[Federal Register: August 8, 2007 (Volume 72, Number 152)]
[Rules and Regulations]
[Page 44370-44371]
[DOCID:fr08au07-3]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-28863; Directorate Identifier 2007-NE-33-AD;
Amendment 39-15149; AD 2007-16-10]
RIN 2120-AA64

Airworthiness Directives; Teledyne Continental Motors
Reciprocating (TCM) Engine Models IO-550-N, TSIO-520-BE, TSIO-550-A,
TSIO-550-B, TSIO-550-C, TSIO-550-E, and TSIO-550-G

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule; request for comments.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for TCM
IO-550-N, TSIO-520-BE, TSIO-550-A, TSIO-550-B, TSIO-550-C, TSIO-550-E,
and TSIO-550-G reciprocating engines. This AD requires removing before
further flight, certain Kelly Aerospace Power Systems turbochargers,
part number (P/N)<PHONE_NUMBER>, listed by serial number in this AD. This
AD results from four incidents of the turbine rotor separating from the
shaft of the turbocharger. We are issuing this AD to prevent the
turbine rotor from separating from the shaft of the turbocharger due to
a machining defect in the turbocharger compressor. This condition could
result in full engine power loss, loss of engine lubricant, or smoke in
the airplane cabin.

DATES: This AD becomes effective August 23, 2007. The Director of the
Federal Register approved the incorporation by reference of certain
publications listed in the regulations as of August 23, 2007.
    We must receive any comments on this AD by October 9, 2007.

ADDRESSES: Use one of the following addresses to comment on this AD:
     DOT Docket Web site: Go to http://dms.dot.gov and follow

the instructions for sending your comments electronically.
     Government-wide rulemaking Web site: Go to http://www.regulations.gov
 and follow the instructions for sending your

comments electronically.
     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: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
     Fax:<PHONE_NUMBER>.
    Contact Kelly Aerospace Power Systems, 2900 Selma Highway,
Montgomery, AL 36108; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>;
http://www.kellyaerospace.com for the service information identified in

this AD.

FOR FURTHER INFORMATION CONTACT: Kevin Brane, Aerospace Engineer,
Atlanta Aircraft Certification Office, FAA, Small Airplane Directorate,
One Crown Center, 1895 Phoenix Blvd., Suite 450, Atlanta, GA 30349; e-
mail<EMAIL_ADDRESS>telephone<PHONE_NUMBER>; fax (770) 703-
6097.

SUPPLEMENTARY INFORMATION: On July 16, 2007, Kelly Aerospace Power
Systems informed us that there were potential nonconforming
turbochargers, P/N<PHONE_NUMBER> that might have a machining defect in
the compressors of the turbochargers. A machining defect in the
turbocharger compressor leads to a condition where the center bore of
the compressor is not perpendicular to the backface of the compressor.
The machining defect leads to abnormal turbocharger rotor vibration
which results in abnormal wear characteristics. The wear could result
in the turbocharger rotor separating from the shaft. This condition, if
not corrected, could result in full engine power loss, loss of engine
lubricant, or smoke in the airplane cabin.

Relevant Service Information

    We have reviewed and approved the technical contents of Kelly
Aerospace Power Systems Service Bulletins (SBs) No. 026, Revision B,
dated July 27, 2007, and No. 027, dated July 25, 2007. Those SBs list
affected turbochargers by SN, and describe procedures for visually
inspecting the turbocharger.

FAA's Determination and Requirements of this AD

    The unsafe condition described previously is likely to exist or
develop on other engines of the same type design. For that reason, we
are issuing this AD to prevent the turbine rotor from separating from
the shaft of the turbocharger due to a machining defect in the
turbocharger compressor. This condition could result in full engine
power loss, loss of engine lubricant, or smoke in the airplane cabin.
This AD requires replacing certain turbochargers before further flight.
You must use the service information described previously to perform
the actions required by this AD.

FAA's Determination of the Effective Date

    Since an unsafe condition exists that requires the immediate
adoption of this AD, we have found that notice and opportunity for
public comment before issuing this AD 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 was not preceded by notice and an opportunity for public
comment; however, we invite you to send us any written relevant data,
views, or arguments regarding this AD. Send your comments to an address
listed under ADDRESSES. Include ``AD Docket No. FAA-2007-28863;
Directorate Identifier 2007-NE-33-AD'' in the subject line of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of the rule that might
suggest a need to modify it.
    We will post all comments we receive, without change, to http://dms.dot.gov
, including any personal information you provide. We will

also post a report summarizing each substantive verbal contact with FAA
personnel concerning this AD. Using the search function of the DMS Web
site, anyone can find and read the comments in any of our dockets,
including the name of the individual who sent the comment (or signed
the comment on behalf of an association, business, labor union, etc).
You may review the DOT's complete Privacy Act Statement in the Federal
Register published on April 11, 2000 (65 FR 19477-78) or you may visit
http://dms.dot.gov.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://dms.dot.gov
; or in person at the Docket Operations office between 9

a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this AD, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Operations office (telephone<PHONE_NUMBER>) is provided in the
ADDRESSES section. Comments will be available in the AD docket shortly
after receipt.

Authority for this Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, Section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more

detail the scope of the Agency's authority.
    We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701, ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.

Regulatory Findings

    We have determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the national Government and the States, or on the distribution of power
and responsibilities among the various levels of government.
    For the reasons discussed above, I certify that this AD:
    1. Is not a ``significant regulatory action'' under Executive Order
12866;
    2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
    3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
    We prepared a summary of the costs to comply with this AD and
placed it in the AD Docket. You may get a copy of this summary at the
address listed under ADDRESSES.

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

0
Under the authority delegated to me by the Administrator, the Federal
Aviation Administration amends part 39 of the Federal Aviation
Regulations (14 CFR part 39) as follows:

PART 39--AIRWORTHINESS DIRECTIVES

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 adding the following new airworthiness
directive:

2007-16-10 Teledyne Continental Motors: Amendment 39-15149. Docket
No. FAA-2007-28863; Directorate Identifier 2007-NE-33-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective August
23, 2007.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to:
    (1) Teledyne Continental Motors (TCM) models TSIO-520-BE, TSIO-
550-A, TSIO-550-B, TSIO-550-C, TSIO-550-E, and TSIO-550-G
reciprocating engines with a Kelly Aerospace Power Systems
turbocharger, TCM part number (P/N) 646677, with certain serial
numbers (SNs), installed on or after March 20, 2007. These engines
are installed on, but not limited to, Adam Aircraft A500, Columbia
Aircraft Manufacturing LC41-550FG, Mooney Airplane Company M20TN
(Acclaim), and Piper Aircraft Incorporated PA-46-310P (Malibu)
airplanes.
    (2) TCM IO-550-N reciprocating engines modified to Engine
Technologies Incorporated supplemental type certificate (STC)
SE10589SC to install turbocharger, P/N<PHONE_NUMBER>, with certain
SNs, installed on or after March 20, 2007. These engines are
installed on, but not limited to, Cirrus Design Corporation Aircraft
Model SR22 modified to Engine Technologies Incorporated STC
SA10588SC.

Unsafe Condition

    (d) This AD results from four incidents of the turbine rotor
separating from the shaft of the turbocharger. We are issuing this
AD to prevent the turbine rotor from separating from the shaft of
the turbocharger due to a machining defect in the turbocharger
compressor. This condition could result in full engine power loss,
loss of engine lubricant, or smoke in the airplane cabin.

Compliance

    (e) You are responsible for having the actions required by this
AD performed before further flight unless the actions have already
been done.
    (f) If your engine has a turbocharger that was installed before
March 20, 2007, no further action is required.

Engines Modified to Engine Technologies Incorporated STC SE10589SC

    (g) Before further flight, for engines modified to Engine
Technologies Incorporated STC SE10589SC on or after March 20, 2007,
with a turbocharger that has a SN listed in Kelly Aerospace Service
Bulletin (SB) No. 026, Revision B, dated July 27, 2007, replace the
turbocharger.

TCM Engines with Turbocharger TCM P/N 646677

    (h) Before further flight, for engines with a Kelly Aerospace
Power Systems turbocharger, TCM P/N 646677 installed on or after
March 20, 2007, with a turbocharger SN listed in Kelly Aerospace SB
No. 027, dated July 25, 2007, replace the turbocharger.

Alternative Methods of Compliance

    (i) The Manager, Atlanta Aircraft Certification Office, has the
authority to approve alternative methods of compliance for this AD
if requested using the procedures found in 14 CFR 39.19.

Special Flight Permits

    (j) We are limiting the special flight permits for this AD by
allowing a special flight permit only after visually inspecting the
turbocharger using the procedures specified in the Visual Inspection
sections of Kelly Aerospace Power Systems SB No. 026, Revision B,
dated July 27, 2007, and SB No. 027, dated July 25, 2007.

Related Information

    (k) Teledyne Continental Aircraft Engine Mandatory Service
Bulletin (MSB) MSB07-4, dated July 30, 2007, contains additional
information on replacing turbochargers on TCM engines and Cirrus
Service Advisory SA 07-14 R1, dated July 24, 2007, contains
additional information on replacing turbochargers on Cirrus Design
Corporation Aircraft Model SR22 modified to Engine Technologies
Incorporated STC SA10588SC.
    (l) Contact Kevin Brane, Aerospace Engineer, Atlanta Aircraft
Certification Office, FAA, Small Airplane Directorate, One Crown
Center, 1895 Phoenix Blvd., Suite 450, Atlanta, GA 30349; e-mail:
<EMAIL_ADDRESS>telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>,

for more information about this AD.

Material Incorporated by Reference

    (m) You must use Kelly Aerospace Power Systems Service Bulletins
No. 026, Revision B, dated July 27, 2007, and No. 027, dated July
25, 2007, to determine if you have an affected turbocharger
installed. The Director of the Federal Register approved the
incorporation by reference of this service bulletin in accordance
with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Kelly Aerospace
Power Systems, 2900 Selma Highway, Montgomery, AL 36108; telephone
(334) 386-5400; fax<PHONE_NUMBER>; http://www.kellyaerospace.com, for a

copy of this service information. You may review copies at the FAA,
New England Region, 12 New England Executive Park, Burlington, MA;
or at the National Archives and Records Administration (NARA). For
information on the availability of this material at NARA, call 202-
741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html
.

    Issued in Burlington, Massachusetts, on August 1, 2007.
Peter A. White,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 07-3840 Filed 8-6-07; 11:44 am]

BILLING CODE 4910-13-P


[Federal Register Volume 78, Number 178 (Friday, September 13, 2013)]
[Notices]
[Pages 56718-56719]
[FR Doc No: 2013-22309]

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DEPARTMENT OF HEALTH AND HUMAN SERVICES

Food and Drug Administration

[Docket No. FDA-2013-D-1020]

Draft Guidance for Industry on Bioanalytical Method Validation;
Availability

AGENCY: Food and Drug Administration, HHS.

ACTION: Notice.

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SUMMARY: The Food and Drug Administration (FDA) is announcing the
availability of a draft guidance for industry entitled ``Bioanalytical
Method Validation.'' The draft guidance is intended to provide
recommendations regarding analytical method development and validation
for the measurement of drugs and/or metabolites, therapeutic biologics,
and biomarkers for sponsors of investigational new drug applications
(INDs), new drug applications (NDAs), abbreviated new drug applications
(ANDAs), and biologics license applications (BLAs) for therapeutic
biologics regulated by the Center for Drug Evaluation and Research.
This draft guidance may apply to some studies related to the veterinary
drug approval process (Investigational New Animal Drugs (INADs), New
Animal Drug Applications (NADAs), and Abbreviated New Animal Drug
Applications (ANADAs)) regulated by the Center for Veterinary Medicine.
This guidance was originally issued in 2001. FDA is revising the
guidance to reflect advancements in the science and technology of
bioanalytical method validation.

DATES: Although you can comment on any guidance at any time (see 21 CFR
10.115(g)(5)), to ensure that the Agency considers your comment on this
draft guidance before it begins work on the final version of the
guidance, submit either electronic or written comments on the draft
guidance by December 12, 2013.

ADDRESSES: Submit written requests for single copies of the revised
draft guidance to the Division of Drug Information, Center for Drug
Evaluation and Research, Food and Drug Administration, 10903 New
Hampshire Ave., Bldg. 51, Rm. 2201, Silver Spring, MD 20993-0002, or
Communications Staff (HFV-12), Center for Veterinary Medicine, Food and
Drug Administration, 7519 Standish Pl., Rockville, MD 20855. Send one
self-addressed adhesive label to assist that office in processing your
requests. See the SUPPLEMENTARY INFORMATION section for electronic
access to the guidance document.
    Submit electronic comments on the draft guidance to http://www.regulations.gov. Submit written comments to the Division of Dockets
Management (HFA-305), Food and Drug Administration, 5630 Fishers Lane,
Rm. 1061, Rockville, MD 20852.

FOR FURTHER INFORMATION CONTACT: Brian Booth, Center for Drug
Evaluation and Research, Food and Drug Administration, 10903 New
Hampshire Ave., Bldg. 51, Rm. 2186, Silver Spring, MD 20993-0002, 301-
796-1508; or John Kadavil, Center for Veterinary Medicine (HFV-151),
Food and Drug Administration, 7500 Standish Pl., Rockville, MD 20855,
240-276-9589.

SUPPLEMENTARY INFORMATION:

I. Background

    FDA is announcing the availability of a draft guidance for industry
entitled ``Bioanalytical Method Validation.'' The measurement of drug
and/or metabolite, therapeutic biological product, or biomarker
concentrations in in vivo studies provides critical support for many
types of drug and therapeutic biologic development studies. The
accuracy and the reliability of these data are of critical importance
to the interpretation of the study outcomes. The draft guidance
reflects the Agency's view that the reliability of these data is, in
part, assured by adequate method development and validation prior to
study conduct. The method validation should provide assurance that the
samples are unaffected by handling conditions, and that the
measurements are accurate and can be repeated without significant
change.
    The draft guidance provides recommendations for sponsors of INDs,
NDAs, ANDAs, and BLAs regarding measurement of drug, therapeutic
biological product, and biomarker concentrations in nonclinical and
clinical study samples. The guidance provides recommendations for
sponsors of INADs, NADAs, and ANADAs regarding measurement of drug
concentrations in some bioavailability, bioequivalence, and
pharmacokinetic studies. The guidance lists the recommendations for
sample handling and stability; method acceptance criteria for accuracy
and precision; and reproducibility. The guidance also addresses the
fit-for-purpose concept, biomarkers, and novel technologies.
    On May 23, 2001 (66 FR 28526), FDA issued the first version of this
guidance. Since then, substantial scientific and technical advancements
have taken place related to the validation of bioanalytical methods.
FDA revised the guidance to reflect these advancements and is issuing
the revised guidance in draft to solicit public input. The revised
draft guidance contains a number of new sections, including sections on
endogenous compounds, incurred sample reanalysis, biomarker assays, use
of diagnostic kits and new technologies, system suitability, and
examples of report formats for tabular data listings. In addition, FDA
has updated sections where needed, such as the sections on
chromatography and ligand-binding assays. The changes and additions are
intended to reflect the many advances in the field during the last
decade.
    This revised draft guidance is issued consistent with FDA's good
guidance practices regulation (21 CFR 10.115). The draft guidance, when
finalized, will represent the Agency's current thinking on
Bioanalytical Method Validation. It does not create or confer any
rights for or on any person and does not operate to bind FDA or the
public. An alternative approach may be used if such approach satisfies
the requirement of the applicable statutes and regulations.

II. Paperwork Reduction Act of 1995

    This revised draft guidance refers to previously approved
collections of information that are subject to review by the Office of
Management and Budget (OMB) under the Paperwork Reduction Act of 1995
(44 U.S.C. 3501-3520). The collections of information in 21 CFR part 58
have been approved under OMB control number 0910-0119; the collections
of information in 21 CFR part 312 have been approved under OMB control
number 0910-0014; the collections of information in 21 CFR part 314
have been approved under OMB control number 0910-0001; the collections
of information in 21 CFR part 514 have been approved under OMB control
number 0910-0032; the collections of information in 21 CFR part 511
have been approved under OMB control number 0910-0117; and the
collections of information in section 360b(n)(1) (21 U.S.C 512(n)(1))
of the Federal Food, Drug and Cosmetic Act have been approved in OMB
control number 0910-0669.

III. Comments

    Interested persons may submit either electronic comments regarding
this document to http://www.regulations.gov or written comments to the
Division of Dockets Management (see ADDRESSES). It is only necessary to
send one set of comments. Identify comments with the docket number
found in brackets in the

heading of this document. Received comments may be seen in the Division
of Dockets Management between 9 a.m. and 4 p.m., Monday through Friday,
and will be posted to the docket at http://www.regulations.gov.

IV. Electronic Access

    Persons with access to the Internet may obtain the document at
either http://www.fda.gov/Drugs/GuidanceComplianceRegulatoryInformation/Guidances or http://www.regulations.gov.

    Dated: September 7, 2013.
Leslie Kux,
Assistant Commissioner for Policy.
[FR Doc. 2013-22309 Filed 9-12-13; 8:45 am]
BILLING CODE 4160-01-P


[Federal Register Volume 82, Number 201 (Thursday, October 19, 2017)]
[Notices]
[Pages 48739-48741]
[FR Doc No: 2017-22660]

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DEPARTMENT OF TRANSPORTATION

National Highway Traffic Safety Administration

Petition for Exemption From the Federal Motor Vehicle Motor Theft
Prevention Standard; General Motors Corporation

AGENCY: National Highway Traffic Safety Administration, Department of
Transportation (DOT).

ACTION: Grant of petition for exemption.

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SUMMARY: This document grants in full General Motors Corporation's (GM)
petition for an exemption of the Cadillac XT4 vehicle line in
accordance with Exemption from the Theft Prevention Standard. This
petition is granted because the agency has determined that the
antitheft device to be placed on the line as standard equipment is
likely to be as effective in reducing and deterring motor vehicle theft
as compliance with the parts-marking requirements of the Federal Motor
Vehicle Theft Prevention Standard (Theft Prevention Standard).

DATES: The exemption granted by this notice is effective beginning with
the 2019 model year (MY).

FOR FURTHER INFORMATION CONTACT: Hisham Mohamed, Office of
International Policy, Fuel Economy, and Consumer Standards, NHTSA, W43-
437, 1200 New Jersey Avenue SE., Washington, DC 20590. Mr. Mohamed's
phone number is<PHONE_NUMBER>. His fax number is<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: In a petition dated May 29, 2017, GM
requested an exemption from the parts-marking requirements of the Theft
Prevention Standard for its Cadillac XT4 vehicle line beginning with MY
2019. The petition requested an exemption from parts-marking pursuant
to 49 CFR 543, Exemption from Vehicle Theft Prevention Standard, based
on the installation of an antitheft device as standard equipment for
the entire vehicle line.
    Under 49 CFR part 543.5(a), a manufacturer may petition NHTSA to
grant an exemption for one vehicle line per model year. In its
petition, GM

provided a detailed description and diagram of the identity, design,
and location of the components of the antitheft device for the Cadillac
XT4 vehicle line. GM will install the PASS-Key III+ antitheft device as
standard equipment on its Cadillac XT4 vehicle line. The PASS-Key III+
is a passive, transponder-based, electronic immobilizer device. The
major components of the antitheft device are a PASS-Key III+ controller
module, engine control module (ECM), electronically-coded ignition key,
radio frequency (RF) receiver, immobilizer exciter module, three low
frequency antennas and a passive antenna module. GM stated that the
device will provide protection against unauthorized use (i.e., starting
and engine fueling), but will not provide any visible or audible
indication of unauthorized vehicle entry (i.e., flashing lights or horn
alarm). GM stated that the PASS-Key III+ immobilizer device is designed
to be active at all times without direct intervention by the vehicle
operator. GM further stated that activation of the device occurs
immediately after the ignition has been turned off and the key has been
removed and deactivation of the antitheft device occurs automatically
when the engine is started. GM stated that the Cadillac XT4 vehicle
line will be equipped with one of two ignition versions. Specifically,
the Cadillac XT4 will be equipped with either a keyed or keyless
ignition version of its PASS-Key III+ immobilizer antitheft device. GM
also stated that the ``keyed'' ignition version utilizes a special
ignition key and decoder module and its electrical code must be sensed
and properly decoded by the controller module before the vehicle can be
operated. GM further stated that with the ``keyless'' ignition version,
an electronic key fob performs normal remote keyless entry functions
and communicates with the vehicle without direct owner intervention.
Specifically, during operation of the vehicle, when the owner presses
the engine start/stop switch, the vehicle transmits a randomly
generated challenge and vehicle identifier within the passenger
compartment of the vehicle via three low-frequency antennas, controlled
by the passive antenna module. The electronic key receives the data and
if the vehicle identifier matches that of the vehicle, the electronic
key will calculate the response to the vehicle using the challenge and
secret information shared between the key and the vehicle. The
electronic key then transmits the response via a radio frequency
channel to a vehicle mounted receiver, conveying the information to the
PASS-Key III+ control module. The PASS-Key III+ control module compares
the received response with an internally calculated response. If the
values match, the device will allow the vehicle to enter functional
modes and transmit a fixed code pre-release password to the engine
controller over the serial data bus, and enable computation and
communication of a response to any valid challenge received from the
engine controller. If a valid key is not detected, the device will not
transmit a fixed code pre-release password to the engine controller
preventing fuel from being delivered to the engine, enabling starting.
    GM's submission is considered a complete petition as required by 49
CFR 543.7, in that it meets the general requirements contained in 543.5
and the specific content requirements of 543.6.
    In addressing the specific content requirements of 543.6, GM
provided information on the reliability and durability of its proposed
device. To ensure reliability and durability of the device, GM
conducted tests based on its own specified standards. GM provided a
detailed list of the specific tests it used to validate the integrity,
durability and reliability of the PASS-Key III+ device. Some of the
tests GM conducted were for high temperature storage, low temperature
storage, thermal shock, humidity, frost, salt fog, flammability and
others. GM believes that the device is reliable and durable since the
components must operate as designed after each test. GM further stated
that the design and assembly processes of the PASS-Key III+ subsystem
and components are validated for 10 years of vehicle life and 150,000
miles of performance.
    GM further stated that the PASS-Key III+ device has been designed
to enhance the functionality and theft protection provided by its
first, second and third generation PASS-Key, PASS-Key II, and PASS-Key
III devices. GM also referenced data provided by the American
Automobile Manufacturers Association (AAMA) in support of the
effectiveness of GM's PASS-Key devices in reducing and deterring motor
vehicle theft. Specifically, GM stated that data which provide the
basis for GM's confidence that the PASS-Key 111+ system will be
effective in reducing and deterring motor vehicle theft are contained
in the response of the American Automobile Manufacturers Association
(AAMA) to Docket 97-042; Notice I (NHTSA Request for Comments on its
Preliminary Report to Congress on the Effects of the Anti Car Theft Act
of 1992 and the Motor Vehicle Theft Law Enforcement Act of 1984). In
the Report to Congress, AAMA stated the more recent antitheft systems
are more effective in reducing auto theft. AAMA also cited the Highway
Loss Data Institute (HLDI) findings on the effectiveness of antitheft
devices in reducing theft. AAMA noted that vehicles with antitheft
devices are less likely to be stolen for joyriding or transportation
and therefore, their recovery rates are lower.
    GM also noted that theft rate data have indicated a decline in
theft rates for vehicle lines equipped with comparable devices that
have received full exemptions from the parts-marking requirements. GM
stated that the theft rate data, as provided by the Federal Bureau of
Investigation's National Crime Information Center (NCIC) and compiled
by the agency, show that theft rates are lower for exempted GM models
equipped with the PASS-Key-like systems than the theft rates for
earlier models with similar appearance and construction that were
parts-marked. Based on the performance of the PASS-Key, PASS-Key II,
and PASS-Key III devices on other GM models, and the advanced
technology utilized in PASS-Key III+, GM believes that the PASS-Key
III+ device will be more effective in deterring theft than the parts-
marking requirements of 49 CFR part 541.
    Additionally, GM stated that the model year (MY) 2014 Cadillac CTS
and SRX theft rates (per 1000 vehicles produced) are below the 1990/
1991 median rate of 3.5826. Specifically, the theft for the MY 2014
Cadillac CTS is 0.3546 and 0.8481 for the MY 2014 Cadillac SRX vehicle
line. Since the same antitheft device will be used on the 2019 MY
Cadillac XT4, GM believes the statistical data indicates that this
vehicle will also have an acceptable theft rate to obtain an exemption
from the parts marking requirements of 49 CFR part 541. GM was granted
an exemption from the parts-marking requirements by the agency for the
Cadillac CTS vehicle line beginning with MY 2011 (See 74 FR 62385,
November 27, 2009). The average theft rate for the Cadillac CTS and SRX
vehicle lines, based on NHTSA's theft rate data, using 3 MYs data (MYs
2012-2014) are 0.8518 and 0.6020 respectively.
    GM further stated that it believes that PASS-Key III+ devices will
be more effective in deterring theft than the parts-marking
requirements and that the agency should find that inclusion of the
PASS-Key III+ device on the Cadillac XT4 vehicle line is sufficient to
qualify

it for full exemption from the parts-marking requirements.
    GM's proposed device lacks an audible or visible alarm. Therefore,
this device cannot perform one of the functions listed in 49 CFR part
543.6(a)(3), that is, to call attention to unauthorized attempts to
enter or move the vehicle. Based on comparison of the reduction in the
theft rates of Chevrolet Corvettes using a passive antitheft device
along with an audible/visible alarm system to the reduction in theft
rates for the Chevrolet Camaro and the Pontiac Firebird models equipped
with a passive antitheft device without an alarm, GM finds that the
lack of an alarm or attention-attracting device does not compromise the
theft deterrent performance of a device such as PASS-Key III+ device.
In these instances, the agency has concluded that the lack of an
audible or visible alarm has not prevented these antitheft devices from
being effective protection against theft.
    Based on the evidence submitted by GM, the agency believes that the
antitheft device for the Cadillac XT4 vehicle line is likely to be as
effective in reducing and deterring motor vehicle theft as compliance
with the parts-marking requirements of the Theft Prevention Standard
(49 CFR 541).
    Pursuant to 49 U.S.C. 33106 and 49 CFR 543.7(b), the agency grants
a petition for exemption from the parts-marking requirements of Part
541, either in whole or in part, if it determines that, based upon
substantial evidence, the standard equipment antitheft device is likely
to be as effective in reducing and deterring motor vehicle theft as
compliance with the parts-marking requirements of Part 541. The agency
finds that GM has provided adequate reasons for its belief that the
antitheft device for the Cadillac XT4 vehicle line is likely to be as
effective in reducing and deterring motor vehicle theft as compliance
with the parts-marking requirements of the Theft Prevention Standard
(49 CFR part 541). This conclusion is based on the information GM
provided about its device.
    The agency concludes that the device will provide four of the five
types of performance listed in Sec.  543.6(a)(3): Promoting activation;
preventing defeat or circumvention of the device by unauthorized
persons; preventing operation of the vehicle by unauthorized entrants;
and ensuring the reliability and durability of the device.
    For the foregoing reasons, the agency hereby grants in full GM's
petition for exemption for the Cadillac XT4 vehicle line from the
parts-marking requirements of 49 CFR part 541, beginning with its model
year (MY) 2019 vehicles. The agency notes that 49 CFR part 541,
Appendix A-1, identifies those lines that are exempted from the Theft
Prevention Standard for a given model year. 49 CFR part 543.7(f)
contains publication requirements incident to the disposition of all
Part 543 petitions. Advanced listing, including the release of future
product nameplates, the beginning model year for which the petition is
granted and a general description of the antitheft device is necessary
in order to notify law enforcement agencies of new vehicle lines
exempted from the parts marking requirements of the Theft Prevention
Standard.
    If GM decides not to use the exemption for this line, it should
formally notify the agency. If such a decision is made, the line must
be fully marked according to the requirements under 49 CFR parts 541.5
and 541.6 (marking of major component parts and replacement parts).
    NHTSA notes that if GM wishes in the future to modify the device on
which this exemption is based, the company may have to submit a
petition to modify the exemption. Part 543.7(d) states that a Part 543
exemption applies only to vehicles that belong to a line exempted under
this part and equipped with the antitheft device on which the line's
exemption is based. Further, Part 543.9(c)(2) provides for the
submission of petitions ``to modify an exemption to permit the use of
an antitheft device similar to but differing from the one specified in
that exemption.''
    The agency wishes to minimize the administrative burden that Part
543.9(c)(2) could place on exempted vehicle manufacturers and itself.
The agency did not intend in drafting Part 543 to require the
submission of a modification petition for every change to the
components or design of an antitheft device. The significance of many
such changes could be de minimis. Therefore, NHTSA suggests that if the
manufacturer contemplates making any changes, the effects of which
might be characterized as de minimis, it should consult the agency
before preparing and submitting a petition to modify.

    Issued in Washington, DC, under authority delegated in 49 CFR
Part 1.95.
Raymond R. Posten,
Associate Administrator for Rulemaking.
[FR Doc. 2017-22660 Filed 10-18-17; 8:45 am]
 BILLING CODE 4910-59-P


[Federal Register Volume 79, Number 37 (Tuesday, February 25, 2014)]
[Notices]
[Pages 10516-10517]
[FR Doc No: 2014-03921]

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

DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

Combined Notice Of Filings

    Take notice that the Commission has received the following Natural
Gas Pipeline Rate and Refund Report filings:

Filings Instituting Proceedings

    Docket Numbers: RP14-467-000.
    Applicants: Gulf South Pipeline Company, LP.
    Description: PAL Neg Rate Agmts Filing (41983, 41984, 41985, 41986,
41989) to be effective 2/12/2014.
    Filed Date: 2/12/14.
    Accession Number: 20140212-5018.
    Comments Due: 5 p.m. ET 2/24/14.

    Docket Numbers: RP14-468-000.
    Applicants: Iroquois Gas Transmission System, L.P.
    Description: 02/12/14 Negotiated Rates--Trafigura (HUB) 7445-89 to
be effective 2/11/2014.
    Filed Date: 2/12/14.
    Accession Number: 20140212-5024.
    Comments Due: 5 p.m. ET 2/24/14.

    Docket Numbers: RP14-469-000.
    Applicants: Northern Natural Gas Company.
    Description: Northern Natural Gas submits for filing a report of
the penalty and daily delivery variance charge (DDVC) revenues for the
period November 1, 2012, through October 31, 2013, that have been
credited to shippers.
    Filed Date: 2/12/14.
    Accession Number: 20140212-5029.
    Comments Due: 5 p.m. ET 2/24/14.

    Docket Numbers: RP14-470-000.
    Applicants: Gulf South Pipeline Company, LP.
    Description: PAL Neg Rate Agmts (41996, 41997, 41998, 42000, 42001,
42004) to be effective 2/12/2014.
    Filed Date: 2/12/14.
    Accession Number: 20140212-5058.
    Comments Due: 5 p.m. ET 2/24/14.

    Docket Numbers: RP14-471-000.
    Applicants: Iroquois Gas Transmission System, L.P.
    Description: 02/12/14 Negotiated Rates--Sequent Energy Management
(HUB) 3075-89 to be effective 2/11/2014.
    Filed Date: 2/12/14.
    Accession Number: 20140212-5091.
    Comments Due: 5 p.m. ET 2/24/14.

    Docket Numbers: RP14-472-000.
    Applicants: Midwestern Gas Transmission Company.
    Description: PAL Negotiated Rate Agreement--NJR Energy Services
Company to be effective 2/13/2014.
    Filed Date: 2/12/14.
    Accession Number: 20140212-5092.
    Comments Due: 5 p.m. ET 2/24/14.

    Docket Numbers: RP14-473-000.
    Applicants: Natural Gas Pipeline Company of America.
    Description: Negotiated Rate Filing--Winsconsin Electric Amendment
to be effective 4/1/2014.
    Filed Date: 2/12/14.
    Accession Number: 20140212-5103.
    Comments Due: 5 p.m. ET 2/24/14.

    Docket Numbers: RP14-474-000.
    Applicants: Iroquois Gas Transmission System, L.P.
    Description: 02/12/14 Negotiated Rates--JP Morgan Ventures Energy
Corp (HUB) 6025-89 to be effective 2/12/2014.
    Filed Date: 2/13/14.
    Accession Number: 20140213-5002.
    Comments Due: 5 p.m. ET 2/25/14.

    Docket Numbers: RP14-475-000.
    Applicants: Iroquois Gas Transmission System, L.P.
    Description: 02/14/14 Negotiated Rates--Trafigura AG (HUB) 7445-89
to be effective 2/13/2014.
    Filed Date: 2/14/14.
    Accession Number: 20140214-5022.
    Comments Due: 5 p.m. ET 2/26/14.

    Docket Numbers: RP14-476-000.
    Applicants: Great Lakes Gas Transmission Limited Par.
    Description: CIAC Agreements to be effective 3/18/2014.
    Filed Date: 2/14/14.
    Accession Number: 20140214-5024.
    Comments Due: 5 p.m. ET 2/26/14.

    Docket Numbers: RP14-477-000.
    Applicants: National Fuel Gas Supply Corporation.
    Description: Fuel Tracker (04/01/14) to be effective 4/1/2014.
    Filed Date: 2/14/14.
    Accession Number: 20140214-5066.
    Comments Due: 5 p.m. ET 2/26/14.

    Docket Numbers: RP14-478-000.
    Applicants: Cameron Interstate Pipeline, LLC.
    Description: Cameron Interstate Pipeline Section 9 Update to be
effective 11/1/2010.
    Filed Date: 2/14/14.
    Accession Number: 20140214-5067.
    Comments Due: 5 p.m. ET 2/26/14.

    Docket Numbers: RP14-479-000.
    Applicants: Equitrans, L.P.
    Description: Rate Schedule NOFT Revisions to be effective 3/31/
2014.
    Filed Date: 2/14/14.
    Accession Number: 20140214-5148.
    Comments Due: 5 p.m. ET 2/26/14.

    Docket Numbers: RP14-480-000.
    Applicants: Iroquois Gas Transmission System, L.P.
    Description: 02/18/14 Negotiated Rates--JP Morgan Ventures Energy
Corp (HUB) 6025-89 to be effective 2/16/2014.
    Filed Date: 2/18/14.
    Accession Number: 20140218-5001.
    Comments Due: 5 p.m. ET 3/3/14.

    Docket Numbers: RP14-481-000.
    Applicants: Tennessee Gas Pipeline Company, L.L.C.
    Description: Rate Schedule PAL to be effective 11/15/2013.
    Filed Date: 2/18/14.
    Accession Number: 20140218-5002.
    Comments Due: 5 p.m. ET 3/3/14.

    Docket Numbers: RP14-482-000.
    Applicants: Natural Gas Pipeline Company of America.
    Description: City of Salem Negotiated Rate to be effective 4/1/
2014.
    Filed Date: 2/18/14.
    Accession Number: 20140218-5003.
    Comments Due: 5 p.m. ET 3/3/14.

    Docket Numbers: RP14-483-000.
    Applicants: Gulf South Pipeline Company, LP.
    Description: PAL Neg Rate Agmt Filing (MacQuarie 42014) to be
effective 2/15/2014.

    Filed Date: 2/18/14.
    Accession Number: 20140218-5066.
    Comments Due: 5 p.m. ET 3/3/14.

    Any person desiring to intervene or protest in any of the above
proceedings must file in accordance with Rules 211 and 214 of the
Commission's Regulations (18 CFR 385.211 and 385.214) on or before 5:00
p.m. Eastern time on the specified comment date. Protests may be
considered, but intervention is necessary to become a party to the
proceeding.

Filings in Existing Proceedings

    Docket Numbers: CP07-398-006.
    Applicants: Gulf Crossing Pipeline Company LLC.
    Description: Abbreviated Joint Application Requesting Amendment of
a Certificate of Public Convenience and Necessity of Gulf Crossing
Pipeline Company LLC, et al under CP07-398, et al.
    Filed Date: 12/19/13.
    Accession Number: 20131219-5247.
    Comments Due: 5 p.m. ET 2/26/14.

    Docket Numbers: CP07-403-002.
    Applicants: Gulf Crossing Pipeline Company LLC.
    Description: Abbreviated Joint Application Requesting Amendment of
a Certificate of Public Convenience and Necessity of Gulf Crossing
Pipeline Company LLC, et al under CP07-398, et al.
    Filed Date: 12/19/13.
    Accession Number: 20131219-5247.
    Comments Due: 5 p.m. ET 2/26/14.

    Docket Numbers: RP13-941-004.
    Applicants: Southern Star Central Gas Pipeline, Inc.
    Description: Rate Case (RP13-941) Interim Settlement Rates Filing
to be effective 2/1/2014.
    Filed Date: 2/12/14.
    Accession Number: 20140212-5090.
    Comments Due: 5 p.m. ET 2/24/14.

    Any person desiring to protest in any of the above proceedings must
file in accordance with Rule 211 of the Commission's Regulations (18
CFR 385.211) on or before 5:00 p.m. Eastern time on the specified
comment date.
    The filings are accessible in the Commission's eLibrary system by
clicking on the links or querying the docket number.
    eFiling is encouraged. More detailed information relating to filing
requirements, interventions, protests, service, and qualifying
facilities filings can be found at: http://www.ferc.gov/docs-filing/efiling/filing-req.pdf. For other information, call<PHONE_NUMBER>
(toll free). For TTY, call<PHONE_NUMBER>.

    Dated: February 18, 2014.
Nathaniel J. Davis, Sr.,
Deputy Secretary.
[FR Doc. 2014-03921 Filed 2-24-14; 8:45 am]
BILLING CODE 6717-01-P


Inlllal pH Final pH Silver Alumlnum Arsenic Boron Barium Berylllum Calcium Cadmium Chromium Copper Iron Potassium Magnesium Manganese Sodium Nickel Lead Selenium Antimony Silicon Strontium Thorium Titanium Thallium Uranium Vanadium Zinc Zhxmlum Mercu@ Table B. 2. Le DH 3 2W Im 2m 3m 12.27 8.33 5,29 6.34 2.96 2.96 2,92 2,85 2,87 2.58 2,88 2.91 : 0.005 0,007 < 0,013 0.005 0.315 0.367 0.471 0.061 : 0.020 < 0.010 < 0,050 < 0.020 : 0.040 < 0.020 < 0,100 0 1,169 : 0,002 c 0,001 < 0.005 0.002 0.002 0.001 0.011 < 0.001 0,121 < 0.041 0.266 0.208 : 0.002 < 0.001 < 0.005 < 0.002 : 0.010 < 0.005 < 0.025 < 0.010 3.07 2.71 1.15 1.53 : 0.100 < 00050 c 0.250 < 0,100 3.59 3,04 4.59 1,73 : 0,040 < 0.020 < 0,100 < 0.040 : 0.002 c 0,001 c 0,006 < 00002 0.213 0.406 0.301 < 0.120 : 0.008 < 0.004 c 0.020 c 0,008 : 0,014 < 0.007 < 0.035 < 0.014 0.036 0.018 0.092 0.023 : 0.020 c 0,010 c 0,050 < 0,020 0.599 0.596 0.459 15,26 : 0.002 < 0.001 < 0.005 < 0.002 : 0,260 < 0,130 < 0.650 0.287 : 0,002 < 0,001 < 0.005 < 0.002 : 0.016 < 0.008 < 0.040 < 0,016 : 0,100 0.075 c 0.250 0.113 : 0.020 < 0.010 < 0.050 < 0,020 0.013 0.011 < 0.025 0.020 : 0,020 < 0,010 < 0.050 < 0.020 723 1337 537 4257 thing results ( milligrams pe pH 5 2W Im 2m 3m 15.34 11.00 11.00 11.33 5,00 5.00 4.63 4.63 5.02 4.69 4.76 4.79 < 0.005 < 0.003 < 0.013 < 0.005 0.225 ` 0,225 0,659 0.205 < 0.020 < 0.010 < 0.050 < 0.020 < 0.040 < 0.020 < 0,100 0! 091 < 0.002 0,001 < 0.005 < 0,002 0.003 0.001 0.012 < 0.001 0.268 0,310 0.223 0.107 < 0.002 < 0.001 < 0.005 < 0.002 < 0.010 c 0.005 c 0.025 c 0.010 3.78 3.33 3,61 3.69 < 0.100 < 0,050 c 0,250 < 0.100 6.11 1.52 7.18 3,78 < 0.040 < 0.020 < 0.100 < 0.040 < 0.002 < 0.001 < 0.006 c 0.002 1396 1210 1482 1425 < 0.008 < 0.004 < 0.020 < 0.008 < ( 3.014 < 0,007 < 0,035 < 0.014 < 0.020 < 0.010 0.052 c 0.020 < 0.020 < 0! 010 < 0.050 < 0! 020 0.559 0.573 0.433 1.98 < 0.002 < 0.001 < 0! 005 < 0.002 < 0.260 < 0.130 c 0.650 < 0,260 < 0.002 < 0.001 < 0,005 < 0.002 < 0.016 < 0.006 < 0.040 < 0.016 < 0.100 0.059 c 0.250 < 0.100 < 0.020 < 0.010 < 0.050 < 0.020 0.021 0.012 c 0.025 0.023 < 0.020 0.011 < 0.050 < 0.020 1368 3986 3111 7745 ter) for the mercury stand: pH 7 2W Im 2m 3m 20.89 14.00 9.00 10,67 7,87 7.87 7.55 7.55 7.28 6,22 6.95 7.39 0.005 < 0.003 < 0.013 < 0,005 0.152 0.056 0.464 < 0.060 0.020 c 0.010 < 0.050 c 0,020 0,040 c 0,020 c 0.100 0,225 0.002 c 0,001 < 0.005 c 0,002 0,003 0,001 0.012 < 0.001 0,080 0.054 c 0.200 < 0,080 0,002 < 0.001 c 0,005 c 0,002 0.010 c 0,005 c 0.025 c 0.010 0.450 0.709 0.552 0.768 0,100 c 0,050 < 0,250 c 0,100 4.75 1.10 7.63 2.83 0,040 c 0,020 < 0.100 < 0.040 0.002 c 0.001 c 0.006 < 0,002 0.232 0.096 0.414 0,272 0.008 < 0.004 c 0.020 c 0,008 0.014 < 0.007 < 0.035 c 0,014 0.024 0,011 0.073 < 0.020 0.020 c 0.010 c 0.050 c 0,020 0.523 0.474 0.442 0,676 0.002 ` c 0.001 c 0.005 < 0,002 0.260 < 0,130 < 0.650 c 0.260 0.002 c 0.001 c 0.005 c 0,002 0.016 < 0,008 < 0,040 c 0,016 0.100 0,063 c 0,250 c 0,100 0.020 c 0,010 < 0.050 < 0.020 0.010 0.010 < 0.025 0.017 0.020 < 0.010 < 0.050 c 0,020 641 2739 1371 3666 rd series 2W Im 2m 3m 12,53 12.53 12.68 12.68 12.73 12.27 12,73 12.79 0.011 < 0.003 0.016 < 0.005 0.205 0.059 0,495 c 00060 0.020 0.010 < 0.050 c 0,020 < 0.040 < 0,020 < 0,100 0,191 0.021 0.014 0! 012 0.012 0.003 0.001 0,012 < 0.001 1328 1235 970 970 < 0.002 < 0,001 < 0,005 < 0,002 0.039 0.016 < 0.025 0.016 0,800 0.380 0.235 0.168 < 0.100 c 0,050 < 0,250 < 0,, 100 7.15 1.13 3.94 2.95 < 0.040 < 0.020 < 0.100 < 0.040 < 0.002 c 0.001 c 0.006 < 0.002 1.336 0.624 0.516 0.415 < 0.008 c 0,004 < 0.020 c 0.008 < 0.014 < 0.007 < 0.035 < 0.014 < 0.020 < 0.010 0.083 c 0.020 < 0.020 < 0,010 < 0,050 < 0.020 1.149 0.909 0$ 686 0.779 1.088 0.819 0,499 0.627 c 0.260 < 0.130 c 0.650 0.264 0.007 0! 005 0.006 c 0.002 c 0.016 < 0.008 < 0.040 < 0,016 0.101 0.069 c 0,250 0.147 < 0.020 < 0.010 < 0.050 < 0$ 020 0.014 0.006 c 0.025 0.016 < 0.020 < 0.010 < 0.050 c 0.020 5231 6594 4534 11259 ` Results are in micrograms per liter. + Time Weight( g)

Inllial pH Final pH Silver Aluminum Arsenic Boron Barium Beryllium Calcium Cadmium Chromium Copper Iron Potassium Magnesium Manganese Sodium Nickel Lead Selenium Antimony Silicon Slrontlum Thorium Titanium Thallium Uranium Vanadium Zinc Zirconium kiwK TaMe B. 3. pH 3 2W Im 2m 3m 7.97 12.18 13.79 14.79 2.96 2.85 3.05 3.05 3.37 3.33 3.76 3.83 < 0.005 2,00 < 0,020 < 0,040 0.011 0.003 677 < 0,002 0.016 c 0.008 7,69 6.85 1.36 0.087 4.71 0.017 c 0.014 < 0.020 < 0.020 4.78 0.244 < 0.260 0.004 C0.016 c 0,100 0,026 0.042 0.022 8,55 < 0,013 < ().() 13 4.58 6.92 < 0.050 < 0.050 < r). lr) o < 0.100 0.029 0.039 0.008 0.014 1063 1249 < o. rJrJ5 < r). oo5 0.033 0.029 < 0,020 < 0,020 12.90 19.60 3.90 9.80 2.53 3.22 0! 139 0.295 7.99 10.22 0.023 0.027 < ().() 35 c r), 035 c 0.050 0.078 c rj, fJ5r3 < r). 05rJ 17,16 29,04 0.346 0.391 < 0,650 < 0,650 0.007 0.007 < 0.040 < 0.040 C o, 250 c 0,250 < rJ, 05r3 c r3405rJ 06133 0.169 < ().() 50 < 0.050 41.3 c 0.050 < 0.005 6.65 < (). 02()

0.153 0.035 < 0.001 1334 < (). orjp 0.032 < 0.008 17,57 7,05 3.89 0.363 9.79 0.034 < r3, r) 14 < rj. 02r_ l < r). opr)

34.33 0,562 c 0.260 < (),() 02 0.016 < rJ. lrJ( J 0.038 0.421 < 0.020 5.86 Leaching results ( milligram: pH 5 2W Im 2m 3m 11.76 11.03 12.72 12.10 5.00 5.06 < 0.005 c 0.060 < 0.020 < 0,040 0.021 0.003 977 < 0.002 < 0.010 c 0,008 3.46 9.43 1.46 0.089 1379 0.015 < 0.014 < 0.020 < 0.020 10.54 0.361 c 0.260 0.006 c 0.016 < 0.100 0.025 0.06 0,031 38.16 4,63 4.89 4.89 4.61 5.06 5.20 < 0,013 < ().() 13 0.011 0.647 0.757 0.161 < 0.050 < 0.050 0.032 < o, lr) r) c rJ, lr) rj < & r) 40 0.029 0.035 0.044 0.009 0.013 c 0.001 986 1155 1136 < 0.( 11) 5 < r). r305 0.003 < 0,025 c 0.025 0.016 < 0.020 < 0.020 C o, oot3 7,67 5,56 5,91 4.38 11.50 7,50 2.08 2.49 8.22 0.142 0.144 0,167 1515 1341 1311 < r), rJ2r) 0.021 0,025 < 0,035 < 0,035 c 0.014 < rj, r) 50 c r), rJ5rJ c 0,020 < 0,050 c o, rJ50 0.032 16,84 23.26 26.20 0.287 0.320 0,676 < 0,650 < 0.650 1.559 0.006 0.006 < 0.002 < 0.040 < 0.040 0.030 c 0,250 < 0,250 0.570 < 0.050 < 0.050 0.053 0,47 1.302 36,41 0,052 c 0.050 < 0.020 54.0 20.38 10.44 ? er liter) for the LANL series pH 7 2W Im 2m 3m 8.28 11.56 19.29 16.04 7.87 7.55 8.06 8.06 5.83 6.08 7.07 5.62 : 0.005 0.126 : 0.020 : 0.040 0.012 0.003 645 : 0,002 c 0.010 : 0.008 : 0,100 7.30 0.57 0.004 4.50 : 0.008 : 0.014 : 0,020 : 0.020 8.78 0,227 : 0.260 0.004 : 0.016 : 0.100 : 0.020 0,010 0,024 8.20 < (). rJ13 0.207 < o. 05rJ < r). lol)

0.023 0.009 926 < (). r)() 5 c 0.025 < O, r) po c 0,250 3.14 0.82 0.007 7.22 < 0.020 < (). 035 < o. 05r)

< 0.050 14.81 0.282 < 0,650 0.005 < rJ, 04( J c o. 250 < r3. r350 < 0.025 < (). 05r)

7.44 < (). r) 13 0.371 < r3.050 ° < 0.100 0.034 0,009 1481 < 0.005 < 0.025 0.022 < 0.250 9.10 1.356 0.087 12.12 < 0,020 < 0,035 0.055 < 0.050 22.04 0.500 c 0,650 0.007 < 0.040 c 0.250 < 0.050 0.092 c 0,0513 52 < ( J. or) 5 < 0.060 < (),() 20 0,139 0.026 < (). 001 1382 < (). 002 < O. ol( l < 0,008 < 0.100 6.12 1.32 0.011 9.32 c 00008 < (),() 14 < 0.020 < (), r) zr)

23.73 0.562 < 0,260 < 0.002 0.019 0.156 0.021 0.050 < 0,020 21.0 PH 12.5 2W Im 2m 3m 9.08 9.09 13.34 15.68 12.53 12.68 12.48 12.48 12.60 12.20 10.66 9.59 < 0.005 0.013 c 0.013 0.006 0.132 0.236 0.543 c 0.060 < 0.020 < 0.050 < 0,050 0.023 < 0.040 < 0. lOO < 0.100 0.130 0.037 0.062 0.087 0.096 0,003 0.008 0.012 0.002 1653 1637 1610 2033 < 0.002 < 0,005 < 0.005 0,003 0.013 c 0.025 c 0.025 < 0.010 c 0.008 0.040 0.037 c 0.006 < 0.100 < 0,250 c 0.250 < 0,100 6.16 3,92 9.87 7.46 0.042 c 0.100 0,112 0.521 < 0.002 0.007 < 0.006 0.004 6.06 7.08 9.38 11.15 < 0, oo8 < 0,020 < 0,020 0.011 < 0.014 < 0,035 < 0,035 < 0.014 < 0.020 < 0.050 0.073 < 0.020 < 0.020 < 0,050 < 0.050 < 0,020 1,16 1.45 4.59 20,52 1.17 1.18 1.09 1.46 c 0.260 c 0.650 c 0,650 0.273 0.009 0.010 0.009 < 0.002 < 0.016 < 0,040 c 0.040 0.023 c 0.100 c 0.250 c 0.250 0.218 < 0.020 < 0,050 < 0.050 0.025 c 0.010 c 0.025 < 0.025 0.068 0,032 c 0.050 c 0.050 < 0.020 8.62 5,86 12.83 11,57 ` Results are in micrograms per liter. FTime Weight( g)

Inltlal pH Final pH Silver Aluminum Arsenic Boron Barium Beryllium Calcium Cadmium Chromium Copper w Iron ~ Potassium Magnesium Manganese Sodium Nickel Lead Selenlum Antimony Sllicm Strontium Thorium Titanium Thallium Uranium Vanadium Zinc Zirconium lK! Q .   Table B. pH 3 m Im 2m 3m 8,66 15.38 15.01 16.11 2,96 3.41 : 0.005 0.310 : 0,020 : 0.040 0.006 0.003 1261 : 0,002 : 0.010 0.012 1,51 7.48 5.23 0,024 17.42 : 0.008 : 0.014 0.024 : 0.020 3.22 0,431 0.260 0.007 00016 : 0.100 0.020 0.023 0.026 2.85 3.05 4,43 4.65 < OJJI) 5 < 0.013 0.220 0.200 <().() 20 < 0.050 < 0.040 < 0.100 0.024 0.027 0.003 0.003 2225 2061 < o, orJ2 < (), 005 0.019 < 0.025 < 0.008 0.025 2.35 1.62 3.28 6.94 9.59 9.30 0.043 0,029 26,46 25,56 0.008 cO. 020 < 13,014 < ( 3.035 c 0.020 < 0.050 < (), 020 < 0.050 5.99 7.02 0,874 0.615 < 0.260 c 0.650 0.012 0.014 < 0.016 < ( 3.040 0.113 0.337 0.027 < 0.050 0.012 0.260 0.042 < 0.050 3.05 4.71 < (),()() 5 0.145 0,021 0.158 0,024 < r). ol) l 2151 < 0,()() 2 0.015 < 0.008 1.98 2.68 9.93 0.032 29,11 < oooo8 < 0.014 < 0,020 < 0.020 7,20 0.869 0.408 < (). 002 < 0, o16 0.265 0.020 0.036 < 0.020 12.33 4.47 5.03 80.2 . . . . pH 5 2W Im 2m 3m 10.47 27,78 19.33 18.80 Leaching results ( milligrams per liter) for the FERN series pH 7 2W Im 2m 3m 10.70 22.07 20,40 20,36 5.00 4.63 5,04 5,96 : 0.005 < 0,005 : 0.060 c 0,060 0,022 0.026 : 0.040 c 0.040 0.011 0,055 0.004 0.003 1596 3313 : 0.002 < 0.002 : 0.010 < 0,010 0.014 0.009 1.863 0! 980 4.56 5.94 6.73 6,28 0.022 0.016 1483 1362 : 0,008 c 0,006 : 0.014 < 0,014 : 0.020 c 0.020 : 0.020 < 0.020 3.43 11.19 0,591 1.531 0.260 < 0.260 0.009 0.017 0.016 c 0,016 : 0.100 0,121 : 0,020 < 0.020 0.01 < (). 01 0.025 0.040 4,89 4.89 7.43 7.36 < 0.013 c 0,005 c 0.150 c 0.060 < 0.050 0.023 < 0.100 < 0.040 0.037 0.031 < 0! 003 c 0.001 2344 2207 < 0.005 < 0.002 c 0.025 c 0,010 0,030 < 0.008 c 0,250 c 0,100 9.66 4.57 3.12 1.25 0.024 < 0.002 1470 1316 < 0.020 c 0.008 < 0.035 < 0,014 < 0.050 c 0.020 < 0.050 < 0,020 8,40 7.09 0,784 0.913 < 0.650 0.281 0.014 c 0,002 0.049 c o, of6 0.277 0,288 < 0.050 < 0.020 0,060 0.011 0.056 < 0.020 10.07 28.3 125 184 7,87 9.08 < 0.005 0.201 < 0,020 < 0.040 0,006 0.004 1547 < 0,002 < 0,010 0,012 < 0.100 4,38 0.22 c 0.002 24,2 : 0.006 c 0.014 : 0,020 : 0,020 4.45 0,554 : 0.260 0.008 : 0.016 < 0.100 < 0,020 < 0.010 0,026 15.7 7.55 9.02 0,013 0.160 < o. ozr)

< 0.040 0.022 0.003 3373 < ( J. 002 < 0.010 0,049 < 0.100 4.69 0.56 0.005 44.2 0.030 < 0.014 < 0.020 0.057 5.71 1,355 < 0.260 0.013 < 0.016 < (). 1() 0 0.172 c ().() 10 0.220 73.0 8.06 9.01 0.016 0.189 0.056 < 0.100 0.033 0.004 2876 < (), 005 < 0.025 0.054 c 0.250 9.64 0.556 < 0.006 40.0 < 0.022 < 0,035 < 0.050 < 0.050 6.89 0,920 < 0,650 0.014 0,114 c 0,250 0.092 0.046 0.062 200 8,06 7.29 < 0.005 < 0,060 0,020 0.178 0.030 < o. or) l 2301 < 0.( 1( 12 < (). 01()

< 0.006 < 0.100 4.61 0.621 < (). 003 37,37 < 0.008 < (),() 14 < 0.020 < 0.020 7.90 0.969 0.382 < (),() 02 0.017 0.303 < (), 020 0.014 < 0,020 107.8 pH 12.5 2w Im 2m 3m 7,72 17.53 20,94 16.26 12,53 12.68 12,48 12.48 12,56 12,39 10.27 9.23 c 0,005 0.013 0.027 < 0,005 0.170 0.161 0.281 c 0,060 0.022 0.021 < 0.050 0.027 < 0,040 < 0.040 < (). 1() 0 0.203 0.022 0.036 0.039 0.047 0.004 0.003 0.004 < 0,001 2018 5070 4614 4219 < ().() 02 < 0.002 < (),() 05 < r), of) z 0. O1O < 0.010 0.033 < 0.010 0.027 0,057 0.096 < 0.008 < 0.100 c 0,100 < 0.250 < 0.100 6.15 4,54 14.40 7.73 0.051 0.322 0,850 0.611 < 0.002 0.005 c 0.006 c 0.002 16.6 35.1 42.7 36.18 < 0.008 0.024 0.032 c 0. oo6 < 0,014 < 0.014 c 0,035 < 0,014 < 0.020 < 0,020 < 0,050 < 0.020 < 0.020 0,047 0.054 < 0.020 1,11 2.33 4.46 5,30 1.26 2,69 2.08 2,23 : 0.260 < 0,260 < 0.650 0.629 0.011 0.024 0.019 < 0,002 : 0.016 < 0,016 0.127 0.028 < 0,100 c 0.100 c 0.250 0.466 < 0.020 0! 139 0.193 < 0,020 < (). 010 < Ooolrj 0.038 < 0,010 < 0.020 0.154 0.204 c 0,020 15.1 42.0 1223 2G4 " Results are in micrograms per liter.  . .

Time Weight( g)

Initial pH Final pH Silver Aluminum Arsenic Boron Barium Beryllium Calclum Cadmium Chromium Copper Iron Potassium Magnesium Manganese Sodium Nickel Lead Selenlum Antimony Silicon Strontium Thorium Titanium Thalllum Uranium Vanadium Zinc Zirconium Mercurya Table B pH 3 2W Im 2m 3m 24.25 4.66 11.39 9.55 2,96 2,85 3.05 3.05 5.83 5.20 6.31 6.54 < 0.005 c 0.013 c 0,013 0.203 0.520 0.270 < 0.020 < 0.050 < 0.050 0.258 0.188 0.293 < 0.002 < 0.005 < 0.005 0.004 0.006 0.007 8.36 3.26 5.63 < 0.002 < 0.005 c 0.005 < 0.010 0,039 < 0.025 < 0.008 < 0.020 c 0.020 1,206 < 0.250 c 0,250 6.65 1.81 7.01 1049 414 817 0.060 00081 0.174 483 138 223 < 0.008 < 0.020 < 0.020 < 0.014 < 0,035 < 0.035 < 0.020 < 0.050 < 0.050 < 0,020 < 0,050 < 0.050 1,265 1.084 0.692 0.023 0,008 0,016 < 0.260 < 0.650 < 0.650 < 0! 002 < 0! 005 c 0.005 c 0.016 c 0.040 < 0.040 c 0.100 < 0.250 c 0.250 c 0,020 < 0.050 < 0.050 156 276 200 0.140 0.246 0.166 16.0 76 4.47 < 0,005 < 0.060 c 0,020 0.432 0.004 c 0.001 4.91 c 0.002 < r), olr)

< 0.008 0.636 4.83 915 0.069 238 < 0,008 < 0.044 0.021 0.021 0,294 0.014 < 0,260 < 0.002 < 0,016 0.102 < 0.020 110 < O, t) zl)

62.5 5. Leaching results ( milligr: DH 5 2W Im 2m 3m 30.68 8,76 8.47 9.74 5,00 4.63 4.89 4.89 7.59 5.49 6.60 7.30 < 0.005 < 0.013 < 0.013 < 0.005 < 0.060 0,219 < 0,150 < 0.060 < 0.020 < 0$ 050 < 0.050 < 0.020 < 0.040 < 0! 100 < 0.100 < 0.040 0.004 c 0,005 c 0.005 0.004 0.004 0.007 9.79 5,37 < 0.002 < 0.005 < 0.010 < 0.025 < 0.008 < 0.020 0.185 < 0,250 9.25 2.30 468 509 0.005 0.025 1954 1569 < 0.008 < 00020 < 0.014 < 0,035 < 0.020 < 0.050 < 0.020 < 0$ 050 0.893 0,794 0.029 0.014 < 0.260 < 0.650 < 0,002 c 0.005 c 0.016 < 00040 < 0.100 c 0.250 < 0.020 c 0,050 75.1 166.2 0.089 0,168 0.006 c 0.001 4.70 4.48 < 0.005 < 0.002 c 0.025 c 0.010 < 0,020 < 0, oo8 c 0.250 0.123 7.53 3.05 391 471 0.121 0.003 1477 1464 c 0.020 c 0.008 < 0,035 c ().( 314 < 13,050 < (), 020 < 0.050 < 0.020 0.446 0.423 0,014 0.013 < 0,650 < 0.260 < 0.005 c 0,002 < 0.040 < 0.016 c 0.250 c 0.100 < 0.050 c 0,020 67,1 33.4 0.072 c 0.020 12,9 108.5 34.3 213 ns ~ er liter) for the OR series t) H 7 2W Im 2m 3m

17.60 5.46 8.10 8.99 7.87 7.55 8.06 8.08 10.50 10.36 10,71 10,69 ...

: 0.005 c 0,013 c 0.013 c 0,005 0! 155 0.362 0.271 < 0.060 : 0.020 c 0.050 c 0.050 < 0.020 0.116 0.105 0.149 0.291 : 0,002 c 0,005 c 0,005 c 0,002 0! 004 0.007 0.009 < 0.001 3.23 1.29 1.40 1.13 : 0.002 c 0.005 < 0.005 c 0.002 : 0,010 c 0.025 < 0,025 < 0,010 : 0,008 < 0.020 c 0.020 0.009 : 0,100 c 0,250 c 0.250 < 0,100 5,20 1.30 8.78 9.79 52.03 21.82 16,49 13.86 : 0.002 c 0,006 0.117 < 0,002 323 100 155 173 : 0.008 c 0.020 c 0.020 c 0.008 : 0,014 c 0,035 c 0,035 c 0,014 : 0,023 < 0.050 < 0,050 < 0.020 : 0.020 c 0,050 < 0.050 ` c 0.020 0,748 0.728 0.397 0.326 0.008 < 0.005 0.005 0,003 : 0,260 c 0,650 c 0.650 c 0.260 : 0,002 < 0,005 c 0.005 c 0.002 : 0,016 < 0.040 < 0.040 < 0,016 : 0,100 c 0.250 c 0.250 c 0,100 : 0.020 c 0,050 c 0.050 < 0.020 00116 0,345 0.185 0,136 : 0,020 c 0.050 c 0.050 < 0.020 4.46 21.5 < 0.050 7.25 Pti 12.5 2W Im 2m 3m 16.32 6,64 8.32 12.27 12.53 12.53 12.48 12.48 12.52 12.22 12.25 12.03 : 0,005 0.181 : 0,020 0.407 0.016 0.004 989 : 0,002 0.010 0.006 : 0.100 7.42 0.051 : 0.002 312 : 0,008 : 0.014 : 0.020 : 0.020 2.086 0.796 : 0.260 0.005 : 0.016 : 0,100 : 0.020 2.77 : 0.021 52.5 < r). ofl 3 0.366 < r). r35( 3 0.205 0.010 0.007 568 < (). 0() 5 c 0,025 < rJ, 02rJ < 0.250 2.32 0.107 < 0.006 123 < (). 020 < 0,035 < r). 050 < 0,050 1.214 0.453 < 0.650 0.005 < 0.040 c 0.250 < r3.050 1.70 < 0.050 81.2 < 0,013 0.006 0,232 < 0,060 < ( 3.05r) < rJ. 02( l 0,280 0,468 0.016 0.016 0.007 < 0.001 588 561 < 0.005 < 0.002 < 0.025 c 0.010 0.021 < 0.008 < 0,250 c 0.100 12.88 4.55 < OOlr)() 0.079 0.116 c 0.002 168 233 < 0,020 < 0, oo8 < 0,035 < 0.014 < 0,050 < (), 02()

< (),() 50 < o, r320 0.966 0.582 0.665 0,742 < 0,650 < 0,260 < 0,005 < 0.()() 2 = 0.040 c 0.016 c 0, z50 0.112 < ( 3. rj54 < ( 3.020 1.59 0.97 < 0.050 < 0.020 14.23 24.2 ` Results are in micrograms per liter. l Time Weight( g)

Inltlal pH Final pH Silver Alumlnum Arsenic Boron Barium Beryllium Calcium Cadmium Chromium Copper w Iron & Potassium Magneslurn Manganese Sodium Nickel Lead Selenium Antimony Slllcon Strontium Thorium Tltanlum Thalllum Uranium Vanadium Zinc Zirconium Mercurya Table B pH 3 2W Im 2m 3m 7.00 5,37 5.38 6.07 2.96 2.85 2.92 2,92 4.84 6.02 5,68 8.75 : 0,005 < 0.005 c 0,013 < 0,005 0,185 0.107 0.199 c 0.060 : 0.020 c 0.020 c 0,050 c 0.020 0.377 0.900 0.688 0! 971 0.017 0.026 0.026 0.035 0.003 0.003 0.004 < 0,001 13,31 16.49 14.86 13.21 : 0,002 c 0.002 c 0,005 < 0.002 : 0.010 c 0.010 c 0.025 c 0,010 : 0,006 < 0.008 < 0.020 c o, oo8 0.616 1.282 0.366 0,622 8! 61 4.15 8.42 5.40 768 1229 1083 1346 0.026 0.050 0.152 0.004 826 683 634 614 : 0.008 < 0.008 < 0.020 c 0.008 : 0,014 c 0.014 c 0.035 < 0.014 : 0,020 c 0,020 c (). 050 0.021 : 0,020 c 0.020 c 0,050 0.022 1.417 1.754 1.001 0,449 0.081 0.067 0.061 0.045 : 0,260 < 0,260 < 0.650 < 0,280 0.002 0.002 < 0.005 < 0,002 : 0,016 c 0,016 < 0,040 c 0,016 : 0.100 < 0.100 < 0.250 < 0.100 ~ 0.020 < 0,020 c 0.050 c 0,027 132.9 101.7 212.3 12.6 0.121 0.112 0.189 0.05 210 192 293 8.2 i. Leaching results ( milligrar pH 5 2W Im 2m 3m 7.13 5.65 6.22 4.90 5.00 4.63 4.72 4.80 7.32 5.54 7.56 7.59 < (),() 05 < 0,()() 5 < (),() 13 < (),() 05 < 0,060 < 0,060 < 0,150 < 0,060 < 0.020 < 0.020 < 0,050 < 0.020 < & r) 40 0.056 0.166 0.183 0.017 0,021 0,026 0,026 0,003 0.003 0.003 < 0,001 10.47 14.51 15.25 12.73 < (). 002 < (), 0() 2 < 0,005 < r), ooz c 0.010 c 0.010 < 0,025 < 0.010 < 0. oo8 < 0, oo8 < 0.020 < 0, oo8 < 0.100 0.258 < 0.250 0.107 12,33 4.224 7.14 4,24 381 536 587 524 0,008 0,008 0,116 < 0,002 1976 1845 2079 1606 < 0.008 c 0.008 c 0.020 c 0.008 < 0.014 < 0.014 < 0,035 c 0.014 < 0.020 < 0.020 < 0,050 < 0! 020 < 0,020 c 0,020 < 0.050 < 0.020 1.138 1.155 0.745 0.342 0.046 0.060 0.070 0.051 c 0,260 c 0,260 < 0.650 c 0,260 : 0! 002 < 0.002 < 0,005 < 0.002 : 0.016 < 0,016 < 0.040 c 0.016 : 0.100 c 0.100 c 0,250 < 0.100 : 0.020 < 0.020 c 0,050 c 0.020 72.42 70,48 58.02 36.4 0.078 0$ 084 0.078 0.039 65.0 133 80.0 288 s per liter) for the ID series pH 7 2W Im 2m 3m 5.41 4,95 15,28 7,51 7.87 7.55 8.06 6.06 10.51 10.35 10,64 10.74 < 0.005 < 0,005 < 0,013 < 0,005 0.110 00080 c 0.150 0,092 < 0.020 < 0.020 < 0,050 < 0,020 0.363 0.719 1.033 1.228 0.010 0.012 0,015 0,017 0.003 0,003 0.005 c 0,001 4.39 4.71 7,66 4.18 < 0.002 < 0.002 < 0.005 < 0.002 < 0.010 < 0.010 c 0.025 < 0.010 c 0.008 c 0,006 < 0.020 < 0,008 < 0.100 c 0.100 < 0,250 c 0.100 8.24 2.87 9.61 11.7 25.6 21,3 35.1 16.6 c 0.002 < 0,002 0.109 < 0.002 646 561 1866 960 c 0.008 < 0.008 < 0,020 c 0,008 < 0.014 < 0.014 < 0,035 < 0.014 c 0.020 < 0$ 020 < 0.050 < 0.020 : 0.020 < 0,020 < 0.050 c 0,020 0.921 0.873 0.896 0.646 0.025 0.026 0.058 0.027 : 0.260 < 0,260 < 0,650 c 0,260 : 0.002 < 0.002 < 0.005 < 0.002 : 0.016 < 0,016 < 0.040 < 0,016 : 0.100 c 0.100 < 0,250 < 0.100 : 0.020 < 0,020 c 0.050 0,026 0.063 0.112 0.129 0.107 < 0.020 < 0.020 < 0.050 0,058 13.4 10.6 < 0,050 9.38 PH 12.5 2W Im 2m 3m 5,50 5.21 4.77 5.75 12,53 12.53 12.61 12.61 12,41 12.19 12.72 12.84 < 0.005 < 0,005 0.028 c 0.005 0.122 0.063 0,152 c 0.060 < 0.020 < 0! 020 < 0.050 < 0.020 1.46 1.33 1.58 1.56 0.027 0.034 0.053 0.054 0.003 0.003 0.003 c 0.001 709 540 1057 1048 < 0.002 < 0! 002 < 0,005 < 0.002 c 0.010 c 0,010 c 0.025 < 0.010 0,037 < 0,008 c 0.020 c 0.008 : 0.100 c 0.100 c 0.250 c 0.100 8.32 4.41 7.49 4.39 0.094 0.107 0.117 0.108 : 0.002 < 0,002 0.112 < 0.002 640 491 524 602 : 0.008 c 0,008 c 0,020 c o. oo8 : 0.014 < 0.014 < 0,035 < 0.014 : 0.020 < 0.020 < 0.050 < 0.020 : 0.020 < 0,020 < 0.050 < 0.020 1,132 1.112 1.637 0.732 0.701 0.571 0.610 0.655 : 0,260 c 0,260 c 0,650 < 0.260 0.004 0.003 < 0,005 c 0.002 : 0.016 c 0.016 < 0.040 < 0.016 : 0,100 c 0,100 c 0.250 < 0.100 : 0.020 0.021 < 0.050 0.020 4.03 1.34 2.31 2.27 c 0.020 0.028 0.052 0.021 33.1 70.2 406 110 ` Results are in micrograms per liter, 0RNIJTM 13728 INTERNAL DISTRIBUTION 1. T. B: Co& ey 2. J. Devore 3. R. M. Barrington 4. C. M. Kendrick 5. P. Kirk 6. K. T. ~~ SOIl 7 11. C. H. Mattus 12. M. I. Morris  13. T. E. Myrick 14. S. M. Robinson 15. R. D. Spence 16. Central Research Library 17. Laboratory Records  RC 18 19. Laboratory Records  for submission to OSTI EXTERNAL DISTRIBUTION 20. John Austiq U. S. EPA OSW/ 5302W, 401 M Street, WashingtorLDC20460 21. Heather Holmes Bums, Westinghouse Savannah River Company, P. O. Box 616,724 21E, Aikeu South Carolina 29862 22. Mary Cunningham, U. S. EP& OSW/ 5302W, 401 M Stree~ Washington, DC 20460 23. Ron Fontan~ DOE Idaho Operations, 850 Energy Drive, Idaho Falls, Idaho 83401 1235 24. G. A. Hulet, Idaho National Engineering and Environmental Laboratory, 2525 N. Freemon~ Idaho Falls, Idaho 83415 3875 25. D. A. Hutchins, U. S. DOE, 55 Jefferson Avenue, MS EW97, Oak Ridge, Tennessee 37830 26. Norm Jacobs, Nuclear Fuel Services, 1205 Banner Hill Roa& Erw@ Tennessee 37650 27. Datid S. KossorL Rutgers University, Department of chemical and Biochemical Engineefig, 98 Brett Roa& Engineering Bldg., C 258, Piscataway, New Jersey 98854 8058 28. Josh Lewis, U. S. EPA OSW/ 5302W, 401 M Street, WashingtoIL DC 20460 29. Cavanaugh Mirns, U. S. DOE, 55 Jefferson Avenue, MS EW 97, Oak Ridge, Tennessee 37830 30. Bill Owe% DOE Idaho Operations, 2525 N. Freemont, Idaho Falls, Idaho 83415 3875 31. Lynn Schwendirmq DOE Idaho Operations, 2525 N. Freemong Idaho Falls, Idaho 83415 8102 32. Robin M. Stewart, ADA Technologies, Inc., 304 Inverness Way South, Suite 365, EnglewOO& c. olo~ o 80112 33. R. Eric Williams, Idaho National Engineering and Environmental Laboratory, 2525 N. Freemon~ Idaho Falls, Maho 83415 3875


[Federal Register Volume 80, Number 118 (Friday, June 19, 2015)]
[Notices]
[Page 35346]
[FR Doc No: 2015-15107]

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

DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. ER15-1914-000]

87RL 8me LLC; Supplemental Notice That Initial Market-Based Rate
Filing Includes Request for Blanket Section 204 Authorization

    This is a supplemental notice in the above-referenced proceeding of
87RL 8me LLC's application for market-based rate authority, with an
accompanying rate tariff, noting that such application includes a
request for blanket authorization, under 18 CFR part 34, of future
issuances of securities and assumptions of liability.
    Any person desiring to intervene or to protest should file with the
Federal Energy Regulatory Commission, 888 First Street NE., Washington,
DC 20426, in accordance with Rules 211 and 214 of the Commission's
Rules of Practice and Procedure (18 CFR 385.211 and 385.214). Anyone
filing a motion to intervene or protest must serve a copy of that
document on the Applicant.
    Notice is hereby given that the deadline for filing protests with
regard to the applicant's request for blanket authorization, under 18
CFR part 34, of future issuances of securities and assumptions of
liability, is July 6, 2015.
    The Commission encourages electronic submission of protests and
interventions in lieu of paper, using the FERC Online links at http://www.ferc.gov. To facilitate electronic service, persons with Internet
access who will eFile a document and/or be listed as a contact for an
intervenor must create and validate an eRegistration account using the
eRegistration link. Select the eFiling link to log on and submit the
intervention or protests.
    Persons unable to file electronically should submit an original and
5 copies of the intervention or protest to the Federal Energy
Regulatory Commission, 888 First Street NE., Washington, DC 20426.
    The filings in the above-referenced proceeding are accessible in
the Commission's eLibrary system by clicking on the appropriate link in
the above list. They are also available for electronic review in the
Commission's Public Reference Room in Washington, DC. There is an
eSubscription link on the Web site that enables subscribers to receive
email notification when a document is added to a subscribed docket(s).
For assistance with any FERC Online service, please email
<EMAIL_ADDRESS>or call<PHONE_NUMBER> (toll free). For TTY,
call<PHONE_NUMBER>.

    Dated: June 15, 2015.
Kimberly D. Bose,
Secretary.
[FR Doc. 2015-15107 Filed 6-18-15; 8:45 am]
 BILLING CODE 6717-01-P