ML16280A218

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
NL-16-109
Download: ML16280A218 (57)

Text

TOO I I I / v I I 90 I I -I j I ::c l I-a: f I Q !O :a I 7 .... I < I-Cl 70 I-I I.I.. I 0 .... 60 z ...., u I a: ..... A. 50 -I z: 0 -,_ '° a:: ..... I .,, z ->-30 .... I -> -,_ 20 u I < ..... a:: 10 / 0 I -f/ I I I I I I I I 0 1 2 3 ' TI"E FRO" ROD RELEASE (SEC) INDIAN POINT UNIT No. 2 UFSAR FIGURE 14.0-1 REACTIVITY INSERTION vs TIME FOR REACTOR TRIP MIC. No. 1999MC3969 I REV. No. 17A

'--0 -1 10 :::J :z: -2 10 0 5 10 f5 20 25 30 Time (Seconds)

INDIAN POINT UNIT No. 2 UNCONTROLLED RCCA WITHDRAWAL FROM A SUBCRITICAL CONDITION NUCLEAR POWER vs TIME UFSAR FIGURE 14.1-1 I REV. No. 19

.---.. 0 c .E 0 :z: --0 c 0 :.;::::; <..> E' LL ...__, x :::s LL ...... 0 (1) ::r:: .a .7 6 .5 .4 ,3 .2 .1 5 (\ 10 15 20 25 30 Time (Seconds)

INDIAN POINT UNIT No. 2 UNCONTROLLED RCCA WITHDRAWAL FROM A SUBCRITICAL CONDITION HEAT FLUX vs TIME, AVG. CHANNEL UFSAR FIGURE 14.1-2 I REV. No. 19

-*-uei Center l ine empe ature ----Fuel Ave age Tem p era t ure 2500 ......------------------.

Q) 1500 !..... :J 0 !..... g_ 1000 E Q) f-Q) 500 :J LL 0 ! 0 1' I \ r ; ; \ \ \ ' ' ' ' ' ' 5 10 15 20 25 30 Time (Seconds)

INDIAN POINT UNIT No. 2 UNCONTROLLED RCCA WITHDRAWAL FROM A SUBCRITICAL CONDITION FUEL AVERAGE TEMPERATURE vs TIME AT HOT SPOT UFSAR FIGURE 14.1-3 I REV. No. 19 750 ""'O ..2 600 (._) 550 F-----__J 0 5 10 15 20 25 30 (Seconds)

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 I REV. No. 19

-0 0+-"---'--'--r--'--"'-'-r-'--'--....._.r----'---'--'--r-...__....__..--;

0 2 4 6 8 10 TIME (SECONDS) 1.2 ---.. 0 1.1 c .E 1 0 :z: 0 .9 .8 .7 6 .5 4 0 2 8 10 INDIAN POINT UNIT No. 2 UNCONTROLLED RCCA BANK WITHDRAWAL FROM FULL POWER WITH MINIMUM REACTIVITY FEEDBACK (70 pcm/sec WITHDRAWAL RATE). NUCLEAR POWER ANO CORE HEAT FLUX vs TIME UFSAR FIGURE 14.1-5 I REV. No. 19 2320 2300 L.i.J 5 2280 (/') (/') LlJ g: 2260 a::: L.i.J '.:::::! 2240 a::: ::::> (/') (/') 2220 CL 2200-l-'--'--'--.---'--'---'--r---'--'--"--,--'---'--'--r-'--'--'"-I

() 2 4 6 8 iO TIME (SECONDS)

.---. 1170 Q5 ..£1: u 1165 :.0 :::i (_) ..__,. i160 .J155 1150 1145 1140 \ 1135 0 2 4 6 8 10 (SECONDS)

INDIAN POINT UNIT No. 2 UNCONTROLLED RCCA BANK WITHDRAWAL FROM FULL POWER WITH MINIMUM REACTIVITY FEEDBACK (70 pcm/sec WITHDRAWAL RATE), PRESSURIZER PRESSURE AND WATER VOLUME vs TIME UFSAR FIGURE 14.1-6 I REV. No. 19

.--. 576......-------------------, w_ I v ID g, 574 572-1-----

4 3.5 3 **2.5 2 15 0 2 ' ' 4 6 8 10 T!ME (SECONDS)

INDIAN POINT UNIT No. 2 UNCONTROLLED RCCA BANK WITHDRAWAL FROM FULL POWER WITH MINIMUM REACTIVITY I FEEDBACK (70 pcm/sec WITHDRAWAL RATE). CORE WATER AVERAGE TEMPERATURE AND DNBR vs TIME UFSAR FIGURE 14.1-7 REV. No. 19 i.2-.------------------

0 c:: .8 .Q u .6 .___, 0:::: L.i..J .4 Q.. .2-_J (.) :::> z I) 20 60 80 100 120 140 160 TIME (SECONDS) 1.2 1.1 ..--.. 0 c: .E 1 0 z 0 .9 c:: .Q u .8 0 '-1--iS .6 :r: 5 .4 0 20 40 120 140 160 INDIAN POINT UNIT No. 2 UNCONTROLLED RCCA BANK WITHDRAWAL FROM FULL POWER WITH MINIMUM REACTIVITY FEEDBACK (1 pcm/sec WITHDRAWAL RATE), NUCLEAR POWER AND CORE HEAT FLUX vs TIME UFSAR FIGURE 14.1-8 I REV. No. 19

...-.... 0 2350 -w 0:: :::> (./') 2300 0:: 0.... ffi 2250 N 0:: :::> (./') 2200 0:: 0.... 2150 0 ..l.-.:--'-r20....l-l.-'-r40-l-...l-'-,60r-'--'-'-80r-'-.l..-.J.-1,-00"'--'--'-1.-20...._._

..... 1-r40-'-'---"-!160 w ::?: 3 1400 0:: w !;;;: 1300 3:: 0:: w N 5 1200 (./') (,/) w 0:: 0.... TIME (SECONDS) 1100 ..j......L.-'--'-...,...-'-'--"-r-'--'-r--'--'--"--r-'---'--T--'--'r-'--r-._,_.---'-'-1 0 20 40 50 80 100 120 140 160 TIME (SECONDS)

INDIAN POINT UNIT No. 2 UNCONTROLLED RCCA BANK WITHDRAWAL f'ROM f'ULL POWER WITH MINIMUM REACTIVITY FEEDBACK (1 pcm/sec WITHDRAWAL RATE). PRESSURIZER PRESSURE ANO WATER VOLUME vs TIME UFSAR FIGURE 14. 1-9 I REV. No. 19

-595 ..,.------------------.

w_ I &S g, 590 a:::: CD z: Cl 3 2.5 2 1.5 20 40 0 20 40 60 80 100 120 140 160 TIME (SECONDS) 60 80 100 120 140 160 TIME (SECONDS)

INDIAN POINT UNIT No. 2 UNCONTROLLED RCCA BANK WITHDRAWAL FROM FULL POWER WITH MINIMUM REACTIVITY FEEDBACK (1 pcm/sec WITHDRAWAL RATE). CORE WATER AVERAGE TEMPERATURE AND DNBR vs TIME UFSAR FIGURE 14.1-10 I REV. No. 19

--Minimum Feedback ----Mox\mum Feedback 2.2 --------------------, 2 1.6 -1 10 I / I , / / --'-.. "'HIGH NEUTRON OT.& T TRIP ...---'....__---+--FLUX TRIP ' \ \\I \ I II ' 0 I 2 10 10 10 Reactivity Addition Rate [pcm/second]

INDIAN POINT UNIT No. 2 MINIMUM DNBR VERSUS REACTIVITY INSERTION RATE, ROD WITHDRAWAL FROM 100 PERCENT POWER UFSAR FIGURE 14.1-11 I REV. No. 19

--Mir;;mum Feedback ----Maximum F'eedbock 2.4 2.3 2.2 2.1 1.7 1.5 1-5 _, io OfoTTRIP t .... I ', I I I ..._ I ' I 'I HIGH NEUTRON FLUX TRIP 18 1d Reactivity Addition Rate (pcm/second]

J 10 INDIAN POINT UNIT No. 2 MINIMUM DNBR VERSUS REACTIVITY INSERTION RATE, ROD WITHDRAWAL FROM 60 PERCENT POWER UFSAR FIGURE 14.1-12 I REV. No. 19

--Min i mum ;"eedbock ----Mcxirr\um Feedbock 2-4 -,-------------------..

2.3 2.2 2.1 = 2 = 1.9 c::: ::i§ 1.8 1.7 1.6 1.5 1.4 -* 10 OTL\TTRIP I J\ __ -' HIGH NEUTRON FLUX TRIP 18 1d 16 16 Reactivity Addition Rate [pcm/second]

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

o 100 Time (seconds) 0 .s 6 .4 .2 0 INDIAN POINT UNIT No. 2 DROPPED ROD INCIDENT MANUAL ROD CONTROL NUCLEAR POWER AND CORE HEAT FLUX AT BOL (SMALL NEGATIVE MTC) FOR DROPPED RCCA OF WORTH -400 PCM UFSAR FIGURE 14.1-14 I REV. No. 19 620 0 50 100 150 200 Time (seconds) 620 ....-------------------, 0 50 100 150 200 INDIAN POINT UNIT No. 2 DROPPED ROD INCIDENT MANUAL ROD CONTROL CORE AVERAGE ANO VESSEL INLET TEMPERATURE AT BOL (SMALL NEGATIVE MTC) FOR DROPPED RCCA OF WORTH -400 PCM UFSAR FIGURE 14.1-15 I REV. No. 19 Time (seconds)

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 UFSAR FIGURE 14.1-16 REV. No. 19 1.2 0 .6 w__ '--" .4 I-0 .2 <l> u :::> :z 0 0 50 100 150 200 1.2-.------------------, 0 .8 .6 .4 .2 0 0 50 100 200 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 -400 PCM UFSAR FIGURE 14.1-17 I REV. No. 19 I I 620 ..--.. LL.. 600 580 560 540 520 500 Time (seconds)

INDIAN POINT UNIT No. 2 DROPPED ROD INCIDENT MANUAL ROD CONTROL CORE AVERAGE ANO VESSEL INLET TEMPERATURE AT EOL (LARGE NEGATIVE MTC) FOR DROPPED RCCA OF WORTH -400 PCM UFSAR FIGURE 14. 1-18 REV. No. 19 2600 2400 t 2200 [> 2000 N >-::::l en U) J: 1800 0 50 100 150 200 Time (seconds)

INDIAN POINT UNIT No. 2 DROPPED ROD INCIDENT MANUAL ROD CONTROL PRESSURIZER PRESSURE AT EOL (LARGE NEGATIVE MTC) FOR DROPPED RCCA OF WORTH -400 PCM UFSAR FIGURE 14.1-19 I REV. No. 19

.2 O-l--'--"--'--!-.J-.J.-'--+--'--'---'--+--'-......_.--t-_.__._..._._, 0 4 6 8 10 TIME (SECONDS) 1.2.....------------------, :i .8 XO ::I :z: .... .... o .6 :x:g .4 .2 0-1--_.i..-'--!-.J-.J.-'--+--'--'--+--'-""---'--t--'--'--"'-1 0 2 4 6 8 10 TIME (SECONDS)

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. 19 311: 9 750 .... Su-zi.s -VI 700 w'-8 ....... ;I. b ..... 65() 600 0 1.2 311: 9 .8 :zo :::>Z ;;Ji.. .6 go a.Z oe 98 .4 !J--.2 .... 0 0 2 2 4 6 8 10 TIME (SECONDS) 4 6 8 10 TIME (SECONDS)

INDIAN POINT UNIT No. 2 LOSS OF ONE PUMP OUT OF FOUR TOTAL CORE FLOW AND FAULTED LOOP FLOW vs TIME UFSAR FIGURE 14. 1 -21 REV. No. 19

___ 5 3 2 0 2 4 6 10 2 TIME (SECONDS) 4 6 Tll.!E (SECONDS) 8 INDIAN POINT UNIT No. 2 LOSS OF ONE PUMP OUT OF FOUR PRESSURIZER PRESSURE AND DNBR vs TIME UFSAR FIGURE 14.1-22 I REV. No. 19 1.2.....-----------------, 04--'--'--+--"--'-'--f--'--'--+_.__.__'-t"_.__._......, 0 4 6 8 10 TIME (SECONDS)

.2 04--'--"--+--'--'--+--'--'--l--'--'-'-+_._-'-"'-i 0 2 4 6 8 10 TIME (SECONDS}

INDIAN POINT UNIT No. 2 FOUR PUMP LOSS OF FLOW -UNDERVOLTAGE NUCLEAR POWER AND CORE HEAT FLUX vs TIME UFSAR FIGURE 14.1-23 I REV. No. 19 800 700 !3u-600 zu.i -en u.i';;)-o::t: g.._, 500 g 400 300 0 4 6 8 10 TIME (SECONDS) 1.2 9,..,. .8 23 0::0 tiz ::EL>. 3o .6 §?5 n.-gti .4 .:IE .2 0 ll 2 4 & 8 10 TIME (SECONDS)

INDIAN POINT UNIT No. 2 FOUR PUMP LOSS OF FLOW -UNDERVOLTAGE TOTAL CORE FLOW AND RCS LOOP FLOW VS TIME UFSAR FIGURE 14.1-24 I REV. No. 19 0 2 TIME (SECONDS) 4 6 TIME (SECONDS)

INDIAN B 10 POINT UNIT No. 2 FOUR PUMP LOSS OF FLOW -UNDERVOLTAGE PRESSURIZER PRESSURE AND DNBR vs TIME UFSAR FIGURE 14.1-25 I REV. No. 19 1.2---------------------.

TIME (SECONDS)

.2 0 2 4 6 8 10 TIME (SECONDS)

INDIAN POINT UNIT No. 2 FOUR PUMP LOSS OF FLOW -UNDERFREQUENCY NUCLEAR POWER AND HEAT FLUX vs TIME UFSAR FIGURE 14.1-26 I REV. No. 19 800 700 ): g 600 r... 5'6' 500 z:ll.I 400 8---e 300 200 100 0 2 4 8 10 TIME (SECONDS) 1.2 ): g,.....

.8 (.)_ :::lz: 3:5 .6 .4

.2 I) 0 2 4 6 8 10 TIME (SECONDS)

INDIAN POINT UNIT No. 2 FOUR PUMP LOSS OF FLOW -UNOERFREQUENCY TOTAL CORE FLOW ANO RCS LOOP FLOW vs TIME UFSAR FIGURE 14.1-27 I REV. No. 19

0 2 3 2 0 2 4 6 TIME (SECONDS) 4 6 TIME (SECONDS) 8 10 B INDIAN POINT UNIT No. 2 FOUR PUMP LOSS OF FLOW -UNDERFREOUENCY PRESSURIZER PRESSURE AND DNBR vs TIME UFSAR FIGURE 14.1-28 I REV. No. 19 u t j ca 1=-i I&. 1).6 in IM la. -G.2 0 0

• 4 * ,, ... (Stt::ONDS) 1100 -2500 w IE u 2JOO I . -21i00 -0 4

• I 18 "nYE: (SEC'ONDS)

INDIAN POINT UNIT No. 2 LOCKED ROTOR NUCLEAR POWER AND RCS PRESSURE vs TIME UFSAR FIGURE 14. 1 -29 I REV. No. 22

• 5 11WE: {S!CtlNtlS) a 4 ti Tl WE: (SE:COMD$:)

Hl INDIAN POINT UNIT No. 2 LOCKED ROTOR TOTAL CORE FLOW AND FAULTED LOOP FLOW vs TIME UFSAR FIGURE 14.1-30 I REV. No. 22

0 f 6 llM£

'O INDIAN POINT UNIT No. 2 LOCKED ROTOR FUEL CLAD INNER TEMPERATURE vs TIME UFSAR FIGURE 14.1-30A I REV. No. 22

,--..., 1.2------------------, 0 c:

z: w s 2300 (./) (./) w g::: 2200 a::: w 20 40 60 TIME (SECONDS) 80 100 2100 I (/) (./) 2000 CL 1900

-"--'---'--r-1

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

0 20 40 60 80 100 TIME (SECONDS)

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 j REV. No. 19 I 20 40 60 80 100 TIME (SECONDS) 1700-.------------------, ---0 *u; -..S 1600 w ::::;;: 1500 §; a::: 1400 ES 1300 N a::: {

0 2b 40 60 80 100 TIME (SECONDS)

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 3.5 3 a::: §@ 2.5 a 2 1.5 1+-""---"-"--,--'---'-'-r-'--'--'---r-"--'-_._-r-_._...__'-1 0 20 40 60 80 100 TIME (SECONDS)

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 TIME --Iii'!' L{)lller -----Prtthirlz*r Pr1<U1!Jre

oo INDIAN POINT UNIT No. 2 LOSS OF LOAD WITHOUT PRESSURIZER SPRAY AND PORV, NUCLEAR POWER AND PRESSURIZER PRESSURE vs TIME UFSAR FIGURE 14.1-37 I REV. No. 22

l{f .w, lifJ TI ME 1;ror1 0:::: L.&.J !ZOO t !C(t:i goo (I 20 4lll 31) 100 llME f!!;\E \""' INDIAN POINT UNIT No. 2 LOSS OF LOAD WITHOUT PRESSURIZER SPRAY AND POWER OPERATED RELIEF VALVES, AVERAGE COOLANT TEMPERATURE AND PRESSURIZER WATER VOLUME vs TIME UFSAR FIGURE 14.1-38 I REV. No. 22 40* 60 (SECONDS)

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 I REV. No. 22 0 10 1 10 2 10 Ti me (seconds) 3 10 4 10 1800 -------------------, _.-.._ C) 17DD u :.0 ::::> s 1600 Cl> E ::::> g 1500 \ rv \ 1400 { 1300 { o_ "'---------

0 10 \ iO 2 10 3 10 4 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 FIGURE 14.1-43, sht.1 REV. No. 19 1.2 -...---------------------i u_ '--' '--(!) :;:: 0 o_ .6 --4 -J 0 10 1 10 2 10 Time (seconds) 3 10

• 10 1.2----------------

.--.. Cl .s: 1 E 0 :z: 0 .a .4 ..,_, Cl :1 (!) ::r: <l.> ..._ 0 (..) 0 10 I 1 10 \ I 2 iO ( ' \ seconas; I :l 10

• 10 INDIAN POINT UNIT No. 2 LOSS OF NORMAL FEEDWATER, OFFSITE POWER AVAILABLE, HIGH Tavg PROGRAM, NUCLEAR POWER AND CORE HEAT FLUX vs TIME UFSAR FIGURE 14.1-43, sht.21 REV. No. 19

--HO LEG ----CO 0 LEG SA RATION 700 ...,----------------------.

N g-540 .3 0 10 ------------.,.,, I 10 --HO LEG ----CO 0 LEG SA URATION / ,, 2 10 Time (seconds) 3 1()

• 10 700 ....--------------------.

0 ;o I 10 2 10 (seconds) l 10

• 10 INDIAN POINT UNIT No. 2 LOSS OF NORMAL FEEDWATER, OFFSITE POWER AVAILABLE, HIGH Tavg PROGRAM, LOOP 21 AND LOOP 23 TEMPERATURE vs TIME UFSAR FIGURE 14.1-43, sht.3IREV.

No. 19 1200 c;-1100 * (/j CL ----1000 E 900 0 <I.) u:; 800 C'.J 0.. 0 0 700 -' 600 0 10 t 10 z 10 Time (seconds)

J 10 4 10 1000 -::::> (.() (.() (JJ '-CL 900 E 0 (JJ u:; ,.,., 800 C'J I ..::: 700 !--------./

........ 1 0 I 2 l 4 10 10 10 10 10 Time (seconds)

INDIAN POINT UNIT No. 2 LOSS OF NORMAL FEEDWATER, OFFSITE POWER AVAILABLE, HIGH Tavg PROGRAM, STEAM GENERATOR 21 AND STEAM GENERATOR 23 PRESSURE vs TIME UFSAR FIGURE 14.1-43, sht.41 REV. No. 19

.....--. 0 :.;:; *c: 0 3: 0 c;: if) (..) a::: 0 _...., 0 ;..-J.2 1 .8 .6 .4 .2 0 0 10 1 10 2 10 Time (seconds) l-I 3 10 4 10 .I

............

-'-'-'-'-'-1 l 10 2 lO Time (seconds)

J 10 4 10 INDIAN POINT UNIT No. 2 LOSS OF NORMAL FEEDWATER, OFFSITE POWER AVAILABLE, HIGH Tavg PROGRAM ,TOTAL RCS FLOW AND PRESSURIZER RELIEF vs TIME UFSAR FIGURE 14.1-43, sht.5 I REV. No. 19 1.2 ...----------------------, -::::;-;i .8 .... 00 a. :z .6 .... 00 .4 ... .._. .2 .... 0 I . 0 50 100 150 200 TIME (SECONDS) 1.2 .8 I-.6 .4-.2 -o.r........_....._......_'--1....._--'-_._-'--+-_.::::::::i=::::::==l===-----........i o 100 1so 2m TIME (SECONDS)

INDIAN POINT UNIT No. 2 FEEOWATER SYSTEM MALf'UNCTION EXCESSIVE FEEOWATER FLOW -HFP CONDITIONS MANUAL ROD CONTROL NUCLEAR POWER ANO CORE HEAT FLUX vs TIME UFSAR FIGURE 14.1-45, sht.1 I REV. No. 19 1600-l--'--"'--'--l--l--J..-l--'---'---l--'--'--'---'-+

1-'------'--"--1 0 so 100 1So 200 TIME (SECONDS) 4 .... 0:: m 3 i-z 0 2 I-I fl s'o 100 150 200 TIME (SECONDS)

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 80 -7-;:;:-Ji! " 40 g.l _s ....... 20 0 ' ' ' 0 sQ 100 150 200 TIME (SECONDS}

580 1 f .i! 570 -E! 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 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 \ \ 0 / 3:: 1400 1300 I I J: b-t _____ _/ 1200 +r ___;.-.!..-.l.....'-'.,.;_u

' 1 T""j 1 ,.,

I 4' C 0 1 2 J

• 10 1 0 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 '{ Q5 I I "" .4 0 Q_ l '-.2 J I 0 Q) I u ::::> 0 t :z:: ' 1 * ! I' I I ' I I t I r It li l 0 1 2 J

• 10 10 iO 10 10 Time (seconds) 1.2 ' -:::::-. 0 c 1 .E 0 :z 0 .a c .Q 0 0 .6 '-Lt-...__. x ::::> A 0 (l) ::r: Q) .2 -0 (_) 0 r r 0 '1 l J 4 1 0 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 {

f-.... ' ,,-, j_ I ' !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 Q) __, (// -800 C'-l Cl.. 0 0 700 ......J 600 0 l 2 3

• 10 10 10 10 10 Time (seconds) 1200 ('\ 0 1100 I *us Cl.. "'---' 2 1000 :::l en "' 900{ w } (/) "" 800 I C'-l Cl.. 0 I 0 700 _l 600 ,. I '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 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 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 :

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 0 z 0

• I I I I I I I 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 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