Text

Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26, Chapter 14, Safety Analysis, Figures 14.0-1 to 14.1-67
	ML16280A218
Person / Time
Site:	Indian Point
Issue date:	09/19/2016
From:	; Entergy Nuclear Operations
To:	; Office of Nuclear Reactor Regulation
Shared Package
ML16280A161	List: ML16280A153; ML16280A159; ML16280A160; ML16280A162; ML16280A163; ML16280A164; ML16280A165; ML16280A166; ML16280A167; ML16280A168; ML16280A187; ML16280A188; ML16280A189; ML16280A190; ML16280A191; ML16280A192; ML16280A193; ML16280A194; ML16280A195; ML16280A196; ML16280A197; ML16280A198; ML16280A206; ML16280A207; ML16280A208; ML16280A209; ML16280A210; ML16280A211; ML16280A212; ML16280A213; ML16280A214; ML16280A215; ML16280A216; ML16280A217; ML16280A218; ML16280A220; ML16280A221; ML16280A222; ML16280A223; ML16280A224; ML16280A228; ML16280A229; NL-16-109, HI-2094289, Licensing Report on the Inter-Unit Transfer of Spent Fuel at the Indian Point Energy Center; NL-16-109, Indian Point 2 Improved Technical Specifications Bases; NL-16-109, Indian Point 2 Technical Requirements Manual; NL-16-109, Indian Point Unit No. 2 Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26, Chapter 10, Steam and Power Conversion System; NL-16-109, Indian Point Unit No. 2 Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26, Chapter 10, Steam and Power Conversion System, Figure 10.1-1, Revision 21 to Figure 10.2-9; NL-16-109, Indian Point Unit No. 2 Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26, Chapter 10, Steam and Power Conversion System, Figures 10.2-1 to 10.2-7; NL-16-109, Indian Point Unit No. 2 Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26, Chapter 11, Waste Disposal and Radiation Protection System; NL-16-109, Indian Point Unit No. 2 Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26, Chapter 11, Waste Disposal and Radiation Protection System, Drawing No. 9321-F-2719-136 to Drawing No. 9321-F-2730-75; ... further results
References
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HFP CONDITIONS MANUAL ROD CONTROL PRESSURIZER PRESSURE AND DNBR vs TIME UFSAR FIGURE 14.1-45, sht.2 j REV. No. 19

80 60 --

7-;:;:-

Ji! "

~f 40 g.l

_s.......

20 0

' ~

0 sQ 100 150 200 TIME (SECONDS}

580 1

f

.i!

570 -

E!

~

~i 560 -

°'i' E!o f

550 -

8 540 0

50 100 150 200 TIME (SECONDS)

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

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

2360 ~

I~ r0 f

2340 i r

]: 2320 {

JI I

2300 I

2280 I

a-s

2! 2260

I Cf)

Cf) 2: 2240 CL 2220 2200 0

\\

2 l

10 10 10 10 10 Time (seconds) 1800....------------------.,

f \\ I \\

~1500

~

\\

0

/

3:: 1400

~

-~ 1300 I

I J:

b-t _____

_/

1200 +r ___;.-.!..-.l.....'-'.,.;_u

' 1T""j ----"---'--'~'~'

1,., ~~~!

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I 4' C

0 1

2 J

10 10 10 10 10 I

\\

11me l seconds j INDIAN POINT UNIT No. 2 LOSS OF ALL AC POWER, HIGH Tavg PROGRAM, PRESSURIZER PRESSURE AND PRESSURIZER WATER VOLUME vs TIME UFSAR FIGURE 14.1-50, sht.1 I REV. No. 19

':l I

1 0 *1

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0 c 1

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0

.6 Lt-x

~ A 0

(l)

r:

Q)

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0

(_)

0 r

r 0

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J 4

10 10 10 10 10 (seconds)

INDIAN POINT UNIT No. 2 LOSS OF ALL AC POWER, HIGH Tavg PROGRAM, NUCLEAR POWER AND CORE HEAT FLUX VS TIME UFSAR FIGURE 14.1-50, sht.2 REV. No. 19

u...

HOT LEG

COLD LEG SA URATION

~ 660

<l.>

620 580 N 1-

/'-----------

g-s40

__,/

0

_J 500 I

I ll I

' !\\

'1 j

I I

0 l

2 J

10 10 10 10 Time (seconds)

HOT EG

COLD LEG SATURATION u...

~ 660

--- - -- ----- - ------ -- ____......... --4"-..,~_,.... -_

... -----.. __.,.---,\\. ___...,,.,,-

(1) 620 {

580}1-----~~

f-j_

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!54-0L ___ m 5001 I

11 1

I G

I 2

10 10 10 r

ilme l seconds;

. " I 4

1()

I

" I 4

10 INDIAN POINT UNIT No. 2 LOSS OF ALL AC POWER TO THE STATION AUXILARIES, HIGH Tavg PROGRAM, LOOP 21 AND LOOP 23 TEMPERATURE vs TIME UFSAR FIGURE 14.1-50, sht.3 REV. No. 19

1200 c;-1100

. u:;

Cl..

'-._./

1000 I

E 900 0

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(// -

800 C'-l Cl..

0 0

700

......J 600 0

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3 10 10 10 10 10 Time (seconds) 1200

('\\

0 1100 I

us Cl..

2 1000

l en

~ 900{

w

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(/)

"" 800 I

C'-l Cl..

0 I

0 700

_l 600

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'1 0

2 J

10 10 10 10 10 r

(

d \\

1me,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

1.2------------------,

0 c::

.a

.Q u

0 6

.6 3::

0 lJ...

(/)

.4 u

a:::

0 0

.2 f--

0-+--'-..__._'-'-'-'-'....-_.._~.............--~~...........,-~~---,

0 10 0

10 1

10 I

10 2

10 Time (seconds) 2 10 Time (seconds) 3 10 J

10

~

10 4

10 INDIAN POINT UNIT No. 2 LOSS OF ALL AC POWER TO THE STATION AUXILARIES, INTERMEDIATE Tavg PROGRAM, TOTAL RCS FLOW AND PRESSURIZER RELIEF RATE vs TIME UFSAR FIGURE 14.1-50, sht.SIREV. No. 19

16 15 14 13 12 Vl 11 L;J 0::

10

..J <

9 8

L;J 7

(l.

I-6 Vl 5

LL.

4 0

ci 3

z L;J 2

1 j:::

5 0

IE 86 87 88 89 90 91 u

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.) = 1.1 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

w tl..

1-If) 5 4

3

~ t-~~*==:::t:::=:C::1:::L1:::=~1:::::::=l~:;:l::=:=l===l===~l=:l~:l~~~I~

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

= ((SY TYPE 2 F.R.) * (OPERATING HOURS)] / (CALENDAR YEARS)

= [(2.05E-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

V'l 5

~~.d'=::::t::::=L1==}1=====1~1==~,====1~=,~=~1=:1~~~,:*:,~J 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 SLOPE OF ANALYSIS FAILURE LINE

= 2.05-07 /HR

= ((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

Vl 11 w

a::

i 10

...J <

9 i....

"Of-8 WJ 7

a..

6 u

5 i....

4 0

0 3

z w

2

?::

1 j

0

i

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

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

u 5

4 3

~

2 0 z 0

I I

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

ACTUAL DATA CV TYPE 5 F'AILURF.: RAT£

= 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

ProbabHily of Destructive Overspeed (y....-')

Initial Case 1E

._..~..___..___, WHEN JUSTIRED USING THE APPROPRIATE

'--i,.,--........... -i CURVE, NOMINAL TEST INTERVALS UP TO 3 MONTHS ARE RECOMMENDED.

Turt>Jn* Valve Test lnt.rval (months)

Curve 11:

SlUVeillaoce o4 stop valve discs occurs every 18 months. Testing o4 valve freedom of movement oocurs at inteJVals of 1 to 6 months (horizonlal axis).

Cul'V9 12:

Surveillance of stop valve discs occurs evfJfY 24 months. Tt.sting of valve freedom of movement occtn 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

ML16280A218

Text

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