[Federal Register Volume 76, Number 211 (Tuesday, November 1, 2011)]
[Rules and Regulations]
[Pages 67343-67346]
[FR Doc No: 2011-28053]

-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-1162; Directorate Identifier 2011-NM-186-AD;
Amendment 39-16856; AD 2011-23-05]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Model 737-300, -400,
and -500 Series Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

-----------------------------------------------------------------------

SUMMARY: We are superseding an existing airworthiness directive (AD)
for certain Model 737-300, -400, and -500 series airplanes. That AD
currently requires repetitive inspections for cracking of the 1.04-inch
nominal diameter wire penetration hole, and applicable related
investigative and corrective actions. This AD reduces the compliance
times for those actions. This AD was prompted by reports of cracking in
the frame, or in the frame and frame reinforcement, common to the 1.04-
inch nominal diameter wire penetration hole intended for wire routing;
and recent reports of multiple adjacent frame cracking found before the
compliance time required by the existing AD. Such cracking could reduce
the structural capability of the frames to sustain limit loads, and
result in cracking in the fuselage skin and subsequent rapid
depressurization of the airplane. We are issuing this AD to correct the
unsafe condition on these products.

DATES: This AD is effective November 16, 2011.
    The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of November 16,
2011.
    We must receive any comments on this AD by December 16, 2011.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Fax:<PHONE_NUMBER>.
     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 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
    For service information identified in this AD, contact Boeing
Commercial Airplanes, Attention: Data & Services Management, P.O. Box
3707, MC 2H-65, Seattle, Washington 98124-2207; telephone (206) 544-
5000, extension 1; fax<PHONE_NUMBER>; email<EMAIL_ADDRESS>
Internet https://www.myboeingfleet.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<PHONE_NUMBER>.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://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 docket contains this AD, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Office (phone:<PHONE_NUMBER>) is in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Wayne Lockett, Aerospace Engineer,
Airframe Branch, ANM-120S, Seattle Aircraft Certification Office (ACO),
FAA, 1601 Lind Avenue SW., Renton, Washington 98057-3356; phone: (425)
917-6447; fax:<PHONE_NUMBER>; email<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Discussion

    On August 26, 2009, we issued AD 2009-02-06 R1, Amendment 39-16015
(74 FR 45979, September 8, 2009), for certain Model 737-300, -400, and
-500 series airplanes. That AD requires repetitive inspections for
cracking of the 1.04-inch nominal diameter wire penetration hole in the
frame and in the frame reinforcement, between stringers S-20 and S-21,
on both the left and right sides of the airplane, and applicable
related investigative and corrective actions. That AD resulted from
reports of cracking in the frame, or in the frame and frame
reinforcement, common to the 1.04-inch nominal diameter wire
penetration hole intended for wire routing. We issued that AD to detect
and correct cracking in the fuselage frames and frame reinforcements,
which could reduce the structural capability of the frames to sustain
limit loads, and result in cracking in the fuselage skin and subsequent
rapid depressurization of the airplane.

Actions Since AD Was Issued

    Since we issued AD 2009-02-06 R1, Amendment 39-16015 (74 FR 45979,
September 8, 2009), we received a report of four adjacent cracked
frames at body station (BS) 500B, BS 500C, BS 500D, and BS 520 in the
forward cargo compartment between S-20L and S-21L on a Model 737-300
series airplane. The cracks at BS 500B and BS 500C were completely
through the frame and fail-safe chord. The BS 500B frame was also
cracked on the right-hand side. The cracks were discovered when the
airplane had accumulated 44,535 total flight cycles and 44,876 total
flight hours--before the compliance time required by AD 2009-02-06 R1.

Relevant Service Information

    AD 2009-02-06 R1, Amendment 39-16015 (74 FR 45979, September 8,
2009), referred to Boeing Alert Service Bulletin 737-53A1279, dated
December 18, 2007, as the appropriate source of service information for
the required actions. Boeing has since revised this service bulletin.
We reviewed Boeing Alert Service Bulletin 737-53A1279, Revision 1,
dated September 2, 2011, which shortens the compliance time to 30,000
total flight cycles, with a grace period of 30 or 90 days, and reduces
the repetitive interval from 14,000 to 4,500 flight cycles. The
procedures are unchanged from those specified in

Boeing Alert Service Bulletin 737-53A1279, dated December 18, 2007.

FAA's Determination

    We are issuing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of the same type design.

AD Requirements

    This AD requires accomplishing the actions specified in the service
information described previously, except as discussed under
``Differences Between the AD and the Service Information.''

Differences Between the AD and the Service Information

    Boeing Alert Service Bulletin 737-53A1279, Revision 1, dated
September 2, 2011, specifies to contact the manufacturer for
instructions on how to repair certain conditions, but this proposed AD
would require repairing those conditions in one of the following ways:
     In accordance with a method that we approve; or
     Using data that meet the certification basis of the
airplane, and that have been approved by the Boeing Commercial
Airplanes Organization Designation Authorization (ODA) whom we have
authorized to make those findings.
    Boeing Alert Service Bulletin 737-53A1279, Revision 1, dated
September 2, 2011, specifies compliance with the Part 4 inspection by
the later of 4,500 flight cycles or 90 days--both after the date on
this service bulletin. In some cases, this compliance time might occur
before the Part 2 inspection. This AD (in paragraph (h)) therefore
requires the Part 4 inspection within 4,500 flight cycles after
accomplishment of the most recent Part 2 or Part 4 inspection, with a
grace period of 90 days. We have coordinated this difference with
Boeing.
    For certain airplanes that have accumulated 40,000 or more total
flight cycles, Boeing Alert Service Bulletin 737-53A1279, Revision 1,
dated September 2, 2011, specifies a 30-day compliance time for the
Part 2 inspection. Paragraph (k)(2) of this AD extends that compliance
time to 90 days for those airplanes, if the original chem.-milled
fuselage skins have been replaced with solid skins. This difference has
been coordinated with Boeing.

FAA's Justification and Determination of the Effective Date

    An unsafe condition exists that requires the immediate adoption of
this AD. The FAA has found that the risk to the flying public justifies
waiving notice and comment prior to adoption of this rule because
cracking in multiple adjacent fuselage frames and frame reinforcements
reduces the structural capability of the frames to sustain limit loads,
and result in cracking in the fuselage skin and subsequent rapid
depressurization of the airplane. Therefore, we find that notice and
opportunity for prior public comment are impracticable and that good
cause exists for making this amendment effective in less than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments before it becomes effective. However, we invite
you to send any written data, views, or arguments about this AD. Send
your comments to an address listed under the ADDRESSES section. Include
the Docket No. FAA-2011-1162 and directorate identifier 2011-NM-186-AD
at the beginning of your comments. We specifically invite comments on
the overall regulatory, economic, environmental, and energy aspects of
this AD. We will consider all comments received by the closing date and
may amend this AD because of those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.

Costs of Compliance

    We estimate that this AD affects 605 airplanes of U.S. registry. We
estimate the following costs to comply with this AD:

                                                                     Estimated Costs
--------------------------------------------------------------------------------------------------------------------------------------------------------
              Action                        Labor cost               Parts cost           Cost per product                Cost on U.S. operators
--------------------------------------------------------------------------------------------------------------------------------------------------------
Inspection........................  16 work-hours x $85 per     None...............  $1,360 per inspection       $822,800 per inspection cycle.
                                     hour = $1,360 per                                cycle.
                                     inspection cycle.
--------------------------------------------------------------------------------------------------------------------------------------------------------

    We estimate the following costs to do any necessary related
investigative actions that would be required based on the results of
the HFEC inspections. We have no way of determining the number of
aircraft that might need this inspection:

                                               On-Condition Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Cost per
                 Action                              Labor cost                   Parts cost           product
----------------------------------------------------------------------------------------------------------------
On-condition inspection.................  2 work-hours x $85 per hour =    None....................         $170
                                           $170.
----------------------------------------------------------------------------------------------------------------

     We have received no definitive data that would enable us to
provide a cost estimate for the on-condition repair or optional
modification specified in this AD.

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

    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),
    (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.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the
Administrator, the FAA amends part 39 of the Federal Aviation
Regulations (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 FAA amends Sec.  39.13 by removing airworthiness directive (AD)
2009-02-06 R1, Amendment 39-16015 (74 FR 45979, September 8, 2009), and
adding the following new AD:

2011-23-05 The Boeing Company: Amendment 39-16856; Docket No. FAA-
2011-1162; Directorate Identifier 2011-NM-186-AD.

(a) Effective Date

    This AD is effective November 16, 2011.

(b) Affected ADs

    This AD supersedes AD 2009-02-06 R1, Amendment 39-16015 (74 FR
45979, September 8, 2009).

(c) Applicability

    This AD applies to The Boeing Company Model 737-300, -400, -500
series airplanes, certificated in any category; as identified in
Boeing Alert Service Bulletin 737-53A1279, Revision 1, dated
September 2, 2011.

(d) Subject

    Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 53, Fuselage.

(e) Unsafe Condition

    This AD was prompted by reports of four cracked frames at
certain body stations (BS) in the forward cargo compartment. We are
issuing this AD to detect and correct cracking in the fuselage
frames and frame reinforcements, which could reduce the structural
capability of the frames to sustain limit loads, and result in
cracking in the fuselage skin and subsequent rapid depressurization
of the airplane.

(f) Compliance

    Comply with this AD within the compliance times specified,
unless already done.

(g) Inspection

    At the applicable time specified in paragraph 1.E.,
``Compliance,'' of Boeing Alert Service Bulletin 737-53A1279,
Revision 1, dated September 2, 2011, except as required by
paragraphs (k)(1), (k)(2), and (k)(4) of this AD: Do a high
frequency eddy current (HFEC) surface or HFEC hole/edge inspection
for any cracking of the 1.04-inch nominal diameter wire penetration
hole in the frame and frame reinforcement between stringer S-20 and
S-21, in accordance with Part 2 of the Accomplishment Instructions
of Boeing Alert Service Bulletin 737-53A1279, Revision 1, dated
September 2, 2011.

(h) Repetitive Inspection

    Within 4,500 flight cycles after accomplishment of the most
recent inspection specified in Part 2 or Part 4 of the
Accomplishment Instructions of Boeing Alert Service Bulletin 737-
53A1279, Revision 1, dated September 2, 2011, or within 90 days
after the effective date of this AD, whichever occurs later: Do an
HFEC hole/edge inspection for cracking of the 1.04-inch nominal
diameter wire penetration hole in the frame and frame reinforcement
between S-20 and S-21, in accordance with Part 4 of the
Accomplishment Instructions of Boeing Alert Service Bulletin 737-
53A1279, Revision 1, dated September 2, 2011. Repeat the inspection
thereafter at intervals not to exceed 4,500 flight cycles.

(i) Repair

    If any cracking is found during any inspection required by
paragraph (g) or (h) of this AD: Before further flight, repair the
crack including doing all related investigative and applicable
corrective actions, in accordance with the Accomplishment
Instructions of Boeing Alert Service Bulletin 737-53A1279, Revision
1, dated September 2, 2011, except as required by paragraph (k)(3)
of this AD. All related investigative and applicable corrective
actions must be done before further flight. Accomplishment of the
requirements of this paragraph terminates the repetitive inspection
requirements of paragraph (h) of this AD for the repaired location
of that frame.

(j) Optional Terminating Action

    Accomplishment of the preventive modification, including doing
all related investigative and applicable corrective actions,
specified in Part 5 of the Accomplishment Instructions of Boeing
Alert Service Bulletin 737-53A1279, Revision 1, dated September 2,
2011, except as required by paragraph (k)(3) of this AD, terminates
the repetitive inspection requirements of paragraph (h) of this AD
for the modified location of that frame, provided the modification
is done before further flight after an inspection required by
paragraph (g) or (h) of this AD has been done, and no cracking was
found on that frame location during that inspection.

(k) Exceptions to Service Bulletin Specifications

    The following exceptions apply in this AD.
    (1) Where paragraph 1.E., ``Compliance,'' of Boeing Alert
Service Bulletin 737-53A1279, Revision 1, dated September 2, 2011,
refers to a compliance time ``from date on Revision 1 of this
service bulletin,'' this AD requires compliance within the specified
compliance time after the effective date of this AD.
    (2) For airplanes meeting all of the criteria specified in
paragraphs (k)(2)(i), (k)(2)(ii), and (k)(2)(iii) of this AD: The
compliance time for the initial inspection specified in Part 2 of
the Accomplishment Instructions of Boeing Alert Service Bulletin
737-53A1279, Revision 1, dated September 2, 2011, and required by
paragraph (g) of this AD, may be extended to 90 days after the
effective date of this AD.
    (i) Model 737-300 series airplanes in Group 1, line numbers 1001
through 2565 inclusive;
    (ii) Airplanes that have accumulated 40,000 or more total flight
cycles as of the effective date of this AD; and
    (iii) Airplanes on which the modification specified in Boeing
Service Bulletin 737-53-1273, dated September 20, 2006; Revision 1,
dated December 21, 2006; Revision 2, dated June 4, 2007; Revision 3,
dated December 7, 2009; or Revision 4, dated July 23, 2010; has been
done, including any configuration or deviation that has been
approved as an AMOC during accomplishment of these service
bulletins, by the Boeing Commercial Airplanes Organization
Designation Authorization (ODA) that has been authorized by the
Manager, Seattle Aircraft Certification Office (ACO) to make those
findings.
    (3) Where Boeing Alert Service Bulletin 737-53A1279, Revision 1,
dated September 2, 2011 specifies to contact Boeing for appropriate
repair instructions: Before further flight, repair the crack using a
method approved in accordance with the procedures specified in
paragraph (m) of this AD.

    (4) The ``Condition'' column of paragraph 1.E., ``Compliance,''
of Boeing Alert Service Bulletin 737-53A1279, Revision 1, dated
September 2, 2011, refers to total flight cycles, ``at the date of/
on this service bulletin.'' However, this AD applies to the
airplanes with the specified total flight cycles as of the effective
date of this AD.

(l) Credit for Actions Accomplished in Accordance With Previous Service
Information

    Actions done in accordance with Boeing Alert Service Bulletin
737-53A1279, dated December 18, 2007, before the effective date of
this AD are acceptable for compliance with the corresponding actions
required by paragraphs (g), (h), (i), and (j) of this AD.

(m) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Seattle ACO, 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 manager of the
ACO, send it to the attention of the person identified in the
Related Information section of this AD. Information may be emailed
to<EMAIL_ADDRESS>    (2) 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.
    (3) An AMOC that provides an acceptable level of safety may be
used for any repair required by this AD if it is approved by Boeing
Commercial Airplanes ODA that has been authorized by the Manager,
Seattle ACO to make those findings. For a repair method to be
approved, the repair must meet the certification basis of the
airplane, and the approval must specifically refer to this AD.
    (4) AMOCs approved for paragraphs (h) and (i) of AD 2009-02-06
R1, Amendment 39-16015 (74 FR 45979, September 8, 2009), are
approved as AMOCs for the corresponding provisions of paragraphs
(g), (h), and (i) of this AD.

(n) Related Information

    For more information about this AD, contact Wayne Lockett,
Aerospace Engineer, Airframe Branch, ANM-120S, Seattle ACO, FAA,
1601 Lind Avenue SW., Renton, Washington 98057-3356; phone: (425)
917-6447; fax:<PHONE_NUMBER>; email<EMAIL_ADDRESS>
(o) Material Incorporated by Reference

    (1) You must use the following service information to do the
actions required by this AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the incorporation by
reference (IBR) under 5 U.S.C. 552(a) and 1 CFR part 51 of the
following service information on the date specified:
    (i) Boeing Alert Service Bulletin 737-53A1279, Revision 1, dated
September 2, 2011, approved for IBR November 16, 2011.
    (2) If you accomplish the optional actions specified by this AD,
you must use the following service information to perform those
actions, unless the AD specifies otherwise. The Director of the
Federal Register approved the incorporation by reference (IBR) of
the following service information on the date specified:
    (i) Boeing Alert Service Bulletin 737-53A1279, Revision 1, dated
September 2, 2011, approved for IBR November 16, 2011.
    (3) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone
(206) 544-5000, extension 1; fax<PHONE_NUMBER>; e-mail
<EMAIL_ADDRESS>Internet https://www.myboeingfleet.com.
    (4) You may review copies of the service information at the FAA,
1601 Lind Avenue SW., Renton, Washington. For information on the
availability of this material at the FAA, call<PHONE_NUMBER>.
    (5) You may also review copies of the service information that
is incorporated by reference at the National Archives and Records
Administration (NARA). For information on the availability of this
material at an NARA facility, call<PHONE_NUMBER>, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

    Issued in Renton, Washington, on October 20, 2011.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-28053 Filed 10-31-11; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 82, Number 187 (Thursday, September 28, 2017)]
[Rules and Regulations]
[Pages 45202-45205]
[FR Doc No: 2017-20840]

-----------------------------------------------------------------------

ENVIRONMENTAL PROTECTION AGENCY

40 CFR Part 82

[EPA-HQ-OAR-2017-0213; FRL-9968-68-OAR]
RIN 2060-AT43

Protection of Stratospheric Ozone: Refrigerant Management
Regulations for Small Cans of Motor Vehicle Refrigerant

AGENCY: Environmental Protection Agency (EPA).

ACTION: Direct final rule.

-----------------------------------------------------------------------

SUMMARY: EPA is taking direct final action to correct an editing
oversight that led to a potential conflict in a prior rulemaking as to
whether or not containers holding two pounds or less of non-exempt
substitute refrigerants for use in motor vehicle air conditioning that
are not equipped with a self-sealing valve can be sold to persons that
are not certified technicians, provided those small cans were
manufactured or imported prior to January 1, 2018. This action
clarifies that those small cans may continue to be sold to persons that
are not certified as technicians under sections 608 or 609 of the Clean
Air Act.

DATES: This rule is effective on December 27, 2017 without further
notice, unless EPA receives adverse comment by October 30, 2017. If EPA
receives adverse comment, we will publish a timely withdrawal in the
Federal Register informing the public that the rule will not take
effect.

ADDRESSES: Submit your comments, identified by Docket ID No. EPA-HQ-
OAR-2017-0213, at http://www.regulations.gov. Follow the online
instructions for submitting comments. Once submitted, comments cannot
be edited or removed from Regulations.gov. EPA may publish any comment
received to its public docket. Do not submit electronically any
information you consider to be Confidential Business Information (CBI)
or other information whose disclosure is restricted by statute.
Multimedia submissions (audio, video, etc.) must be accompanied by a
written comment. The written comment is considered the official comment
and should include discussion of all points you wish to make. EPA will
generally not consider comments or comment contents located outside of
the primary submission (i.e., on the web, cloud, or other file sharing
system). For additional submission methods, the full EPA public comment
policy, information about CBI or multimedia submissions, and general
guidance on making effective comments, please visit http://www2.epa.gov/dockets/commenting-epa-dockets.

FOR FURTHER INFORMATION CONTACT: Sara Kemme by regular mail: U.S.
Environmental Protection Agency, Stratospheric Protection Division
(6205T), 1200 Pennsylvania Avenue NW., Washington, DC 20460; by
telephone:<PHONE_NUMBER>; or by email<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION

I. Why is EPA using a direct final rule?

    EPA is publishing this direct final rule without a prior proposed
rule because we view this as a noncontroversial action and anticipate
no adverse comment. This rule makes a minor change in regulatory text,
which is intended to resolve a potential conflict in the current
regulatory text and to ensure that the regulatory text conforms to the
EPA's intention when finalizing the regulatory text at issue. However,
in the ``Proposed Rules'' section of today's Federal Register, we are
publishing a separate document that will serve as the proposed rule to
make this revision to the regulatory text if adverse comments are
received on this direct final rule. We will not institute a second
comment period on this action. Any parties interested in commenting
must do so at this time. In this action, EPA is not making, and is not
seeking comment on, any changes to the regulations at 40 CFR part 82,
subpart F other than the revision discussed in this notice. For further
information about commenting on this rule, see the ADDRESSES section of
this document.
    If EPA receives adverse comment, we will publish a timely
withdrawal in the Federal Register informing the public that this
direct final rule will not take effect. In that case, we would address
all public comments in any subsequent final rule based on the proposed
rule. If no adverse comment is received by October 30, 2017, this
direct final rule will be effective on December 27, 2017 without
further notice and no further action will be taken on the proposed
rule.

II. Does this action apply to me?

    Categories and entities potentially affected by this action include
entities that distribute or sell small cans of refrigerant for use in
motor vehicle air conditioning (MVAC). Regulated entities include, but
are not limited to, manufacturers and distributors of small cans of
refrigerant (NAICS codes 325120, 441310, 447110) such as automotive
parts and accessories stores and industrial gas manufacturers. This
list is not intended to be exhaustive, but rather to provide a guide
for readers

regarding entities likely to be regulated by this action. To determine
whether your facility, company, business, or organization could be
regulated by this action, you should carefully examine the regulations
at 40 CFR part 82, subpart F. If you have questions regarding the
applicability of this action to a particular entity, consult the person
listed in the FOR FURTHER INFORMATION CONTACT section.

III. What should I consider as I prepare my comments for EPA?

    A. Submitting CBI. Do not submit this information to EPA through
www.regulations.gov or email. Clearly mark the part or all of the
information that you claim to be CBI. For CBI information in a disk or
CD ROM that you mail to EPA, mark the outside of the disk or CD ROM as
CBI and then identify electronically within the disk or CD ROM the
specific information that is claimed as CBI). In addition to one
complete version of the comment that includes information claimed as
CBI, a copy of the comment that does not contain the information
claimed as CBI must be submitted for inclusion in the public docket.
Information so marked will not be disclosed except in accordance with
procedures set forth in 40 CFR part 2.
    B. Tips for Preparing Your Comments. When submitting comments,
remember to:
     Identify the rulemaking by docket number and other
identifying information (subject heading, Federal Register date and
page number).
     Follow directions--The agency may ask you to respond to
specific questions or organize comments by referencing a Code of
Federal Regulations (CFR) part or section number.
     Explain why you agree or disagree; suggest alternatives
and substitute language for your requested changes.
     Describe any assumptions and provide any technical
information and/or data that you used.
     If you estimate potential costs or burdens, explain how
you arrived at your estimate in sufficient detail to allow for it to be
reproduced.
     Provide specific examples to illustrate your concerns, and
suggest alternatives.
     Explain your views as clearly as possible, avoiding the
use of profanity or personal threats.
     Make sure to submit your comments by the comment period
deadline identified.

IV. What action is the agency taking?

    Section 608 of the Clean Air Act (CAA) bears the title ``National
Recycling and Emission Reduction Program.'' Under the structure of
section 608, this program has three main components. First, section
608(a) requires EPA to establish standards and requirements regarding
use and disposal of class I and II substances, including a
comprehensive refrigerant management program to limit emissions of
ozone-depleting refrigerants. The CAA directs EPA to include
regulations that reduce the use and emissions of class I and II
substances to the lowest achievable level and that maximize the
recapture and recycling of such substances. The second component,
section 608(b), requires that the regulations issued pursuant to
subsection (a) contain requirements for the safe disposal of class I
and class II substances. The third component, section 608(c), prohibits
the knowing venting, release, or disposal of ozone-depleting
refrigerants and their substitutes during the maintenance, service,
repair, or disposal of air-conditioning and refrigeration appliances or
industrial process refrigeration.
    EPA first issued regulations under section 608 of the CAA on May
14, 1993 (58 FR 28660), to establish the national refrigerant
management program for ozone-depleting refrigerants recovered during
the maintenance, service, repair, and disposal of air-conditioning and
refrigeration appliances. These regulations were intended to
substantially reduce the use and emissions of ozone-depleting
refrigerants. EPA revised these regulations through subsequent
rulemakings published on August 19, 1994 (59 FR 42950), November 9,
1994 (59 FR 55912), August 8, 1995 (60 FR 40420), July 24, 2003 (68 FR
43786), March 12, 2004 (69 FR 11946), January 11, 2005 (70 FR 1972),
May 23, 2014 (79 FR 29682), and April 10, 2015 (80 FR 19453). For a
more detailed summary of the history of EPA's Refrigerant Management
Program see the discussion in the most recent update to these
regulations at 81 FR 82272, 82275 (Nov. 18, 2016).
    On November 9, 2015, EPA proposed the most recent updates to the
refrigerant management regulations under section 608 of the CAA (80 FR
69458). Among other things, EPA proposed to extend the sales
restriction to non-exempt substitute refrigerants with an exception for
small cans of refrigerant for use in MVAC. That is, the proposed
revisions would have restricted the sale of non-exempt substitute
refrigerants to certified technicians, with an exception for small cans
(two pounds or less) of non-exempt substitute refrigerant for the
servicing of MVACs \1\ if the cans had a self-sealing valve. EPA
requested comments on several aspects of this proposal including a
scenario that would have included a sell-through provision for all
small cans manufactured or imported prior to that effective date. 80 FR
69481. The proposal further stated that:
---------------------------------------------------------------------------

    \1\ In this context, containers that meet these criteria are
referred to interchangeably as ``small cans of MVAC refrigerant,''
``small cans of refrigerant for MVAC servicing,'' or simply ``small
cans.''

    For manufacture and import of small cans of refrigerant for MVAC
servicing, EPA is proposing a compliance date of one year from
publication of the final rule. EPA is also proposing to allow small
cans manufactured and placed into initial inventory or imported
before that date to be sold for one additional year. For example, if
the rule is published on July 1, 2016, small can manufacturers would
have until July 1, 2017, to transition their manufacturing lines to
add self-sealing valves. Manufacturers, distributors, and auto parts
stores would be able to sell all small cans manufactured and placed
into initial inventory or imported prior to July 1, 2017, until July
1, 2018. EPA seeks comments on this proposed implementation
---------------------------------------------------------------------------
timeline. [80 FR 69509]

    On November 18, 2016, EPA published a rule finalizing the proposed
restriction that non-exempt substitute refrigerants may only be sold to
technicians certified under sections 608 or 609 of the CAA. (81 FR
82280). In the case of refrigerant for use in MVAC, EPA finalized the
exemption for the sale of certain small cans of non-ozone-depleting
substitutes with a self-sealing valve to allow the do-it-yourself
community to continue servicing their personal vehicles. Id. However,
the agency did not finalize the sell-through provision. The preamble to
the final rule states that, ``EPA is requiring that small cans of non-
exempt substitute refrigerant be outfitted with self-sealing valves by
January 1, 2018. Based on comments, EPA is not finalizing the proposal
to prohibit the sale of small cans that do not contain self-sealing
valves that were manufactured or imported prior to that requirement
taking effect.'' Id. The preamble further stated:

    With regards to small cans of MVAC refrigerant, manufacturers,
distributors and retailers of automotive refrigerant supported the
proposed ``manufacture-by'' date of one year from publication of the
final rule, but commented that they oppose a sell-through date for
small cans that do not have self-sealing valves. They commented that
such a requirement would be inefficient, burdensome, costly, and
environmentally problematic. It would require all retailers to know
of the requirement and establish processes for returning unsold cans
back to

the manufacturer for destruction. More likely, the cans may be
improperly disposed of, which would negate the environmental benefit
of the new provisions. One commenter stated that a ``manufacture-
by'' date would shift EPA's burden in ensuring compliance from a few
manufacturers to thousands of retailers. Furthermore, commenters
cited EPA's July 2015 SNAP rule (80 FR 42901; July 20, 2015) which
listed HFC-134a as unacceptable for use as an aerosol as of a
``manufacture-by'' date, rather than a ``sell-by'' date. [81 FR
82342]

    EPA described its intention to allow the continued sale of small
cans without self-sealing valves that were manufactured or imported
before the January 1, 2018, compliance date as follows:

    In response to the comments received on EPA's proposal to allow
small cans manufactured and placed into initial inventory or
imported before that date to be sold for one additional year, EPA is
not finalizing the sell-through requirement and is finalizing only a
date by which small cans must be manufactured or imported with a
self-sealing valve. EPA agrees that this is the least-burdensome
option and that it avoids the potential for any unintended
consequences of a ``sell-by'' date. [81 FR 82342]

    These intentions were also expressed in the regulatory text at 40
CFR 82.154(c)(2), which was revised in the November 2016 rule to state:
``Self-sealing valve specifications. This provision applies starting
January 1, 2018, for all containers holding two pounds or less of non-
exempt substitute refrigerant for use in an MVAC that are manufactured
or imported on or after that date. (i) Each container holding two
pounds or less of non-exempt substitute refrigerant for use in an MVAC
must be equipped with a single self-sealing valve that automatically
closes and seals when not dispensing refrigerant . . . .'' However,
because of an editing error, another provision, 40 CFR
82.154(c)(1)(ix), contains text that could be construed as
contradicting the Agency's clearly expressed intent to allow non-
technicians to purchase, and retailers to sell, small cans of
refrigerant for use in MVAC that were manufactured or imported before
the January 1, 2018, compliance date irrespective of whether they have
a self-sealing valve. The relevant text in 40 CFR 82.154(c)(1) provides
that beginning January 1, 2018 no person may sell or distribute any
non-exempt substitute for use as a refrigerant unless it ``is intended
for use in an MVAC and is sold in a container designed to hold two
pounds or less of refrigerant, has a unique fitting, and has a self-
sealing valve.
    The Automotive Refrigeration Products Institute and the Auto Care
Association inquired about whether the language in 40 CFR
82.154(c)(1)(ix) effectively negates the provision in 40 CFR
82.154(c)(2) and the preamble discussion showing EPA's intention to
allow small cans of refrigerant for use in MVAC manufactured or
imported before January 1, 2018, to continue to be sold without self-
sealing valves. EPA is publishing this direct final rule to revise the
regulatory text, so that persons in possession of small cans of
refrigerant for use in MVAC without self-sealing valves that were
manufactured or imported before January 1, 2018, can be assured that
they will be able to sell off their existing inventories without
disruption.
    This action will eliminate burden associated with regulatory
uncertainty in this area. The Automotive Refrigeration Products
Institute and the Auto Care Association informed EPA that the lack of
clarity surrounding the status of small cans of refrigerant for use in
MVAC without self-sealing valves that were manufactured or imported
before the compliance date is already creating confusion. Unless
resolved, this lack of clarity could unnecessarily influence sales of
automotive refrigerant during 2017. This is because retailers may not
want to stock large numbers of these small cans of refrigerant for use
in MVAC unless they are given some assurance that they will be able to
sell off any remaining inventory after January 1, 2018. There is also
the concern that if clarity is not provided by January 1, 2018,
retailers may feel compelled to manually pull cans without self-sealing
valves from their shelves and return the cans to their supplier(s).
This rule will eliminate the cost of that stranded inventory and also
eliminate other non-quantified burdens associated with the removal of
such cans from the market, such as the labor involved in segregating
small cans with self-sealing valves from those without self-sealing
valves and physically pulling those from shelves.

V. Statutes and Executive Orders Review

A. Executive Order 12866: Regulatory Planning and Review and Executive
Order 13563: Improving Regulation and Regulatory Review

    This action is not a significant regulatory action and was
therefore not submitted to the Office of Management and Budget (OMB)
for review.

B. Paperwork Reduction Act (PRA)

    This action does not impose any new information collection burden
under the PRA. OMB has previously approved the information collection
activities contained in the existing regulations and has assigned OMB
control number 2060-0256. These changes do not add information
collection requirements beyond those currently required under the
applicable regulations.

C. Regulatory Flexibility Act (RFA)

    I certify that this action will not have a significant economic
impact on a substantial number of small entities under the RFA. In
making this determination, the impact of concern is any significant
adverse economic impact on small entities. An agency may certify that a
rule will not have a significant economic impact on a substantial
number of small entities if the rule relieves regulatory burden, has no
net burden or otherwise has a positive economic effect on the small
entities subject to the rule. This action clarifies that small cans of
refrigerant for use in MVAC may be sold to persons who are not
certified technicians even if they are not equipped with a self-sealing
valve, so long as those small cans are manufactured or imported prior
to January 1, 2018. We have therefore concluded that this action will
have no net regulatory burden for all directly regulated small
entities.

D. Unfunded Mandates Reform Act

    This action does not contain any unfunded mandate as described in
UMRA, 2 U.S.C. 1531-1538, and does not significantly or uniquely affect
small governments. This action corrects a potential conflict in the
refrigerant management regulations as to whether or not small cans of
refrigerant for use in MVAC could be sold to non-technicians if they
were manufactured or imported prior to January 1, 2018, and do not have
a self-sealing valve. This action clarifies that those small cans of
refrigerant for use in MVAC may be sold to persons who are not
certified technicians.

E. Executive Order 13132: Federalism

    This action does not have federalism implications. It 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.

F. Executive Order 13175: Consultation and Coordination With Indian
Tribal Governments

    This action does not have tribal implications as specified in
Executive Order 13175. This action corrects a potential conflict in the
refrigerant management regulations as to whether or not small cans of
refrigerant for use in MVAC could be sold to non-technicians if they
were manufactured or imported prior to January 1, 2018, and do not have
a self-sealing valve. Thus, Executive Order 13175 does not apply to
this action.

G. Executive Order 13045: Protection of Children From Environmental
Health Risks and Safety Risks

    The EPA interprets Executive Order 13045 as applying only to those
regulatory actions that concern environmental health or safety risks
that the EPA has reason to believe may disproportionately affect
children, per the definition of ``covered regulatory action'' in
section 2-202 of the Executive Order. This action is not subject to
Executive Order 13045 because it does not concern an environmental
health risk or safety risk.

H. Executive Order 13211: Actions That Significantly Affect Energy
Supply, Distribution, or Use

    This action is not subject to Executive Order 13211, because it is
not a significant regulatory action under Executive Order 12866.

I. National Technology Transfer and Advancement Act

    This rulemaking does not involve technical standards.

J. Executive Order 12898: Federal Actions To Address Environmental
Justice in Minority Populations and Low-Income Populations

    The EPA believes that this action does not have disproportionately
high and adverse human health or environmental effects on minority
populations, low-income populations and/or indigenous peoples, as
specified in Executive Order 12898 (59 FR 7629, February 16, 1994).
    This action does not affect the level of protection provided to
human health or the environment. This action corrects a potential
conflict in the refrigerant management regulations as to whether or not
small cans of refrigerant for use in MVAC could be sold to non-
technicians if they were manufactured or imported prior to January 1,
2018, and do not have a self-sealing valve. This action clarifies that
those small cans of refrigerant for use in MVAC may be sold to persons
who are not certified technicians. The documentation for this decision
is contained in Docket No. EPA-HQ-OAR-2017-0213, where EPA's assessment
of the underlying regulatory changes that led to this correction found
no disproportionately high and adverse human health or environmental
effects on minority populations, low-income populations and/or
indigenous peoples.

K. Congressional Review Act (CRA)

    This action is subject to the CRA, and EPA will submit a rule
report to each House of the Congress and to the Comptroller General of
the United States. This action is not a ``major rule'' as defined by 5
U.S.C. 804(2).

List of Subjects in 40 CFR Part 82

    Environmental protection, Air pollution control, Chemicals,
Reporting and recordkeeping requirements.

    Dated: September 21, 2017.
E. Scott Pruitt,
Administrator.

    For the reasons set forth in the preamble, the Environmental
Protection Agency amends 40 CFR part 82 as follows:

PART 82--PROTECTION OF STRATOSPHERIC OZONE

0
1. The authority citation for part 82 continues to read as follows:

    Authority:  42 U.S.C. 7414, 7601, 7671-7671q.

0
2. In Sec.  82.154, revise paragraph (c)(1)(ix) to read as follows:

Sec.  82.154  Prohibitions.

* * * * *
    (c) * * *
    (1) * * *
    (ix) The non-exempt substitute refrigerant is intended for use in
an MVAC and is sold in a container designed to hold two pounds or less
of refrigerant, has a unique fitting, and, if manufactured or imported
on or after January 1, 2018, has a self-sealing valve that complies
with the requirements of paragraph (c)(2) of this section.
* * * * *
[FR Doc. 2017-20840 Filed 9-27-17; 8:45 am]
 BILLING CODE 6560-50-P


[Federal Register Volume 77, Number 6 (Tuesday, January 10, 2012)]
[Notices]
[Page 1536]
[FR Doc No: 2012-184]

-----------------------------------------------------------------------

SECURITIES AND EXCHANGE COMMISSION

[Release No. 34-66097; File No. SR-Phlx-2011-149]

 Self-Regulatory Organizations; NASDAQ OMX PHLX LLC; Order
Approving Proposed Rule Change To Delete Exchange Rule 795 ``Member
Officer or Director''

January 4, 2012.

I. Introduction

    On November 3, 2011, NASDAQ OMX PHLX LLC (``Exchange'') filed with
the Securities and Exchange Commission (``Commission''), pursuant to
Section 19(b)(1) of the Securities Exchange Act of 1934 (``Act'') \1\
and Rule 19b-4 thereunder,\2\ a proposed rule change to delete Exchange
Rule 795 ``Member Officer or Director.'' The proposed rule change was
published in the Federal Register on November 21, 2011.\3\ The
Commission received no comments on the proposal. This order approves
the proposed rule change.
---------------------------------------------------------------------------

    \1\ 15 U.S.C. 78s(b)(1).
    \2\ 17 CFR 240.19b-4.
    \3\ See Securities Exchange Act Release No. 65745 (November 14,
2011), 76 FR 72018.
---------------------------------------------------------------------------

II. Description of Proposal

    The Exchange proposes to delete current Exchange Rule 795 ``Member
Officer or Director.'' Exchange Rule 795 provides that a member of the
Exchange shall not be an officer or director of, or own or control,
directly or indirectly, a substantial interest in a corporation engaged
in the securities business which is not a member organization of the
Exchange, except with the written permission of the Exchange.

III. Commission Findings and Discussion

    After careful review, the Commission finds that the proposed rule
change is consistent with the requirements of Section 6 of the Act,\4\
and the rules and regulations thereunder applicable to a national
securities exchange. In particular, the Commission finds that the
proposed rule change is consistent with Section 6(b)(5) of the Act,\5\
which requires, among other things, that the rules of the exchange be
designed to prevent fraudulent and manipulative acts and practices, to
promote just and equitable principles of trade, to remove impediments
to and perfect the mechanism of a free and open market and a national
market system, and, in general, to protect investors and the public
interest.\6\
---------------------------------------------------------------------------

    \4\ 15 U.S.C. 78f.
    \5\ 15 U.S.C. 78f(b)(5).
    \6\ In approving this proposed rule change, the Commission has
considered the proposed rule's impact on efficiency, competition,
and capital formation. 15 U.S.C. 78c(f).
---------------------------------------------------------------------------

    The Exchange represented that Exchange Rule 795 was adopted prior
to the Exchange's demutualization in 2004 and that, prior to
demutualization there may have been an interest in the Exchange being
notified of, and approving, a member's role in another entity. The
Exchange further represented that it has not utilized Exchange Rule 795
in over 10 years and does not believe that the Exchange should be in a
position to control an Exchange member's role in another entity.
    The Commission believes that the proposal should clarify the
Exchange's rulebook by removing an outdated and unused rule. Further,
the Commission believes that deletion of Exchange Rule 795 could allow
Exchange members to conduct transactions with regard to other
corporations engaged in the securities business which are not Exchange
member organizations more expeditiously. Accordingly, the Commission
finds that the proposal would promote just and equitable principles of
trade and remove impediments to and perfect the mechanism of a free and
open market, and is consistent with the requirements of the Act.

IV. Conclusion

    It is therefore ordered, pursuant to Section 19(b)(2) of the
Act,\7\ that the proposed rule change (SR-Phlx-2011-149) be, and it
hereby is, approved.
---------------------------------------------------------------------------

    \7\ 15 U.S.C. 78s(b)(2).

    For the Commission, by the Division of Trading and Markets,
pursuant to delegated authority.\8\
---------------------------------------------------------------------------

    \8\ 17 CFR 200.30-3(a)(12).
---------------------------------------------------------------------------

Kevin M. O'Neill,
Deputy Secretary.
[FR Doc. 2012-184 Filed 1-9-12; 8:45 am]
BILLING CODE 8011-01-P


.001159261 0.75367708 0 0 0 0 0 0 0 573.5926 0.0154 2753.042 0.0739 3205.7679 0.0861 719.6146437 0.011485158 690.1464563 0.011014842 0 0 2.208885884 0 0 0 0 0 0 0 0.492496275 0 0.492496275 0 229.8281095 0.002944143 216.9705929 0.002779435 466.3681638 0.005974267 617.6933466 0.007912771 693.9304872 0.008889384 1150.0955 0.0147 0 0 0 0 0 0 515.3782424 0.006620043 574.5384576 0.007379957 Page 1771 Raw EPA219b_ BART_ 13 Pech 2010 2717.7209 0.0203 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1.885732345 0 0 0 39.8326 0.0011 219.0909878 0.001682342 197.6443122 0.001517658 176.1017 0.0038 0.675656904 0 0.675656904 0 81.22355292 0.003157568 111.7023471 0.004342432 0.273507599 0 0 0 0 0 Page 1772 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 210.2309517 0.005788742 176.9871234 0.004873368 212.0158249 0.005837889 415.9416595 0.01116204 605.0904405 0.01623796 2321.1536 0.0296 0.026683925 0 0 0 0.066506015 0 0.125084568 0 0.219996221 0 0.44704086 0 0.44704086 0 127.3395 0.0027 89.83453333 0.0024 89.83453333 0.0024 89.83453333 0.0024 933.5623315 0.019389935 941.4532459 0.019553828 2039.315123 0.042356237 2897.1118 0.0434 1225.4213 0.0156 1726.5064 0.0221 2661.915485 0.022341516 0 0 17.34233869 0 28.33180328 0 0 0 0 0 0 0 0 0 2.104998127 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.75112951 0 0.75112951 0 Page 1773 Raw EPA219b_ BART_ 13 Pech 2010 2.62082716 0 2.62082716 0 2.571606586 0 2.571606586 0 406.2865 0.0058 0 0 0 0 0 0 0 0 0 0 3013.983 0.0784 0 0 0 0 0 0 0 0 0 0 0 0 164.747 0.0027 208.1017 0.0034 0 0 0 0 390.1898 0.0009 938.9671 0.002 222.2084 0.0037 453.6616373 0.000847278 1006.960821 0.00184337 1134.316082 0.00207651 1245.4798 0.0016 2884.322297 0.00528012 0 0 0 0 1356.991904 0.017329831 1350.677964 0.017249197 1354.087492 0.017292739 1349.03634 0.017228232 3775.736 0.0147 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2803.5458 0.021 2711.0032 0.0203 0 0 1524.0729 0.0018 0 0 0 0 0 0 Page 1774 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 403.0329627 0.000752722 618.9402 0.0011 1037.3363 0.0019 0 0 0 0 0 0 330.4940582 0 178.0763152 0 393.5292 0 644.4293703 0 410.7591 0 325.7341435 0 337.8346565 0 0.951507324 0 5778.382426 0.10658006 5928.462755 0.109348235 5805.037619 0.107071705 0 0 0 0 0 0 0 0 0 0 0 0 0 0 918.6196676 0.01174249 881.2133803 0.011264335 919.958419 0.011759603 922.005921 0.011785776 896.8846459 0.011464657 867.0383661 0.011083139 3908.5135 0.0153 3674.5109 0.0144 17.3863 0 10.80673488 0 10.80673488 0 12.58353486 0 141.9705502 0 32.98172946 0 32.98172946 0 32.98172946 0 32.98172946 0 32.98172946 0 32.98172946 0 32.98172946 0 Page 1775 Raw EPA219b_ BART_ 13 Pech 2010 32.98172946 0 0 0 0 0 438.4710656 0.003903908 1.040255683 0 1.040255683 0 0.73099048 0 0.273058966 0 0.273058966 0 0.273058966 0 3.703376975 0 6.49818814 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 5.417695329 0 0.81239266 0 157.943872 0 157.943872 0 177.686856 0 3.324656248 0 23.1942 0 23.1942 0 23.1942 0 23.1942 0 0 0 0 0 4.116817809 0 8.216107149 0 8.216107149 0 8.216107149 0 8.216107149 0 0.140348926 0 0.140348926 0 6.166405479 0 0.978794521 0 0.216275862 0 0.216275862 0 0.17302069 0 0.216275862 0 0.216275862 0 0.216275862 0 0 0 0 0 0 0 0 0 0 0 Page 1776 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 4.287163147 0 0 0 0 0 0 0 0 0 411.0334 0.0018 135.9251031 0 135.9251031 0 135.9251031 0 135.9251031 0 57.58715893 0 57.58715893 0 162.25995 0.004 162.25995 0.004 0.215877958 0 2.445474645 0 0.606725355 0 2.900726414 0 43.49245 0 43.49245 0 20.60354357 0 0.154519642 0 4.602386324 0 0 0 0 0 0 0 3.797557332 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.083939171 0 0.083939171 0 0.083939171 0 8.577684211 0.000757895 16.08315789 0.001421053 16.08315789 0.001421053 0.182592343 0 0.182592343 0 Page 1777 Raw EPA219b_ BART_ 13 Pech 2010 0.182592343 0 0.182592343 0 0.182592343 0 0.182592343 0 0.182592343 0 0.182592343 0 0.182592343 0 1.29505 0 1.29505 0 21.06571921 0 21.06571921 0 14.74600345 0 19.04991634 0.00168823 18.98641662 0.001682603 16.19242889 0.001434996 22.50213815 0.001994171 128.07 0.0115 107.1602 0.0097 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1.407704348 0 1.407704348 0 1.407704348 0 1.407704348 0 1.407704348 0 1.87693913 0 1.87693913 0 70.7488 0.0099 0 0 0.147272127 0 0.147272127 0 0.301238441 0 0.417717305 0 0 0 0 0 0 0 0 0 0 0 0 0 155.385456 0 74.6815 0 0 0 0 0 0 0 3.891036585 0 2.1727 0 Page 1778 Raw EPA219b_ BART_ 13 Pech 2010 0.099073786 0 0.099073786 0 2.79785057 0 2.79785057 0 2.723114901 0 2.723114901 0 2.67003894 0 2.67003894 0 14.18059386 0 14.18059386 0 14.18059386 0 20.06194615 0 25.74046167 0 19.86758133 0 0 0 0 0 0 0 8.998850261 0 0 0 0 0 16.628 0 13.83855319 0 18.68204681 0 72.56237002 0 47.61332998 0 29.66875359 0 29.66875359 0 14.8343768 0 0 0 0 0 0 0 1.250596354 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1.29275 0 1.29275 0 0 0 0 0 0 0 0 0 0.265465019 0 0.265465019 0 Page 1779 Raw EPA219b_ BART_ 13 Pech 2010 1.727106634 0 0.839887015 0 0.839887015 0 0.839887015 0 0.839887015 0 0 0 0 0 0 0 0 0 0 0 0 0 0.711123821 0 0.711123821 0 0.705293395 0 0.705293395 0 0.273426045 0 0.273426045 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 7.478767008 0 40.00272752 0 88.92010565 0 88.92010565 0 104.9094087 0 0 0 0 0 2.262443451 0 2.262443451 0 0 0 0 0 2.262443451 0 0 0 0 0 651.9031 0.0164 0.168455425 0 0.168455425 0 0 0 0 0 0 0 0.269554189 0 0.269554189 0 1.694091621 0 0.813825792 0 0.813825792 0 0.813825792 0 0 0 Page 1780 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 132.097838 0 1.03845549 0 0 0 76.75794978 0 20.70243237 0 76.85071866 0 20.72745311 0 66.46019645 0 20.70578032 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 915.10286 0.008268727 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 4.869750553 0 1.06844575 0 15.37700995 0 1.684625685 0 15.52012147 0 15.52012147 0 1.878517949 0 1.76995923 0 0 0 0 0 Page 1781 Raw EPA219b_ BART_ 13 Pech 2010 0 0 15.57733603 0 15.57733603 0 15.57733603 0 15.57733603 0 15.57733603 0 24.20802221 0 16.62985874 0 0 0 0.104288866 0 0.104288866 0 0.083431093 0 448.1891 0.0011 0.221143014 0 0.221143014 0 0.019959027 0 2.585264153 0 0.628591531 0 58.50579905 0 19.26270888 0 67.80926585 0 21.43620723 0 14.01295786 0 1.644299671 0 115.4453905 0 1.224395067 0 1.339928985 0 4.033894025 0 4.211712637 0 66.33295513 0 22.35678897 0 375.8668505 0.003346514 902.0574 0.0081 457.8973 0.0076 0 0 106.2954492 0 106.2954492 0 106.2954492 0 51.77381326 0 46.38557853 0 554.1603 0.0092 77.35584044 0 31.44436808 0 863.0701 0.0078 2395.7615 0.0563 126.2845235 0 126.2845235 0 71.88384209 0 2.7993 0 1.4271 0 1.4271 0 Page 1782 Raw EPA219b_ BART_ 13 Pech 2010 1.4271 0 0 0 0 0 0 0 5611.5466 0.1114 207.059702 0 207.059702 0 9.710097377 0 0 0 0 0 0 0 0 0 0 0 497.0779 0.00135 497.0779 0.00135 0.561056133 0 0.561056133 0 105.4013786 0 105.4013786 0 116.3292807 0 105.4013786 0 105.4013786 0 116.3292807 0 0 0 131.6978461 0 93.6518017 0 0 0 0.089571578 0 0.089571578 0 0.089571578 0 0.089571578 0 77.8753 0 22.44655643 0 0.065126042 0 0.096138442 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1783 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2.474660735 0 2.474660735 0 0.057402234 0 0.057402234 0 0.057402234 0 0.057402234 0 0.057402234 0 0.019134078 0 0 0 0 0 0 0 0 0 2.318439265 0 2.318439265 0 0 0 0 0 0 0 7.854420581 0 7.854420581 0 7.854420581 0 134.3208441 0 129.5258983 0 129.9208577 0 4.619032748 0 0 0 0 0 0 0 Page 1784 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1785 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.741696208 0 0.741696208 0 0.221279956 0 0.221279956 0 0.167010359 0 0.221636681 0 0.221636681 0 0.221636681 0 0.167928038 0 0 0 0 0 0 0 0 0 1468.769836 0.00178929 2060.959764 0.00251071 895.6011 0.0011 0 0 0 0 0 0 130.7542615 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 228.3395528 0 180.6790612 0 1360.851 0.0034 0 0 0 0 Page 1786 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0.566133814 0 0.83218408 0 54.05682745 0 34.87537255 0 0 0 0 0 115.7289463 0 0 0 490.970925 0.0025 490.970925 0.0025 490.970925 0.0025 490.970925 0.0025 26.01730058 0 26.01730058 0 14.92419885 0 104.5358846 0 1.053389108 0 0 0 353.747684 0.003149577 5.889 0 2.12659828 0 2.031288553 0 1.947892542 0 89.6373 0.0018 0.109393668 0 0.109393668 0 0 0 0 0 0 0 0 0 43.6998535 0 43.6998535 0 31.16355219 0 1635.918 0.0384 0.1596 0 0.155166667 0 0.150733333 0 0 0 0 0 0 0 206.57197 0 206.57197 0 9.641282417 0 0.221621514 0 0.221621514 0 0.221621514 0 0.221621514 0 0.221621514 0 0.22069437 0 Page 1787 Raw EPA219b_ BART_ 13 Pech 2010 0.22069437 0 0.22069437 0 0.22069437 0 0.817847165 0 22.43313076 0 22.43313076 0 22.43313076 0 28.51278163 0 21.41706924 0 21.41706924 0 21.41706924 0 31.108593 0 0 0 135.9242015 0 135.9242015 0 72.15309697 0 4.199820806 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1.660662321 0 6.910829765 0 0 0 0 0 0 0 28.4398 0.0009 67.13623593 0 24.92765549 0 0 0 34.4592 0 36.29638147 0 35.81807855 0 19.3985 0 0.442155467 0 0.442155467 0 45.69458946 0 45.69458946 0 24.81366026 0 0 0 0 0 103.914362 0 49.69817311 0 0 0 5.586381851 0 0 0 0 0 Page 1788 Raw EPA219b_ BART_ 13 Pech 2010 0 0 2.549593467 0 0.1121 0 0.1121 0 0.1121 0 46.6066 0 321.2721546 0 137.9169454 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.017765029 0 0.017765029 0 0.017765029 0 0.017987419 0 0 0 0 0 0 0 0 0 452.5771058 0 452.5771058 0 452.5771058 0 452.5771058 0 Page 1789 Raw EPA219b_ BART_ 13 Pech 2010 491.6100088 0 491.6100088 0 0 0 0 0 0 0 0 0 0.158860308 0 0.641419846 0 0.641419846 0 0.5657 0 1.964535847 0 0.447708469 0 0.067293198 0 0.067293198 0 0.067293198 0 0.062116798 0 0.046587599 0 17.6402 0 17.6402 0 8.0183 0 264.0446031 0 264.0446031 0 264.0446031 0 0 0 3.623 0 0 0 2.9715 0 117.4939844 0 185.1004975 0 98.17515682 0 0 0 0 0 0 0 0 0 0 0 1.420511817 0 1.420511817 0 0.305185489 0 0.305185489 0 0.305185489 0 0.285483846 0 0.285483846 0 0.285483846 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1790 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 459.8776 0.0011 748.2013 0.0457 0 0 0 0 130.2734709 0 130.2734709 0 138.3005911 0 0 0 0 0 137.384564 0 58.79855808 0 0 0 0 0 0.214134272 0 0.214134272 0 0.214134272 0 0 0 0 0 0.085218219 0 0.085218219 0 0.085218219 0 0.085218219 0 0.319568322 0 0.319568322 0 4.029770843 0 4.029770843 0 4.029770843 0 8.2455 0 4.624169207 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 39.8621 0 16.6865 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.007074684 0 0.006632516 0 0.007074684 0 Page 1791 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0.088793454 0 0.088793454 0 0.088793454 0 0.088793454 0 96.4513593 0 23.91490652 0 423.7345 0.0042 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 342.5707149 0 660.1555899 0 342.5707149 0 660.1555899 0 0 0 0 0 0 0 0 0 0.832001583 0 143.9071498 0 0.184626841 0 0.184626841 0 0.184626841 0 0.278730665 0 0.278730665 0 0.278730665 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1792 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 5.002558253 0 344.0494926 0 131.2212595 0 12.52378013 0 5.9969 0 0 0 0 0 375.4793988 0 219.9778296 0 50.3695141 0 50.3695141 0 46.6201718 0 0 0 0 0 0 0 0 0 0.162885689 0 0.162885689 0 0.162885689 0 178.6557356 0 178.6557356 0 97.41516445 0 97.41516445 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 83.64394304 0 83.64394304 0 29.99785696 0 29.99785696 0 5.389915334 0 8.933784666 0 0 0 0 0 Page 1793 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 12.9983 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.088823263 0 0.088823263 0 0.088823263 0 0.088823263 0 0.088823263 0 0.088823263 0 0 0 0.14935 0 0 0 0 0 0.14935 0 0 0 0 0 0 0 0 0 0 0 0 0 0.242055563 0 0.086334916 0 40.42515124 0 22.28846176 0 Page 1794 Raw EPA219b_ BART_ 13 Pech 2010 187.5187212 0 112.3208584 0 0.208973094 0 0.208973094 0 0 0 0 0 0 0 23.19668241 0 23.19668241 0 23.19668241 0 22.39665277 0 361.9577 0 36.2293287 0 0 0 0 0 0 0 14.11121999 0 78.95006855 0 78.95006855 0 75.7013629 0 0 0 305.161 0 426.8481815 0 449.9389262 0 24.90043321 0 13.41856679 0 36.626 0 0 0 0 0 11.1361 0 0 0 19.55401107 0 9.090267562 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 25.4397591 0 25.4397591 0 25.4397591 0 Page 1795 Raw EPA219b_ BART_ 13 Pech 2010 37.9381468 0 37.9381468 0 37.9381468 0 80.78443781 0 14.17371122 0 14.17371122 0 14.17371122 0 8.136135469 0 8.136135469 0 8.136135469 0 17.85925 0 17.85925 0 355.1508676 0 355.1508676 0 359.3553647 0 576.1409229 0 576.1409229 0 634.8803542 0 0 0 0 0 0 0 0 0 0 0 10.48123153 0 3.703368473 0 774.2583301 0 779.6401333 0 393.6363284 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 26.96291944 0 218.2210091 0 218.2210091 0 119.9016534 0 0 0 0 0 0 0 Page 1796 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 713.2278837 0 713.2278837 0 713.2278837 0 713.2278837 0 0.253520419 0 0.253520419 0 0.130078554 0 0.130078554 0 0.130078554 0 0.130078554 0 0.215189318 0 0.215189318 0 544.3820239 0 544.3820239 0 544.3820239 0 544.3820239 0 640.5128507 0 640.5128507 0 332.7839169 0 332.7839169 0 371.3381511 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 114.801419 0 59.849081 0 0 0 0 0 0 0 0 0 0 0 518.4620338 0 518.4620338 0 587.5903049 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1797 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 546.9162266 0 125.0295766 0 562.5424045 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 9.596124444 0 9.596124444 0 7.796851111 0 284.6559262 0 284.6559262 0 520.1277269 0 0 0 0 0 26.82298942 0 26.82298942 0 26.82298942 0 19.29625015 0 19.29625015 0 0 0 227.0034001 0 227.0034001 0 227.0034001 0 578.4925356 0 36.61415803 0 36.61415803 0 0 0 0 0 27.08103388 0 27.08103388 0 27.08103388 0 0 0 0 0 Page 1798 Raw EPA219b_ BART_ 13 Pech 2010 0 0 9.165064266 0 9.165064266 0 9.165064266 0 9.165064266 0 471.4567705 0 471.4567705 0 0 0 449.6140114 0 449.6140114 0 449.6140114 0 449.6140114 0 491.7501024 0 491.7501024 0 568.2231964 0 568.2231964 0 598.3056009 0 0.105728718 0 0.105728718 0 0.10540955 0 0.10540955 0 0 0 0 0 0 0 0 0 0.203764011 0 0.203764011 0 0.09297774 0 0.09297774 0 0.334688776 0 0.334688776 0 0.654929272 0 0.654929272 0 0.466661538 0 0.466661538 0 0.466661538 0 45.37029219 0 48.29740781 0 21.55567259 0 21.55567259 0 21.55567259 0 17.29992397 0 17.29992397 0 244.5586 0 244.5586 0 494.8660383 0 276.3537617 0 235.4303068 0 235.4303068 0 176.8464863 0 601.6090712 0 Page 1799 Raw EPA219b_ BART_ 13 Pech 2010 601.6090712 0 601.6090712 0 50.20085495 0 50.20085495 0 584.1068952 0 381.6165048 0 47.6851 0 15.44571126 0 15.44571126 0 5.274505532 0 5.274505532 0 77.0202 0 73.67438721 0 75.31159582 0 73.67438721 0 87.1434941 0 87.1434941 0 9.086354391 0 9.086354391 0 9.007003525 0 9.007003525 0 9.007003525 0 9.007003525 0 7.342454629 0 7.342454629 0 7.342454629 0 7.342454629 0 7.342454629 0 0 0 0 0 1.933921914 0 1.933921914 0 1.933921914 0 1.933921914 0 5.223864371 0 5.223864371 0 0 0 0 0 0 0 0 0 285.8975196 0 285.8975196 0 285.8975196 0 285.8975196 0 427.2882548 0 427.2882548 0 0 0 104.7633999 0 104.7633999 0 150.4783381 0 110.4013233 0 Page 1800 Raw EPA219b_ BART_ 13 Pech 2010 110.4013233 0 110.4013233 0 112.8908858 0 112.8908858 0 126.7142596 0 3.982521228 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 8.71932683 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2.439821519 0 2.439821519 0 2.439821519 0 2.439821519 0 5.386437386 0 5.386437386 0 5.386437386 0 5.386437386 0 5.386437386 0 7.574813225 0 7.574813225 0 7.574813225 0 7.574813225 0 7.574813225 0 7.574813225 0 7.574813225 0 7.574813225 0 3.054515596 0 3.054515596 0 3.054515596 0 3.054515596 0 3.054515596 0 3.054515596 0 3.054515596 0 3.054515596 0 2.757805784 0 2.757805784 0 2.757805784 0 2.757805784 0 2.757805784 0 Page 1801 Raw EPA219b_ BART_ 13 Pech 2010 2.757805784 0 1.960093367 0 1.960093367 0 7.785993744 0 7.785993744 0 154.9584678 0 74.97990375 0 10.92135467 0 12.26758228 0 12.26758228 0 17.18406899 0 17.18406899 0 0 0 0 0 0 0 0 0 1.725408942 0 1.725408942 0 1.725408942 0 1.725408942 0 1.725408942 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 29.63889819 0 29.63889819 0 29.63889819 0 29.63889819 0 0 0 0 0 0 0 0 0 0 0 0 0 1.955750669 0 6.953780157 0 6.953780157 0 6.953780157 0 1.955750669 0 1.955750669 0 1.955750669 0 1.955750669 0 1.955750669 0 0 0 0 0 Page 1802 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1.89635 0 1.89635 0 28.6123 0 587.1405249 0 254.0267898 0 130.4461894 0 0 0 0 0 0 0 0 0 8.681934062 0 8.681934062 0 8.681934062 0 8.681934062 0 111.9109255 0 239.4095709 0 185.8354012 0 185.8354012 0 185.8354012 0 0 0 0 0 0 0 36.44821212 0 36.44821212 0 47.38267576 0 0 0 0 0 0 0 0 0 0 0 0 0 140.0663742 0 140.0663742 0 140.0663742 0 11.76357841 0 11.76357841 0 11.76357841 0 11.76357841 0 6.829880135 0 6.829880135 0 0 0 0 0 Page 1803 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 27.90036102 0 27.36035403 0 27.90036102 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 140.7866213 0 140.7866213 0 135.572302 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 259.1677371 0 115.1856609 0 0 0 0 0 0 0 0 0 1629.7684 0.0073 0 0 0.204778481 0 0 0 0 0 4.166381602 0 4.166381602 0 4.166381602 0 26.97076667 0 26.97076667 0 26.97076667 0 7.473414047 0 7.473414047 0 7.473414047 0 7.473414047 0 7.473414047 0 4.356482663 0 4.356482663 0 3.735360455 0 3.735360455 0 Page 1804 Raw EPA219b_ BART_ 13 Pech 2010 3.735360455 0 3.735360455 0 3.735360455 0 503.591354 0 503.591354 0 544.238592 0 0 0 10.08633013 0 10.08633013 0 0 0 67.44124469 0 67.44124469 0 67.44124469 0 67.44124469 0 3.988321918 0 3.988321918 0 43.35508587 0 43.35508587 0 3.518275379 0 3.518275379 0 0 0 4.989077155 0 4.989077155 0 0 0 0 0 3.74193777 0 0 0 0 0 1.094979296 0 1.094979296 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1.054164366 0 Page 1805 Raw EPA219b_ BART_ 13 Pech 2010 1.054164366 0 1.054164366 0 1.054164366 0 1.054164366 0 1.054164366 0 1.054164366 0 1.054164366 0 0.188616647 0 0.188616647 0 0 0 0 0 222.4409 0.0033 2119.176914 0.006241815 2090.783186 0.006158185 2.049159127 0 0 0 0 0 0 0 1.834940049 0 0 0 0 0 0 0 0 0 3230.950193 0.012656973 3872.4115 0.0152 2.049159127 0 0 0 2891.7789 0.0247 5.997057457 0 0.239526721 0 0.239526721 0 0 0 0 0 835.3065 0.0217 0 0 0 0 0 0 610.73 0.0097 1198.4974 0.019 0 0 0 0 655.8357105 0.010543115 694.0153895 0.011156885 1191.8064 0.0192 2950.072 0.0475 0 0 0 0 0 0 0 0 0 0 0 0 Page 1806 Raw EPA219b_ BART_ 13 Pech 2010 662.7152 0.0172 0 0 0 0 5597.357955 0.071544078 5594.725775 0.071510434 5475.327684 0.069984317 5387.456685 0.068861171 4626.57724 0.023745106 4550.54706 0.023354894 6959.579212 0.186936013 7096.93677 0.19062547 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2819.1286 0.0094 4620.437378 0.052282208 4377.5238 0.056 4802.6321 0.0188 9518.3574 0.0477 5200.7073 0.0276 5027.4903 0.025 3352.247943 0.047978949 3103.660657 0.044421051 3193.4382 0.0039 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2691.076815 0.0685257 2685.131185 0.0683743 0 0 4590.0241 0.0279 0 0 5088.196982 0.105563968 5183.250718 0.107536032 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1807 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 18.37905 0 18.37905 0 2229.8213 0.0505 4000.4855 0.0156 0 0 0 0 0 0 0 0 466.833765 0 466.833765 0 1006.896356 0 466.833765 0 466.833765 0 995.4543518 0 91.20143209 0 56.86344292 0 36.99549299 0 5.186468796 0 5.255391969 0 5.233853478 0 36.59134054 0 56.81565852 0 56.76787411 0 56.76787411 0 37.15093623 0 7133.129688 0.060819183 7141.135445 0.060887442 9.990584074 0 4827.392943 0.051307393 4675.461557 0.049692607 4550.6589 0.0484 0 0 0 0 0 0 0 0 0 0 1702.764839 0.024401095 1702.611961 0.024398905 0 0 0 0 0 0 1914.5878 0.0515 5230.4654 0.1405 6146.909202 0.145882622 6395.331366 0.151778345 6199.849332 0.147139033 Page 1808 Raw EPA219b_ BART_ 13 Pech 2010 522.3249536 0 522.3249536 0 225.857179 0 225.857179 0 3576.0046 0.014 3966.460225 0.05070917 3938.400274 0.050350437 106.1557703 0 106.0904616 0 119.6601718 0 106.1557703 0 106.1557703 0 119.6964544 0 6.688415396 0 6.704042535 0 6.563398286 0 6.642038081 0 2860.93457 0.041427464 2849.436478 0.041260967 5884.616252 0.08521157 5841.0618 0.0886 5554.803 0.0415 5909.247 0.1538 8.836421372 0 8.836421372 0 213.3183186 0 213.3183186 0 213.3183186 0 328.1820286 0 4863.8001 0.0436 4066.7854 0.0844 4234.9482 0.0879 3137.237985 0.041790639 2988.502715 0.039809361 0 0 0 0 0 0 0 0 0 0 0 0 2.583945914 0 454.9935 0.0068 0 0 0 0 5776.5525 0.0989 5333.6502 0.0913 6858.2359 0.11 0 0 0 0 5462.575439 0.029513568 5457.553061 0.029486432 Page 1809 Raw EPA219b_ BART_ 13 Pech 2010 5428.749527 0.031176154 4209.709516 0.113084155 4091.059063 0.109896884 4781.575223 0.128395705 16.9573 0 3677.876 0.0763 0 0 0 0 0 0 3205.7696 0.0431 3843.3473 0.0491 117.2424606 0 117.2424606 0 108.8837111 0 133.0800914 0 143.7484954 0 148.4777879 0 5042.9904 0.019733333 5042.9904 0.019733333 5042.9904 0.019733333 4981.1065 0.0195 4954.7151 0.0147 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1096.7342 0.0177 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.652954786 0 0.652954786 0 0.664826679 0 0.664826679 0 0.664826679 0 3.480430639 0 Page 1810 Raw EPA219b_ BART_ 13 Pech 2010 3.480430639 0 3.480430639 0 3.480430639 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.480430639 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.480430639 0 454.6026513 0 454.6026513 0 454.6026513 0 454.6026513 0 3.480430639 0 3.480430639 0 3.480430639 0 3.480430639 0 3.480430639 0 3.480430639 0 1056.644 0 1056.644 0 3398.768458 0.079061466 2001.949862 0.007801834 2001.008438 0.007798166 0 0 3817.1419 0.0994 4487.7834 0.1168 4411.078023 0.112533998 4412.332477 0.112566002 0 0 0 0 6437.418349 0.161935129 6796.489521 0.170967668 7029.85571 0.176838063 4073.004507 0.109377231 4190.138493 0.112522769 6738.749433 0.1695152 4598.2625 0.1235 4747.9419 0.1276 0 0 3410.9571 0.0287 3294.125772 0.027692841 3236.6099 0.008 Page 1811 Raw EPA219b_ BART_ 13 Pech 2010 9753.454003 0.124660371 9712.711097 0.124139629 0 0 0 0 0 0 0 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 3.629591952 0 5133.4897 0.1218 5074.2322 0.0955 0.558801075 0 2922.874927 0.041884978 2921.500433 0.041865281 4860.71 0.0727 4811.934166 0.129230386 4809.671334 0.129169614 3577.4418 0.0849 3234.192776 0.034381383 3181.254424 0.033818617 3714.75427 0.093445723 0 0 0 0 0 0 4309.3639 0.0617 0 0 2763.0307 0.0743 2924.841572 0.021869676 2859.268557 0.021379373 4259.394979 0.031848422 3878.786392 0.029002529 1370.6992 0.0238 0 0 0 0 0 0 0 0 0 0 0 0 4567.1939 0.0829 4638.6248 0.0841 4555.4331 0.0791 0 0 Page 1812 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 4024.859495 0.015733262 3956.677605 0.015466738 0 0 0 0 0 0 0 0 0 0 0 0 111.5132698 0.004369179 0 0 0 0 0 0 0 0 0 0 215.6981 0.0084 0 0 19.20387206 0 0 0 76.05859672 0 136.6831472 0 136.6831472 0 136.6831472 0 136.6831472 0 93.31781131 0 93.31781131 0 93.31781131 0 93.31781131 0 4201.1125 0.0314 2143.4095 0.0087 2143.4095 0.0087 2161.1843 0.0054 2175.4235 0.0054 2980.130728 0.016049999 2980.130972 0.016050001 3.69035 0 3.69035 0 3.69035 0 3.69035 0 0 0 4549.002388 0.071747113 6746.920254 0.181233754 Page 1813 Raw EPA219b_ BART_ 13 Pech 2010 6698.144298 0.179923548 7124.710171 0.191381833 6837.276076 0.183660865 0 0 0 0 0 0 0 0 0 0 0 0 0 0 10405.7012 0.0529 4.915323117 0 5.027801907 0 4.825340085 0 4.877830187 0 2779.114263 0.035514788 3128.935337 0.039985212 5025.4021 0.0197 4987.155 0.0637 0 0 0 0 6.227416122 0 6.325934778 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 4.737351358 0 4.638274297 0 4.660291421 0 4.90559091 0 0 0 0 0 8.706057211 0 0.8048 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 3.37063E 06 0 0 0 0 0 0 0 5.384622919 0 5.544007758 0 Page 1814 Raw EPA219b_ BART_ 13 Pech 2010 5.410469109 0 0.272476607 0 0.335355842 0 0.503033775 0 0.503033775 0 0.191151632 0 0.482909405 0 0 0 0 0 0 0 623.6818 0.0079 648.9231458 0.008266592 2550.0518 0.0326 3818.4531 0.0488 464.4581271 0.005916704 464.4581271 0.005916704 1255.910274 0.016060573 1457.572426 0.018639427 3.501806882 0 3217.9903 0.0129 3103.7516 0.0124 3228.6078 0.0126 3259.9429 0.0128 0 0 43.53994158 0 43.53994158 0 0 0 0 0 3783.869784 0.171977251 3767.269116 0.171222749 0 0 5906.213616 0.014564505 5894.449484 0.014535495 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1815 Raw EPA219b_ BART_ 13 Pech 2010 0.290519324 0 0.290519324 0 0.290519324 0 0.290519324 0 0.290519324 0 0.290519324 0 0.22674171 0 0.22674171 0 0.187285306 0 0.187285306 0 0.187285306 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.487627857 0 0.935830261 0 0.935830261 0 0.913474316 0 1.052918267 0 0.135768909 0 0.291718606 0 0.615622795 0 0.175574862 0 0.211348254 0 0.050878321 0 0 0 0.357703537 0 0.308294383 0 0.357703537 0 0 0 0 0 3.237376918 0 0 0 0.798422403 0 0.798422403 0 0 0 0.599828774 0 0.599828774 0 0.333411829 0 Page 1816 Raw EPA219b_ BART_ 13 Pech 2010 0.333411829 0 0.142057687 0 0.10455795 0 0.394032147 0 0.394032147 0 0 0 1.995852293 0 0.818440372 0 0.863909282 0 1.354047707 0 1.422078139 0 0.525551896 0 0 0 0 0 0 0 1818.1008 0.0271 6.958791077 0 6.958791077 0 7.45264411 0 1750.367763 0.023293417 1689.748966 0.022486718 0 0 0 0 194.2670401 0 4.82491229 0 4.82491229 0 4.82491229 0 7030.329279 0.188836377 7434.858838 0.19970214 4769.202955 0.119970686 0 0 0.897274701 0 1.173635309 0 1.173635309 0 0.598077676 0 0.598077676 0 0.598077676 0 0.598077676 0 0.598077676 0 2.29900028 0 2.311090677 0 0.687789345 0 1.973688044 0 1.933782131 0 0.687789345 0 0.897274701 0 0.897274701 0 0 0 0 0 0 0 5.499207695 0 Page 1817 Raw EPA219b_ BART_ 13 Pech 2010 15.27131263 0 5.470346116 0 6.021300733 0 4936.9723 0.1285 0 0 0 0 5.298851859 0 5.082318223 0 5.408363124 0 5.511652157 0 0.103788683 0 0.154250052 0 0.14484089 0 0.311965 0 0 0 0.158801124 0 997.7256605 0.012749324 0 0 0.75553569 0 0.727832715 0 0.75553569 0 0.749239559 0 0.730351167 0 0.783214358 0 0.798422403 0 35.87573793 0 3.346540311 0 3.346540311 0 1.058479986 0 0 0 0 0 2.627037158 0 0 0 0.679196791 0 0.679196791 0 0.679196791 0 0.679196791 0 0.679196791 0 3.191886212 0 0 0 0 0 0 0 3.498534131 0 3.498534131 0 33.8987977 0 85.33145628 0 0 0 0 0 2586.232439 0.010131346 572.1647564 0 0 0 Page 1818 Raw EPA219b_ BART_ 13 Pech 2010 0.805509689 0 0.805509689 0 2161.9498 0.0458 1641.556 0.0138 3383.504436 0.090872727 0 0 0.638737923 0 0.638737923 0 0.223558273 0 0.255495169 0 0.526958786 0 0.638737923 0 1.00480539 0 1.00480539 0 1.507208086 0 0.231162299 0 0.520115152 0 0.520115152 0 3331.138993 0.01304245 2.859427374 0 4.061243746 0 4.061243746 0 11.8544412 0 11.8544412 0 0.534055635 0 1.563995428 0 0.634805139 0 0.991868746 0 0.984112642 0 1.919681203 0 0 0 0 0 4.530016045 0 9.059917846 0 0 0 539.9255797 0 4.198240957 0 4.198240957 0 0 0 19.9845 0 0 0 0 0 36.35272662 0 1.266830213 0 1.266830213 0 0.836442518 0 0.836442518 0 0.836442518 0 0.836442518 0 0.836442518 0 0.669154014 0 Page 1819 Raw EPA219b_ BART_ 13 Pech 2010 0.669154014 0 0.833529572 0 0.833529572 0 0.833529572 0 0.833529572 0 0.833529572 0 0 0 0 0 5.04499298 0 5.04499298 0 1.144651319 0 0.657645128 0 0.83700289 0 0.484837441 0 0 0 0 0 1.151669602 0 0 0 1.974523553 0 1.974523553 0 1.359354769 0 1.470428389 0 1.974523553 0 0 0 0 0 0 0 0 0 0 0 0 0 5709.853013 0.091005151 5748.133688 0.049010295 7221.193017 0.061570037 7437.348462 0.063413042 0 0 1333.381421 0.015856504 1323.878479 0.015743496 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1820 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 880.9968895 0.014058607 885.705356 0.014133743 876.7164654 0.013990302 4084.186587 0.065094849 0 0 0 0 0 0 2027.305166 0.032350951 2454.364608 0.0391658 3797.614433 0.06060086 3714.099537 0.059268162 3747.199 0.028 1896.720128 0.030267125 1953.76213 0.031177379 5.712312692 0 5.712312692 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 21.9096 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 55.41543488 0 55.41543488 0 55.18693198 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1821 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 24.4841 0 24.4841 0 124.2790175 0 194.1859648 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 30.76091444 0 35.56918556 0 0 0 0 0 0 0 0 0 2779.4609 0.007 16.08421232 0 16.08421232 0 16.08421232 0 16.08421232 0 3223.018967 0.003778855 3259.088733 0.003821145 0 0 0 0 0 0 0 0 0 0 0 0 0 0 178.5225204 0 90.31139669 0 2786.4054 0.0055 102.7652583 0 0 0 0 0 5.545875098 0 0 0 0 0 0 0 Page 1822 Raw EPA219b_ BART_ 13 Pech 2010 1073.433007 0.01709898 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 907.4506 0.0091 772.3733767 0.012303326 852.7009361 0.013582884 1065.733879 0.017006568 1089.166908 0.017380504 2683.545855 0.04328491 2710.215845 0.04371509 0 0 0 0 0.485430558 0 0.485430558 0 0.485430558 0 0.485430558 0 0.092659919 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 72.51950688 0 9.288693366 0 29.58768824 0 29.58768824 0 10.36512606 0 Page 1823 Raw EPA219b_ BART_ 13 Pech 2010 48.56807007 0 40.7665 0 463.7089982 0 0.40495339 0 0.40495339 0 0 0 0 0 0 0 0 0 231.2549069 0 150.0084931 0 4.857864426 0 0 0 0 0 0 0 0 0 23.6499429 0 23.6499429 0 128.911627 0.002080478 131.330873 0.002119522 710.31668 0.01131481 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2.4122 0 0 0 0 0 7.799 0 0 0 0 0 4800.2026 0.129 37.6057 0 0 0 0 0 480.7761507 0 463.9657958 0 305.4549536 0 4202.1703 0.0623 0 0 0 0 0 0 0 0 0 0 0 0 443.0781738 0 443.0781738 0 Page 1824 Raw EPA219b_ BART_ 13 Pech 2010 420.812939 0 0 0 2.488767751 0 2.00774544 0 1.246762575 0 0.633936685 0 0.633936685 0 0.633936685 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1.50035323 0 0.276229185 0 0.454652494 0 0.454652494 0 0.842834793 0 0.604251343 0 0.607956233 0 0.607956233 0 0.607956233 0 0.658261036 0 0 0 0 0 0 0 0 0 0.8177 0 3.376175 0 3.376175 0 3.376175 0 3.376175 0 0 0 0 0 0 0 0 0 0 0 1154.7321 0.0016 0 0 0 0 0 0 0.151122727 0 0.141677566 0 0.142858211 0 0.478287366 0 0.478287366 0 0.416753292 0 0.416753292 0 0.416753292 0 Page 1825 Raw EPA219b_ BART_ 13 Pech 2010 0.416753292 0 0.416753292 0 0 0 0 0 0 0 0 0 0 0 0 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0.151565864 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.144276394 0 0 0 0.044253625 0 0.044253625 0 5.880268819 0 5.880268819 0 0.030215375 0 0.030215375 0 8.60447E 07 0 4.30223E 07 0 Page 1826 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 751.5545 0.0138 0 0 0 0 469.8430788 0 469.8430788 0 622.1370423 0 0 0 86.49230363 0 3.557385276 0 4.030550546 0 0 0 0 0 304.1633 0.0007 380.6045 0.0078 7.49022E 06 0 7.49022E 06 0 8.25064E 06 0 8.25064E 06 0 2.4054 0 131.4712299 0 90.4275 0.0018 94.49006237 0 99.38315833 0 99.38315833 0 4.213504792 0 0 0 0 0 5.16605E 06 0 5.16605E 06 0 5.16605E 06 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.558801075 0 0.558801075 0 0 0 16.60929911 0 18.34700089 0 Page 1827 Raw EPA219b_ BART_ 13 Pech 2010 922.6907555 0 0 0 0 0 0 0 0 0 216.1942 0.0053 63.79339559 0.003236765 119.5003044 0.006063235 238.2805 0.004 0 0 0 0 4.434896512 0 0 0 240.8413878 0 0 0 0 0 16.68648633 0 9.55921367 0 89.08521103 0 9.925005124 0 145.9787772 0 68.8185664 0 1.077185882 0 0 0 0 0 0 0 0 0 0 0 12.49518141 0 0 0 0 0 0 0 0 0 15.39859249 0 0 0 15.39859249 0 12.49518141 0 1.604389066 0 0 0 0 0 0 0 0 0 0 0 42.60689598 0 26.78840402 0 0 0 452.1377 0.0011 0 0 0 0 0 0 515.5959966 0 Page 1828 Raw EPA219b_ BART_ 13 Pech 2010 515.5959966 0 515.5959966 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2.796854516 0 2.796854516 0 2.796854516 0 29.5355356 0 0.82205641 0 0.82205641 0 0.82205641 0 0.82205641 0 0.82205641 0 0.82205641 0 0.82205641 0 0.82205641 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1829 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 98.67894795 0 1.239329594 0 3287.1916 0.0081 0 0 0 0 0 0 0 0 0 0 0 0 0.570927997 0 0.59646145 0 0.545394545 0 0 0 1.338090021 0 0.182317335 0 0.182317335 0 0.182317335 0 0.182317335 0 0.182317335 0 0 0 8.26544E 06 0 8.26544E 06 0 8.26544E 06 0 8.26544E 06 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 20.84779665 0 20.84779665 0 26.27551187 0 26.27551187 0 3.602671668 0 3.602671668 0 Page 1830 Raw EPA219b_ BART_ 13 Pech 2010 2.402030919 0 2.402030919 0 3.002538648 0 0 0 0 0 164.6516 0 6.78234E 06 0 6.78234E 06 0 6.78234E 06 0 0 0 0 0 20.71835637 0 20.71835637 0 0 0 0 0 0 0 238.823776 0 238.823776 0 275.0091966 0 29.58688086 0 29.58688086 0 29.58688086 0 29.58688086 0 28.41012383 0 28.41012383 0 2.576059094 0 8.647454502 0 8.647454502 0 1.815664189 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 104.2340573 0 104.2340573 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1831 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2.413083927 0 2.413083927 0 3.16545 0 3.16545 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1832 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 57.80668226 0 57.80668226 0 57.80668226 0 57.80668226 0 5224.9111 0.1049 19.76593206 0 19.76593206 0 19.76593206 0 19.76593206 0 23.7668214 0 19.76593206 0 19.76593206 0 19.76593206 0 19.76593206 0 25.17088316 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 3.858286402 0 3.858286402 0 3.858286402 0 3.858286402 0 3.858286402 0 3.858286402 0 0 0 0 0 0 0 0 0 0 0 0 0 0.629496688 0 0.629496688 0 0.629496688 0 0.629496688 0 Page 1833 Raw EPA219b_ BART_ 13 Pech 2010 131.3879348 0 0 0 0 0 7.049031181 0 7.049031181 0 0 0 5.540967924 0 5.540967924 0 1.846989308 0 1.846989308 0 1.846989308 0 1.846989308 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 5299.4106 0.0275 973.2266369 0.012945078 943.8941631 0.012554922 1290.545063 0.020864577 1407.87026 0.022761404 0 0 0 0 0 0 6.806467021 0 6.928739095 0 6.806467021 0 6.928739095 0 6.928739095 0 6.806467021 0 6.928739095 0 6.806467021 0 6.928739095 0 6.928739095 0 0 0 Page 1834 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 4.58135471 0 5.667234924 0 5.667234924 0 4.881972106 0 5.606144149 0 4.76816371 0 2.030362531 0 2.030362531 0 2.030362531 0 0 0 0 0 0 0 0 0 4370.4028 0.1138 4235.6984 0.1138 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.259250934 0 0.318952578 0 0.710301652 0 0.191697839 0 0 0 0.659403537 0 8367.579278 0.133744468 8367.579278 0.133744468 0 0 0 0 4.750354226 0 56.38559887 0 92.48873247 0 8.663413148 0 8.663413148 0 8.663413148 0 5.057796251 0 4.757852812 0 4.904075238 0 4.74285564 0 4.821590793 0 8.988291142 0 56.43338327 0 8.988291142 0 24.8033662 0 Page 1835 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 66.38348041 0 66.38180087 0 88.51018752 0 88.51018752 0 1.268676431 0 1483.872443 0 24.1992 0 24.1992 0 24.1992 0 24.1992 0 0 0 4169.095214 0.034991309 4155.183655 0.034874549 4168.69774 0.034987973 4170.685106 0.035004653 0 0 0 0 293.1994109 0 285.4836369 0 308.6309588 0 297.0572979 0 3367.200328 0.028307159 3349.8878 0.0399 266.3366505 0 266.3366505 0 266.3366505 0 266.3366505 0 266.3366505 0 266.3366505 0 640.1231971 0 0 0 0 0 0 0 0 0 0 0 9867.634575 0.042526337 9809.005125 0.042273663 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1836 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1649.1712 0.003 0 0 0 0 3823.7071 0.0777 2717.578043 0.003314748 2857.364357 0.003485252 2024.7038 0.0037 2133.5124 0.0027 4352.7326 0.0248 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 419.5939112 0.001383775 884.2692888 0.002916225 2847.2992 0.0095 0 0 0 0 2721.964622 0.009044465 4470.827578 0.014855535 77.05908839 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1760.9018 0.0059 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1837 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 1.752916753 0 0 0 0 0 0 0 0 0 0 0 0 0 1792.015135 0.037178443 2603.859665 0.054021557 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1992.9377 0.0187 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1954.1263 0.0525 1.834177795 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 4011.471481 0.051249181 Page 1838 Raw EPA219b_ BART_ 13 Pech 2010 3889.24481 0.049687655 0 0 0 0 0 0 0 0 2748.410833 0.035135896 2715.417436 0.034714106 2721.203173 0.034788071 2742.624858 0.035061927 0 0 0 0 0 0 0 0 0 0 0 0 0 0 833.7891 0.0173 2696.1707 0.0542 2401.613225 0.049817639 2.423433216 0 1.229000198 0 1.229000198 0 1.151379132 0 974.8495219 0.012441787 976.1365781 0.012458213 2107.7504 0.0424 4125.193935 0.085570575 2512.20964 0.052111786 2.378948045 0 2.219957984 0 2.378948045 0 2.378948045 0 2.219957984 0 2.378948045 0 2.378948045 0 2.135655782 0 1335.603232 0.017063916 1327.206461 0.016956637 1338.96194 0.017106827 1338.316034 0.017098575 1341.803924 0.017143137 1333.01961 0.017030907 4534.0788 0.058 4286.52441 0.054763163 4731.679 0.0605 0 0 0 0 0 0 2.779200448 0 2.736844423 0 2.671681461 0 Page 1839 Raw EPA219b_ BART_ 13 Pech 2010 2.932333311 0 5.631541176 0 5.775202941 0 5.789569118 0 5.818301471 0 5.775202941 0 5.875766176 0 6.033794118 0 5.847033824 0 5.746470588 0 5.588442647 0 5.775202941 0 5.775202941 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 3181.2118 0.0494 0 0 1822.096322 0.020617792 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 143.269 0.0027 0 0 0 0 0 0 0 0 780.8286 0.0123 2843.987 0.0364 0 0 0 0 0 0 0 0 0 0 0.548549295 0 Page 1840 Raw EPA219b_ BART_ 13 Pech 2010 0.548549295 0 1.225062041 0 0.737436552 0 0.858672532 0 0.705680911 0 3.841525016 0 0 0 3.657521075 0 0 0 0 0 0 0 3.103570345 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.233588278 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1841 Raw EPA219b_ BART_ 13 Pech 2010 1.175963593 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page 1842 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 816.9849 0.0032 792.3037 0.0031 1595.4807 0.0063 0 0 0 0 0 0 1.722686192 0 0 0 0 0 0 0 0 0 0 0 0.28194813 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1625.1758 0.0063 1554.9097 0.009 Page 1843 Raw EPA219b_ BART_ 13 Pech 2010 2292.2542 0.0476 1657.850687 0.021191954 1673.946325 0.021397701 1665.898506 0.021294828 1649.802868 0.02108908 1754.424514 0.022426437 1612.6383 0.0246 0 0 0 0 1106.501659 0.014133058 1095.693471 0.013995007 1516.66247 0.019371935 3799.6234 0.0486 0 0 0 0 0 0 729.7120481 0.009313695 727.5661519 0.009286305 2932.343134 0.037470615 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 259.6478441 0.003282661 340.1728 0.0051 349.3972559 0.004417339 665.0544 0.0085 0 0 15.89868333 0.000483333 15.89868333 0.000483333 15.89868333 0.000483333 15.89868333 0.000483333 15.89868333 0.000483333 15.89868333 0.000483333 0 0 0 0 1808.530743 0.024088388 3304.7558 0.044 4062.186804 0.05410554 4069.734553 0.054206071 0 0 0 0 0 0 1341.986139 0.005249444 2697.180561 0.010550556 2.370228161 0 Page 1844 Raw EPA219b_ BART_ 13 Pech 2010 865.1101345 0.017964843 959.2821381 0.019920416 948.0052455 0.01968624 978.9337819 0.020328501 0 0 0 0 0 0 3960.3075 0.0822 0 0 0 0 0 0 0 0 169.9985145 0 0 0 169.9985145 0 2353.695499 0 1220.892102 0 2296.318762 0 14.73984167 0 4.212998486 0 4.213306899 0 1961.544646 0 114.0043512 0 1598.700071 0 3.159980174 0 162.8133427 0 0 0 69.18663818 0 0 0 877.0661939 0 1560.881397 0 0 0 14.40586201 0 1433.5349 0 925.2400029 0 925.2400029 0 5.37157307 0 735.4771697 0 11.68975622 0 269.5107909 0 11.68975622 0 11.68975622 0 35.06926867 0 123.5719 0 18.90769389 0 1085.14594 0 0 0 449.6582604 0 0 0 2.708979266 0 34.74788136 0 Page 1845 Raw EPA219b_ BART_ 13 Pech 2010 0 0 0 0 3.014875233 0 0.437124767 0 8.423728814 0 463.7552 0 198.7402849 0 42.36153192 0 5.160923146 0 810.7728482 0 1332.428662 0 92.1212 0 15.82326923 0 1122.680091 0 8.21489226 0 207.116544 0 0 0 176.0490624 0 0 0 264.0735936 0 0 0 11.19091641 0 377.69692 0 4.739623297 0 7.848343303 0 0 0 0 0 0 0 261.5411472 0 0 0 148.4260972 0 0 0 106.2432323 0 0 0 5.267858071 0 5.267858071 0 849.4851878 0 0 0 164.7670467 0 47.74241285 0 5.401506861 0 5.401506861 0 5.401506861 0 5.401506861 0 779.5542063 0 1.367534655 0 81.35649596 0 2193.536666 0 5420.428545 0 204.5517998 0 264.5844 0 Page 1846 Raw EPA219b_ BART_ 13 Pech 2010 24.66868828 0 4.739623297 0 810.7728482 0 0 0 229.9247418 0 229.9247418 0 0 0 1567.955838 0 1567.955838 0 6.84662371 0 3135.911677 0 13.69324742 0 6.84662371 0 4.2119 0 19.62085826 0 3.924171651 0 4.739623297 0 32.63405435 0 0 0 254.7852791 0 0 0 254.7852791 0 77.38326525 0 33.16425653 0 0 0 1754.132388 0 10.53131191 0 5.002935702 0 1733.154698 0 494.28845 0 476.9302828 0 0 0 5.724673939 0 164.9352865 0 0 0 936.4731022 0 389.5655978 0 47.74241285 0 15.79296754 0 15.79296754 0 0 0 0 0 267.0671183 0 89.02237277 0 746.5729679 0 2316.955226 0 54.68040119 0 992.9808111 0 24.0201 0 2.105880969 0 3.159748865 0 Page 1847 Raw EPA219b_ BART_ 13 Pech 2010 494.28845 0 799.3500353 0 0.5265 0 1634.285548 0 1634.285548 0 4.739623297 0 1131.073476 0 725.7715189 0 948.5422078 0 0 0 0.347151296 0 17.54888616 0 8.843905003 0 18.95849319 0 92.03757791 0 166.951872 0 141.9090912 0 212.8636368 0 0 0 10.53571614 0 834.7322253 0 1783.165463 0 7.373287072 0 1783.165463 0 7.373287072 0 33.69166408 0 25.26874806 0 8.422916019 0 284.2838556 0 0 0 3464.685361 0 0 0 2878.6669 0 2313.100007 0 2313.100007 0 2.621996003 0 2.621996003 0 1716.236301 0 139.6419311 0 83.53950181 0 1440.380691 0 83.53950181 0 1440.380691 0 3.159393574 0 250.4000258 0 26.58309231 0 251.8496511 0 251.8496511 0 351.3302633 0 0 0 2955.1261 0 Page 1848 Raw EPA219b_ BART_ 13 Pech 2010 0 0 108.2921293 0 22.64486686 0 23.69811649 0 469.3930892 0 391.1609077 0 14.20491787 0 16.84553334 0 0 0 0 0 0 0 1.895427043 0 1727.825846 0 1727.825846 0 1.895427043 0 463.7552 0 169.2332 0 0 0 0 0 1012.755856 0 0.294427121 0 0.294427121 0 1981.30656 0 4.739623297 0 0 0 11.93243997 0 11.93243997 0 23.86846003 0 23.86846003 0 7.663676402 0 952.1723 0 3.937581123 0 8.426613797 0 574.0796906 0 108.1783472 0 48.28631375 0 2.383901754 0 56.56495992 0 0 0 0.4212 0 264.5844 0 941.053132 0 23.46329469 0 23.61788258 0 244.9858441 0 0 0 489.8475714 0 0 0 18.59315343 0 18.59315343 0 37.18630686 0 Page 1849 Raw EPA219b_ BART_ 13 Pech 2010 37.18630686 0 394.7130159 0 7.2787 0 596.2985918 0 321.0838571 0 4.950273221 0 8.899959302 0 73.96045087 0 0 0 927.4685531 0 0 0 927.4685531 0 0 0 927.4685531 0 927.4685531 0 0 0 2.738771547 0 24.46836441 0 661.7587058 0 5.160923146 0 2734.733555 0 102.7694299 0 303.7824481 0 0 0 367.4787679 0 105.6994385 0 0 0 0 0 257.2351363 0 4.739623297 0 189.5771235 0 2.316469066 0 0 0 0 0 279.7353211 0 117.3652924 0 0 0 0 0 291.1530893 0 122.1557125 0 531.3221 0.0013 4.739623297 0 594.0396 0 13.85001759 0 15.7945 0 0 0 55.25612979 0 26.59071095 0 2922.2735 0.0115 141.0358046 0 141.0358046 0 Page 1850 Raw EPA219b_ BART_ 13 Pech 2010 2351.641945 0 91.71095908 0 45.85547954 0 877.0661939 0 0 0 169.9985145 0 0 0 169.9985145 0 1667.063635 0 1594.665807 0 1594.665807 0 565.1681 0 7.848343303 0 155.2095947 0 353.9672053 0 0 0 0 0 7.756009852 0 7.756009852 0 102.2758999 0 102.2758999 0 102.2758999 0 102.2758999 0 2.316469066 0 2673.691156 0 409.1035997 0 3.693338025 0 3.693338025 0 7.38667605 0 204.5517998 0 0 0 0 0 25.95195763 0 5.002935702 0 5.113425477 0 5.266248108 0 3257.491611 0 5.557148843 0 360.9737644 0 2330.011361 0 460.5634177 0 115.8784776 0 140.5485571 0 618.0945578 0 618.0945578 0 47.74241285 0 5.2648 0 20.2247745 0 0 0 2.216002815 0 2523.7824 0.0063 Page 1851 Raw EPA219b_ BART_ 13 Pech 2010 6148.846425 0 3661.550005 0 24.75136611 0 0 0 0 0 0 0 0 0 0 0 0 0 199.6469 0.00055 199.6469 0.00055 1016.866929 0.013007874 1016.866929 0.013007874 960.9146711 0.012292126 1370.4117 0.0034 63.73879586 0 Page 1852