ML16330A239

Updated Final Safety Analysis Report, Chapter 14, Safety Analysis, Appendix 14A Thru Appendix 14G

ML16330A239
Person / Time
Site:	Turkey Point
Issue date:	10/29/2016
From:	Florida Power & Light Co
To:	Office of Nuclear Reactor Regulation
Shared Package
ML16330A191	List: L-2016-198, Redacted Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 14, Safety Analysis L-2016-198, Redacted Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 2, Site and Environment L-2016-198, Redacted Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 3, Reactor L-2016-198, Redacted Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 4, Reactor Coolant System L-2016-198, Redacted Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 6, Engineered Safety Features L-2016-198, Redacted Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 8, Electrical Systems L-2016-198, Redacted Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 9, Auxiliary and Emergency Systems L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Appendix 9.6A, Fire Protection Program Report L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Appendix B, Questions and Responses Related to Initial NRC Review of Operating License Application L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Appendix a, a Functional Evaluation of the Components of the Systems Which Are Shared by the Two Units L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 1, Introduction and Summary L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 10, Steam and Power Conversion Systems L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 11, Waste Disposal and Radiation Protection System L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 12, Conduct of Operations L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 13, Initial Tests and Operations L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 14, Safety Analysis, Appendix 14A Thru Appendix 14G L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 15, Technical Specifications L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 16, Aging Management Programs and Time-Limited Aging Analysis Activities L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 5, Structures L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, Chapter 7, Instrument and Control L-2016-198, Turkey Point, Units 3 & 4, Updated Final Safety Analysis Report, List of Effective Pages ML16330A177 ML16330A180 ML16330A184 ML16330A186 ML16330A189 ML16330A190 ML16330A235 ML16330A236 ML16330A237 ML16330A239 ML16330A240 ML16330A241 ML16330A242 ML16330A243 ML16330A244 ML16330A245 ML17051A042 ML17051A093 ML17051A094 ML17051A096 ML17051A097 ML17051A098
References
L-2016-198
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Text

APPENDIX 14A

TURKEY POINT PLANT UNIT 3 CYCLE 28 RELOAD CHARACTERISTICS AND PARAMETERS

14A-i Revised 03/11/2016 C28 TABLE OF CONTENTS Section Title Page

1.0 INTRODUCTION

AND

SUMMARY

........................................................ 14A-1

1.1 Introduction

............................................................................... 14A-1 1.2 General Description .................................................................. 14A-1

Appendix A Turkey Point Unit 3 Cycle 28..........

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

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

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

... 14A-A1 Core Operating Limits Report (COLR)

14A-ii Revised 03/11/2016 C28 LIST OF TABLES Table Title Page 14A-1 Fuel Assembly Design Parame ters ......................-----------.14A-2 Turkey Point Unit 3 - Cycle 28 14A-2 Kinetics Characteristics..............

.................................................................... 14A-3 Turkey Point Unit 3 - Cycle 28 14A-3 Shutdown Requirements and Margins .........................................................14A-4 Turkey Point Unit 3 - Cycles 27 and 28

LIST OF FIGURES

Figure 14A-1 Reference Core Loading Pattern .................................................................. 14A-6 Turkey Point Unit 3 Cycle 28 14A-2 Burnable Absorber Locations

......................................................................... 14A-7 Turkey Point Unit 3 Cycle 28

14A-iii Revised 03/11/2016 C28C28

1.0 INTRODUCTION

and

SUMMARY

1.1 Introduction

This report presents reload characteristics and parameters associated with Turkey Point Unit 3 Cycle 28. The Cycle 28 core is a full core with 15x15 Upgrade fuel assemblies in Regions 28, 29 and 30. 1.2 General Description The Turkey Point Unit 3 reactor core is comprised of 157 fuel assemblies arranged in the core loading pattern configuration shown in Figure 14A-1.

All fuel assemblies have axial blankets at both the top and bottom of the fuel stack to reduce neutron leakage and to improve uranium utilization. Regions 28, 29 and 30 fuel assemblies are 8 inch long, with 2.6 w/o enriched UO 2 annular pellets. The design parameters for the Cycle 28 core are provided in Table 14A-1.

The Cycle 28 core uses a single type of burnable absorber, the Westinghouse Integral Fuel Burnable Absorber (IFBA) rods composed of ZrB 2 coated fuel pellets with 2.2125 mg 10B/in. The active absorber length is 120 inches. Their locations in the core are shown in Figure 14A-2.

The core design parameters for Cycle 28 are as follows:

Parameter Current Licensing Basis

Core Power (MW t) 2644 Pressurizer Pressure (psia) 2250 Core Inlet Temperature 1 (F) 549.2 Core Inlet Temperature 2 (F) 550.2 Thermal Design Flow (gpm) 260,700 Minimum Measured Flow (gpm) 270,000 Average Linear Power Density (kW/ft) 6.714

1. Based on Thermal Design Flow.

2. Based on Minimum Measured Flow.

The core kinetics characteristics and shutdown requirements and margins are provided in Tables 14A-2 and 14A-3, respectively. The Core Operating Limits Report (COLR) for Cycle 28 is provided in Appendix A.

14A-1 Revised 03/11/2016 C28C28C28C28C28 Table 14A-1 Fuel Assembly Design Parameters Turkey Point Unit 3 - Cycle 28

14A-2 Revised 03/11/2016 Region 28A 28B 28C 29A 29B 29C 29D 29E 30A 30B 30C Enrichment 1 (w/o U235) 3.797 3.797 4.210 3.987 4.196 4.393 4.393 4.939 3.900 4.100 4.500 Density 1 (% Theoretical) 95.65 95.65 95.46 95.49 95.63 95.81 95.81 95.81 95.50 95.50 95.50 Number of Assemblies 8 4 16 5 24 20 4 16 20 20 20 Approximate Burnup at Beginning of 30,986 33,139 37,533 25,963 26,183 22,180 24,308 25,690 0 0 0 Cycle 28 (MWD/MTU) 2 Fuel Type Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Number of IFBA/Assembly 100 116 32 148 148 48 100 148 8@64 12@148 148 16@48 4@80 Total Number of IFBA 800 464 512 740 3552 960 400 2368 2288 2960 1088 Fuel Rods/Region Axial Blankets (AB) 3 YES YES YES YES YES YES YES YES YES YES YES AB Annular Pellets YES YES YES YES YES YES YES YES YES YES YES AB Enrichment (w/o) 2.6 2.6 2.6 2.6 2.6 2.6 2.6 2.6 2.6 2.6 2.6 ZIRLO TM Cladding NO NO NO NO NO NO NO NO YES YES YES 1 As-built values for burned regions and design values for fresh region 2 Based on an assumed Cycle 27 burnup of 20,226 MWD/MTU (LW) 3 Axial blankets in all regions are 8 inch long. C28 Table 14A-2 KINETICS CHARACTERISTICS TURKEY POINT UNIT 3 - Cycle 28

Moderator Temperature Current Limit Cycle 28 Coefficient (pcm/°F)

a. Most positive +5.0 ( 70% RTP) +1.1 (HZP, 541°F, (linear ramp to 0 at 2000MWD/MTU), linear ramp 100% RTP) to 0 at 100% RTP

b. Most negative 32.2 Doppler Coefficient (pcm/°F) -2.9 to -1.0 -1.97 to -1.22 Most Negative to Least Negative Delayed Neutron Fraction, eff 0.0044 to 0.0075 0.0048 to 0.0064 Minimum to Maximum Maximum Differential Rod

<100 58.3 Worth of Two Banks Moving Together at HZP (pcm/in)

Shutdown Margin (pcm)

a. BOC 1000* 3512 1770** b. EOC 1770 2073

• MODES 1 through 4 with at least 1 RCP running

• • MODE 4 without RCPs running and MODE 5

14A-3 Revised 03/11/2016 C28C28 Table 14A-3 Shutdown Requirements and Margins Turkey Point Unit 3 - Cycles 27 and 28 Cycle 27 Cycle 28 BOC EOC BOC EOC Control Rod Worth (%) All Rods Inserted Less 5.69 5.72 5.98 5.95 Worst Stuck Rod (1) Less 7% 5.29 5.32 5.56 5.53 Control Rod Requirements (%) Reactivity Defects (Doppler, 1.98 3.52 2.05 3.46 TAVE, Void, and Redistribution)

Rod Insertion Allowance (RIA) --- --- --- --- RCCA Repositioning Allowance (see note)

(2) Total Requirements 1.98 3.52 2.05 3.46 Shutdown Margin (1) - (2) (%) 3.31 1.80 3.51 2.07 Required Shutdown Margin (%) 1.00 1.77 1.00 1.77

Note: Additional margin to accommodate a 22 °F cooldown is not available for the EPU cycles. The RIA term is already included in the Reactivity Defects term in the methodology used to compute the shutdown margin.

14A-4 Revised 03/11/2016 C28C28C28 Table 14A-4 DELETED

14A-5 Revised 03/11/2016

Figure 14A-1 Reference Core Loading Pattern Turkey Point Unit 3 Cycle 28

14A-6 Revised 03/11/2016 C28 Figure 14A-2 Turkey Point Unit 3, Cycle 28 Burnable Absorber and Source Rod Locations

TYPE TOTAL

1. 1. I (Total number of fresh IFBA Rods) ----------6336

14A-7 Revised 03/11/2016 C28

Appendix A Turkey Point Unit 3 Cycle 28 Core Operating Limits Report (COLR)

14A-A1 Revised 03/11/2016 C28 Turkey Point Unit 3 Cycle 28 Core Operating Limits Report (COLR)

1.0 INTRODUCTION

This Core Operating Limits Report for Turkey Point Unit 3 Cycle 28 has been prepared in accordance with the requirements of Technical Specification 6.9.1.7.

The Technical Specifications (TS) affected by this report are listed below with the section and page for each one of the TS addressed in this COLR document. Section Technical Specification Page 2.1 2.1.1 Reactor Core Safety Limits 14A-A3 2.2 2.2.1 Reactor Trip System Instrumentation Setpoints 14A-A3-14A-A4 2.3 3.1.1.1 Shutdown Margin Limit for MODES 1, 2, 3, 4 14A-A4 2.4 3.1.1.2 Shutdown Margin Limit for MODE 5 14A-A4 2.5 3.1.1.3 Moderator Temperature Coefficient 14A-A5 2.6 4.1.1.3 MTC Surveillance at 300 ppm 14A-A5 2.7 3.1.3.2 Analog Rod Position Indication System 14A-A5 2.8 3.1.3.6 Control Rod Insertion Limits 14A-A5 2.9 3.2.1 Axial Flux Difference 14A-A5 2.10 3.2.2 Heat Flux Hot Channel Factor F Q(Z) 14A-A5 2.11 3.2.3 Nuclear Enthalpy Rise Hot Channel Factor 14A-A6 2.12 3.2.5 DNB Parameters 14A-A6 Figure Description A1 Reactor Core Safety Limit - Three Loops in Operation 14A-A7 A2 Required Shutdown Margin vs Reactor Coolant Boron Concentration 14A-A8 A3 Turkey Point Unit 3 Cycle 28 Rod Insertion Limits vs Thermal Power 14A-A9 A4 Axial Flux Difference as a Function of Rated Thermal Power 14A-A10

14A-A2 Revised 03/11/2016 C28C28C28 Turkey Point Unit 3 Cycle 28 Core Operating Limits Report (COLR)

2.0 Operating

Limits The cycle-specific parameter limits for the specifications listed in the Introduction are presented below and listed sequentially by Technical Specification (TS). These limits have been developed using the NRC-approved methodologies specified in TS 6.9.1.7.

2.1 Reactor

Core Safety Limits - Three Loops in Operation (TS 2.1.1)

- Figure A1 (page 14A-A7)

In Modes 1 and 2, the combination of Thermal Power, reactor coolant system highest loop average temperature and pressurizer pressure shall not exceed the limits in Figure A1.

2.2 Reactor

Trip System Instrumentation Setpoints (TS 2.2.1)

NOTE 1 on TS Table 2.2-1 Overtemperature T - 1 = 0s, 2 = 0s Lead/Lag compensator on measured T - 3 = 2s Lag compensator on measured T - K 1 = 1.31 - K 2 = 0.023/ F - 4 = 25s, 5 = 3s Time constants utilized in the lead-lag compensator for Tavg - 6 = 2s Lag compensator on measured Tavg - T 583.0 F Indicated Loop Tavg at RATED THERMAL POWER

- K 3 = 0.00116/psi - P' 2235 psig Nominal RCS operating pressure

- f 1 (I) = 0 for q t - q b between - 18% and + 7%. For each percent that the magnitude of q t - q b exceeds - 18%,

the T Trip Setpoint shall be automatically reduced by 3.51% of its value at RATED THERMAL POWER; and For each percent that the magnitude of q t - q b exceeds + 7%, the T Trip Setpoint shall be automatically reduced by 2.37% of its value at RATED THERMAL POWER.

Where q t and q b are percent RATED THERMAL POWER in the top and bottom halves of the core respectively, and q t + q b is total THERMAL POWER in percent of RATED THERMAL POWER.

14A-A3 Revised 03/11/2016 C28 Turkey Point Unit 3 Cycle 28 Core Operating Limits Report (COLR)

NOTE 2 on TS Table 2.2-1 Overtemperature T The Overtemperature T function Allowable Value shall not exceed the nominal trip setpoint by more than 0.5% T span for the T channel, 0.2% T span for the Pressurizer Pressure channel, and 0.4% T span for the f(l) channel. No separate Allowable Value is provided for Tavg because this function is part of the T value. NOTE 3 on TS Table 2.2-1 Overpower T - K 4 = 1.10 - K 5 0.0/ F For increasing average temperature

- K 5 = 0.0/ F For decreasing average temperature

- 7 0 s Time constants utilized in the lead-lag compensator for Tavg - K 6 = 0.0016/ F For T > T"

- K 6 = 0.0 For T T" - T" 583.0 F Indicated Loop Tavg at RATED THERMAL POWER - f 2 (I) = 0 For all I NOTE 4 on TS Table 2.2-1 Overpower T The Overtemperature T function Allowable Value shall not exceed the nominal trip setpoint by more than 0.5% T span for the T channel. No separate Allowable Value is provided for Tavg because this function is part of the T value. 2.3 Shutdown Margin Limit for MODES 1, 2, 3 and 4 (TS 3.1.1.1)

- Figure A2 (page 14A-A8)

2.4 Shutdown

Margin Limit for MODE 5 (TS 3.1.1.2)

- 1.77% k/k

14A-A4 Revised 03/11/2016 C28 Turkey Point Unit 3 Cycle 28 Core Operating Limits Report (COLR)

2.5 Moderator

temperature coefficient (MTC) (TS 3.1.1.3)

- + 5.0 x 10

-5 k/k/ F BOL, HZP, ARO and from HZP to 70% Rated Thermal Power (RTP) - From 70% RTP to 100% RTP the MTC decreasing linearly from < + 5.0 x 10

-5 k/k/ F to < 0.0 x 10

-5 k/k/ F - Less negative than - 41.0 x 10

-5 k/k/ F EOL, RTP, ARO

2.6 Moderator

temperature coefficient (MTC) Surveillance at 300 ppm (TS 4.1.1.3)

- Less negative than - 35.0 x 10

-5 k/k/F (-35 pcm/ F) Within 7 EFPD of reaching equilibrium boron concentration of 300 ppm. The Revised Predicted near - EOL 300 ppm MTC shall be calculated using the algorithm contained in WCAP-13749-P-A: Revised predicted MTC = Predicted MTC + AFD Correction - 3 pcm/ F If the Revised Predicted MTC is less negative than the SR 4.1.1.3.b 300 ppm surveillance limit and all the benchmark criteria contained in the surveillance procedure are met, then an MTC measurement in accordance with SR 4.1.1.3.b is not required to be performed. The neutronics methods used with WCAP-13749-P-A are those described in WCAP-11596-P-A, "Qualification of the Phoenix-P/ANC Nuclear Design System for Pressurized Water Reactor Cores," June 1988.

2.7 Analog

Rod Position Indication System (TS 3.1.3.2)

- Figure A3 (page 14A-A9) The All Rods Out (ARO) position for all shutdown Banks and Control Banks is defined to be 228 steps withdrawn.

2.8 Control

Rod Insertion Limits (TS 3.1.3.6)

- Figure A3 (page 14A-A9) The control rod banks shall be

limited in physical insertion as specified in Figure A3 for ARO =228 steps withdrawn.

2.9 Axial

Flux Difference (TS 3.2.1)

- Figure A4 (page 14A-A10)

14A-A5 Revised 09/01/2016 C28C28C28C28C28 Turkey Point Unit 3 Cycle 28 Core Operating Limits Report (COLR) 2.10 Heat Flux Hot Channel Factor F Q(Z) (TS 3.2.2)

- [FQ]L = 2.30 - K(z) = 1.0 For 0' z 12' where z is core height in ft 2.11 Nuclear Enthalpy Rise Hot Channel Factor (TS 3.2.3)

- FH RTP = 1.600 PFH = 0.3

2.12 DNB Parameters (TS 3.2.5)

- RCS Tavg < 585.0 o F

- Pressurizer Pressure > 2204 psig

14A-A6 Revised 03/11/2016 C28C28 Figure A1 Reactor Core Safety Limit - Three Loops in Operation

14A-A7 Revised 03/11/2016

Figure A2 Required Shutdown Margin vs Reactor Coolant Boron Concentration

14A-A8 Revised 03/11/2016

FIGURE A3 Turkey Point Unit 3 Cycle 28 Rod Insertion Limits vs Thermal Power ARO = 228 Steps Withdrawn, Overlap = 100 Steps

14A-A9 Revised 03/11/2016 C28 FIGURE A4 Axial Flux Difference as a Function of Rated Thermal Power Turkey Point Unit 3 Cycle 28

14A-A10 Revised 03/11/2016 C28

APPENDIX 14B

TURKEY POINT PLANT UNIT 4 CYCLE 29 RELOAD CHARACTERISTICS AND PARAMETERS

14B-i Revised 07/21/2016 C28 TABLE OF CONTENTS

Section Title Page

1.0 INTRODUCTION

AND

SUMMARY

......................................................................14B-1

1.1 Introduction

................................................................................................14B-1 1.2 General Description ...................................................................................14B-1 Appendix A Turkey Point Unit 4 Cycle 29 ...........

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

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

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

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

.......14B-A1 Core Operating Limits Report (COLR)

14B-ii Revised 07/21/2016 C28 LIST OF TABLES

Table Title Page

14B-1 Fuel Assembly Design Parameters................................................................................ 14B-2 Turkey Point Unit 4 - Cycle 29

14B-2 Kinetics Characteristics.................................................................................................. 14B-3 Turkey Point Unit 4 - Cycle 29 14B-3 Shutdown Requirements and Margins........................................................................... 14B-4 Turkey Point Unit 4 - Cycles 28 and 29

LIST OF FIGURES Figure 14B-1 Reference Core Loading Pattern.................................................................................... 14B-6 Turkey Point Unit 4 Cycle 29 14B-2 Burnable Absorber Locations........................................................................................ 14B-7 Turkey Point Unit 4 Cycle 29

14B-iii Revised 07/21/2016 C28C28C28C28C28

1.0 INTRODUCTION

and

SUMMARY

1.1 Introduction

This report presents reload characteristics and parameters associated with Turkey Point Unit 4 Cycle 29. The Cycle 29 core is a fullcore with 15x15 Upgrade fuel assemblies in Region 28, 29, 30, and 31.

1.2 General

Description The Turkey Point Unit 4 reactor core is comprised of 157 fuel assemblies arranged in the core loading pattern configuration shown in Figure 14B-1.

All fuel assemblies have axial blankets at both the top and bottom of the stack to reduce neutron leakage and to improve uranium utilization. Regions 28, 29, 30, and 31 fuel assembly blankets are 8 inches long, with Natural UO 2 annular pellets in Region 28 and 2.6 w/o enriched UO 2 annular pellets in the other regions. The design parameters for the Cycle 29 core are provided in Table 14B-1.

The Cycle 29 core uses a single type of burnable absorber, the Westinghouse Integral Fuel Burnable Absorber (IFBA) rods composed of ZrB 2 coated fuel pellets with 2.2125 mg 10 B/in. The active absorber length is 120 inches. Their locations in the core are shown in Figure 14B-2.

The core design parameters for Cycle 29 are as follows:

Parameter Current Licensing Basis Core Power (MW t) 2644 Pressurizer Pressure (psia) 2250 Core Inlet Temperature 1 (°F) 549.2 Core Inlet Temperature 2 (°F) 550.2 Thermal Design Flow (gpm) 260,700 Minimum Measured Flow 270,000 Average Linear Power Density 3 (kW/ft) 6.714 1. Based on Thermal Design Flow. 2. Based on Minimum Measured Flow.

The core kinetics characteristics and shutdown requirements and margins are provided in Tables 14B-2 and 14B-3, respectively. The Core Operating Limits Report (COLR) for Cycle 29 is provided in Appendix A.

14B-1 Revised 07/21/2016 C28C28C28C28C28 Table 14.B-1 Fuel Assembly Design Parameters Turkey Point Unit 4 Cycle 29 Region 28C 29B 29C 29D 29F 30A 30B 30C 30D 30E 30F 30G 31A 31B 31C Enrichment 1 (w/o U 235) 4.006 4.009 4.009 4.405 4.405 3.807 3.807 3.807 4.199 4.400 4.400 4.400 3.900 4.100 4.400 Density 1 (% Theoretical) 95.67 95.88 95.88 95.71 95.71 95.65 95.65 95.65 95.05 95.91 95.91 95.91 95.50 95.50 95.50 Number of Assemblies 1 4 4 8 8 8 4 20 8 8 8 8 12 36 20 Approximate Burnup at BOC 29 23,088 33,351 33,387 36,575 36,555 25,160 24,969 24,780 24,181 21,437 22,062 23,725 0 0 0 (MWD/MTU)2 Fuel Type Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Upgrade Number of IFBA/Assembly 116 100 148 32 148 80 116 148 116 48 64 80 4@16 8@148 4@100 20@116 12@148 8@16 8@32 4@80 Total Number of IFBA 116 400 592 256 1184 640 464 2960 928 384 512 640 1248 4496 704 Fuel Rods/Region

Axial Blankets (AB) 3 YES YES YES YES YES YES YES YES YES YES YES YES YES YES YES AB Annular Pellets YES YES YES YES YES YES YES YES YES YES YES YES YES YES YES AB Enrichment (w/o) NAT U 2.6 2.6 2.6 2.6 2.6 2.6 2.6 2.6 2.6 2.6 2.6 2.6 2.6 2.6 Optimized ZIRLO TM Cladding NO NO NO NO NO NO NO NO NO NO NO NO YES YES YES Notes 1. As built values for burned regions and design values for fresh regions. 2 Based on assumed Cycle 28 burnup of 19,292 MWD/MTU (Long Window). 3. Axial blankets in all regions are 8 inches long.

14B-2 Revised 07/21/2016 C28 Table 14B-2 KINETICS CHARACTERISTICS TURKEY POINT UNIT 4 - Cycle 29 Moderator Temperature Coefficient (pcm/°F) Current Limit Cycle 29

a. Most positive +5.0 (70% RTP) +2.2 (HZP, 541 °F, 2000 (linear ramp MWD/MTU), linear ramp to 0 at 100% RTP) rate to 0 at 100% RTP

b. Most negative -41 -36.2 Doppler Coefficient (pcm/°F) -2.9 to -1.0 -1.94 to -1.22 Delayed Neutron Fraction eff (%) 0.44 to 0.75 0.48 to 0.65

Maximum Differential Rod 100 57.8 Worth of Two Banks Moving Together at HZP (pcm/in)

Available Shutdown Margin (%) a. BOC 1.00* 3.197 1.77** b. EOC 1.77 1.865

• MODES 1 through 4 with at least 1 RCP running ** MODE 4 without RCPs running and MODE 5

14B-3 Revised 07/21/2016 C28C28C28C28C28 Table 14B-3 Shutdown Requirements and Margins Turkey Point Unit 4 - Cycles 28 and 29 Cycle 28 Cycle 29 BOC EOC BOC EOCControl Rod Worth (%) All Rods Inserted Less Worst Stuck Rod 5.78 5.79 5.47 5.68 (1) Less 7% 5.37 5.38 5.09 5.29 Control Rod Requirements (%) Reactivity Defects (Doppler, TAVE, Void, and Redistribution) 1.97 3.41 1.89 3.42 Rod Insertion Allowance (RIA) RCCA Repositioning Allowance (see note) --- --- --- ---

(2) Total Requirements 1.97 3.41 1.89 3.42 Shutdown Margin (1) - (2) (%) 3.41 1.97 3.20 1.87 Required Shutdown Margin (%) 1.00 1.77 1.00 1.77

Note: Additional margin to accommodate a 22 °F cooldown is not available for EPU cycles. The RIA term is already included in the Reactivity Defects term in the methodology used to compute the shutdown margin.

14B-4 Revised 07/21/2016 C28 Figure 14B-1 Turkey Point Unit 4, Cycle 29 Reference Core Loading Pattern 14B-5 Revised 07/21/2016 C28 Figure 14B-2 Turkey Point Unit 4, Cycle 29 Burnable Absorber and Source Rod Locations

14B-6 Revised 07/21/2016 C28

Appendix A Turkey Point Unit 4 Cycle 29 Core Operating Limits Report (COLR)

14B-A1 Revised 07/21/2016 C28 Turkey Point Unit 4 Cycle 29 Core Operating Limits Report

1.0 Introduction

This Core Operating Limits Report for Turkey Point Unit 4 Cycle 29 has been prepared in accordance with the requirements of Technical Specification 6.9.1.7. The Technical Specifications (TS) affected by this report are listed below with the section and page for each one of the TS addressed in this COLR document. Section Technical Specification Page 2.1 2.1.1 Reactor Core Safety Limits 14B-A3 2.2 2.2.1 Reactor Trip System Instrumentation Setpoints 14B-A3-14B-A4 2.3 3.1.1.1 Shutdown Margin Limit for MODES 1, 2, 3, 4 14B-A4 2.4 3.1.1.2 Shutdown Margin Limit for MODE 5 14B-A4 2.5 3.1.1.3 Moderator Temperature Coefficient 14B-A5 2.6 4.1.1.3 MTC Surveillance at 300 ppm 14B-A5 2.7 3.1.3.2 Analog Rod Position Indication System 14B-A5 2.8 3.1.3.6 Control Rod Insertion Limits 14B-A5 2.9 3.2.1 Axial Flux Difference 14B-A5 2.10 3.2.2 Heat Flux Hot Channel Factor F Q(Z) 14B-A5 2.11 3.2.3 Nuclear Enthalpy Rise Hot Channel Factor 14B-A6 2.12 3.2.5 DNB Parameters 14B-A6 Figure Description A1 Reactor Core Safety Limit - Three Loops in Operation 14B-A7 A2 Required Shutdown Margin vs Reactor Coolant Boron Concentration 14B-A8 A3 Turkey Point Unit 4 Cycle 29 Rod Insertion Limits vs Thermal Power 14B-A9 A4 Axial Flux Difference as a Function of Rated Thermal Power 14B-A10

14B-A2 Revised 07/21/2016 C28C28C28 Turkey Point Unit 4 Cycle 29 Core Operating Limits Report

2.0 OPERATING

LIMITS The cycle-specific parameter limits for the specifications listed in the Introduction are presented below and listed sequentially by Technical Specification (TS). These limits have been developed using the NRC-approved methodologies specified in TS 6.9.1.7.

2.1 Reactor

Core Safety Limits - Three Loops in Operation (TS 2.1.1) - Figure A1(page 14B-A7)

In Modes 1 and 2, the combination of Thermal Power, reactor coolant system highest loop average temperature and pressurizer pressure shall not exceed the limits in Figure A1. 2.2 Reactor Trip System Instrumentation Setpoints (TS 2.2.1) NOTE 1 on TS Table 2.2-1 Overtemperature T - 1 = 0s, 2 = 0s Lead/Lag compensator on measured T - 3 = 2s Lag compensator on measured T - K 1 = 1.31 - K 2 = 0.023/ F - 4 = 25s, 5 = 3s Time constants utilized in the lead-lag compensator for Tavg - 6 = 2s Lag compensator on measured Tavg - T 583.0 F Indicated Loop Tavg at RATED THERMAL POWER

- K 3 = 0.00116/psi - P' 2235 psig Nominal RCS operating pressure

- f 1 (I) = 0 for q t - q b between - 18% and + 7%. For each percent that the magnitude of q t - q b exceeds - 18%, the T Trip Setpoint shall be automatically reduced by 3.51% of its value at RATED THERMAL POWER; and For each percent that the magnitude of q t - q b exceeds +7%, the T Trip Setpoint shall be automatically reduced by 2.37% of its value at RATED THERMAL POWER.

Where q t and q b are percent RATED THERMAL POWER in the top and bottom halves of the core respectively, and q t + q b is total THERMAL POWER in percent of RATED THERMAL POWER.

14B-A3 Revised 07/21/2016 C28 Turkey Point Unit 4 Cycle 29 Core Operating Limits Report NOTE 2 on TS Table 2.2-1 Overtemperature T The Overtemperature T function Allowable Value shall not exceed the nominal trip setpoint by more than 0.5% T span for the T channel, 0.2% T span for the Pressurizer Pressure channel, and 0.4% Tspan for the f(I) channel. No separate Allowable Value is provided for Tavg because this function is part of the T value. NOTE 3 on TS Table 2.2-1 Overpower T - K 4 = 1.10 - K 5 0.0/ F For increasing average temperature

- K 5 = 0.0/ F For decreasing average temperature

- 7 0 s Time constants utilized in the lead-lag compensator for Tavg - K 6 = 0.0016/ F For T > T"

- K 6 = 0.0 For T T" - T" 583.0 F Indicated Loop Tavg at RATED THERMAL POWER

- f 2 (I) = 0 For all I NOTE 4 on TS Table 2.2-1 Overpower T The Overpower T function Allowable Value shall not exceed the nominal trip setpoint by more than 0.5% T span for the T channel. No separate Allowable Value is provided for Tavg because this function is part of the T value. 2.3 Shutdown Margin Limit for MODES 1, 2, 3 and 4 (TS 3.1.1.1) - Figure A2 (page 14B-A8)

2.4 Shutdown

Margin Limit for MODE 5 (TS 3.1.1.2) - > 1.77 % k/k

14B-A4 Revised 07/21/2016 C28 Turkey Point Unit 4 Cycle 29 Core Operating Limits Report

2.5 Moderator

temperature coefficient (MTC) (TS 3.1.1.3) - < + 5.0 x 10

-5 k/k/ F BOL, HZP, ARO and from HZP to 70% Rated Thermal Power (RTP)

- From 70% RTP to 100% RTP the MTC decreasing linearly from < + 5.0 x 10

-5 k/k/ F to < 0.0 x 10

-5 k/k/ F - Less negative than - 41.0 x 10

-5 k/k/ F EOL, RTP, ARO

2.6 Moderator

temperature coefficient (MTC) Surveillance at 300 ppm (TS 4.1.1.3) - Less negative than - 35.0 x 10

-5 k/k/F (-35 pcm/ F) Within 7 EFPD of reaching equilibrium boron concentration of 300 ppm.

The Revised Predicted near - EOL 300 ppm MTC shall be calculated using the algorithm contained in WCAP-13749-P-A: Revised predicted MTC = Predicted MTC + AFD Correction - 3 pcm/ F If the Revised Predicted MTC is less negative than the SR 4.1.1.3.b 300 ppm surveillance limit and all the benchmark criteria contained in the surveillance procedure are met, then an MTC measurement in accordance with SR 4.1.1.3.b is not required to be performed. The neutronics methods used with WCAP-13749-P-A are those described in WCAP-11596-P-A, "Qualification of the Phoenix-P/ANC Nuclear Design System for Pressurized Water Reactor Cores," June 1988

2.7 Analog

Rod Position Indication System (TS 3.1.3.2)

- Figure A3 (page 14B-A9)

The All Rods Out (ARO) position for all shutdown Banks and Control Banks is defined to be 229 steps withdrawn.

2.8 Control

Rod Insertion Limits (TS 3.1.3.6) - Figure A3 (page 14B-A9)

The control rod banks shall be limited in physical insertion as specified in Figure A3 for ARO = 229 steps withdrawn.

2.9 Axial

Flux Difference (TS 3.2.1) - Figure A4 (page 14B-A10)

14B-A5 Revised 09/20/2016 C28C28C28C28 Turkey Point Unit 4 Cycle 29 Core Operating Limits Report 2.10 Heat Flux Hot Channel Factor F Q(Z) (TS 3.2.2) - [F Q]L = 2.30 - K(z) = 1.0 For 0' < z < 12' where z is core height in ft 2.11 Nuclear Enthalpy Rise Hot Channel Factor (TS 3.2.3)

- FH RTP = 1.600 PFH = 0.3 2.12 DNB Parameters (TS 3.2.5) - RCS Tavg < 585.0 o F - Pressurizer Pressure > 2204 psig

14B-A6 Revised 07/21/2016 C28 Figure A1 Reactor Core Safety Limit - Three Loops in Operation 14B-A7 Revised 07/21/2016

Figure A2 Required Shutdown Margin vs Reactor Coolant Boron Concentration

14B-A8 Revised 02/24/2015

Figure A3 Turkey Point Unit 4 Cycle 29 Rod Insertion Limits vs Thermal Power ARO = 229 Steps Withdrawn, Overlap = 101 Steps

14B-A9 Revised 07/21/2016 C28 Figure A4 Axial Flux Difference as a Function of Rated Thermal Power Turkey Point Unit 4 Cycle 29

14B-A10 Revised 07/21/2016 0 20 40 60 80100120-50-40-30-20-1001020304050Percent of RATED THERMAL POWER (%)Axial Flux Difference (%)(-9,100)(+6,100)(-30,50)(+20,50)UNACCEPTABLE OPERATIONUNACCEPTABLE OPERATIONACCEPTABLE OPERATIONC28

APPENDIX 14 C TURKEY POINT UNITS 3 AND 4 UPDATED FSAR

MODIFICATION OF THE TURBINE RUNBACK SYSTEM

THIS APPENDIX HAS BEEN ENTIRELY DELETED

FLORIDA POWER AND LIGHT COMPANY

14C-1 Rev. 12 5/95

APPENDIX 14D

FLORIDA POWER AND LIGHT COMPANY

TURKEY POINT UNITS 3 AND 4

DELETED IN ITS ENTIRETY REFER TO CHAPTER 9, SECTION 9.5 AND CHAPTER 14, SECTION 14.2.1.3

HIGH DENSITY SPENT FUEL STORAGE RACKS

14D-1 Revised 09/29/2005

APPENDIX 14E

FLORIDA POWER AND LIGHT COMPANY

TURKEY POINT UNITS 3 AND 4

DELETED IN ITS ENTIRETY REFER TO CHAPTER 9, SECTION 9.5 AND CHAPTER 14, SECTION 14.2.1.3

SPENT FUEL STORAGE FACILITY MODIFICATION

SAFETY ANALYSIS REPORT

14E-i Revised 09/29/2005 APPENDIX 14F ENVIRONMENTAL CONSEQUENCES OF A LOSS-OF-COOLANT ACCIDENT

This appendix contains the original licensing basis LOCA dose analysis. This

analysis has been replaced with a revised analysis that can be found in

Section 14.3.5.

The results of analyses described in this section demonstrate that the

amounts of radioactivity released to the environment in the event of a

loss-of-coolant accident (which has an exceedingly low probability of

occurrence) are substantially less than the guidelines specified in 10 CFR

100. In summary, the computed thyroid dose values are (using the release

assumption of TID-14844):

North Boundary South Low Population Exclusion Radius Boundary Distance

Integrated Dose 4164 ft 5582 ft 5 miles 0-2 hour dose, rem 93 65 9 0-31 day dose, rem 109 75 10

Loss-of-Coolant Accident

The loss-of-coolant accident has the potential for the highest off site

doses, compared to all other accidents. The loss of coolant accident may

result in a significant amount of clad rupture; however, since the fuel does

not melt, only a limited quantity of fission products are released. If it is

assumed that all the rods fail and that all the fission products in the gap

spaces were released, the total release from the core would be less than 5%

of the saturation quantities of the radioactive iodines and noble gases.

For analytical purposes the amount of radioactive fission products that could

be released from the core have been calculated according to the fundamental

assumptions given in Reference 1 (TID 14844). This calculational model has

been widely used in evaluating the capability of PWR containment systems in

the event of the core melt down. However, it should be pointed out that no

accident of this magnitude has been described for these units; in fact, an

accident of this magnitude is not considered credible.

14F-1 Rev. 10 7/92 The TID 14844 model assumes that 50% of the total core iodine inventory is released, and that one half of this amount becomes plated out onto surfaces

within the containment. The remaining one half, or 25% of the total core

iodine inventory, is assumed to be in the containment atmosphere and

available for leakage. As a function of time the charcoal filter system

collects and retains the iodine, and thereby the amount of iodine available

for leakage is substantially reduced.

The TID 14844 model also assumes that 100% of the total core noble gas

inventory and 1% of the total core solid fission product inventory are

released into the containment.

Core Inventory of Iodines and Noble Gases

The total core inventory was calculated on the basis of the reactor having

been operated as follows: (1) 2300 MW(t), (2) 625 days of full-power

operation to produce 1-129 and the stable isotopes, and (3) except for I-129, full-power operation to reach the saturation inventory of the radioactive

isotopes. Table 14F-1 gives information on the major iodine isotopes

computed for the Turkey Point core, based on data given in TID 14844. Table

14F-2 gives information on the major noble gas isotopes.

Iodines and Noble Gases in Containment Atmosphere

The amount of noble gases in the containment atmosphere at time zero (according to the TID 14844 model) is the total amount listed in Table 14F-2.

These gases are assumed to be completely mixed in the atmosphere, and

available for leakage.

The amount of iodine in the containment atmosphere at time zero (according to

the TID 14844 model, 25% of total) adds up to the following:

Total of I-127 and I-129 2,550 grams, stable Total of I-131, I-132, I-133, I-134 and 1-135 152 grams, radioactive Total Iodine in Containment 2,702 grams

14F-2 Rev. 10 7/92 The iodine, when released from the core, has been observed by those working in the field to be essentially composed of elemental iodine with little more

than a trace of organic iodides. Upon reaching the containment, and as a

function of time, some of the elemental iodine reacts with organic materials

to form organic iodides, typified by methyl iodide. Also, some hydrogen

iodide is formed.

The percentage of the iodine in the containment atmosphere that becomes

converted into methyl iodide is not precisely known. The best evidence

indicates that the value lies between an infinitesimal amount and 5%. It is

stated in Reference 2 that "Although there is only a small amount of

information available on which to base a judgement, a value of 10% for

organic (nonremovable) iodides in the total available for leakage is

considered very conservative...". For dose calculations the elemental iodine

was taken as 95% and the methyl iodide as 5%.

With respect to iodine cleanup, the dose calculations are based on the

removal that occurs only in the charcoal filter units and the 50% plateout

previously mentioned. That is a conservative assumption since cleanup will

also be achieved as follows:

1. Some iodine will be deposited on particles in the atmosphere. Some of these particles will be entrained by the containment borated spray

water. The remainder of the particles will be collected in the HEPA

filters.

2. Based on information given in Reference 3, and companion reports, the elemental iodine (and iodides other than organic) in the atmosphere may

be effectively cleaned up by the containment spray water. This cleanup

by the water is not permanent (since no iodine retaining agent is

added) in that the iodine will seek an equilibrium distribution between

the water and the air in accordance with its partition factor.

14F-3 Rev. 10 7/92 Iodine Cleanup With Emergency Containment Filter Units The capability of the emergency containment filter units to collect elemental

iodine and methyl iodide is indicated by a "decontamination factor" (DF),

which in turn depends upon a "removal constant" (). Removal constants were computed on the basis of the equation and numerical values given in Table

14F-3. The following removal constants were computed:

Number of Filter Elemental Iodine Methyl Iodide

Units Operating a b 3 (total installed) 3.53 2.74

2 (minimum safeguards) 2.35 1.83

The general decontamination factor equation is given in Table 14F-4. With

the use of this equation the following decontamination factors were

calculated, based on the iodine in the containment being composed of 0.95

elemental iodine and 0.05 methyl iodide:

2 Filter Units 3 Filter Units

Operating Operating

Time period DF DF 0-2 hours 4.68 6.97

2-12 hours > l00* > l00*

12 hours1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br /> - 31 days > l00* > l00*

Containment Assumptions

The containment design leak rate is 0.25% per day (2.9 x 10

8) fraction/sec) at the design pressure of 59 psig. In the event of a loss-of-coolant

accident the containment pressure will rise to some value less than 59 psig, and will then decrease to near atmospheric pressure due to the action of the

containment sprays and emergency containment coolers.

• These values were arbitrarily limited in order to obtain a finite number in the dose calculations.

14F-4 Rev. 10 7/92 For the dose calculations the pressure of the containment was assumed toremain at 59 psig for the entire length of the period, and thereby the leak

rate was taken as a fixed value of 0.25% per day. This assumption tends to

be very conservative, particularly for the "12 hour1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br />s-31 days" period.

Atmospheric Dispersion Model

For calculational purposes, the pressurized air-steam mixture in the

containment was assumed to leak out at the established leak rate given above.

This leakage from the containment becomes dispersed into the atmosphere and

the dose rate to an individual at any specific location is a function of

source concentration, time, distance, and atmospheric dispersion.

Dilution multipliers (x/Q), which reflect relative concentrations of

radioactivity in the atmosphere as a function of distance from the

containment, were calculated in accordance with equations and meteorological

conditions given in Tables 14F-5 and 14F-6.

No credit was taken for the building wake effect for either the "2-12 hours" period or the "12 hour1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br />s-31 days" period. This introduces some conservatism

near the site boundary, but the error diminishes with distance. The values

of y and z were taken from Reference 4.

The dilution multiplier values (in seconds/cubic meter) for the stated

conditions at various locations are tabulated below:

North Boundary South Low Population Exclusion Radius Boundary Distance

Time period 4164 ft 5582 ft 5 miles 0-2 hours 154 x 10

-6 108 x 10

-6 15.0 x 10

-6 2-12 hours 108 x 10

-6 66 x 10

-6 6.5 x 10

-6 12 hours1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br /> - 31 days 4.32 x 10

-6 2.64 x 10

-6 0.24 x 10

-6

14F-5 Rev. 10 7/92 Thyroid Dose Computations The thyroid doses for various time periods were calculated according to the

equation and values given in Table 14F-7.

The following values were obtained:

North Boundary South Low Population Exclusion Radius Boundary Distance

Integrated Dose 4164 ft 5582 ft 5 miles 0-2 hour dose, rem 93 65 9

0-31 day dose, rem 109 75 10

These values demonstrate that the amount of radioactivity that would be

released to the environment in the event of a loss-of-coolant accident give

dose values that are substantially less than the guidelines specified in 10

CFR 100.

Several parameter studies were performed in order to indicate the change in

thyroid dose values that would result in the event of a deviation in an

original assumption. For example, it was found that the doses remain almost

unaffected in case of filter unit fan failure after a brief period of time.

The above given dose values were based on two filter units operating

continuously for the duration of the accident. The principal cleanup occurs

within the first two hours; in fact, within this period of time the iodine

concentration will be reduced to less than 2% of the original concentration.

14F-6 Rev. 10 7/92 After two hours, the filter units serve to continue cleaning the air of residual amounts of iodine. The following tabulation illustrates the

insensitivity of the dose values due to equipment malfunction after two

hours.

Dose at Exclusion Radius, rem

Classification Condition 0-2 hours 0-31 days

Normal Two filter units operating 93 109 31 days or longer.

Abnormal One filter unit operating 93 110 31 days or longer. Second filter unit operating for first 2 hours2.314815e-5 days <br />5.555556e-4 hours <br />3.306878e-6 weeks <br />7.61e-7 months <br /> only.

Abnormal Two filter units operating 93 111 first 2 hours2.314815e-5 days <br />5.555556e-4 hours <br />3.306878e-6 weeks <br />7.61e-7 months <br /> only.

In case a filter unit does fail after operating for a period of time, the

radioactive decay heat is absorbed by the borated water spray system to the

filters, thereby holding the collected iodine within the charcoal.

Another example is the sensitivity of the system to the methyl iodide

content, since it cannot be established at this time precisely what fraction

of the iodine will be in the methyl iodide form. Calculations were made to

examine the variation in the 0-2 hour dose at the north boundary that would

occur if the methyl iodide content in the containment atmosphere varied from

0% to as much as 15%.

Methyl Iodide, Fraction

.00

.05

.10

.15 DF 4.75 4.68 4.62 4.56 Dose, rem 92 93 94 95

For the calculations it was assumed that two filter units were operating with

a of 2.35 for elemental iodine and a of 1.83 for methyl iodide, as given earlier. One concludes from the above that the exact amount of methyl iodide

does not need to be known since the total dose varies very little.

14F-7 Rev. 10 7/92 A third example is the sensitivity of the system to unfilterable iodide. The concept of an unfilterable form of airborne iodine is hardly consistent with

any physical model of filtration. It is possible, but not reasonable, on the

basis of a thorough examination of the data (refer to references given in

Reference 5), that some forms of iodine might be removed at very low

efficiencies. It is a simplified approach to the calculations to assume that

there is a form of iodine which is "unfilterable," or will be removed at zero

percent efficiency, even though this does not agree with experimental data.

In order to show sensitivity, calculations were made on the assumption of

varying amounts of unfilterables to determine the variation in the 0-2 hour

dose at the north and south boundaries, and the 0-31 day dose at a distance

of 5 miles, with the unfilterable iodine varying in concentration from zero

to 15% of the iodine concentration in the containment atmosphere. The

results, with 2 filter units operating, were as follows:

Fraction of Iodine that is Unfilterable:

Integrated Dose

.00

.05

.10

.15 0-2 hr Dose, rem, North Boundary 92 108 125 142 0-2 hr Dose, rem, South Boundary 64 76 88 100

0-31 day Dose, rem, at 5 Miles 10 16 22 28

In reviewing the results computed on this basis, it is seen that the doses

are all much less than 300 rem, even with the unfilterable content being 15%.

Although the applicant does not believe that this calculational model is the

proper one to use, it should be noted that the calculated dose values are

low.

Short-term Thyroid Doses at Beach and Scout Camps

The maximum thyroid doses have also been considered for areas within the site

boundary temporarily occupied by the public assuming the TID-14844 accident

analysis model. These areas are the Turkey Point Beach at 2000 feet, the

Girl Scout Camp at 2300 feet and the Boy Scout Camp at 2900 feet from the nearest containment structure. The respective /Q values at these distances, considering the volume source correction, are 3.2 x 10

-4 , 2.8 x 10

-4 and 2.3 x 10-4 sec/M 3 for the period of 0 to 2 hours2.314815e-5 days <br />5.555556e-4 hours <br />3.306878e-6 weeks <br />7.61e-7 months <br /> following the postulated LOCA.

14F-8 Rev. 10 7/92 By selection of a very conservative value of 59 psig maximum containment pressure for the leakage driving function over the entire initial two hours, the effective maximum containment leak rate is 0.25% / day. The resultant

maximum two hour thyroid dose at the indicated locations, generated from an

initial 95% elemental iodine and 5% methyl iodide atmospheric constituency, are:

Turkey Point Beach 190 rem Girl Scout Camp 170 rem Boy Scout Camp 138 rem

These values point out the requirement for the site evacuation procedure to

be implemented within the initial 2 hour2.314815e-5 days <br />5.555556e-4 hours <br />3.306878e-6 weeks <br />7.61e-7 months <br /> period, which will be provided and

followed.

Whole Body Dose Computations

Whole body doses resulting from the accident were also computed. The major

contribution is the dose from immersion in the plume. The direct radiation

dose from the containment is insignificant due to the shielding provided by

its walls.

Direct doses were calculated assuming immersion in a semi-infinite cloud

containing a uniform distribution of the gas isotopes which have leaked from

the containment. Cloud concentrations assumed were those actually calculated

at the centerline of the plume.

The following whole body doses from the passing cloud were computed:

North Boundary South Low Population Exclusion Radius Boundary Distance

Integrated Dose 4164 ft 5582 ft 5 miles 0-2 hour dose, rem 3.1 2.2 0.4 0-31 day dose, rem 5.2 3.5 0.6 These values are small compared to the guidelines specified in 10 CFR 100.

14F-9 Rev. 10 7/92 Radiological Assessment of Containment Purge The radiological doses due to a postulated loss of coolant accident presented

in the proceeding analyses assumed that there was no containment purging

occurring at the onset of the accident. Discussed herein are the results of

an analysis performed to determine the incremental radiological dose at the

site boundary and low population zone assuming the purge valves are fully

open when the accident initiates and close upon receipt of signal as

designed. These incremental doses, when added to those previously presented

in Section 14.3.5, provide a maximum set of doses for a LOCA with containment

purge. The results of this evaluation are presented in the following tables:

(6)

THYROID DOSE (rem)

Increment Due

Location LOCA To Purging Total

Site Boundary - 93 10 103 (0-2 hour)

Low Population Zone - 9 1 10 (0-2 hour)

WHOLE BODY (rem)

Increment Due

Location LOCA To Purging Total

Site boundary - 3.1 .002 3.1 (0-2 hour)

Low Population Zone - .4

.0002 .4 (0-2 hour)

The major assumptions which were used in the evaluation of the incremental

dose are listed below:

1. The containment purge valves are closed 5 seconds after the containment high pressure signal is transmitted. There is a 2.7 second delay before

14F-10 Rev. 10 7/92 the increased containment pressure is detected which results in a total of 7.7 seconds for valve closure (8 seconds was conservatively assumed).

2. Radioactive releases via the purge valves during closure is from the Reactor Coolant System only.

3. The primary coolant iodine activity corresponds to the maximum limit of 30 Ci/gm Dose Equivalent.

4. It is conservatively assumed during the initial 8 seconds that 5O% of the blowdown (worst FSAR case) from the break flashes and becomes

homogeneously mixed in the containment atmosphere. All of the iodine in

the flashed steam is assumed to become airborne.

5. The flow through the purge valves is assumed to be a mixture of steam and water. Frictionless flow through the valves is assumed.

6. FSAR meteorology is assumed.

7. Standard TID 14844 methodology was used to calculate the incremental doses.

The results clearly indicate that the anticipated dose caused by a LOCA with

containment purging at the onset of the accident is well within the limits of

10 CFR 100.

14F-11 Rev. 10 7/92 References

1. J. J. DiNunno, F. D. Anderson, R. E. Baker, and R. L. Waterfield, Calculation of Distance Factors for Power and Test Reactor Sites, USAEC Report TID-14844, March 23, 1961.

2. Supplemental Safety Evaluations by the Division of Reactor Licensing, United States Atomic Energy Commission, in the Matter of Florida Power

and Light Company, Turkey Point Units 3 & 4, July 12, 1968.

3. Nuclear Safety Program Annual Progress Report for Period Ending December 31, 1967, Oak Ridge National Laboratory, ORNL-4228, April 1968.

4. W. F. Hilsmeier and F. A. Gifford, Jr., Graphs for Estimating Atmospheric Dispersion, Report ORO-545, Weather Bureau Research Station, Oak Ridge, Tenn., August 23, 1962.

5. Supplement No. 14 to Application for Licenses, re Florida Power & Light Company, Turkey Point Units 3 & 4, USAEC Docket Nos. 50-250, 50-251, March 14, 1968.

6. R. E. Uhrig (FPL) letter #L-79-346, to A. Schwencer (NRC), dated December 13, 1979, "Containment Purge".

14F-12 Rev. 10 7/92 TABLE 14F-1 IODINE ISOTOPES AND THEIR ESTIMATED QUANTITIES FOR A FULL CORE INVENTORY AT TIME ZERO

Isotope Half-Life Grams Curies

I-127 Stable 2,040 0

I-129 1.72 x 10 7 years 8,170 ~ 0 I-131 8.05 days 452 57.7 x 10 6 I-132 2.4 hours4.62963e-5 days <br />0.00111 hours <br />6.613757e-6 weeks <br />1.522e-6 months <br /> 8.25 87.5 x 10 6 I-133 20.8 hours9.259259e-5 days <br />0.00222 hours <br />1.322751e-5 weeks <br />3.044e-6 months <br /> 109.7 129.5 x 10 6 I-134 52.5 minutes 5.35 151.3 x 10 6 I-135 6.68 hours7.87037e-4 days <br />0.0189 hours <br />1.124339e-4 weeks <br />2.5874e-5 months <br /> 31.9 117.2 x 10 6

Lumping all radioactive isotopes into an I-131 equivalent 109 x 10 6

Rev. 10 7/92 TABLE 14F-2 NOBLE GAS ISOTOPES AND THEIR ESTIMATED QUANTITIES FOR A FULL CORE INVENTORY AT TIME ZERO

Isotope Half-Life Curies

Kr-83m 114 minutes 10.6 x 10 6

Kr-85 10.76 Years 0.83 x 10 6

Kr-85m 4.36 hours4.166667e-4 days <br />0.01 hours <br />5.952381e-5 weeks <br />1.3698e-5 months <br /> 25.5 x 10 6

Kr-87 78 minutes 47.3 x 10 6

Kr-88 2.77 hours8.912037e-4 days <br />0.0214 hours <br />1.273148e-4 weeks <br />2.92985e-5 months <br /> 64.3 x 10 6

Xe-131m 12.0 days 0.46 x 10 6

Xe-133m 2.3 days 3.08 x 10 6

Xe-133 5.27 days 128.4 x 10 6

Xe-135m 15.6 minutes 41.5 x 10 6

Xe-135 9.13 hours1.50463e-4 days <br />0.00361 hours <br />2.149471e-5 weeks <br />4.9465e-6 months <br /> 32.0 x 10 6

Rev. 10 7/92 TABLE 14F-3 EQUATION FOR REMOVAL CONSTANT

= n v e m 60 V

= removal constant, per hour n = number of filter units operating

v = atmosphere flow through each filter unit, cu ft/min

e = charcoal filter efficiency, fraction

m = atmosphere mixing factor, fraction

V = free volume of containment, cu ft

Elemental iodine Methyl iodide

a b

v 37,500 37,500

e 0.9 0.7

m 0.9 0.9

v 1.55 x 10 6 1.55 x 10 6

Rev. 10 7/92 TABLE 14F-4 GENERAL DECONTAMINATION FACTOR EQUATION

DF = 1

F a = filterable elemental iodine, fraction of total iodine in containment

atmosphere.

F b = filterable methyl iodide, fraction of total iodine in containment atmosphere.

F c= unfilterable iodine and iodide; engineering tests indicate no components to be unfilterable; therefore, this is assumed to

be zero.

t 1= time of operation prior to the period under consideration, hours.

t 2= time of operation during the period under consideration, hours.

Rev. 10 7/92 F + t e - 1 e F + t e - 1 e F c2b t-t-b2a t-t-a2b1b2a1a TABLE 14F-5 DILUTION MULTIPLIER EQUATIONS

Time period

X = concentration, curies/cu. meter

Q = source strength, curies/second

~ = average wind speed, meters/second

~i = wind speed for condition i, meters/second y= horizontal dispersion parameter, meters z= vertical dispersion parameter, meters zi= vertical dispersion parameter for condition i, meters c = building shape factor (selected as 0.5)

A = cross-sectional area of building normal to wind (1750 sq meters)

= sector size, radians x = distance from source, meters

f = fraction of time wind blows in sector

F i= fraction of time condition i exists

Rev. 10 7/92 0-2 hours cA) + ( 1 = Q zy 2-12 hours x /2 1 = Q z 12 hours1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br /> - 31 days x /2 F f = Q z i i i TABLE 14F-6 METEOROLOGICAL CONDITIONS

Time period Condition

0-2 hours Stability category, Pasquill F;

Wind speed, 2 meters/sec;

Wind direction, unvarying.

2-12 hours Stability category, Pasquill F;

Wind speed, 2 meters/sec;

Wind direction,10 degree sector.

12 hours1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br /> - 31 days Wind direction, 22.5 degree sector;

Wind blowing in this sector 25% of

the time with the following

variable conditions:

Stability Wind speed

Fraction category meters/sec

.25 F 2

.50 D 5

.25 C 4

Rev. 10 7/92 TABLE 14F-7 THYROID DOSE EQUATION AND SPECIFIC VALUES

_ x 1 DCF Dose ( in rem) = t BLA Q DF

t = time period, hours

B = breathing rate, cu. meters/hour

L = reactor building leak rate, per second

_

A = average inventory of equivalent I-131 available for leakage

assuming no filter unit cleanup during the period, curies

x = atmospheric dilution multiplier, seconds/cu. meter Q

DF = iodine decontamination factor for the period; that is, the ratio

of iodine without cleanup to iodine with cleanup

DCF = dose conversion factor for I-131, rem/curie

0-2 hours 2-12 hours 12 hours1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br /> - 31 days t 2 10 732

B 1.25 1.00 .834

L 2.9 x 10

-8 2.9 x 10

-8 2.9 x 10

-8 _

A 26.17 x 10 6 23.04 x 10 6 5.24 x 10 6

DF (2 units) 4.68 100 100

DCF 1.48 x 10 6 1.48 x 10 6 1.48 x 10 6 x Refer to tabulation given in paragraph "Atmospheric Q Dispersion Model".

Rev. 10 7/92 APPENDIX 14G HISTORICAL DISCUSSION OF CONTAINMENT PRESSURE TRANSIENT MARGINS ASSOCIATED WITH CONTAINMENT STRUCTURAL PRESSURE OF 59 PSIG

INTRODUCTION

This appendix contains the original FSAR discussion of the containment design

pressure margins associated with the original containment structural

capability pressure of 59 psig. Since the original containment structural

capability pressure of 59 psig has been replaced with the licensed design

basis pressure (55 psig) approved by the Atomic Energy Commission (AEC)

during the operating license stage, this discussion is of historical

importance only and does not apply to the current licensed containment design

pressure or to the basis for calculating the minimum required prestress

forces for the containment post-tensioning system. Refer to the engineering

evaluation contained in Reference 1.

BACKGROUND

The licensed containment design basis pressure of 55 psig was established

during the very early stages of plant licensing and has carried through to

current licensing documents. The PSAR and FSAR indicated that a 55 psig

reference containment design pressure was conservatively established for the

design basis (29-inch double-ended pipe break) loss-of-coolant accident (LOCA), based on a 49.9 psig calculated peak pressure plus a 10% safety

margin; and the structural proof test was conducted at 115% design pressure

to check structural integrity. Refer to PSAR Sections 5.4.1.a and 12.2.3 (Reference 2), and to original (1970) FSAR Section 5.1.1, (Reference 3).

Other LOCA study cases, assuming partial safeguards availability, were also

considered. These study cases did not constitute licensed design basis

accident scenarios, but rather provided an indication of potential

containment performance requirements beyond-the-licensing-basis for purposes

of establishing conservative design margins for the containment structures.

14G-1 Rev. 11 11/93 These scenarios were developed in response to Atomic Energy Commission (AEC) questions, and to address uncertainties as to the availability of primary

system accumulators. As a result, some of these other cases assumed partial

safeguards operation with no core cooling, which were conditions that are

beyond the required postulation of a single active or passive failure. Refer

to PSAR Supplement 2, Questions 1.0 and 3.0 (Reference 4). For instance, the

AEC requested that a "no-core-cooling" case be considered, in which partial

safeguards equipment, operating on diesel power, introduced all the safety

injection water directly into the sump. This case resulted in a maximum

pressure of 58.5 psig. However, the value of 55 psig came about as the

result of the design basis analysis which assumed that partial safeguards

equipment, operating on diesel power, provided core cooling by having 2/3 of

the safety injection water flow paths reach the core.

To accommodate these hypothetical, beyond-the-licensing-basis scenarios, the

containment structure was designed with additional margins to withstand a

pressure of 59 psig; however, the licensed design basis LOCA analysis

calculated peak pressure was 49.9 psig, and "55 psig [was] considered as

nominal structural design pressure, thus allowing a margin of 10% over the

calculated peak accident pressure." Refer to original 1970 FSAR, Section

5.1.1 - Reference 3).

CONTAINMENT MARGIN EVALUATIONS

Evaluation of the capability of the containment and associated cooling

systems to absorb energy additions without exceeding the containment design

pressure requires consideration of two periods of time following a postulated

large area rupture of the reactor coolant system.

The first period is the blowdown phase. Since blowdown occurs too rapidly

for the containment cooling systems to be activated, there must be sufficient

energy absorption capability in the free volume of the containment (with due

credit for energy absorption in the containment structures) to limit the

resulting pressure below design.

14G-2 Rev. 11 11/93 The second period is the post-blowdown period where the containment cooling systems must be able to absorb any postulated post-blowdown energy additions

and continue to limit the containment pressure below design.

Margin - Blowdown Peak to Design Pressure

Point A in Figure 14G-1 corresponds to the internal energy at the end of a DE

break blowdown, 195 x 10 6 Btu. In order for the pressure to increase to design pressure (59 psig) the internal energy must be increased to 231 x 10 6 Btu (Point B). The allowed energy addition is therefore 36 x 10 6 Btu. Since energy transferred to the containment from the core is in the form of steam

the total transferred core energy corresponding to allowed energy addition is

as follows:

h fg 921.9 Q core = Q allowed = 36 x 10 6 x = 28.4 x 10 6 Btu h g 1177.6

This allowable value of energy which could be transferred from the core to the containment without increasing the transient containment pressure to

design pressure can be compared to the energy stored in the reactor vessel

and transferred to the steam generator during blowdown for the double ended

break. The thick metal of the reactor vessel was not considered since a

negligible amount of this energy can be transferred in the short blowdown

time.

Stored in the core 15.0 x 10 6 Btu Core internals Metal 0.3 x 10 6 Btu Transferred to Steam Generators 1.4 x 10 6 Btu

16.7 x 10 6 Btu Thus, the containment has the capability to limit containment pressure below

design even if all of the available energy sources were transferred to the

containment at the end of blowdown. This would also include no credit for

14G-3 Rev. 11 11/93 energy absorption in the steam generator. For this to occur an extremely high core to coolant heat transfer coefficient is necessary. This would

result in the core and internals being completely subcooled and limit the

potential for release of fission products.

Additional Energy Added as Superheat

Line A to C on Figure 14G-1 represents a constant mass line extended into the

superheated region. Comparison of the energy addition allowable for the

superheated case relative to the saturated case shows a lesser ability of the

containment to absorb an equivalent amount of energy as superheat. An

addition of 8.5 x 10 6 Btu of energy after blowdown would cause the containment pressure to increase to design. The recombination of hydrogen

and oxygen from 9.6% Zr-H 2 O reaction completed before the end of blowdown would be required to generate 8.5 x 10 6 Btu's of energy. For the case analyzed, the core was assumed to be in a subcooled state, and no Zr-H 2 O reaction would be possible. In order for Zr-H 2 O reaction to occur before the end of blowdown all of the stored initial energy must remain in the core. If

this occurred a blowdown peak containment pressure of only 44.2 psig would be

reached instead of 49.9 psig in the case analyzed. Lines D and E on Figure

14G-1 represent the superheat energy addition required to increase the

pressure to the design pressure and this corresponds to the hydrogen oxygen

recombination energy from a 15.8% Zr-H 2 O reaction.

It is, therefore, concluded that the containment has the capability to absorb

the maximum energy addition from any loss-of-coolant accident without

reliance on the containment cooling system. In addition, a substantial

margin exists for energy additions from arbitrary energy sources much greater

than any possible.

Margin - Post Blowdown Energy Additions

The Safety Injection System is designed to rapidly cool the core and stop

significant addition of mass and energy to the containment.

14G-4 Rev. 11 11/93 However, the following cases are presented to demonstrate the capability of the containment to withstand post accident energy additions without credit

for core cooling.

Case 1 : Blowdown from a large area rupture with continued addition of the core residual energy and hot metal energy to the containment as

steam.

Case 2 : Same as Case I but with the energy addition from a maximum Zirconium - water reaction.

Figure 14G-2 presents the containment pressure transient for Case 1. For

this case the decay heat generated for a 2300 MWt core operated for an

infinite time is conservatively assumed. This decay heat is added to the

containment in the form of steam by the boiling off of water in the reactor

vessel. For this case injection water merely serves as a mechanism to

transfer the residual energy to the containment as it is produced. Injection

water is in effect throttled at the required rate.

In addition, all the stored energy in the core and internals which is

calculated to remain at the end of blow down is added in the same way during

the time interval between 12.7 and 36.5 seconds (corresponds to accumulator

injection time). Also all the sensible heat of the reactor vessel is added

as steam exponentially over 2000 seconds time interval.

The containment cooling system capability assumed in the analysis was one of

two available containment spray pumps and two of three available emergency

containment coolers. This is the minimum equipment available considering the

single failure criterion in the emergency power system, the containment spray

system and the fan cooler system.

The containment heat removal capability started at 60 seconds exceeds the

energy addition rate and the pressure does not exceed the initial blowdown

value. An extended depressurization time results due to the increased heat

load on the containment coolers.

14G-5 Rev. 11 11/93 It should be emphasized that this situation is highly unrealistic in that continued addition of steam to the containment after blowdown could not

occur. The accumulator and Safety Injection System acts to rapidly reflood

and cool the core.

Figure 14G-3 presents the containment pressure transient for Case 2. To

realistically account for the energy necessary to cause a metal-water

reaction, sufficient energy must be stored in the core. Storing the energy

in the core rather than transferring it to the coolant causes a decrease in

the blowdown peak.

The reaction was calculated using the parabolic rate equation developed by

Baker and assuming that the clad continues to react until zirconium oxide

melting temperature of 4800 o F is reached. An additional 10% reaction of the unreacted clad is assumed when the oxide melting temperature is reached. A

total reaction of 32.3% has occurred after 1000 seconds. If the reactions

were to be steam limited, they could result in a higher total reaction but at

a much later time. The reaction provided by the parabolic rate equation

therefore, imposes the greatest load on the containment cooling system.

As in Case 2, the residual heat and sensible heat is added to the containment

as steam. The energy from the Zr-H 2 O reaction is added to the containment as it is produced. The hydrogen was assumed to burn as it entered the

containment from the break.

The blowdown peak was reduced to 44 psig and a peak pressure of 57.7 psig was

reached at 600 seconds. At this time the heat removal capability of the

containment cooling system assumed to be operating (one containment spray

pump and two fan coolers) exceeded the energy addition from all sources.

For comparison the containment pressure transients for Cases 1, 2 and the

double ended blowdown are replotted in Figure 14G-4. It is concluded that

operation of the minimum containment cooling system equipment provides the

capability of limiting the containment pressure below its design pressure

with the addition of all available energy sources and without credit for the

cooling effect from the safety injection system.

14G-6 Rev. 11 11/93 DISCUSSION OF ENERGY SOURCES USED IN CASES 1 AND 2

The following is a summary of the energy sources and the containment heat

removal capacities used in the containment capability study. Figure 14G-5

presents the rate of energy addition from core decay heat, Zr-H 2 O reaction energy, and the hydrogen-oxygen recombination energy. The heat removal

capability for the partial containment cooling (one spray pump and two fan

coolers) is also presented. These heat removal values are for operation with

the containment at design pressure.

The integrated heat additions and heat removals for Cases 1 and 2 are plotted

in Figures 14G-6 and 14G-7, respectively. These curves are presented in a

manner that demonstrates the capability of the containment and the cooling

systems to absorb energy. The integrated heat removal capacity is started at

the internal energy corresponding to design pressure, while the integrated

heat additions begin from the internal energy calculated at the end of

blowdown for each case. The upper line on each curve is the containment

structures and containment cooling systems capability to absorb energy

additions without exceeding design pressure. The lower curve for each are

the energy addition curves, and since these energy additions are the maximum

possible with no credit for core cooling, there is more than adequate

capability to absorb arbitrary additions.

The curves in Figures 14G-8 and 14G-9 present the individual contribution of

the heat removal and heat addition source, respectively.

14G-7 Rev. 11 11/93 REFERENCES

1. Engineering Evaluation JPN-PTN-SENP-93-008,"No Significant Hazards Evaluation Related to Containment Design Pressure Technical

Specification and UFSAR Changes," Revision 0, dated April 23, 1993.

2. Turkey Point Units 3 and 4 Preliminary Safety Analysis Report (PSAR), Sections 5.4.1.a and 12.2.3, submitted by Application dated March 22, 1966.

3. Turkey Point Units 3 and 4 (original) Final Safety Analysis Report (FSAR), Section 5.1.1, "Containment Structure Design Bases," Revision

4, dated August 12, 1970.

14G-8 Revised 05/14/2005