View source for NL-13-130, Indian Point, Unit 2, Updated Final Safety Analysis Report (Ufsar), Rev. 24, Chapter 5 - Figure 5.3-1 Through Figure 5.2-29

{{Adams
| number = ML13291A304
| issue date = 09/26/2013
| title = Indian Point, Unit 2, Updated Final Safety Analysis Report (Ufsar), Rev. 24, Chapter 5 - Figure 5.3-1 Through Figure 5.2-29
| author name = 
| author affiliation = Entergy Nuclear Operations, Inc
| addressee name = 
| addressee affiliation = NRC/NRR
| docket = 05000247
| license number = DPR-026
| contact person = 
| case reference number = NL-13-130
| document type = Updated Final Safety Analysis Report (UFSAR)
| page count = 76
}}

=Text=
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51:'.co,\u vuq.-* POINT UNIT No. FIGURE 5.1-23 2 REINFORCING DETAIL MIC. No. 1999MC3762 I REV. No. 17A n 4'-6 EXTERI-OR WALL 2'-0 OP I FLOOR 0 PS PRIMARY SHIELD WALL INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.1 -24 REACTOR CAVITY PIT MIC. No. 1999MC3763 REV. No. 17 A Er::i?UIPMEAIT HAT::././
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'[CONT a INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.1 -26 TORSIONAL EFFECTS MIC. No. 1999MC3765 I REV. No. 17 A  
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PIPING INDIAN POINT UNIT No. 2 UFSAR FIGURE 5. 1 -30 TYPICAL PIPING PENETRATION MIC. No. 1999MC3769 REV. No. 17 A All2 TEST COIJIJ*-, .; 
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= :.. .ooeq INDIAN POINT UNIT No. 2 UFSAR FIGURE 5. 1 -33 CONTAINMENT-STRESSES ON PENETRATIONS AND LINER -SHEET 7 MIC. No. 1999MC3772 I REV. No. 17 A ct I -rl 7. 0 !-\) w (f) D:'.'. 0 _J l-w '\..) ifl <:( t/) (THIS FIGURE DEPICTS ORIGINAL HISTORICAL DESIGN DATA AND DOES NOT REFLECT THE CURRENT CONFIGURATION OR ANALYSIS.) 
(/) (/) (/) \==! (Y) 0::: 0::: 0::: CD CD CD (Y) _J _J _J <( <( <( L. I-I-I-z z z 0 w w w 0::: 0::: 0::: w w w }-LL LL LL u ::J ::J ::J Ul 0 (/) 0 0 VJ 0::: 0::: 0::: 0::: 0 CD 0 0 0::: _J CD <( I-_J _J z _J _J <( <( w <( <( z z 0::: z z 0 0 w 0 0 ::J ::J LL ::J ::J I-I-I-I-::J 'Z " " 0 " " V'l 0 z z 0::: z z !J.J 0 0 0 0 *__; _J _J () _J _J Q "-'Z. *w v 111 0 e @ e @0 D m ..J er I n; I L. 0 -l-J w (/J INDIAN POINT UNIT No. 2 UFSAR FIGURE 5. 1 -34 ASSUMED PIPE RUPTURE ACCIDENT BREAK LOCATIONS MIC. No. 1999MC3773 REV. No. 17 A 2.7 (3. 9) 4.0 (5. 4) -1. 8 (-5.3) For Section location, see Figure 5.1-43 2.6 (20.6) 2.4 (17.0) -4.2 (6.8) -6.9 (8.4) -9.2 (SO. 8) (THIS FIGURE DEPICTS ORIGINAL HISTORICAL DESIGN DATA AND DOES NOT REFLECT THE CURRENT CONFIGURATION OR ANALYSIS.) 
' \ 0.0 (1. 2) MIC. -0.6 {4. 3) 2.6 (3. 7) 2.6 (-3.9) / -2.6 ...,"':' (-25.4) 
/ (6.1) -3.4 (-30. 6) -4.6 (-11.4) -5.3 <iz. ffitDRAULIC 
,,/"./ 'SNUB8eRS INDIAN POINT UNIT No. UFSAR FIGURE 5. 1 -35 STEAM GENERATOR SUPPORT -SECTION 1 -1 2 No. 1999MC377 4 I REV. No. 17A For Section location, see Figure 5.1-43 0.0 
: 1. 7 (-2.6) 4.3 (5.6) 2.1 (21.8) 1.4 (24.C) -4.0 (-10.0) -12.6 (49. 2) -6.S (-15.0)\ -2.7 (5.4) 0.1 (1. 7) \. / 1.3 (9.2) /.6.6 -4.3 (24.1) 
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1.1 (9.4) INDIAN POINT UNIT No. UFSAR FIGURE 5.1-36 (THIS FIGURE DEPICTS ORIGINAL HISTORICAL DESIGN DATA AND DOES NOT REFLECT THE CURRENT CONFIGURATION OR ANALYSIS.)
STEAM GENERATOR SUPPORT -SECTION 2-2 2 MIC. No. 1999MC3775 
!REV. No. 17A 0.0 3.1 (-5.8) 3.2 (-6.1) -2.0 (-28.1) .12 ( 2. 2) '
0.8 // -4 3
____ . For Section location, see Figure 5.1-43 -4.5 (-15.2) -12.2 (-54.8) (THIS FIGURE DEPICTS ORIGINAL HISTORICAL DESIGN DATA AND DOES NOT REFLECT THE CURRENT CONFIGURATION OR ANALYSIS.) 
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9.9 (15.1) INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.1-37 STEAM GENERATOR SUPPORT-SECTION 3-3 MIC. No. 1999MC3776 REV. No. 17 A o.c (1. 27) ': 
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0.1 (l. 4) !----'-For Section location, see Figure 5.1-43 (THIS FIGURE DEPICTS ORIGINAL HISTORICAL DESIGN DATA AND DOES NOT REFLECT THE CURRENT CONFIGURATION OR ANALYSIS.) 
-2.5 (-5. 5) 1. 0 (8.3) .///,, INDIAN POINT UNIT No. UFSAR FIGURE 5.1 -38 STEAM GENERATOR SUPPORT -SECTION 4-4 2 MIC. No. 1999MC3777 IREV. No. 17A  
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For Section location, see Figure 5.1-44 (THIS FIGURE DEPICTS ORIGINAL HISTORICAL DESIGN DATA AND DOES NOT REFLECT THE CURRENT CONFIGURATION OR ANALYSIS.)
INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.1 -39 STEAM GENERATOR SUPPORT-PLAN LOCATION ELEVATION 60 AND 63 MIC. No. 1999MC3778 IREV. No. 17A -----------
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PLAN 3-3 A.T EL. o" '1-4 .i-1 1-i PLAN /\I E:L. G3'-o" (THIS FIGURE DEPICTS ORIGINAL HISTORICAL DESIGN DATA AND DOES NOT REFLECT THE CURRENT CONFIGURATION OR ANALYSIS.)
INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.1-40 STEAM GENERATOR SUPPORT-PLAN LOCATION ELEVATION 60 AND 63 MIC. No. 1999MC3779 IREV. No. 17A For Section location, see Figure 5.1-44 11.1 (60.7 3.1 2.6 -4.0 (36.75; { ..1.._ *** (-21.7) (-12.3) 
(-14.7) 29.3 (-61.3) 30. 4. (-60.0) 31. 6 (56.2) l. 8 (13.4) {-27 .6) I i 1 ' -...* 7 \-*-* .... I , ?7 ") f l. 6 i '1 1 8' 1, -. .J * ) 1. 0 (16.5) 1lfh SE<:T10N 1-1 -A -3.4 (-9.9) 3.2 (-16.0) -2.8 1 I. 7 -. 
-7.2 (-:C;.3) -21. 0 (-J4.2) -22.0 (40.0) -22.0 32.0) INDIAN POINT UNIT No. UFSAR FIGURE 5.1-41 (THIS FIGURE DEPICTS ORIGINAL HISTORICAL DESIGN DATA AND DOES NOT REFLECT THE CURRENT CONFIGURATION OR ANALYSIS.)
PUMP SUPPORT-SECTION 2-2 AND 3-3 2 MIC. No. 1999MC3780 I REV. No. 17A For Section location, see Figure 5.1-44 -3.3 -19.S -1.6 (-10.9) -4.3 (-10.3) INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.1 -42 (THIS FIGURE DEPICTS ORIGINAL HISTORICAL DESIGN DATA AND DOES NOT REFLECT THE CURRENT CONFIGURATION OR ANALYSIS.)
PUMP SUPPORT-SECTION 3-3 MIC. No. 1999MC3781 REV. No. 17A ISOMETRIC Of ;yp1CJ\L STEftJ-.'\ 
{ 5UPPORT INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.1 -43 ISOMETRIC VIEW-STEAM GENERATOR SUPPORT MIC. No. 1999MC3782 IREV. No. 17A ISOME.iR\C OF TYPI( 1\L REA.C.TOR COOLANT PIJMP ( SUPPORT' TOP OF&deg; supporrr STRUCTURC:.
61'-11 3/4" INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.1-44 ISOMETRIC VIEW-REACTOR COOLANT PUMP SUPPORT MIC. No. 1999MC3783 REV. No. 17 A A B REACTOR PIPE VESSEL WEIGHT BREAK & PIPING REACTION CASE II p (lb) 934,000 -R (lb) 322,000 -T (lb) 140,000 1,187,00C 
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MAXIMUM FORCES ACTING ON A REACTOR VESSEL SUPPORT c D PIPE URTH-RUAKEZ BREAK I& VERTICA CASE Ill DIRECTION 525,000 395,000 --no,ooo 969,000 I A+B A+c A+D 934,000 1,459,00C l ,329,00C 322,000 322 ,000 322,00( l,327,000 850,00(] IL ,109 ,ooc PIPE BREAK CASE II IS BETWEEN PUMP AND ELL ON REACTOR NOZZLE I l .....
b PIPE BREAK CASE III IS AT STEAM GENERATOR INLET Tl R-RADIAL T-TANGENTIAL P-VERTICAL p (THIS FIGURE DEPICTS ORIGINAL HISTORICAL DESIGN DATA AND DOES NOT REFLECT THE CURRENT CONFIGURATION OR ANALYSIS.)
PLAN EARTHQUAKE IN Z DIRECTION ACTS NORMAL TO REACTOR COOLANT OUTLET LINE INDIAN POINT UNIT No. 2 UFSAR FIGURE 5. 1 -45 MAXIMUM FORCES ACTING ON A REACTOR VESSEL SUPPORT MIC. No. 1999MC3784 REV. No. 17A  
: 2,.4Ml(5"'/ . f1a* INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.1 -46 PLAN VIEW 60 FT -0 IN. MIC. No. 1999MC3785 REV. No. 17 A  
\ 2 11 aMK.C. 801 2*/!JMX.C 801 2 2 Z*"MJ<C..802 TY!! LAYER <P) REACTOR RING SCALE 1.(: 1'.0 INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.1-47 TYPICAL LAYER-REACTOR RING MIC. No. 1999MC3786 REV. No. 17 A  
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t.JQ* *LOCATION LOCATIOtJ STRUCTURAL!
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1N5Tl<:cJME>J.TATIOIJ t.ECl1:5'>AR:T FOR INDIAN POINT UNIT No. 2 UFSAR FIGURE 5. 1-56 CONTAINMENT PROOF TEST GROSS DEFORMATION MEASUREMENTS MIC. No. 1999MC3795 I REV. No. 17A I Item 1 Pressurizer Relief Tank to Gas Analyzer Item 2 Pressurizer Relief Tank N2 Supply Item 3 Pressurizer Relief Tank Makeup er: w N er: :J (/) (/) w a::: Q_ RCS STANDPIPE a::: w a::: a::: <( OJ wl _J i7i (/) ::2: TO VENT HEADER (ITEM 19) PRESSURIZER RELIEF TANK -MAKEUP 548 13 I-z w <( I-z 0 u ASWI Although the Pressurizer Relief Tank is missile protected, these penetrating lines can become exposed to containment atmosphere if the pressurizer discharge header is breached during the accident.
4136  I I S-1 I INDIAN POINT UNIT No. UFSAR FIGURE 5.2-1 2 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3411 I REV. No. 17A VALVE POSITIONS ARE NOT CONTROUED BY THIS FIGURE Item 4 Residual Heat Removal Return Item 5 Residual Heat Removal Loop To Safety Injection Pumps RWST Item 6 Residual Heat Removal Loop Out Item 7 Containment Sump Recirculation Line @ ----r---------1 I RESIDUAL I R cs HEAT I 731 741A NOTE: RECIRCULATION PUMP 14" ORN Line No. 10 I has 6" thick insulation between valves 730 and 731 730 r------------1 I RESIDUAL I 1 HEAT REMOVAL 1.__m-i I 744 L ___
N 2 (IVSWS) N2 (IVSWS) I ' I I ---,-_ _J I S.l.S. I (CLOSED I I SYSTEM) I I I I{ I l-H---_____.._---------4-!.-
7 CONTAINMENT' SUMP MISSILE BARRIER N2 -Manual N2 Pressurization SS -Sampling System ENTIRE SYSTEM SHOWN IS SEISMIC CLASS I DESIGN CONTAINMENT NOTE: A 3/16" hole is drilled through the upstream disc (nearest containment) of 885A and the downstreom disc (RHR Loop Side) of 8858 to prevent pressure locking. INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-2 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3382 REV. No. 17 A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE RCS ) < \ \ \ \ > ( REGEN. HX MISSILE BARRIER I RCS AUX. SPRAY RCS 2108 2048 211 212 210A 204A MISSILE BARRIER ITEM 8 LETDOWN LINE T PRT 2008 t 200C j FROM RHR LOOP CONTAINMENT SLOPE ASWI I 201@ @I I s-1-, eves (CLOSED SYSTEM) PRT -PRESSURIZER RELIEF TANK ITEM 9 CHARGING LINE REGEN. HEAT 1--9 374 CONTAINMENT--1 SLOPE INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-3 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3383 REV. No. 17 A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE DT -ITEM 10 REACTOR COOLANT PUMP SEAL-WATER SUPPLY LINES MSWI I ,__ ___
250,A,B,C,D 
(_) 0:: MISSILE I BARRIER! 251,E,F,G,H I L @ I L SLOPE A l-coNTAINMENT 
@ 241,A,B,C,D 4925,4926 4927,4928 ENTIRE SYSTEM SHOWN IS SEISMIC CLASS 1 DESIGN ITEM 11 REACTOR COOLANT PUMP SEAL-WATER RETURN (/) Q_ L Q_ (_) 0:: MISSILE :--1 BARRIER I -, EXCESS I LIETDOWN I HX 218 I PR L_J 215 DT CONTAINMENT-I REACTOR COOLANT DRAIN TANK 11 01 I ASWI SLOPE p 223 I I I HCV-30031 I
I S-1 ......._ --1 (CLOSED SYSTEM) P -TRIPPED CLOSED BY CONTAINMENT ISOLATION SIGNAL PHASE B PRT -PRESSURIZER RELIEF TANK INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-4 eves CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3385 IREV. No. 17A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE ITEM 12 REACTOR COOLANT SYSTEM SAMPLE LINES MISSILE BARRIERJ I LcoNTAINMENT I ASWI T I I 12 T I I (f) u 0::: L 956E I I SAMPLING (f) u 0 I SYSTEM 956F I  o::: 954A 955A SLOPE s-1-----1 ITEM 13 FUEL TRANSFER TUBE DOUBLE GASKETED SPENT FUEL PIT BLIND/ FANGE AAJ 
..... 0 MISSILE BARRIER---!
I s-1-----1 I---CONTAINMENT INDIAN POINT UNIT No. UFSAR FIGURE 5.2-5 2 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3386 I REV. No. VAL VE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE 17A ITEM 14 CONTAINMENT SPRAY HEADERS RWST 869A 878A @   SEE NOTE 1 I 1 14 LC ---,---D.O 867A (/) Q_ L ::) I Q_ MSWI >-<( 8788 O::'. Q_ (/) LC I-z w L z <( 8698 I-@ z  0 u SEE NOTE 1 I I ---14 O::'. D.O. 8678 I w O::'. I-L ___ O::'. z <( 1m w L I w z MSWI _J <( (/) I-(/) z L 0 u RWST -REFUELING WATER STORAGE TANK ENTIRE SYSTEM SHOWN IS SEISMIC CLASS 1 DESIGN NOTE 1: FLANGED ELBOW USED DURING REFUELING OPERATIONS TO FILL REACTOR REFUELING CAVITY AND CANAL INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-6 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3387 REV. No. 17 A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE O:::'. w O:::'. m 856A 8568 856C 856F 856D ITEM 15 SAFETY INJECTION HEADERS ITEM 16 SAFETY INJECTION TEST LINE t <( OJ I.[) OJ t m OJ Lf) OJ 1-z I z 4: 1-z 0 u 15 15 <( N I.[) OJ m N Lf) OJ 6) I MSWI _J --, I MSW! I I D.O. I ASWI 8508 -,---849A (/) Q_ 2 :::> Q_ z 0 i== u w I --:> z I >-I I-w I LL <( I (/) -I I 8498 I I L ___ ENTIRE SYSTEM SHOWN IS SEISMIC CLASS 1 DESIGN (/) (/) RWST -REFUELING WATER STORAGE TANK 2 INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-7 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3388 jREV. No. VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE 17A ITEM 17 ACCUMULATOR N 2 SUPPLY (/) 0::: D 2 ...._ __ 111111111111--c.::....i 
<{ _J ::::> 2 OPS I") ..q-0) I > (.) :r: C B fj;'I (.) ...._ __ 111111111111--=--J <{ 0 I-(/) 0::: 0 <{ _J ::::> 2 ::::> (.) (.) <{ 2 0 0::: LL !----MISSILE I BARRIER A 891 18 0) 0 0) 0) 0 0) I N2 TRUCK FILL 1----'--------'--11-11--__:I
___ SU PPL Y I (650 PSIG) I (S-1)_.,._
__ l ITEM 18 ACCUMULATOR SAMPLE 956G T T I 956H : I (S-1)---1 ASWI !CONTAINMENT INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-8 CONTAINMENT ISOLATION SYSTEM PENETRATION SCH EMA TICS MIC. No. 1999MC3389 I REV. No. 17A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE  
(/) CL 0 0 _J (/) 0 O'.'. ITEM 19 PRIMARY SYSTEM VENT HEADER AND N2 SUPPLY LINE ITEM 20 REACTOR COOLANT DRAIN TANK TO GAS ANALYZER ITEM 21 RCDT PUMP DISCHARGE O'.'. I w O'.'. O'.'. <( m w _J (/) I (/) 2 I L_ I (SLOPE 19 l/T ASWI T .-----------, f-z w 2 z <( f-z 0 0 1+----..VENT HEADER 6) @I 1786 17871 (s-1)----l t----rl-411-N2 SUPPLY I (100 PSIG) T 5460 1616 I I I ASWI I I (S-1)-1 I I ASWI I I (S-1)-I @) I (s-1)-1 INDIAN POINT UNIT No. UFSAR FIGURE 5.2-9 2 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3390 
!REV. No. 17A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE ITEM 22 REACTOR COOLANT PUMP COOLING WATER IN p p 770 COMPONENT COOLING WATER LOOP (CLOSED SYSTEM) ITEM 23 REACTOR COOLANT PUMP WATER OUT (6 in.) (/) Q_ ::::?: p ::::> Q_ I ...... +-...i___D_R_A_I ::::?: 0 0:::: LL p @ MISSILE I BARRIER-----j I L-ASWI I LsLOPE r-coNTAINMENT 786 COMPONENT COOLING WATER LOOP (CLOSED SYSTEM) ITEM 24 REACTOR COOLANT PUMP COOLING WATER OUT (3 in.) (/) Q_ ::::?: ::::> Q_ () p p 0:::: 
::::?: COMPONENT COOLING WATER LOOP 0 0:::: LL @ L-ASWI SLOPE 789 (CLOSED SYSTEM) ENTIRE COMPONENT COOLING WATER SYSTEM IS SEISMIC CLASS 1 DESIGN INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-10 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3391 1REV. No. VAL VE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE 17A ITEM 25 RESIDUAL HEAT EXCHANGER COOLING WATER IN ITEM 26 RESIDUAL HEAT EXCHANGER COOLING WATER RETURN :r: u x w f-w_J :r: <( u _J 0:: <( >-::::J f-0'--"' i7i w 0::: MISSILE BARRIER s .. ! I \ ,,,, 820A s 818A 25 26 8188 8228 ,,, s 8208 CONTAINMENT ENTIRE SYSTEM SHOWN IS SEISMIC CLASS 1 DESIGN S -OPEN S.I. SIGNAL, PHASE A INDIAN POINT UNIT ,--I I 2 w I f-(/) I >-
2 I (.'.) w zf-_(/) _J >-0 (/) 0 uo w f-(/) zo W_j zu 0'--"' 0.. 2 0 u L __ No. UFSAR FIGURE 5.2-11 2 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3392 I REV. No. VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE 17A ITEM 27 RECIRCULATION PUMP COOLING WATER SUPPLY ITEM 28 RECIRCULATION PUMP COOLING WATER RETURN MISSILE BARRIER (/) Q_ 2 ::) Q_ '\ z / ) 
/ 5 "----0 0::: 0 w 0::: '\ ' I / 27 28 753H 753G 753A CONTAINMENT 
,---2 w (/) >-(/) ,.---.. 2 ow z1-_ lf! _J >-0 (/) 0 00 w I-(/) zo W_l zo a..._., Q_ 2 0 0 L __ _ ENTIRE COMPONENT COOLING SYSTEM IS SEISMIC CLASS 1 DESIGN INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-12 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3393 I REV. No. 17A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE ITEM 29 EXCESS LETDOWN HEAT EXCHANGER COOLING WATER IN ITEM 30 EXCESS LETDOWN HEAT EXCHANGER COOLING WATER OUT ITEM 31 CONTAINMENT SUMP PUMP DISCHARGE ITEM 31 A SAMPLING SYSTEM RETURN TO CONTAINMENT SUMP ,---T ......,..__
2 29 w f-790 (f) >-I (f) ,-.... 2 ASWI C)W zf-I _(() _J >-I 0 (f) \ 0 I 00 w T f-(f) zo W_j zo 0 ..__.., 30 (L 2 0 () T T L ___ 31 WASTE I HOLDUP TANK L -t-s-1 I ASWI I I I I T I T I 31A FROM SAMPLING 5132 4399 SYSTEM 0  ----MISSILE '---CONTAINMENT BARRIER ENTIRE COMPONENT COOLING SYSTEM IS SEISMIC CLASS 1 DESIGN INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-13 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3394 I REV. No. 1 7 A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE MISSILE---!
BARRIER I ITEM 32 CONTAINMENT AIR SAMPLE IN ITEM 33 CONTAINMENT AIR SAMPLE OUT ITEM 34 AIR EJECTOR DISCHARGE TO CONTAINMENT I 32 GAS AND PARTICULATE MONITORS I 33 S-1 ----J T AA T I I PCV-1229 @ PCV-12301 1 S-1 --------l I-CONTAINMENT AA -AU TOMA TIC PRESSURIZATION WITH AIR FROM PENETRATION PRESSURIZATION SYSTEM INDIAN POINT UNIT No. UFSAR FIGURE 5.2-14 2 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3395 I REV. No. 17A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE ITEM 37 STEAM GENERA TOR BLOWDOWN/SAMPLE ( 4 PENETRATIONS) 851 0:: f-0:: z <( w m 2 w z _J :::{ i7i I (f) 0 2 (_) SLOPE PCV-1214 PCV-1215 PCV-1216 PCV-1217 I I ASWI PCV-1214A T PCV-1215A PCV-1216A PCV-1217A I I I (s-1)---1 BLOWDOWN TANK SAMPLING SYSTEM
* THIS DRAIN LINE HAS BEEN REMOVED ON STEAM GENERA TOR 21 INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-15 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3396 IREV. No. 17A VAL VE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE 2 23 2004 11:47:03 AM vnd1999MC3397-1-17B.DWG ITEM 39 10" VENTILATION SYSTEM COOLING WATER IN (5) ITEM 40 1 O" VENTILATION SYSTEM COOLING WATER OUT (5) ITEM 40A 2" VENTILATION SYSTEM MOTOR COOLING WATER OUT (5) ,,.-.._ :::::?: w (f) (f) O:::'. 0 w _J,,.-.._
w 0 _J fJ) 0 <( 0 uu d ..._.., z o._ <( LL..._.., ,,.-.._
O:::'. w w f-(_'.) fJ) NZ >-0:::'. fJ) Ou,,.-.._
o f-x _J w Ow<( fJJ :::::?: u 0 f--_J z<( o._ u <(W ..._.., LL I..._.., 
.___4'-"0-+------l SWN 44A (A) 40A BARRIER SWN 71A (A)
SWN 44B (B1) SWN 718 (B) 40-1 COOLING WATER SUPPLY WATER RETURN TO DISCHARGE CHANNEL I RM I= RADIATION MONITORS ENTIRE SYSTEM SHOWN IS SEISMIC CLASS 1 DESIGN ALL MOV'S ARE DEENERGIZED OPEN PLANT MANAGEMENT MAY DESIGNATE THE "A" OR THE "B" VALVE(S) IN THE 41, 44 AND 71 SERIES AS THE REQUIRED CONTAINMENT ISOLATION VALVE(S).
DESIGNATION OF THE "B" VALVE(S) IN THE SWN-44 SERIES REQUIRES THE CODESIGNA TION OF THE RESPECTIVE 51 SERIES VALVE(S) AS ADDITIONAL REQUIRED CONTAINMENT ISOLATION VALVE(S).
CONTAINMENT ISOLATION VALVE SURVEILLANCE REQUIREMENTS MUST HAVE BEEN SATISFIED FOR THE DESIGNATED VALVE(S).
INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-1 6 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3397 I REV. No. 178 VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE 3 2 2004 6:40:53 AM vnd1999MC3398-1-17B.DWG ITEM 41 SERVICE AIR 1---ASWI J .. Ill I SA-24 ' SA-24-1 \
SERVICE AIR v I @L.C. @ L.C.I TYPICAL I I INSIDE CONTAINMENT L (s-1 _J I I I OUTSIDE CONTAINMENT ITEM 43 WELD CHANNEL PRESSURIZATION AIR SUPPLY 43 43 INSIDE OUTSIDE PCV-1111-1 
@ PENETRATION PRESSURIZATION SYSTEM 1------(CLOSED SYSTEM) PCV-1111-2 
@ ALL PIPING IN PRESSURIZATION SYSTEM IS SEISMIC CLASS 1 CONTAINMENT CONTAINMENT ITEM 44 SPARE I w <( m w _J i7i I 580A @ INSIDE I OUTSIDE CONTAINMENT CONTAINMENT INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-17 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3398 I REV. No. 178 VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE ITEM 45 AUXILIARY STEAM SUPPLY ITEM 46 AUXILIARY STEAM CONDENSATE RETURN ITEM 47 CITY WATER I I (S-1)-----, \*5 L.C. I 5 AUX. STEAM SUPPLY @ I I I I I I ASWI I I I I I I I I 5 1*6 J I ..... UH-44H: *coNDENSATE RETURN @ L.C. I I L.C. L.C.1 
.... Cl TY WATER MW-17-1 MW-17 I @ I @ I CONTAINMENT I (s-1)----_J I I ASWI INDIAN POINT UNIT No. UFSAR FIGURE 5.2-18 2 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3399 lREV. No. VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE 17A ITEM 48 PURGE SUPPLY DUCT ITEM 49 PURGE EXHAUST DUCT I CVI I CVI I I .... I ..... FROM PURGE SUPPLY FANS FCV-1170 FCV-1171 I I @ I  I I !--MISSILE (S-1)...,.._
_J CONTAINMENT AA I CVI CVI I I I I I I I .... TO PURGE EXHAUST FANS I FCV-1172 FCV-1173 I @  ITEM 50 CONTAINMENT PRESSURE RELIEF CVI I PCV-1190 I I 0 !---MISSILE BARRIER I I I CONTAINMENT---j CVI CVI AA I If---!-: ------I ..
* AN PCV-1191 PCV-1192 I PLANT VENT @ @ I I (s-1)----J AA I INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-19 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3400 I REV. No. 17 A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE ITEM 51 RECIRCULATION PUMP DISCHARGE SAMPLE LINE I SIS
____ _____.. .. SAMPLING 993 T SYSTEM PRESS. STEAM SPACE (RCS) PRESS. LIQUID SPACE (RCS) INSIDE OUTSIDE CONTAINMENT I I I I N 2 (1VSWS) ENTIRE SYSTEM SHOWN IS SEISMIC CLASS 1 ITEM 52 PRESSURIZER STEAM SPACE SAMPLE ITEM 53 PRESSURIZER LIQUID SPACE SAMPLE T T 52 SAMPLING 950 951 956A 9568 I SYSTEM @ ' I (s-1)---1 ASWI T 53 SAMPLING 952 953 956C 956D I SYSTEM @ ' I cs-1)---1 ASWI INSIDE OUTSIDE CONTAINMENT INDIAN POINT UNIT No. '/ *-UFSAR FIGURE 5.2-20 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3401 
!REV. No. VAL VE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE 17A ITEMS 54, 55, AND 56 CONTAINMENT PRESSURE INSTRUMENTATION LINES (CLOSED SYSTEM) (CLOSED SYSTEM) L.O. I ,__ __ 54 L.O. i-----55 L.O. 1-----56 _J \ 1814C (CLOSED SYSTEM) CONDENSATE POT INSIDE OUTSIDE CONTAINMENT ENTIRE SYSTEM SHOWN IS SEISMIC CLASS 1 INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-21 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3402 REV. No. 17 A VAL VE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE ITEM 57 POSTACCIDENT CONTAINMENT SAMPLING LINES (SUPPLY AND RETURN) 5 7 L.O. FAN UN IT 23 18750 FAN UN IT 7'---_L ._O-;. 24 1875E FAN UNIT 57 L.O. 21 I 1875A FAN UNIT 57 L.O. 22 1875C FAN UNIT Is? L.O. 25 1875F INSIDE I OUTSIDE CONTAINMENT CONTAINMENT 1 57 L.O. RETURN A 1875G 57 L.O. RETURN B 0 _J SOV-5018 SOV-5019 0  CX) CX) l() SOV-5020 SOV-5021 0  ENTIRE SYSTEM SHOWN IS SEISMIC CLASS 1 TO H2 I 02 ANALYZER SOV-5022 SOV-5023 0 H2 I 02 ANALYZERS 1875H SOV-5024 SOV-5025 0  INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-22 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3403 REV. No. 17 A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE ITEM 58 SP ARE I: I ;AA ss/ :I OUTSIDE INSIDE CONTAINMENT INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-23 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3404 IREV. No. 17A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE ITEMS 59, 60, 61, and 62 SPARE I: ;AA 59 / :1 I 1rAA I I lrAA I I lrAA I INSIDE OUTSIDE CONTAINMENT INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-24 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3405 I REV. No. 17 A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE POSTACCIDENT (P.A.) CONTAINMENT VENTING SYSTEM ITEM 64 INSTRUMENT AIR/P.A. VENTING SUPPLY LINE ITEM 65 P.A. VENTING EXHAUST LINE TYPICAL 64 IA-39 0 65 E-2 0 T PCV-1228  E-1  E-3  E-5 EA-1 INSTRUMENT AIR ENTIRE SYSTEM SHOWN IS SEISMIC CLASS 1 TO VENT STACK 1411---AA INSIDE OUTSIDE CONTAINMENT INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-25 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3406 IREV. No. VAL VE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE 17A ITEM 66 DELETED ITEM 67 CONTAINMENT LEAK TEST AIR LINE (2) I i--I -r-167 __ ---il H><J-J @  SEISMIC CLASS 1 INSIDE OUTSIDE CONTAINMENT INDIAN POINT UNIT No. 2 UFSAR FIGURE 5.2-26 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3407 I REV. No. 17A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE ITEM 69 PERSONNEL AIR LOCK (2)  -----85D 85C 95D 95C SEE NOTE 2 5800* 5801
* SEE NOTE 1 85B 95B INNER DOOR ------EQUALIZING BALL VALVE INTERLOCKED WITH DOOR ENTIRE SYSTEM SHOWN IS SEISMIC CLASS 1 DEISGN CONTAINMENT INSIDE -----OUTSIDE SEE NOTE 1 85A 95A OUTER DOOR SPRING LOADED CHECK VALVE NOTE 1 : 85A & 95A MAY BE OPEN WHEN 85B & 95B ARE CLOSED. 85B & 95B MAY BE OPEN WHEN 85A & 95A ARE CLOSED. 2 TEST VALVES 5800 & 5801 ARE LOCATED AT 83 FT. & 95 FT. AIRLOCKS RESPECTIVELY INDIAN POINT UNIT No. UFSAR FIGURE 5.2-27 2 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3408 I REV. No. 17A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE ITEM 70 STEAM GENERA TOR LEVEL INDICATION LINES (2) PRESURIZER LEVEL INDICATION LINES (1) PRESSURIZER PRESSURE INDICATION LINES (1) I 
.... TO INDICA TIORS llP500 llP501 llP502 llP503 INSIDE OUTSIDE CONTAINMENT llP504 llP505 llP506 llP507 INDIAN POINT UNIT No. UFSAR FIGURE 5.2-28 2 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3409 I REV. No. 17A VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE VALVES LEGEND FOR SYMBOLS, CONTAINMENT ISOLATION SYSTEM OPERATORS Globe Air diaphragm Diaphragm (DIA) Air cylinder C><J Gate Motor Double Disc Gate (DDV) Solenoid Check --Stem 11"1 I Butterfly (BV) Relief T Test Connection Self contained pressure regulator VALVE POSITION (NORMAL) Needle Non-Return (Piston Type) NOTATION ASWI -AUTOMATIC SEAL WATER INJECTION MSWI -MANUAL SEAL WATER INJECTION AA -AUTOMATIC PRESSURIZATION WITH AIR N2 -MANUAL PRESSURIZATION WITH NITROGEN LO -LOCKED OPEN LC -LOCKED CLOSED C><J open closed P -TRIPPED CLOSED BY CONTAINMENT ISOLATION SIGNAL, PHASE A T -TRIPPED CLOSED BY CONTAINMENT ISOLATION SIGNAL, PHASE B S-1 -SEISMIC CLASS I S -OPEN S.I. Signal, Phase A D.O. -DEENERGIZED OPEN CVI -CONTAINMENT VENTILATION ISOLATION (AU TOMA TIC SIGNAL) IVSWS -ISOLATION VALVE SEAL WATER SYSTEM INDIAN POINT UNIT No. UFSAR FIGURE 5.2-29 2 CONTAINMENT ISOLATION SYSTEM PENETRATION SCHEMATICS MIC. No. 1999MC3410 I REV. No. VALVE POSITIONS ARE NOT CONTROLLED BY THIS FIGURE 17A}}