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35.1 INTRODUCTION 35.1.1 Objectives
If plant systems, structures, or components (SSCs) are found
tobe degraded, nonconforming, or subject to an unanalyzed
condi-tion during operation, an evaluation of their functionality
or oper-ability is necessary for the nuclear power generating
station tocontinue operating safely. This evaluation establishes
the abilityof the SSCs to perform their assigned safety functions.
This chap-ter discusses the methodology and acceptance criteria
applicableto this evaluation. It introduces typical SSCs that may
requireoperability evaluations and also provides definitions
related tooperability. Examples of the operating conditions and
events toconsider are described, as are the evaluation methods and
accep-tance criteria for short- and long-term operability.
Several references were used in the preparing the material
pre-sented in this chapter; the most significant of which
include:
(1) USNRC RIS-2005-20 [27](2) ASME B&PV Code, Section XI
[7](3) ASME B&PV Code, Section III, Appendix F [8](4) ASME
O&M Code [9] (5) USNRC Inspection Manual Part 9900 [15]This
chapter discusses basic concepts, definitions, evaluation
methods, and acceptance criteria from these documents as
theyrelate to mechanical systems, their components and
structures.
35.1.2 Operability and FunctionalityIn U.S. regulatory space
[15], operability determinations are
associated with SSCs described in the plant technical
specifica-tions (TSs) and form the basis for compliance with
regulatoryrequirements and limiting conditions for operation. The
scope ofSSCs considered within the operability determination
processinclude: SSCs required to be operable by TSs and SSCs that
arenot explicitly required to be operable by TSs, but that
performrequired support functions. Conversely, functionality
assess-ments are performed for SSCs not described in the plant
TSs.
From a practical standpoint these distinctions serve as a
meansdifferentiating the evaluation processes employed to assess
the fit-ness for service if safety related and non-safety related
SSCs. Infact the fundamental basis for either operability or
functionalityrests in the measure of the SSCs capability to perform
its intend-ed function(s). For the most part the technical
evaluation methods
and acceptances criteria employed to make these determinationare
common for technical specification and non-technical specifi-cation
SCCs.
35.1.2.1 Operable /Operability. The U.S. NRC StandardTechnical
Specifications [28, 29, 30, 31, 32, 33] define operable/operability
as follows:
A system, subsystem, train, component, or device shall
beOPERABLE or have OPERABILITY when it is capable ofperforming its
specified safety functions, and when all neces-sary attendant
instrumentation, controls, normal or emergencyelectrical power,
cooling and seal water, lubrication and otherauxiliary equipment
that are required for the system, subsys-tem, train, component, or
device to perform its function(s) arealso capable of performing
their related support function(s).Several variations of the
preceding definition exist in the plant
specific Technical Specifications. In all cases, however, a
licenseesplant-specific definition should be accepted as governing
how oneapplies the terms operable and operability. The specified
functionsreferenced in the foregoing definition are the specified
safetyfunctions described in the current licensing basis for the
facility.The following are some examples of specified safety
functions forseveral SSCs.
For piping:
(1) structural integrity where structural failure would
interfere withother systems being able to perform their safety
functions;
(2) pressure integrity to the extent that leakage is limited to
lev-els permitted by the licensing basis and through-wall
flawsremain stable when subjected to faulted loads; and
(3) ability to pass required flow rates.For supports:
(1) Motion control of the system or component within the lim-its
required for the system or component to perform its safetyfunction
or else to maintain the structural integrity of thesystem or
component.
For valves:
(1) pressure integrity to the extent that leakage is limited to
lev-els permitted by the licensing basis;
FUNCTIONALITY ANDOPERABILITY CRITERIAStephen R. Gosselin and Guy
H. DeBoo
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(2) structural integrity; and (3) the ability to open or close
as required in the licensing basis.In addition to providing the
specified safety functions, a sys-
tem, subsystem, train, component, or device (referred to as
systemin this section) is expected to perform as designed, tested,
andmaintained. When system capability is so degraded that it
cannotperform with reasonable certainty or reliability, the system
shouldbe judged inoperable even if it is shown to provide the
specifiedsafety functions [15]. Required action ranges included in
theacceptance criteria of ASME O&M Code [9] or Section XI [7]
areexamples of degraded capabilities for SSCs. Plant
TechnicalSpecifications also contain limiting values, such as
leakage rateand set point pressure, for component performance.
These valuesconstitute the technical specification-based
operability verificationcriteria that, if they are not met,
necessitate the entering of theapplicable limiting Condition for
Operation (LCO) and AllowedOutage Times (AOTs).
In some cases, the ASME O&M Coderequired or
SectionXIrequired action ranges for certain components may be
moreconservative than the plant technical specification limits.
However,the component in question must be declared inoperable even
if theexisting performance meets the technical specification safety
limitbecause of the imposed ASME operability limit. An example is
apump that is capable of delivering rated flow but exhibits
vibrationin excess of the reference values and falls in the
required actionrange.
The discussion in this section accentuates the often
complex,sometimes inconsistent, nature of operability concepts and
criteria.Common practice involves a process having a consensus of
regula-tor viewpoints, plant-specific technical specification
requirements,applicable Codes and Standards, regulatory
commitments, andother licensing-basis compliance requirements.
The general scope of SSCs that might require operability
deter-minations include:
(1) Safety-related SSCs that are relied upon to: (a)
ensurereactor-coolant pressure boundary integrity; (b) shut
downand/or maintain the reactor in a safe shutdown condition; or(c)
prevent or mitigate the consequences of accidents thatcould result
in potential offsite exposure comparable to theguidelines in 10 CFR
50.34(a)(1), 50.67(b)(2), or 100.11, asapplicable [11].
(2) SSCs whose failure could prevent any of the SSCs
identifiedin (a), (b), and (c) from performing their require
functions.
(3) SSCs that are required to function by safety analyses
orplant evaluations that are a part of the current licensingbasis.
These analyses and evaluations include those that aresubmitted to
support any license amendment requests,exemption requests, or
relief requests, and also those sub-mitted to demonstrate
compliance with regulations such asfire protection in 10CFR50.48,
environmental qualification(in 10CFR50.49, pressurized thermal
shock (in 10CFR50.61),anticipated transients without scram in
10CFR50.62, andstation blackout in 10CFR50.63 [11].
(4) SSCs that are subject to: 10CFR50, Appendix B;
10CFR50,Appendix A, Criterion 1; plant facility Technical
Specifi-cations; or plant Technical specifications through the
defin-ition of operability (i.e., support SSCs outside
technicalspecifications) [5]
(5) SSCs described in the Updated Final Safety AnalysisReport
(UFSAR).
35.1.2.2 Functional /Functionality. As previously mentioned,the
U.S. NRC [15] defines functionality as an attribute of SCCs
notcontrolled by the plant technical specifications which
warrantprogrammatic controls to ensure SSC availability and
reliability(e.g., quality standards and records in Appendix B to 10
CFR 50,maintenance rule in 10 CFR 50.65, etc.) or other
functionalityrequirements in the current license basis. A
non-technical specifi-cation SSC is functional when it is capable
of performing itsintended function(s) as specified in the plants
current license basis.
A detailed discussion of the U.S. regulatory requirements
asso-ciated with the scope of operability determinations and
func-tionality assessments is contained in NRC Inspection
ManualPart 9900 [15]. The NRCs distinction between these two
assess-ments is summarized in Figures 35.1 and 35.2.
35.2 MECHANICAL COMPONENTSAND FAILURE MODES
Typical failure modes for SSCs can be determined from exten-sive
industry experience reported in the Nuclear Plant ReliabilityData
System (NPRDS), Licensee Event Reports (LERs), andother industry
studies.
35.2.1 Piping ComponentsSince the early 1990s, significant
attention has been placed on
establishing comprehensive databases that compile all reported
ser-vice induced degradation in operating nuclear power plant
pipingcomponents. The most significant work in this area has been
doneas part of an OECD Pipe Failure Data Exchange (OPDE)
Projectwhich has established an international database of piping
and com-ponent failures (service induced cracks/wall thinning,
leaks, andlarge breaks) in commercial nuclear power plants
worldwide [37].Pipe failure data has been collected from operating
nuclear powerplants worldwide, representing approximately 11,000
commercialreactor operating years from 1970 thru 2007. Considering
that thereare thousands of numbers of piping components in nuclear
powerplants this represents tens of millions of component years of
serviceexperience from which to derive insights.
Figure 35.3 shows the total number reported piping
failuresreported from 1970 through 2007 as a function of the piping
com-ponent in-service life at the time of failure [38]. The
relativelyhigh incidence of failures for the interval 11-15 years
is largelyattributed to IGSCC in BWR plants, FAC in PWR plants, and
cor-rosion of raw water piping in all plant types.
In Figure 35.4, U.S. failure data is organized degradation
mech-anisms. It shows that design/construction defects and
thermalfatigue (which are the degradation mechanisms at the basis
of thecurrent Section XI preservice and inservice inspection
require-ments) account for approximately 8% of the failures in U.S.
com-mercial light water reactor (LWR) plants since 1970. Of these
on1.5% of the failures were primarily due thermal fatigue,
thermalmixing and thermal stratification mechanisms and loading
condi-tions not considered in the original design. Over 87% of the
pip-ing failures resulted from flow accelerated corrosion (FAC),
stresscorrosion cracking (SCC), vibration and fretting fatigue, and
cor-rosion mechanisms including: crevice corrosion,
microbiological-ly induced corrosion (MIC), and pitting.
Figure 35.5 shows all U.S. pipe failure data since 1970
orga-nized by pipe safety classification. Generally service induced
fail-ures in safety related have been evenly distributed throughout
the
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three safety classes. Over 1/3rd of the failures occurred in
non-safety pipe which are normally not reported to the
regulatoryauthorities. The Class 1 piping failures are dominated by
stresscorrosion cracking in BWR piping and Class 2 piping failures
areprimarily associated with vibration fatigue, thermal
stratification
and FAC mechanisms. The Class 3 failures are dominated by
cor-rosion mechanisms. In all causes piping reliability is not a
func-tion of design safety class; but, is dominated by service
loadingand degradation mechanisms not specifically addressed in
theASME Section III design standards.
FIG. 35.1 NRC OPERABILITY DETERMINATION AND FUNCTIONALITY
ASSESSMENT FLOW CHART [15].
FIG. 35.2 NRC SCOPE OF AN OPERABILITY DETERMINATION AS IT
RELATES TO THESCOPE OF A FUNCTIONALITY ASSESSMENT [15].
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FIG. 35.3 PIPING FAILURE TRENDS IN COMMERCIAL NUCLEAR POWER
PLANTS COVERINGTHE PERIOD BETWEEN 1970 THROUGH 2007 [38].
FIG. 35.4 U.S. PIPE FAILURE DATA BY DEGRADATION MECHANISMS AND
OTHERCAUSES [36].
Generally service experience shows that failures (cracks,
wallthinning, leaks, and breaks) in light water reactor (LWR)
pipingdo not correlate with high stress or thermal fatigue usage
valuesreported in plant Design Reports [35]; in fact, service
inducedfailures typically result from either degradation mechanisms
or
loading conditions not specifically considered in the
originalplant design.
The Code stress calculations are used to qualify a design
andprovide reasonable confidence that the plant will provide
reliableservice throughout its design life. For the most part the
peak
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stress and fatigue usage values in the plants Design Reports
donot necessarily provide an accurate indicator of failure
potential[33]. The peak stress and fatigue usage values in the
DesignReports are typically based on extremely conservative
postulatedthermal transient loading conditions and numbers of
cycles. Also,the sequencing of these design thermal transients in
the fatigueanalyses adds significant conservatism. Finally, the
high calculat-ed fatigue usage is dominated by those design
transient load paircombinations that not only result in large
thermal stresses at theinside surface thermal gradients but also
large thermal stress gra-dients through the wall. The large thermal
stresses would result ina low number of allowable stress cycles for
crack initiation (highfatigue usage); however, because of the large
through-wall ther-mal gradient, stresses drop-off rapidly as you
move away from theinside surface. Consequently, if all anticipated
loading conditionsare accounted for, the time to grow a crack
through-wall can besignificantly longer then the original design
and extended life ofthe plant [34].
35.2.2 SupportsEPRI reported failure information on standard
supports in
nuclear power plants, obtained from the Institute of Nuclear
PlantOperations (INPO) NPRDS database [39]. Figure 35.6 providesa
breakdown of standard support service data by failure mode.Most of
the reported degraded supports were associated withmissing/loose
components or improper hanger settings. One thirdsupport problems
involved snubbers. Snubbers frequently faileddrag and motion
criteria and experienced wear, fatigue, lock-up,and seal leakage
mainly due to mechanical vibration.
In Figure 35.7, the breakdown of the NPRDS data is shown
bycause/degradation mechanism. We can see that the cause of
nearly50% of the reported support failures was unknown. These
caseswere typically associated with missing or loose
components,improper hanger settings, and the failure of snubbers to
pass func-tional tests [39].
35.2.3 PumpsTypical failure modes for pumps are the
following:
(1) Fails to start: This failure mode is used to describe
faultsinvolving pumps that do not start upon demand or that
startonly to operate for a brief time period before
trippingoffline.
FIG. 35.5 U.S. PIPE FAILURE DATA BY SAFETY CLASSIFICATION
[36].
FIG. 35.6 STANDARD SUPPORT FAILURES BY FAILUREMODE [39].
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(2) Fails to run: This failure mode indicates that an
operatingpump is automatically or manually tripped off-line to
pre-vent damage to the pump. It also includes pumps that fail
tomeet design and/or operating specifications.
(3) External leakage: This failure mode describes a fault
inwhich the pump is operational but is removed from servicebecause
of excessive leakage of the pumped medium. Acommon example is a
seal or packing leak.
35.2.4 ValvesTypical failure modes for valves are the
following:
(1) Fails to open: Valve fails to fully open on demand. (2)
Fails to close: Valve fails to fully close on demand. Included
are safety/relief valves that fail to reseat. (3) External
leakage: A leak or rupture of the valve that allows
the contained medium to escape from the component bound-ary. The
most common examples are packing or flange leaks.
(4) Plugged (i.e., fails to remain open): This failure mode
refersto any event that would stop or limit the flow through a
nor-mally open valve. However, the following are not consid-ered
plugged valves: those that fail to open or those that areeither
intentionally or unintentionally closed by humanactivity when they
are required to be open. Two examples ofa plugging event are (a) a
valve disc that separates from the stem and falls into
the closed position, and (b) the air supply to an air-operated
valve that fails, allow-
ing the valve to close. (5) Fails to operate as required: The
fails-to-operate-
as-required mode is to be used whenever (a) a valve fails to
meet specific requirements such as
stroke time, or (b) a valve loses its ability to control system
parameters.
(6) Fails to open/fails to close: This failure mode is used
whenspecific information regarding whether the valve failed toopen
or failed to close is not available.
(7) Internal leakage (reverse leakage): This failure mode is
usedto describe internal leakage through a check valve.
(8) Opens (prematurely): This failure mode applies strictly
torelief and safety valves. Valve opening before its
pressuresetting is a typical example of this mode, but the cause is
notalways a pressure transient.
35.3 OPERABILITY/FUNCTIONALITYEVALUATIONS
35.3.1 Conditions Requiring Assessment Conditions requiring
functionality evaluations are usually iden-
tified through the inservice inspection and testing programs
andaugmented inspection programs such as GL 88-01
intergranularstress-corrosion cracking (IGSCC) and flow-accelerated
corrosion(FAC) inspection programs. Some examples of conditions
identi-fied by the inservice inspection and testing programs are
wall-thinning from an FAC mechanism, snubber failures and pipe
ornozzle cracking from fatigue and IGSCC mechanisms,
leakageexceeding TS limits for valves, and excessive pump
vibrations. Insome instances, a system-operating excursion subjects
a systemand its components to an unanalyzed condition that requires
anevaluation.
Unanticipated operating events require operability
evaluations.Examples of such events include fluid transients such
assteam/water hammer and steam/vapor bubble collapse; tempera-ture
and pressure excursions; and thermal stratification. Flow-induced
system vibration from pump operation, cavitation, two-phase flow
conditions and acoustic pressure waves are known tolead to snubber
wear, piping erosion, and fatigue failure, especiallyin
socket-welded fittings.
Functionality evaluations are required for temporary
loadingconditions such as lead shielding, rigging for maintenance
ormodification installation and scaffolding support. The loading
tobe considered in conjunction with the temporary loads is
depen-dent on the system operating status while the temporary
conditionexists. The seismic load is not considered with the
temporary con-dition if the affected system is declared out of
service and thesystems seismic failure does not undermine the
ability of othersystems or components to perform their safety
functions.
A functionality evaluation is required for as-built/as-found
con-ditions that are not consistent with the design-basis
configuration.Examples of these conditions include support system
discrepan-cies, which might consist of such missing, damaged, or
failedsupports as weight supports that slide off their stanchions,
a snub-ber failing to activate and provide the required restraint,
or sup-port members found to have missing or undersized
welds.Additional or unwanted restraints, such as snubbers that lock
upor exceed the drag force restrictions, or a support design
withinsufficient rotational clearance, are all examples of other
sup-porting system discrepancies.
35.3.2 Scoping Operability Evaluations Determining the
conditions to be evaluated requires a clearly
defined scope of the operability determination. To define
thescope of the evaluation, the following actions are required:
(1) Identifying the equipment or SSC that is degraded,
poten-tially nonconforming, or subject to the unanticipated
event.
(2) Establishing the safety functions performed by
theequipment.
FIG. 35.7 STANDARD SUPPORT FAILURES BY ROOTCAUSE [39].
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(3) Assessing the possible failure mechanisms. (4) Defining the
operating events or loading conditions concur-
rent with the evaluation period. (5) Determining the basis for
declaring the affected system
operable through any of the following conditions:
(a) analysis; (b) test or partial test; (c) operating
experience; or (d) engineering judgment.
Each of the conditions stated in sections 35.2.1 through
35.2.4require an operability evaluation to be performed. This
evaluationshould consider the operational status of the SSC for the
time periodduring which it is degraded or nonconforming. As one
determinesthe operating events and loading conditions for the
evaluation, it isimportant to distinguish between an SSC that was
restored to itslicensing basis and one that is expected to operate
in the degraded ornonconforming condition. The evaluation of an SSC
that wasrestored to its current licensing basis is based on all
operating eventsthat actually occurred while the SSC was in the
nonconforming ordegraded condition. Included in such operating
events are any of theunanticipated events (described previously)
that were determined tohave occurred. However, the evaluation does
not include design-basis loads that did not occur, such as a
loss-of-coolant accident(LOCA), post-LOCA thermal modes, and
seismic loads.
An example of a degraded and nonconforming SSC notrestored to
its current licensing basis is a degraded snubber foundduring the
Inservice Testing program to have exceeded its draglimit. An
operability evaluation is required to determine theimpact of the
excessive drag on the piping system. When seismicand LOCA events
did not occur, only the thermal modes that didoccur since the last
time the snubber was determined to haveoperated normally are
considered in the evaluation. A root-causeanalysis would need to be
performed to ensure that some unantic-ipated operating event, such
as waterhammer or system vibration,
did not degrade the snubber. If the root-cause analysis
determinesthat some unanticipated operating event did occur, the
evaluationwould include this unanticipated event. The root-cause
analysisshould be performed to establish that the degradation
mechanismor nonconformance was eliminated and also to determine
whichother SSCs may be impacted by it.
If the SSC is to continue operating while in the degraded
condi-tion, the operability evaluation must demonstrate its
functionality,as previously defined, for design-basis events
required by plantlicensing commitments. If the SSC has been
degraded by anunanticipated operating event, the operability
evaluation mustdemonstrate its functionality for the design-basis
events and theeffects of the unanticipated operating event. The
effects of theunanticipated operating event would need to be
included in theoperability evaluation until the cause of the event
can be eliminat-ed or contingencies are put in place to
significantly reduce thepossibility of the event occurring.
Additionally, if an SSC that hadbeen degraded by an unanticipated
operating event is restored toits design-basis condition, an
operability evaluation must demon-strate the functionality of the
SCC for its design-basis events andthe effects of the unanticipated
operating event.
Following the guidance proposed by the ASME Section XITask Group
on operability, only the failure mechanisms and loadsfrom the
faulted or Service Level D condition are required for
theevaluation. In keeping with this philosophy,
displacement-controlled loading is not considered for piping or
pressure bound-ary items. (Displacement-controlled loading refers
to self-limitingloads such as thermal expansion, thermal-anchor
movement, andseismic-anchor movement.) For support designs
susceptible tononductile failure, such as buckling and anchor-bolt
failure, orsupport designs that deform so severely that an active
componentmight be unable to perform its required safety function,
the ther-mal-anchor motion and seismic-anchor motion loadings must
beconsidered. Table 35.1 presents this load consideration
philoso-phy in a matrix form.
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35.4 ASME CODE REQUIREMENTSThe ASME B&PV Code Section III
[8], Section XI [7], and the
ASME O&M Code [9] all contain requirements directly and
indi-rectly related to the operability of components. The Section
IIIrules encompass requirements for the design, construction,
stamp-ing, and overpressure protection for nuclear plant items.
Theserules are for new construction and give consideration to
mechani-cal and thermal stresses caused by cyclic operation; they
typicallydo not address deterioration that might occur in service
becauseof radiation effects, corrosion, erosion, or other material
degrada-tion mechanisms. The rules of this section are not
applicable tovalve operators, controllers, position indicators,
pump impellers,and other nonpressure-retaining items (except for
those within thescope of Subsection NF), as well as motor drives
and instruments.
Functional acceptability aspects of some components are
notmentioned in Section III; for other components, a
disclaimerstatement is provided. Such a disclaimer is provided for
valves,for example, stating that Code valve design acceptability
require-ments are not intended to ensure functional adequacy of
thevalves. However, rules are provided for pressure-relief valves
thatcover set pressure, lift, blowdown, and closure (NX-7000)
[8].
The rules of Section XI and the O&M Code, on the other
hand,are more directly related to various aspects of component
oper-ability. These Codes define inspection and testing
requirements toidentify degraded and nonconforming conditions for
SSCs. Eachdefines the acceptance criteria and evaluation
methods.
The following paragraphs itemize some specific
stipulationsapplicable to pumps and valves from the O&M Code
and vesselsand piping from Section XI. The pumps and valves covered
bythese stipulations are components required for the following
con-ditions:
(1) shutting down the reactor to the cold shutdown condition;
(2) maintaining the reactor in a cold shutdown condition; and (3)
mitigating the consequences of an accident.
35.4.1 Valves Valves within the scope of the inservice testing
program are
placed in at least one of the following four categories as
definedin Subsection ISTC of the O&M Code [9]:
Category Avalves for which seat leakage is limited to a
spe-cific maximum amount in the closed position to fulfill
theirrequired functions.
Category Bvalves for which seat leakage in the closed posi-tion
is inconsequential for fulfillment of the required functions.
Category Cvalves that are self-actuating in response to a
sys-tem characteristic, such as pressure (relief valves) or
flow-direction (check valves) to fulfill the required
functions.
Category Dvalves, such as rupture discs or explosively actu-ated
valves, that are actuated by an energy source capable of onlyone
operation.
The test requirements for each of these valve categories
arespecified in ISTC3500 [9] and summarized in Table 35.2.
Theserequirements define test intervals, leakage tests, and stroke
times.
Table 35.3 provides the leak-testing criteria defined in
ISTC-3600 [9]. Valves or valve combinations exceeding the
specifiedcriteria shall be declared inoperable and either repaired
orreplaced. An example of typical leakage rates from an
operatingpressurized water reactor (PWR) is provided in Table
35.4.
Stroke-time acceptance criteria for active Category A and
Bvalves are defined in ISTC-5000 [9] and summarized in Table
35.5.
If a valve fails to exhibit the required change of obturator
positionor exceeds the limiting values of full stroke-time, the
valve shall bedeclared inoperable. Valves declared inoperable may
be repairedor replaced; in some cases, if the data can be analyzed
to deter-mine the cause of deviation, they may even be defined as
operatingwithin limits.
For Category C pressure-relief devices, testing requirementsare
defined in the O&M Code, Appendix I [9]. The general rulefor
pressure-relief valves is that they shall not exceed the
stampedset-pressure criteria by more than 3%. Non-reclosing
pressure-relief devices are not required to be tested. They are
required, by
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the O&M Code, Appendix I [9], to be replaced at least every
fiveyears, unless historical operating experience indicates more
fre-quent replacement is required. Facility Owners may have
testingor replacement criteria varying from what is given here,
which isbased on system and valve design requirements or TS
require-ments. In most cases, if such criteria are not met, valves
arerepaired, refurbished, or replaced.
Category C check valves are exercised for obturator movement.If
a check valve fails to exhibit the required change of
obturatorposition, it shall be declared inoperable.
35.4.2 Pumps For the subject pumps, inservice test parameters
and parameter
ranges are specified in Subsection ISTB of the O&M Code
[9]and examples of the test parameters with acceptance limits
aresummarized in Tables 35.6, 35.7, and 35.8. Figure 35.8
depictsthe pump vibration limits in graphical form.
As shown in Table 35.7, the test parameter ranges are groupedas
acceptable, alert, and required-action for the various parame-ters
considered. The acceptance criteria for these pumps aredefined as
the alert range, which indicates incipient degradationof
performance, and the required action range. If deviations
fallwithin the alert range, the specified frequency of testing
shall bedoubled until the cause of the deviation is determined and
thecondition corrected; if they fall within the required action
range,the pump shall be declared inoperable until the cause of the
devia-tion is determined and the condition corrected.
35.4.3 Snubbers Inservice test requirements for snubbers are
specified in O&M
Code, Subsection ISTD, Inservice Testing of Dynamic
Restraints(Snubbers) in Light-Water Reactor Power Plants [9]. This
sub-sectionspecifies the scope, test intervals, sample sizes, and
operability test
requirements for snubbers. The operability test requirements
forsnubbers include the following parameters:
(1) The breakaway and drag force; (2) The activation-velocity or
acceleration; and (3) The release rate. The acceptance criteria for
each of these tested parameters are
specified as part of the test program and are determined by
therestraint and motion requirements of the restrained
component.Guidelines for determining the generic acceptance
criteriagreater than the manufacturers specified criteria are
provided inEPRI Report NP-6443, Improved Criteria for Snubber
Testing[10]. These improved criteria for snubber operability are
basedon the restraint requirements of the piping system or
componentbeing restrained. By evaluating the piping system or
componentthermal flexibility, increased snubber drag or breakaway
forcesmay be justified.
35.4.4 Piping The rules of Section XI [7] define requirements
for the evalua-
tion and acceptance of degraded piping components.
Theserequirements have been developed for piping that is flawed
ordegraded from a corrosion mechanism and are used to demon-strate
the piping fitness for service when subjected to design-basisloads.
(More detailed information regarding the flaw
evaluationrequirements for piping is found in Chapter 29 of this
book.) Forthe specific case of through-wall flaws in Class 3
moderate-ener-gy piping in which the maximum operating temperature
does notexceed 200F and the maximum operating pressure does
notexceed 250 psig, Code Case N-513 [25] specifies flaw
evaluationmethods and acceptance criteria to justify the temporary
accep-tance of this condition. The USNRC has approved the use of
thisCode Case in the revision of 10CRF50.55a [11].
35.4.5 Reactor Vessel The rules of Section XI [7] define
requirements for the evalua-
tion and acceptance of flaws and radiation embrittlement the
reac-tor vessel. These requirements are used to demonstrate the
ves-sels fitness for service when it is subject to design-basis
loads.(More detailed information regarding flaw evaluation
require-ments is found in Section 29.) Appendix E of Section XI
Code [7]provides evaluation methods and acceptance criteria for the
reac-tor vessel when it is subject to pressure in excess of the
pressure-temperature limits required by 10CFR50.60 and Appendix G
of10CFR50 [11]. Meeting the requirements of this appendix
ensuresadequate structural integrity for returning the vessel to
service.The Appendix E evaluation method reduces some of the
margins
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inherent in the development of pressure-temperature limits
byreducing both the postulated flaw depth and the safety factor
onthe pressure-stress intensity factor, and by increasing the
vesselmaterial fracture-toughness. This increase in vessel material
frac-ture-toughness provides a significant margin for this
structuralintegrity evaluation. The Appendix E evaluation changes
the ves-sel material fracture toughness from Section XI, Appendix G
[7],limits of Kla to the Klc limit defined in Section XI, Appendix
A,Fig. A-4200-1. Figure 35.9 presents the Kla and Klc
fracture-toughness values used for vessel evaluations. It should be
noted thatthe Section XI, Appendix G criteria for developing the
vesselpressure-temperature limits have been modified in Code Case
N640[26] to permit use of the Klc vessel material-fracture
toughness, but
such vessel pressure-temperature limits do not have this
addition-al margin for their structural integrity assessments.
35.5 OPERABILITY EVALUATIONMETHODS
Design analysis methods and acceptance criteria applicable
topiping systems, components and supports inherently
containavailable margins to compensate for uncertainties in the
opera-tion, fabrication, and construction of systems. Generally,
designanalysis methods employ a conservative finite element model
andsmall deformation linearelastic theory to estimate the
system
FIG. 35.8 PUMP VIBRATION LIMITS (Source: Fig. ISTB-5200-1 of the
ASME O&M Code)
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response to the design-basis loads, an approach that
generatesconservative system responses for the following
reasons:
(1) piping system nonlinearity; (2) energy losses from localized
plastic deformation; (3) load redistribution associated with items
(1) and (2) of this
list; (4) conservatism of building structure response spectra;
(5) conservatism of Enveloped/Uniform Response Spectra
analysis method; and (6) conservatism of critical damping
values. These areas of conservatism have been substantiated by
many
research and testing programs. Some of these test programs
arethe Electric Power Research Institute (EPRI) multiple
structurepiping system tests [1], the Heissdampf Reactor (HDR)
tests [2],and the EPRI- and USNRC-sponsored Piping and
FittingDynamic Reliability Program [20].
35.5.1 Piping Systems For piping systems, the evaluation method
used to demonstrate
operability usually is to examine the design-basis analysis
meth-ods for inherent conservative methods. The analytical
methodsgenerally employed for the design basis of the piping are
usuallybased on conservative models, load definitions, and
solutionmethods. Refining the analytical model to include support
andequipment nozzle stiffness values may reduce some of the
conser-vatism inherent in the design basis, which is especially
true whena time-history analysis is performed and support
nonlinearities areincluded. Instead of using a uniform or enveloped
response spec-tra method of analysis, the independent support
motion methoddescribed in Welding Research Council (WRC) Bulletin
352 [3]together with an alternative system damping (such as Code
CaseN-411 [4]) can be used to reduce the response of seismic
and
other building-filtered loads evaluated by response spectra
meth-ods. Section III, Appendix N [8] provides detailed
descriptions ofthese alternative, more rigorous methods that may be
used todetermine system responses to seismic and other
building-filtereddynamic loads. Also, the combination of dynamic
loadingresponses from different events permits the use of the
squarerootsum-of-the-squares method. This combination method is
jus-tified when the predominant frequencies of the events being
com-bined are sufficiently separated to make the probability of
simul-taneous maximum responses for each event very unlikely
[6].
Finally, the load cases used in the evaluation should be
consis-tentwith and limitedthose loads that can realistically
occurduring the period of operation when the piping system is in
thedegraded or nonconforming condition.
35.5.2 Supports For supports, the evaluation method usually used
to demonstrate
operability is a structural analysis method. Although for
supportsand especially expansion anchors, the operability
evaluation may bebased on test results or a combination of test
results and analysis.
Generally, support designs are based on conservative models,load
definitions, and solution methods. Developing more
rigorousanalytical models can be used to redistribute loads in the
supportstructure. In many cases support operability is demonstrated
byevaluating the system or component being supportedan evalua-tion
that is performed to reduce the loads acting through thedegraded or
nonconforming support. In other cases, the system orcomponent
evaluation demonstrates that support functionality isnot needed for
the system or component to perform as required.
35.5.3 Valves Operability evaluations of valves are generally
based on the
determination of margins available in the original
qualification
FIG. 35.9 LOWERBOUND KLA AND KLC TEST DATA REACTOR VESSELS
(Source: Fig. A-4200-1, Appendix A of the ASMEB&PV Code)
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documents. In most cases, the typical parameter to consider is
thedynamic acceleration limit used for the qualification. Valve
quali-fications are often provided for generic specification values
ofseismic demand, which are arbitrarily set limits. For
plant-specificapplications, the actual seismic demand is compared
with thegeneric qualification values for acceptance.
The most effective approach for valve operability evaluation
isto verify that the available margins between the qualified
demandand the demand determined for the conditions requiring
operabilityverification are sufficient for accepting the critical
operabilityparameter (e.g., stress level, deformation, and load).
In caseswhere this direct comparison does not provide the required
relief,efforts may be directed toward realistic determination of
the actualdemand. Methods previously discussed for the reevaluation
ofpiping and support systems may result in sufficiently
reduceddemand at valve locations. Valves may also be analyzed by
usingfinite element methods to assess stress and deformation at
criticallocations for increased loads. These analyses often
indicate onlylocalized high stress and deformation conditions that
do not affectthe valves functionality.
A particular valve operability problem is related to
theincreased torque or thrust requirements to meet certain
systemdemands related to the assigned safety function. In most
cases, itis possible to show analytically that the weakest link on
the postu-lated load paths have sufficient capacity and integrity
to meet theincreased demand. However, in extreme cases in which an
analyt-ical approach does not provide the required verification,
testingmay ensure the functionality. Care must be exercised in
extendingthe applicability of the test results to untested
configurations.
35.5.4 Pumps, Tanks, and Heat Exchangers Typically, equipment
items such as pumps, tanks, and heat
exchangers have allowable nozzle load limits. As with valves,
theVendor Equipment Qualification Report should be reviewed
todetermine the basis of the allowable nozzle loads.
In a typical heat exchanger, the allowable nozzle loads are
usedto check the following:
(1) the nozzle at the junction with the shell; (2) the shell in
the region of the nozzle; (3) gross shell stresses; (4) localized
shell stresses at the saddles; (5) gross stresses in the saddle
supports; and (6) gross loads on the anchor bolts. Items (1) and
(2) of the preceding list use the loads for their
respective nozzles. Items (3)(6), however, use the
combinedeffects of weight, dynamic inertia, operational loads
(e.g., asmotor torque in a pump), and all nozzles.
In many cases, particularly on Class 2 and 3 vessels, item (2)
isthe limiting component; for this item, the local stress analysis
ofthe shell should be reviewed. Such analyses are typically
doneusing the methods of WRC Bulletin 107 [21] and WRC Bulletin297
[22]methods for which vendors occasionally use the
totalthrough-wall stress (i.e., membrane bending, or using
WRCBulletin 107 terminology N, membrane force terms M, andbending
moment terms) when comparing the nozzle stress to theprimary local
membrane allowable, rather than just the membrane(N, terms)
component. For Service Level D conditions, local mem-brane effects
should be checked in the shell at the shell nozzle junc-tion, but
not local membrane plus local bending (PL Pb Q).The requirements
for local checks are taken directly fromAppendix F of the ASME
Boiler and Pressure Vessel Code [8].
Through-wall bending effects (the M terms) are secondary
effectsand, as such, do not need to be considered, which can
providesubstantial relief.
Alternate analyses may be performed by using finite
elementmodels at critical areas to assess the stresses and
deformations.
35.5.5 Specific Inspections For those operability evaluations on
SSCs that have been
restored to their current licensing basis before being placed
backinto service, or on SSCs subjected to a significant
unanticipatedoperating event, an evaluation may be based on
specific augment-ed inspections. Analyzing the degraded or
nonconforming SSC,or analyzing the unanticipated event to identify
those areas of theSSC that are most likely to sustain damage will
guide these aug-mented inspections. The results of the inspection
will be evaluat-ed to demonstrate the functionality of the SSC,
after which theywill be documented. The forthcoming lists describe
the probableinspection areas and the damage that may affect the
performanceof the SSCs. These inspections will be visual and will
includemanual testing for active components. For highly stressed
areaswhere crack initiation may be expected, surface or
volumetricexamination may be required as well.
Whenever damage is found, the results of the inspections
andtests require an engineering evaluation to determine the
function-ality of the affected SSC. The nature of this evaluation
willdepend on the type and extent of the damage found.
35.5.5.1 Piping Systems. This will be a visual inspection of
thepipe to determine whether any significant damage has
occurred.The examination for damage will include the following:
(1) distortion of the piping cross section; (2) local denting or
buckling of the wall; (3) leaks; (4) permanent distortion of
piping; (5) interaction with adjacent SSCs; (6) broken or bent
bolts; (7) distortion of flanged connections; (8) cracked socket
welds; and (9) interferences or unintentional restraints.
35.5.5.2 Component Supports. This will be a visual inspectionof
the supports to determine whether any significant damage
hasoccurred. The examination for damage will include the
following:
(1) buckling of members or rods; (2) local distortion of
members; (3) cracks at welds; (4) pullout of concrete expansion
anchors; (5) broken or bent bolts; (6) stripped-bolt threads; (7)
spalled concrete; (8) distorted baseplate; (9) hydraulic snubber
fluid leaks; and
(10) clearance at rigid supports. The examination for snubbers
and other supports, which are
relied upon to change position, will include manually
strokingthem through their expected range of operation to
determinewhether any internal damage has occurred.
35.5.5.3 Valves. The valves will be visually examined for
leak-age of and damage to bolts, as well as distortion to the yoke
and
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stem. Valves required to change position during the remainder
ofthe operating cycle will be stroked to the extent practicable
todetermine their functionality.
35.5.5.4 Pumps. Pumps that were operating during the eventwill
be monitored for vibration and flow and will also be
visuallyexamined for leakage. Standby pumps that were not operating
dur-ing the event but that may be required to perform a safety
functionwill require testing (to the extent practicable) for
vibration and flowor pressure, and will also require a visual
examination for leakage.
Passive mechanical components (e.g., vessels and heat
exchang-ers) will require a visual examination for leakage as well
as fordamage near the nozzles and anchorages. In addition, heat
exchang-er performance requires monitoring for tube-to-shell
leakage.
35.6 SHORT-TERM OPERABILITYACCEPTANCE CRITERIA
The acceptance criteria presented here are currently being
con-sidered by the ASME Section XI Task Group on Operability
forpublication as a Code Case [18]. These proposed criteria
arebased on industry evaluations of the margins present in the
analyt-ical methods and also in the acceptance criteria used for
design ofthe SSC. For example, for piping systems these industry
investi-gations have lead to alternative evaluation methods and
accep-tance criteria for seismic and other building-filtered loads
duringnormal and upset conditions.
The development of the criteria provided here was based onASME
Section III, Appendix F [8] criteria and is augmented withindustry
testing programs for application to specific piping
systemcomponents.
35.6.1 Short-Term Operability Acceptance Criteriafor Piping
The short-term operability acceptance criteria presented hereare
for piping systems designed to various ASME and ANSICodes and Code
editions [8], [23][24]. The loads to consider inthe operability
evaluations for piping are defined in Table 35.1.These criteria are
intended for piping and typical piping compo-nents. If the
evaluated system includes specialty piping compo-nents such as
flanges and expansion joints, these specialty pipingcomponents are
expected to meet the current licensing-basis ser-vice Level
D/faulted condition limits.
35.6.1.1 Criteria for Piping Designed to ANSI B31.1,
B31.7Classes 1 and 3, or ASME Section III, Classes 2 and
3(Prewinter 1981).
For Level A/normal loads:
(35.1)
For Level D/faulted loads:
(35.2)
(35.3) The criteria presented in the preceding equations were
developed
from the work performed during the seismic upgrade program
for
Pmax 2Pa
PmaxD4t
+ 0.75i (MA + MD)
Z6 2Sy
PD4t
+ 0.75i MAZ
6 Sy
the San Onofre station in California [12]. This program
developedoperability criteria based on a 1% strain acceptance
criterion forcarbon steel piping and 2% strain acceptance criterion
for stainlesssteel piping, which were both approved by the USNRC
[12]. Indeveloping the strain limit acceptance criterion, a stress
acceptancecriterion of 2Sy was shown to be more limiting than that
when thestress values were calculated using elastic methods.
35.6.1.2 Criteria for Piping Designed to ANSI B31.7, Class 1,or
to ASME Section III, Class 1.
For Level A/normal loads:
(35.4)
For Level D/faulted loads:
(35.5)
(35.6) The criteria presented in the preceding equations were
founded
on the evaluations and acceptance criteria specified in
AppendixF of Section III [8]. This stress limit has been specified
as 2Sy ,not the lesser of 3Sm or 2Sy , based on prior acceptance of
thislimit [17].
35.6.1.3 Criteria for Piping Designed to ASME Section
III,Classes 2 and 3, Winter 1981 or Later Edition.
For Level A/normal loads:
(35.7)
For Level D/faulted loads:
(35.8)
(35.9) The criteria presented in the preceding equations were
founded
on the evaluations and acceptance criteria specified in Appendix
Fof Section III [8].
35.6.2 Short-Term Operability Acceptance Criteriafor
Supports
The proposed operability acceptance criteria are developed
forcomponent standard supports, spring hangers, snubbers,
linear-type supports, structural bolts, and concrete expansion
anchors.These criteria were developed to address the load-carrying
capa-bility of the supports. However, the other support failure
modesmust also be addressed when applicable. Support design
stability,including the potential for buckling, should be evaluated
unlessthe system is shown to be functional without the support.
Supportbinding should also be addressed in the support operability
evalu-ation and the operability evaluation for the system. Table
35.1provides guidance to consider for the loadings in the support
eval-uation. If the necessity of including seismic anchor motion
isdetermined, it should be combined with the seismic inertia loadby
a square rootsum-of-the-square method.
Pmax 2Pa
B1 PmaxD
2t+ B2
(MA + MD)Z
6 greater of 3 Sh or 2Sy
B1 PD2t
+ B2 MAZ
6 the greater of 1.5 Sh or Sy
Pmax 2Pa
B1 PmaxD
2t+ B2
(MA + MD)Z
6 2Sy
B1 PD2t
+ B2 MA
Z6 the greater of 1.5Sm or Sy
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35.6.2.1 Component Standard Supports. Component stan-dard
supports are supplied by support manufacturers with definedload
capacities. The following criteria will be used to determinethe
operability of these components when they are subject toService
Level D/faulted condition loads as defined in Table 35.1.
(a) The manufacturers ultimate tested load divided by a
safetyfactor of 1.5 except for the side load on U-bolts,
whichshould be 3.0. In determining this limit, the allowableshould
be modified by the temperature effects on the mate-rial ultimate
strength.
(b) The manufacturers allowable load for Service Level D. (c)
The manufacturers allowable load for Service Level A mul-
tiplied by either of the following: (i) the lesser of 2 or 1.167
(Su /Sy) when Su 1.2 Sy or
(ii) 1.4 when Su 1.2Sy. If the criteria in the preceding list
cannot be met, the criteria in
the paragraphs that follow for linear-type supports can be used
todemonstrate the operability of the standard component.
35.6.2.2 Linear-Type Supports. For linear-type supports,ASME
Section III, Appendix F, paragraph F-1334 [8] provides thebasis for
the operability criteria. The following limits summarizethe
criteria of this subparagraph, although not all of the
criteriaspecified in this subparagraph are presented here.
For Tension Stress, Ft min(1.2Sy, 0.7Su) except at
pinholes,which use min(0.9Sy, 0.5Su).
For Shear Stress, Fv min(0.72Sy, 0.42Su).For Bending Stress, Fb
(f ) Sy for compact sections where
(f ) the plastic shape factor. For noncompact sections,
seeAppendix F, paragraph F-1334.4(c) [8].
For Compression, Fa min(Ft, 0.67Scr).For Combined Axial Tension
and Bending, the stress of members
subjected to both axial tension and bending must be proportioned
tosatisfy the requirements of equation (35.10), which follows.
(35.10)
WhereFa the smaller of 1.2Sy or 0.7SuFor Combined Axial
Compression and Bending, the stresses of
members subjected to both axial compression and bending mustbe
proportioned to satisfy the requirements of equations (20),(21),
and (22) of ASME Section III, NF-3322.1(e)(1) [8].
TheNF-3322.1(e)(1) equations are modified to use the Fa, Fb, and
definitions of Section III, Appendix F, paragraph F-1334.5 [8].
35.6.2.3 Structural Bolts. Structural bolting will meet
therequirements of Section III, Appendix F, paragraph F-1335. For
allstructural bolts, the average tensile stress computed on the
basis ofthe average tensile stress area will not exceed the lesser
of 1.0Sy and0.7Su. The average shear stress will not exceed the
lesser of 0.6Sy and0.42Su. For high-strength structural bolts (Su
100 ksi at operatingtemperature), the maximum stress at the
periphery of the cross sec-tion caused by direct tension plus
bending but excluding stress con-centrationswill not exceed Su. If
structural bolts are subject tocombined tensile and shear loads,
the tensile and shear stresses mustbe proportioned so that the
following equation is satisfied.
(35.11)f2t
F2tb+
f 2yF2yb
1
7
Fe
faFa
+fbxFbx
+fbyFby
1
67
35.6.2.4 Concrete Expansion Anchors. As previouslydescribed in
Section 35.2.5, displacement-controlled loads shouldbe considered
when evaluating the operability of concrete expan-sion anchors. An
exception to this requirement is for undercutanchors if the failure
mode is in the bolt, not in the concrete.
The operability limits for tension and shear loads acting
onconcrete expansion anchors are obtained from the ultimate
capac-ities determined by the manufacturer. A safety factor of 2 on
theselimits is required by the NRC Inspection and
EnforcementBulletin 79-02 [19]. For the bolt ductile failure mode
of undercutanchors, a safety factor of 1.5 may be used. Also,
anchors nearfree edges are subject to shear failure in the concrete
and shoulduse a safety factor of 2. Anchors subject to combined
tension andshear will be evaluated using the following interaction
equation.
(35.12)
Reductions in the tensile and shear capacities of the
expansionanchor caused by center-to-center and edge distance
violationsmust be determined before multiplying by the required
safety fac-tor of 2 or 1.5.
Some anchorages are installed with gaps between the plant
andconcrete or plate-and-bolt head. In these cases, the prying
forcetypically included in such analyses may be neglected.
Anchorbolts with gaps up to in. are shown to develop full capacity
and,therefore, are acceptable [16].
35.6.2.5 Integral Welded Attachments. For integral
weldedattachments to straight pipe, the methodologies defined in
CodeCases N-122 and N-318 will be used for rectangular
attachments,and those defined in Code Cases N-391 and N-392 will be
used forcircular attachments.
The stress limit to use for evaluations based on each of
theseCode Case is 2.0Sy.
35.6.2.6 Spring Hangers. Spring hangers will be evaluated
forloading clearances. The maximum pipe movement will be
checkedagainst the stroke of the hanger, and where the spring
hanger wassubjected to an excessive weight load, the individual
componentswill be evaluated for the excess load.
35.6.2.7 Snubbers. Snubbers that are subject to an
unanticipateddynamic load will be evaluated against the
manufacturers ServiceLevel D allowable or against the one time
allowable test load.
The primary failure mode for snubbers is excess drag and
lock-up. In these cases the impact of the snubber failure on the
pipingsystem requires evaluation, which includes a fatigue
evaluation forpiping systems with fatigue design requirements. As
previouslydiscussed in Section 2.5, the fatigue analysis considers
the operat-ing events and their thermal transients known to occur
while thesnubber is degraded. Using the guidance provided in EPRI
ReportNP-6443 [10], increased snubber breakaway and running
dragloads can be justified; for example, depending on the piping
size,allowable drag loads of 5% of the snubber load rating are
justified.For hydraulic snubbers, the common failure mode is
leakage,resulting in a lack of restraint [14]. This failure mode
requires thesystem or component to be evaluated without the
snubber.
35.7 LONG-TERM OPERABILITY Generic Letter 91-18 provides
specific guidance for long-term
operability by requiring that the degraded or nonconforming SSC
be
18
a FtFtob5/3 + a Fy
Fyob 1.0
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brought back into complete compliance with the licensing
basisrequirements. This task requires the repair or replacement of
the SSCin accordance with ASME Section XI requirements. Alternative
tasksinclude a more detailed, sophisticated analysis to demonstrate
thatthe SSC complies with licensing commitments, as well as
revisingthe licensing basis to make it conform to the required
USNRC reviewand approval to bring the SSC into compliance.
35.8 COMMON TERM DEFINITIONSCurrent Licensing Basis Current
licensing basis (CLB) is the
set of USNRC requirements applicable to a specific plant
com-posed of a licensees written commitments for ensuring
compliancewith and operation within the applicable USNRC
requirements andalso the plant-specific design basis (including all
modifications andadditions to such commitments over the life of the
license) that aredocketed and in effect. The CLB includes the
following:
(1) The USNRC regulations contained in 10CFR Parts 2, 19,20, 21,
30, 40, 50, 51, 55, 72, 73, and 100, as well as appen-dices to
those Parts.
(2) Orders, license conditions, exemptions, and the
TechnicalSpecifications (TSs).
(3) The plant-specific design-basis information defined
in10CFR50.2, as documented in the most recent Final SafetyAnalysis
Report (FSAR) as required by 10CFR50.71.
(4) Docketed licensing correspondence such as licenseeresponses
to USNRC bulletins, generic letters, and enforce-ment actions.
(5) Licensee commitments documented in USNRC safety eval-uations
or licensee event reports.
Design Basis Design basis is the body of plant-specific
designbases information defined by 10CFR50.2.
Design-Basis Events As defined in
10CFR50.49(b)(1)(ii),design-basis events include normal operating
conditions, anticipatedoperating transients, design-basis
accidents, external events, andnatural phenomena for which the
plant was designed to with-stand.
Degraded Condition An SSC condition in which any loss ofquality
or functional capability occurs.
Nonconforming Condition An SSC condition in which thereis
failure to meet requirements of licensee commitments. The
fol-lowing are some examples of nonconforming conditions:
(1) A failure to conform to one or more applicable Codes
orStandards specified in the FSAR.
(2) As-built or as-modified equipment that does not meet
FSARdesign requirements.
(3) Operating experience or engineering reviews that
demon-strate a design inadequacy.
(4) Documentation required by USNRC requirements, such
as10CFR50.49, that is deficient or unavailable.
Full Qualification Full qualification constitutes conforming
toall aspects of the current licensing basis, including Codes
andStandards, Design Criteria, and commitments.
Active Components Those components that perform amechanical
motion to accomplish their assigned safety functions.
35.9 NOMENCLATURE Ag area of gross section of linear support
member Ap pipe cross-sectional (metal) area
b actual width of stiffened and unstiffened
compressionelements
bf flange width of rolled beam or plate girder, in. B1 pressure
stress index from NB-3683 [8]
B2, C2 moment stress indices from NB-3683 [8] Cm coefficient
applied to the bending term in the interaction
equation and dependent upon column curvature causedby applied
moments
D pipe outside diameter E modulus of elasticity of steel, ksi fa
computed axial stress, ksi fb computed bending stress, ksi ft bolt
tensile stress, ksifv bolt shear stress, ksi
Ftb allowable bolt tensile stress at temperaure, ksi Fvb
allowable bolt shear stress at temperature, ksi
Euler stress divided by factor of safety, ksi Fa axial stress
permitted in the absence of bending
moment Fb bending stress permitted in the absence of axial force
Fs allowable related to strength in combined compression
bending Ft tensile stress
Fto allowable tensile stress in a concrete expansion anchor Fv
shear stress
Fvo allowable shear stress in a concrete expansion anchor Fw
stress in a fillet weld
i stress intensification factor K effective length factor
KIa material fracture toughness based on crack arrest KIc
material fracture toughness based on fracture initiation
I for beams, distance between the cross section braced
againsttwist or lateral displacement of the compression flange,
in.
for columns, actual unbraced length of member, in.,
andunsupported length of lacing bar, in.
MA sustained moment MD amplitude of the moment for Level D (all
dynamic loads) Msl amplitude of the moment for Level D/faulted
condition
(reversing dynamic loads only) Msm range of the moment from
Level D/faulted seismic
anchor motion P design pressure
Pcl maximum compressive allowable load of a linearsupport
member
Pmax pressure for Level D/faulted condition that is
coincidentwith loads being evaluated
Pa allowable working pressure or rated pressure for eachpiping
component as determined by the pressuredesign section of the
Construction Code or Code ofRecord
Psm amplitude of the axial force from Level D/faultedseismic
anchor motion
rb radius of gyration about axis of concurrentbending, in.
Scr critical buckling loadSh ASME design stress allowable,
Classes 2 and 3 Sm ASME design stress intensity allowable, Class 1
Su specified minimum tensile strength at temperature Sy specified
minimum yield strength at temperature tf flange thicknesst
wall-thickness
Z pipe section modulus
Fe
ASME_Ch35_p629-644.qxd 5/20/09 9:15 AM Page 643
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