSID.
(i) For airplanes that are subject to the requirements of
paragraph (b) of this AD, and have exceeded the initial inspection
threshold specified in paragraph 4.4, ``Adjustment of Inspection
Requirements and DSG,'' of Section 4, or paragraph 6, ``Inspection
Threshold and Intervals,'' of Section 9, for each SSD: Perform the
initial inspection prior to the accumulation of the number of flight
cycles specified in paragraph 7, ``Additional Information,'' Section
9, of Revision 2 of the SSID.
Note 3: Fatigue ratings are not applicable to these allowances;
therefore, no adjustment is required.
Note 4: Paragraph (i) of this AD provides the ``grace'' periods
for those airplanes that are new to the FLP or that have newly added
or revised SSID requirements in accordance with paragraph (b) of
this AD.
(j) The grace period provided by paragraph (i) of this AD is
also applicable to the thresholds and/or repeat intervals for each
SSD for which the inspection interval or threshold was reduced in
accordance with the requirements of paragraph (b) of this AD.
(k) For FLP airplanes identified in Section 5, ``Fleet Leader
Program,'' of the SSID or Revision 2 of the SSID that are listed in
Section 7, ``SSI Limitation List,'' of the SSID [for airplanes that
are currently being inspected in accordance with paragraph (a) of
this AD] , or Revision 2 of the SSID [for airplanes that are
currently being inspected in accordance with paragraph (b) of this
AD]: Inspect at intervals not to exceed the interval specified for
each SSI, in accordance with the values given in Section 7, ``SSI
Limitation List,'' of the SSID or Revision 2 of the SSID, as
applicable.
(l) For all airplanes: All inspection results, positive or
negative, must be reported to Airbus Industrie in accordance with
either paragraph (l)(1) or (l)(2) of this AD, as applicable.
Information collection requirements contained in this regulation
have been approved by the Office of Management and Budget (OMB)
under the provisions of the Paperwork Reduction Act of 1980 (44
U.S.C. 3501 et seq.) and have been assigned OMB Control Number 2120-
0056.
(1) For FLP airplanes, identified in Section 5, ``Fleet Leader
Program,'' of the SSID or Revision 2 of the SSID: Submit reports in
accordance with the instructions in paragraph 5.2, ``SSIP Inspection
Reporting,'' of Section 5, and paragraph 7.1, ``General,'' of
Section 7 of the SSID [for airplanes that are currently being
inspected in accordance with paragraph (a) of this AD]; or Revision
2 of the SSID [for airplanes inspected in accordance with paragraph
(b) of this AD].
(2) For all airplanes that are subject to Section 6, ``SB
Reference List,'' of the SSID: Submit reports in accordance with the
instructions in the applicable service bulletins identified in
Section 6 of the SSID [for airplanes that are currently being
inspected in accordance with paragraph (a) of this AD]; or Revision
2 of the SSID [for airplanes that are currently being inspected in
accordance with paragraph (b) of this AD].
(m) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be
used if approved by the Manager, Standardization Branch, ANM-113,
FAA, Transport Airplane Directorate. Operators shall submit their
requests through an appropriate FAA Principal Maintenance Inspector,
who may add comments and then send it to the Manager,
Standardization Branch, ANM-113.
Note 5: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Standardization Branch, ANM-113.
Note 6: Alternative methods of compliance previously granted for
AD 93-01-24, amendment 39-8478, continue to be considered as
acceptable alternative methods of compliance with this amendment.
(n) Special flight permits may be issued in accordance with
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) to operate the airplane to a location where
the requirements of this AD can be accomplished.
(o) The actions shall be done in accordance with Airbus
Industrie Supplemental Structural Inspection Document (SSID), dated
September 1989; or Airbus Industrie A300 SSID, Revision 2, dated
June 1994, as applicable. Airbus Industrie A300 SSID, Revision 2,
dated June 1994, contains the following list of effective pages:
------------------------------------------------------------------------
Revision level
Page No. shown on page Date shown on page
------------------------------------------------------------------------
Record of revision.............. 2................ Jun 94
Section 0:
O-LEP 1..................... 2................ Jun 94.
O-TOC 1..................... 2................ Jun 94.
Section 1:
1-LEP 1..................... 2................ Jun 94.
1-TOC 1..................... 1................ Mar 93.
1........................... 1................ Mar 93.
2, 3........................ 2................ Jun 94.
Section 2:
2-LEP 1..................... 2................ Jun 94.
2-TOC 1..................... 1................ Mar 93.
1, 2........................ 1................ Mar 93.
3........................... 2................ Jun 94.
Section 3:
3-LEP 1..................... 2................ Jun 94.
3-TOC 1..................... 2................ Jun 94.
1, 2........................ 2................ Jun 94.
Section 4:
4-LEP 1..................... 1................ Mar 93.
4-TOC 1..................... 1................ Mar 93.
1-3, 7-9, 11-16, 19, 24-38, 1................ Mar 93.
40-46.
4-6, 10, 17, 18, 20-23, 39.. 0................ Sep 89.
Section 5:
5-LEP 1..................... 2................ Jun 94.
5-TOC 1..................... 2................ Jun 94.
1-48........................ 2................ Jun 94.
Section 6:
6-LEP 1..................... 2................ Jun 94.
6-TOC 1..................... 1................ Mar 93.
1........................... 1................ Mar 93.
2-4......................... 2................ Jun 94.
Section 7:
7-LEP 1..................... 1................ Mar 93.
7-TOC 1..................... 1................ Mar 93.
1-10........................ 1................ Mar 93.
Section 8:
8-LEP 1..................... 1................ Mar 93.
8-TOC 1..................... 1................ Mar 93.
1-5......................... 1................ Mar 93.
Section 9:
9-LEP 1-6................... 2................ Jun 94.
9-LEP 7-9................... 2................ Jun 94.
9-TOC 1..................... 1................ Mar 93.
1-3......................... 1................ Mar 93.
4........................... 2................ Jun 94.
526305/1-4...................... 0................ Sep 89.
526305/5........................ 1................ Mar 93.
526305/6........................ 2................ Jun 94.
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536204/1, 2..................... 0................ Sep 89.
536204/3, 4..................... 1................ Mar 93.
536204/5........................ 2................ Jun 94.
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536225/3........................ 2................ Jun 94.
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536301/7-9...................... 2................ Jun 94.
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536311/4........................ 1................ Mar 93.
536311/5, 6..................... 2................ Jun 94.
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536311/7........................ 2................ Jun 94.
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536403/4........................ 0................ Sep 89.
536405/1-3...................... 0................ Sep 89.
536405/4-5...................... 1................ Mar 93.
536405/6........................ 2................ Jun 94.
536405/7........................ 0................ Sep 89.
536407/1-3...................... 0................ Sep 89.
536407/4, 5..................... 1................ Mar 93.
536407/6........................ 2................ Jun 94.
536407/7........................ 0................ Sep 89.
536415/1, 2..................... 1................ Mar 93.
536415/3........................ 2................ Jun 94.
536415/4........................ 0................ Sep 89.
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536502/5, 6..................... 1................ Mar 93.
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536502/10....................... 2................ Jun 94.
536503/1, 2..................... 0................ Sep 89.
536503/3, 4..................... 1................ Mar 93.
536503/5........................ 2................ Jun 94.
536503/6-10..................... 0................ Sep 89.
536506/1, 2..................... 0................ Sep 89.
536506/3, 4..................... 1................ Mar 93.
536506/5........................ 2................ Jun 94.
536506/6-11..................... 0................ Sep 89.
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536509/4........................ 2................ Jun 94.
536509/5........................ 0................ Sep 89.
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536521/3, 4..................... 1................ Mar 93.
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536548/5........................ 2................ Jun 94.
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536596/1, 2..................... 0................ Sep 89.
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536598/1, 2..................... 0................ Sep 89.
536598/3, 4..................... 1................ Mar 93.
536598/5........................ 2................ Jun 94.
536598/6-9...................... 0................ Sep 89.
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536599/7........................ 2................ Jun 94.
536651/1, 2..................... 0................ Sep 89.
536651/3, 4..................... 1................ Mar 93.
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536704/1, 2..................... 0................ Sep 89.
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546001/1........................ 0................ Sep 89.
546001/2, 3..................... 1................ Mar 93.
546001/4........................ 2................ Jun 94.
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536014/1........................ 0................ Sep 89.
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536014/4........................ 2................ Jun 94.
536014/5-7...................... 0................ Sep 89.
556002/1........................ 0................ Sep 89.
556002/2, 3..................... 1................ Mar 93.
556002/4........................ 2................ Jun 94.
556002/5-7...................... 1................ Mar 93.
556003/1-4...................... 0................ Sep 89.
556003/5, 6..................... 1................ Mar 93.
556003/7........................ 2................ Jun 94.
556003/8-10..................... 1................ Mar 93.
556004/1, 2..................... 0................ Sep 89.
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556004/4........................ 2................ Jun 94.
576004/1........................ 0................ Sep 89.
576004/2........................ 1................ Mar 93.
576004/3........................ 2................ Jun 94.
576004/4-6...................... 0................ Sep 89.
576007/1........................ 0................ Sep 89.
576007/2........................ 1................ Mar 93.
576007/3........................ 2................ Jun 94.
576007/4-6...................... 0................ Sep 89.
576009/1........................ 0................ Sep 89.
576009/2........................ 1................ Mar 93.
576009/3........................ 2................ Jun 94.
576009/4-6...................... 0................ Sep 89.
576011/1........................ 0................ Sep 89.
576011/2........................ 1................ Mar 93.
576011/3........................ 2................ Jun 94.
576011/4-6...................... 0................ Sep 89.
576013/1-3...................... 0................ Sep 89.
576013/4........................ 1................ Mar 93.
576013/5-8...................... 2................ Jun 94.
576013/9........................ 2................ Jun 94.
576017/1........................ 0................ Sep 89.
576017/2........................ 1................ Mar 93.
576017/3........................ 2................ Jun 94.
576017/4........................ 0................ Sep 89.
576021/1........................ 0................ Sep 89.
576021/2........................ 1................ Mar 93.
576021/3........................ 2................ Jun 94.
576021/4-6...................... 0................ Sep 89.
576029/1, 2..................... 0................ Sep 89.
576029/3........................ 1................ Mar 93.
576029/4........................ 2................ Jun 94.
576029/5-7...................... 0................ Sep 89.
576031/1........................ 0................ Sep 89.
576031/2........................ 1................ Mar 93.
576031/3........................ 2................ Jun 94.
576031/4-6...................... 0................ Sep 89.
576035/1........................ 0................ Sep 89.
576035/2........................ 1................ Mar 93.
576035/3........................ 2................ Jun 94.
576035/4-6...................... 0................ Sep 89.
576037/1........................ 0................ Sep 89.
576037/2........................ 1................ Mar 93.
576037/3-6...................... 2................ Jun 94.
576037/7........................ 2................ Jun 94.
576041/1-4...................... 0................ Sep 89.
576041/5, 6..................... 2................ Jun 94.
576047/1........................ 0................ Sep 89.
576047/2-6...................... 2................ Jun 94.
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576051/2........................ 1................ Mar 93.
576051/3........................ 2................ Jun 94.
576051/4-6...................... 0................ Sep 89.
576062/1, 2..................... 1................ Mar 93.
576062/3-5...................... 2................ Jun 94.
576063/1-5...................... 2................ Jun 94.
576064/1-6...................... 2................ Jun 94.
576065/1-7...................... 2................ Jun 94.
576067/1-3...................... 2................ Jun 94.
576068/1-3...................... 2................ Jun 94.
576070/1-7...................... 2................ Jun 94.
------------------------------------------------------------------------
This incorporation by reference of Airbus Industrie SSID, dated
September 1989, was approved by the Director of the Federal Register
in accordance with 5 U.S.C. 552(a) and 1 CFR part 51, as of March 9,
1993 (58 FR 6703, February 2, 1993). The incorporation by reference
of Airbus Industrie SSID, Revision 2, dated June 1994, is approved
by the Director of the Federal Register in accordance with 5 U.S.C.
552(a) and 1 CFR part 51. Copies may be obtained from Airbus
Industrie, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex,
France. Copies may be inspected at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the
Office of the Federal Register, 800 North Capitol Street, NW., suite
700, Washington, DC.
(p) This amendment becomes effective on August 9, 1996.
Issued in Renton, Washington, on June 17, 1996.
Darrell M. Pederson,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 96-15953 Filed 7-3-96; 8:45 am]
BILLING CODE 4910-13-U
