ML13291A342

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Updated Final Safety Analysis Report (Ufsar), Rev. 24, Chapter 14 - Figure 14.0-1 Through Figure 14.1-67
ML13291A342
Person / Time
Site: Indian Point Entergy icon.png
Issue date: 09/26/2013
From:
Entergy Nuclear Operations
To:
Office of Nuclear Reactor Regulation
References
NL-13-130
Download: ML13291A342 (56)


Text

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INDIAN POINT UNIT No. 2 UNCONTROLLED RCCA WITHDRAWAL FROM A SUBCRITICAL CONDITION CLAD INNER TEMPERATURE vs TIME AT HOT SPOT UFSAR FIGURE 14.1-4 REV. No. 19

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NUCLEAR POWER ANO CORE HEAT FLUX vs TIME UFSAR FIGURE 14. 1-5 IREV. No. 19

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PRESSURIZER PRESSURE ANO WATER VOLUME vs TIME UFSAR FIGURE 14. 1-6 IREV. No. 19

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CORE WATER AVERAGE TEMPERATURE AND DNBR vs TIME UFSAR FIGURE 14.1-7 REV. No. 19

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NUCLEAR POWER AND CORE HEAT FLUX vs TIME UFSAR FIGURE 14.1-8 I REV. No. 19

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PRESSURIZER PRESSURE AND WATER VOLUME vs TIME UFSAR FIGURE 14. 1-9 I REV. No. 19

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CORE WATER AVERAGE TEMPERATURE AND DNBR vs TIME UFSAR FIGURE 14.1-10 I REV. No. 19

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INDIAN POINT UNIT No. 2 MINIMUM DNBR VERSUS REACTIVITY INSERTION RATE, ROD WITHDRAWAL FROM 10 PERCENT POWER UFSAR FIGURE 14.1-13 I REV. No. 19

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INDIAN POINT UNIT No. 2 DROPPED ROD INCIDENT MANUAL ROD CONTROL PRESSURIZER PRESSURE AT BOL {SMALL NEGATIVE MTC) FOR DROPPED RCCA OF WORTH - 400 PCM

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INDIAN POINT UNIT No. 2 DROPPED ROD INCIDENT MANUAL ROD CONTROL NUCLEAR POWER AND CORE HEAT fLUX AT EOL (LARGE NEGATIVE MTC) FOR DROPPED RCCA OF WORTH -

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INDIAN POINT UNIT No. 2 DROPPED ROD INCIDENT MANUAL ROD CONTROL PRESSURIZER PRESSURE AT EOL (LARGE NEGATIVE MTC) FOR DROPPED RCCA OF WORTH -

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INDIAN POINT UNIT No. 2 LOSS OF ONE PUMP OUT OF FOUR NUCLEAR POWER AND CORE HEAT FLUX vs TIME UFSAR FIGURE 14.1-20 I REV. No. 19

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UNDERVOLTAGE NUCLEAR POWER AND CORE HEAT FLUX vs TIME UFSAR FIGURE 14.1-23 I REV. No. 19

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INDIAN POINT UNIT No. 2 FOUR PUMP LOSS OF FLOW -

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INDIAN POINT UNIT No. 2 LOSS OF LOAD WITH PRESSURIZER SPRAY AND PORV, NUCLEAR POWER AND PRESSURIZER PRESSURE vs TIME UFSAR FIGURE 14.1-31 I REV. No. 19

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INDIAN POINT UNIT No. 2 LOSS OF LOAD WITH PRESSURIZER SPRAY AND PORV, AVERAGE COOLANT TEMPERATURE AND PRESSURIZER WATER VOLUME vs TIME UFSAR FIGURE 14.1-32 I REV. No. 19

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INDIAN POINT UNIT No. 2 LOSS OF LOAD WITH PRESSURIZER SPRAY AND POWER OPERATED RELIEF VALVES DNBR vs TIME UFSAR FIGURE 14.1-33 I REV. No. 19

<<l TIME

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INDIAN POINT UNIT No. 2 LOSS OF LOAD WITHOUT PRESSURIZER SPRAY AND POWER OPERATED RELIEF VALVES, STEAM PRESSURE, vs TIME UFSAR FIGURE 14.1 -39 REV. No. 22

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10 INDIAN POINT UNIT No. 2 LOSS OF NORMAL FEEDWATER, OFFSITE POWER AVAILABLE, HIGH T avg PROGRAM, PRESSURIZER PRESSURE AND PRESSURIZER WATER VOLUME vs TIME UFSAR f'IGURE 14.1-43, sht.1 I REV. No. 19

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INDIAN POINT UNIT No. 2 FEEDWATER SYSTEM MALFUNCTION EXCESSIVE FEEOWATER FLOW -

HFP CONDITIONS MANUAL ROD CONTROL NUCLEAR POWER AND CORE HEAT FLUX vs TIME UFSAR FIGURE 14.1-45, sht.1 I REV. No. 19

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INDIAN POINT UNIT No. 2 FEEDWATER SYSTEM MALFUNCTION EXCESSIVE FEEDWATER FLOW -

HFP CONDITIONS MANUAL ROD CONTROL PRESSURIZER PRESSURE AND DNBR vs TIME UFSAR FIGURE 14.1-45, sht.2 j REV. No. 19

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HFP CONDITIONS MANUAL ROD CONTROL LOOP DELTA -T, AND CORE Tavg vs TIME UFSAR FIGURE 14.1-45, sht.3 I REV. No. 19

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l!me,secon s; INDIAN POINT UNIT No. 2 LOSS OF ALL AC POWER TO THE STATION AUXILARIES, HIGH Tavg PROGRAM, LOOP 21 AND LOOP 23 STEAM PRESSURE vs TIME UFSAR FIGURE 14.1-50, sht.4 REV. No. 19

16 15 14 13 12 Vl 11 w

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9 8

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4 0

ci 3

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E 86 87 88 89 90 91

(,)

92 93 94 95 96 97 98 99 CALENDAR YEAR ANALYSIS FAILURE LINE

  • ACTUAL DATA SV TYPE 1 FAILURE RATE SLOPE OF ANALYSIS FAILURE LINE

= 2.47-06/HR

= [(SY TYPE 1 F.R.) * (OPERATING HOURS)) /

(CALENDAR YEARS)

= [(2.47E-06/HR) * (2.917E+06 HRS)) /

(6.42 CAL. YRS.) = 1. l FAIL/CAL. YR.

INDIAN POINT UNIT No. 2 UFSAR FIGURE 14.1-62 TRACKING 8-95/96 STOP VALVE (SV) TYPE 1 FAILURES STOP VALVE DISC FAILS MIC. No. 2001MB1537 REV. No. 17 A

5 3

I-2 86 87 88 89 90 91 92 93 94 95 96 97 98 99 CALENDAR YEAR

-- ANALYSIS FAILURE LINE

  • ACTUAL OAT A SV TYPE 2 FAILURE RATE SLOPE OF ANALYSIS FAILURE LINE

= 2.05-07 /HR

= ((SV TYPE 2 f.R.) * (OPERATING HOURS)] / (CALENDAR YEARS)

= [(Z.OSE-07 /HR} * (2.917E+06 HRS)) / (6.42 CAL. YRS.) = 0.093 FAIL./CAL. YR.

INDIAN POINT UNIT No. 2 UFSAR FIGURE 14.1-63 TRACKING B-95/96 STOP VALVE (SV) TYPE 2 FAILURES STOP VALVE SPRING FAILS MIC. No. 2001MB1538

!REV. No. 17A

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5 4

3 L....

, L~~===:=J*

0 I

I I

I I

l I

I I

I I

86 87 88 89 90 91 92 93 94 95 96 97 98 99 CALENDAR YEAR ANALYSIS FAILURE LINE

  • ACTUAL OAT A SY TYPE 3 FAILURE RATE

= 2.05-07 /HR SLOPE OF ANALYSIS FAILURE LINE

= ((SV TYPE 3 F.R.) "' (OPERATING HOURS)] /

(CALENDAR YEARS)

= ((2.0SE-07 /HR) "' (2.917E+06 HRS)) /

(6.42 CAL. YRS.) = 0.093 FAIL/CAL. YR.

INDIAN POINT UNIT No. 2 UFSAR FIGURE 14.1-64 TRACKING B-95/96 STOP VALVE (SV) TYPE 3 FAILURES STOP VALVE STICKS OPEN MIC. No. 2001MB1539

!REV. No. 17A

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4 0

0 3

z w

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i
E 86 87 88 89 90 91 92 93 94 95 96 97 98 99

(.)

CALENDAR YEAR ANALYSIS FAILURE LINE

  • ACTUAL OAT A CV TYPE 4 FAILURE RATE SLOPE OF ANALYSIS FAILURE LINE

= 1.22-06/HR

= [(CV TYPE 4 F.R.) * (OPERATING HOURS)) /

(CALENDAR YEARS)

= [(1.22E-06/HR) * (3.925E+06 HRS)] / (6.42 CAL. YRS.) = 0.75 FAIL/CAL. YR.

INDIAN POINT UNIT No. 2 UFSAR FIGURE 14. 1 -65 TRACKING B-95/96 CONTROL VALVE (CV) TYPE 4 FAILURES CONTROL VALVE SPRING BOLT FAILS MIC. No. 2001MB1540 REV. No. 17A

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4 0 z

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86 87 88 89 90 91 92 93 94 95 96 97 98 99 CALENDAR YEAR ANALYSIS FAILURE LINE

  • ACTUAL DATA CV TYPE 5 FAILURE RATE

= 1.53-07 /HR SLOPE OF' ANALYSIS FAILURE LINE

= [(CV TYPE 5 F.R.) * (OPERATING HOURS)) /

(CALENDAR YEARS)

= [(1.53E-07 /HR) * (3.92SE+06 HRS)] /

(6.42 CAL. YRS.) = 0.094 FAIL./CAL. YR.

INDIAN POINT UNIT No. 2 UFSAR FIGURE 14.1-66 TRACKING B-95/96 CONTROL VALVE (CV) TYPE 5 FAILURES CONTROL VALVE STICKS OPEN MIC. No. 2001MB1541 I REV. No. 17A

1E Initial Case

. o::i - :-:...

WHEN JUSTIRED USING THE APPROPRIATE CURVE, NOMINAL TEST INTERVALS UP TO 3 MONTHS ARE RECOMMENDED.

Turt>Jn* Valve Test Interval (months)

Curve #1:

SlUVeillaoce of stop valve discs occurs every 18 months. Testing of valve freedom of movement oocurs at inteJVals of 1 to 6 months (horizonlal axis).

Curve 12:

Surveillance of stop valve discs occurs every 24 months. Tt.sting of valve freedom of movement occurs at intervals of 1 to 6 months (horizontal axis).

Estimated 3.7E-06/r for 3 month test interval for Curve #2 INDIAN POINT UNIT No. 2 UFSAR FIGURE 14.1-67 ANNUAL FREQUENCY OF DESTRUCTIVE OVERSPEED FOR VARIOUS BB-95/96 TURBINE VALVE TEST INTERVAL (1-0N-1 SV-CV TURBINE / 1 OUT OF 4 STEAM PATHS)

MIC. No. 2001MB1542 REV. No. 17A