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FSAR Amendment 107, Figures - Chapters 3, 4, and 5, Part 1 of 4
	ML16180A441
Person / Time
Site:	Comanche Peak
Issue date:	02/01/2016
From:	; Luminant Generation Co
To:	; Office of Nuclear Reactor Regulation
Shared Package
ML16042A346	List: ML16042A344; ML16180A424; ML16180A425; ML16180A426; ML16180A427; ML16180A428; ML16180A429; ML16180A430; ML16180A431; ML16180A432; ML16180A435; ML16180A436; ML16180A437; ML16180A438; ML16180A439; ML16180A440; ML16180A441; ML16180A442; ML16180A443; ML16180A444;
References
	txx-16006, CP-20160003
	Download: ML16180A441 (136)
	v • d • e

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2. REACTOR BLDG.

3. DIESEL BLDG.

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EXCLUSION UNITS 1 AND 2 PROCESS FORG THREADED PIPE FLANGE (BQL TEO J AR TYPICAL MOMENT RESTRAINT AND BREAK EXCLUSION AREA BOUNDARY TO STRUCTURE) 051588067 FIGURE 3.68-5

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                                                             ~ DENOTES BREAK LOCATION PLAN VIEW STEAM GENERATOR REACTOR PRESSURE VESSEL ELEVATION NOTE: 1. Postulated main reactor coolant loop break locations 1 through 8 and branch nozzle breaks 9 through 11 are consid ered for containment design, ECCS and enviornmental qualification. These breaks are not postulated for dyn amic effects.

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2. Branch nozzle breaks 12 and 13 are considered to account fo r the dynamic effects attribu t ib l e COMANCHE PEAK S.E.S.

to the largest RC L postulated breaks after application of LBB to selected l ines. FINAL SAFETY ANALYSIS REPORT UNITS 1 and 2 AMENDMENT 76 MAY l, 1989 Location of Postulated Breaks in Main Reactor Coolant Loop FIGURE 3. 68-9

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~~690 lJ COMANCHE PEAK s. E. s. I FINAL SAFETY ANALYSIS REPORT UNIT 1~~
~~' FlGURE eves SYS1EM AUX. BUll..OING STRESS NOOE BREAK POINT AND RESTRAINT LOCATION 3..llB-64 PROB. 1-51B~~
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FINAL SAFETY ANALYSIS REPORT UNIT 1 eves SYSTEM AUX. BUil.DiNG AMENDMENT 76 STRESS NODE BREAK POINT AND RESTRAINT LOCATION MAY 1, 1989 3.66-85 PROB. 1-51C
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FINAL SAFETY ANALYSIS REPORT UNIT 1 eves SYSTEM AUX. BUILDING AMENDMENT 76 f:'::l.IE ON~,,,,, STRESS NOOE BREAK POINT AND RESlRAlNT LOCATION MAY 1, 1989 FlGURE 3.68-88 PROB. 1-510
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~~FINAL SAFETY ANALYSIS REPORT UNIT 1 eves S'l'S"TEM AUX. BUILDING STRESS NODE BREAK POINT~~
~~~G- AND RESTRAINT LOCATION MAY 1, 1989 AGURE 3.68-87-1 PROB. 1-52X~~
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~~1. Break locations 1 to 13 per Table 3.6B-2.~~
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CPSES/FSAR Figure 3.66-93-1 This figure has been deleted. Amendment 87 December 18, 1992
CPSES/FSAR Figure 3.68-93-2 This figure has been deleted. Amendment 87 December 18, 1992
CPSES/FSAR Figure 3.68-94 This figure has been deleted. Amendment 87 December 18, 1992
CPSES/FSAR Figure 3.68-95 This figure has been deleted. Amendment 87 December 18, 1992
PLANE AT END OF JET CORE ASYMPTOTIC PLA,NE REGION 3 REG I0 N 2 ---o-t--t-i REGION 1 1o* Da JET CORE BREAK PLANE Le__....,......_, La ----i---~ L Amendment 71 May 27, 1988 COMANCHE PEAK S. S. FINAL SAFETY ANALYSIS REPORT UNITS 1 & 2 CIRCUMFERENTIAL PIPE BREAK WITH FULL SEPARATION JET CONE FIGURE 3.68-96A
n z 0 0 w 0::: PLANE AT END ASYMPTOTIC PLANE OF JET CORE
~~/BREAK PLANE -+---~--"'------~ __..____._-+---"-_~~
REGION 2 REGION Le La Amendment 71 May 27 1 1988 COMANCHE PEAK S.E.S. FINAL SAFETY ANALYSIS REPORT UNITS 1 & 2 LONGITUDINAL PIPE BREAK JET CONE FIGURE 3.68-968
Le Dj L Amendment 71 May 27, 1988 COMANCHE PEAK S.E.S. FINAL SAFETY ANALYSIS REPORT UNITS 1 & 2 JET CORE REGION GEOMETRY FOR A CIRCUMFERENTIAL PIPE BREAK WITH FULL SEPERATION FIGURE 3.6B-96C
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I 1 10 1.0 + (fl/De) COMANCHE PEAK S.E.S. FINAL SAFETY ANALYSIS REPORT UNITS 1 and 2 EFFECT OF IRREVERSIBLE LOSSES ON JET SUBCOOLING AMENDMENT 76 MAY 1, 1989 FIGURE 3,6B-96n}}

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