PLA-6080, Proposed Amendments No. 269 and 236: DC Electrical Power Systems Technical Specifications Rewrite Second RAI Response

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Proposed Amendments No. 269 and 236: DC Electrical Power Systems Technical Specifications Rewrite Second RAI Response
ML061930137
Person / Time
Site: Susquehanna  Talen Energy icon.png
Issue date: 06/30/2006
From: Mckinney B
Susquehanna
To:
Document Control Desk, Office of Nuclear Reactor Regulation
References
PLA-6080, TAC MC5153, TAC MC5154
Download: ML061930137 (16)


Text

Britt T. McKinney PPL Susquehanna, LLC "I~u Sr. Vice President &Chief Nuclear Officer 769 Salem Boulevard Berwick, PA 18603 .

Tel. 570.542.3149 Fax 570.542.1504 .5,,.-

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JUN 3 0 2006 U. S. Nuclear Regulatory Commission Attn: Document Control Desk Mail Stop OP1-17 Washington, DC 20555 SUSQUEHANNA STEAM ELECTRIC STATION PROPOSED AMENDMENT NO. 269 TO UNIT 1 LICENSE NPF-14 AND AMENDMENT NO. 236 TO UNIT 2 LICENSE NPF-22: DC ELECTRICAL POWER SYSTEMS TECHNICAL SPECIFICATIONS REWRITE SECOND RAI RESPONSE Docket Nos. 50-387 PLA-6080 and 50-388

References:

1) PLA-5825, B. T. McKinney (PPL) to Document Control Desk (USNRC, ProposedAmendment No. 269 to Unit I License NPF-14 and Amendment No. 236 to Unit 2 License NPF-22:DC ElectricalPowerSystems Technical Specifications Rewrite," dated November 9, 2004.
2) Letterfrom USNRC (R. V. Guzman) to B. T. McKinney (PPL), "Request for Additional Information (RAI) - SSES Units I & 2 DC ElectricalPower Systems TSTF-360 (TA C Nos. MC5153 and MC5154)," dated October 19, 2005.
3) PLA-5995, B. T. McKinney (PPL) to Document Control Desk (USNRC),

ProposedAmendment No. 269 to Unit I License NPF-14 and Amendment No. 236 to Unit 2 License NPF-22: DC ElectricalPower Systems Technical Specifications Rewrite-Response to Requestfor Additional Information (RAI), " dated December 15, 2005.

4) Letterfrom USNRC (R. V. Guzman) to B. T. McKinney (PPL), "Request for Additional Information (RAI) - SSES Units I & 2-Requestfor Additional Information regarding Amendment Application to Revise Technical Specificationson DC ElectricalSystem Requirements (TAC Nos. MC5153 and MC5154)," dated May 31, 2006.
5) Letterfrom USNRC (T. H. Boyce) to Technical Specification Task Force (TSTF),

"Requestfor Public Meeting to Discuss Enclosed Document ElectricalEngineering Branch Concerns with Technical Specification Task Force (TSTF)-360, Revision 1 DC Electrical Rewrite," dated April 11, 2006.

In accordance with the provisions of 10 CFR 50.90, PPL Susquehanna, LLC (SSES) submitted a request for amendment to the Technical Specifications (TS) for Susquehanna Units 1 & 2. (Reference 1). Reference 3 provided PPL's revised amendment request in response to the NRC Request for Additional Information (RAI) in Reference 2.

Document Control Desk PLA-6080 The enclosure to this letter provides the PPL response to each of the four questions in Reference 4. PPL's responses are consistent with the Technical Specification Task Force (TSTF) draft responses to Reference 5, which are to be discussed with NRC at a public meeting scheduled for July 12, 2006.

Attachment 1 contains a draft of the Technical Requirements Manual (TRM)

Section 3.8.7 for the new licensee controlled battery monitoring and maintenance program. Attachment 2 contains a revision to proposed TS Section 5.5.13 previously submitted by Reference 3. This proposed revision does not affect the No Significant Hazards Considerations included with Reference 3.

PPL plans to implement the proposed changes as soon as practical following NRC approval. Therefore, we request NRC complete its review by September 29, 2006 with changes to be implemented within 60 days of NRC approval.

Any questions regarding this request should be directed to Mr. Duane L. Filchner at (610) 774-7819.

I declare under penalty of perjury that the foregoing is true and correct.

Executed on: 'V"-sie 30., a'0o6

  • LB. T. McKinney

Enclosure:

PPL Susquehanna Response to NRC Second Request for Additional Information Attachment 1: PPL Battery Monitoring and Maintenance Program (Draft)

Attachment 2: Revised Markup to Proposed Units 1&2 Technical Specification Section 5.5.13 cc: NRC Region I Mr. A. J. Blamey, NRC Sr. Resident Inspector Mr. R. V. Guzman, NRC Project Manager Mr. R. Janati, DEP/BRP

ENCLOSURE TO PLA-6080 PPL SUSQUEHANNA - RESPONSE TO NRC SECOND REQUEST FOR ADDITIONAL INFORMATION

Enclosure to PLA-6080 Page 1 of 5 Response to NRC Second Request for Additional Information NRC QUESTION 1:

Specific gravity monitoring is used to measure the strength of a battery cell's electrolyte, which is an important component of the battery's chemical reaction, and provides an indication of the battery's state-of-charge. Whereas, float current monitoring may or may not provide an accurate indication of the battery's state-of-charge. Float current monitoring is based on a calculation that is dependent on several variables. The NRC staff has a concern with two variables of this calculation: the applied charging voltage and cell resistance. A change in either of these variables may provide a false indication of the battery's state-of-charge. Provide assurance that float current monitoring will provide an accurate indication of the battery's state-of-charge.

PPL RESPONSE:

Float current monitoring provides an accurate indication and is an acceptable method to determine battery state of charge. Following a discharge, battery state of charge involves charge-discharge reactions related to electric current flow. Therefore, float current monitoring is a more meaningful indicator of state of charge because current is the primary means of discharging and charging the battery. Also, specific gravity readings have an inherent time lag on both charge and discharge. Therefore, after a discharge, float current monitoring is an accurate method to determine battery state of charge.

Float current monitoring is also an accurate method to monitor battery state of charge during steady-state operations. Since the charging voltage (E) is fixed by the battery charger and the battery internal cell resistance (R) is a very small value, the dominant factor for determining current flow in a battery cell is the internal cell voltage (Eb), where I = (E-Eb)/R. The value of Eb is dependent upon the presence of lead sulfate ions within the cell since the quantity of lead sulfate ions is associated with the state of charge (more lead sulfate is present when a battery is in a discharged state). A small amount of lead sulfate reduces the internal cell voltage, which has the effect of increasing the driving voltage (E- Eb). This results in the current flow through a discharged battery being higher than current flow under steady state fully charged conditions.

The process of charging the battery reduces the presence of lead sulfate in a fully charged battery, as such, E is approximately equal to Eb and the resulting float current is small.

Therefore, the level of float current measured with the proper float voltage applied provides an indication of the battery state of charge at any time. Measured current that is higher than the established float current value indicates a recent discharge has occurred.

Current that is at or below the established float current value provides assurance that the battery is charged.

Enclosure to PLA-6080 Page 2 of 5 Current SSES Technical Specification (TS) Table 3.8.6-1 footnote (c) and the TS Bases identify that it is acceptable to use float current to meet specific gravity limits.

NRC QUESTION 2:

The battery pilot cell is representative of the average battery cell in the battery. Provide assurance that a battery with a battery pilot cell with a voltage of 2.07 volts or slightly greater will remain capable of performing its minimum designed function.

PPL RESPONSE:

The pilot cell is representative of all cells in the battery and it is presently determined by selecting a cell, while connected to the battery charger, with a float voltage greater than 2.2 volts, and with a specific gravity reading equal to the average of all the cells. The 2.13 cell voltage limit specified in the battery monitoring and maintenance program is the limit for taking corrective action (per proposed TS 5.5.13 and draft TRM 3.8.7, ). The 2.07 cell voltage limit in proposed TS 3.8.6 Condition A represents the voltage allowed in current technical specifications. This voltage is consistent with a fully charged battery and provides assurance that sufficient capacity exists to perform the intended function and maintain a margin of safety.

Discharge tests are performed with the battery charger disconnected from the battery.

When the charger is disconnected, the average cell voltage will be below 2.07 for the entire duration of the discharge. This is consistent with the information provided by the battery manufacturer on the discharge curve for any battery. As a discharge starts, the internal resistance of the battery creates a voltage drop due to the discharge current.

(Voltage Drop = Discharge Rate X Battery Internal Resistance). Since the nominal open circuit voltage of a fully charged, 1.215 specific gravity cell is approximately 2.06 VDC; the cell voltage during the discharge will be less than this value.

Pilot cell voltage alone cannot predict the ability of the battery to perform its design function. The entire surveillance and maintenance program consists of periodic tests and inspections necessary to provide assurance the battery is capable of performing its design function.

Therefore, it can be concluded that 2.07 volts is consistent with a battery which will remain capable of performing its minimum designed function.

Enclosure to PLA-6080 Page 3 of 5 NRC OUESTION 3:

As mentioned in Question No. 2, the battery pilot cell is representative of the average battery cell in the battery. Provide assurance that a battery with a battery pilot cell electrolyte temperature slightly greater than or equal to the minimum established design limit will remain capable of performing its minimum designed function.

PPL RESPONSE:

Per the response to Question 2 above, the pilot cell is representative of all cells in the battery and it is presently determined by selecting a cell, while connected to the battery charger, with a float voltage greater than 2.2 volts, and with a specific gravity reading equal to the average of all the cells. The design temperature for the SSES battery cells is 60 degrees F. This parameter is monitored by the licensee controlled battery monitoring and maintenance program (draft TRM Section 3.8.7, Attachment 1). The impact of a single cell temperature being slightly above or below the average does not in itself affect the battery's ability to perform its design function. In addition, each battery is sized with correction factors that include temperature and aging. The battery sizing correction factors for a 60 degree temperature are 1.11 and 1.25 for aging (20 year life). The overall battery sizing correction factor is 1.3875, which is the product of these two factors. This value is utilized in the SSES battery sizing calculations.

The SSES battery room temperatures are essentially the same as the ambient temperature of the adjacent control structure areas because there is no forced cooling to these rooms.

Air is exhausted by design from redundant safety related HVAC systems which serve the rooms (to prevent hydrogen buildup), and makeup air is drawn into the rooms at the ambient temperature from the larger control structure volume. Since batteries have very large thermal inertia and the battery room temperature remains relatively constant at approximately 70 degrees F, it is concluded that the pilot cell temperature is an accurate representation of the temperature of the entire battery bank. The only heat load in a battery room (besides the batteries) is room lighting, which is normally off when the room is unoccupied. Since there is no significant heat load in the room and there is no localized impingement of ventilation air, there will be no localized hot or cold areas in the room and all battery cells are at essentially the same temperature. Further, the room does not have any internal air flow obstructions, which allows the transfer air to distribute evenly in the room. Each room is relatively small, which promotes air mixing within the room.

Based on these physical characteristics, each battery remains at essentially the same uniform temperature and the pilot cell temperature is essentially the same temperature as the other battery cells located in the room.

The present Technical Specification Surveillance requirements ensure the average electrolyte temperature of a battery is checked and verified to be within design criteria on a quarterly basis. The proposed Technical Specification SR 3.8.6.4 verifies the pilot cell

Enclosure to PLA-6080 Page 4 of 5 temperature, which is representative of all the cells in the battery as stated above, is greater than or equal to the minimum established design limit every 31 days. Such monitoring of the pilot cell every 31 days is an improvement over quarterly average temperature monitoring.

Therefore, it can be concluded that a battery with a battery pilot cell electrolyte temperature slightly greater than or equal to the minimum established design limit will remain capable of performing its minimum designed function.

NRC OUESTION 4:

Consistency with the Institute of Electrical and Electronics Engineers (IEEE)

Standard 450-1995, "IEEE Recommended Practice for Maintenance, Testing, and Replacement of Vented Lead-Acid Batteries for Stationary Applications," was used throughout your submittal as the justification for approval. The most recent version of IEEE Standard 450 that has been endorsed by the NRC through Regulatory Guides (RGs) is IEEE Standard 450-1975. The RGs of mention are: RG.1.28, "Installation, Design, and Installation of Large Lead Storage Batteries for Nuclear Power Plants," and RG 1.129, "Maintenance, Testing, and Replacement of Large Lead Storage Batteries for Nuclear Power Plants."

a. Provide a plant specific technical justification for each proposed change in lieu of referencing consistency with the IEEE Standard 450-1995.
b. Provide a copy of the proposed battery monitoring and maintenance program identified in TS 5.5.13.

PPL RESPONSE:

a. Technical justifications in the SSES proposed TS changes were not based on IEEE-450. All references to IEEE-450 were either informational or were provided to identify the contents of the new battery maintenance and monitoring program required as a result of this change. The reference to IEEE-450 1995 in the proposed TS Section 5.5.13 has been removed and replaced with a reference to the licensee controlled program used to provide for battery restoration and maintenance. The revised TS Section 5.5.13 is contained in Attachment 2.
b. PPL formally committed to establish a battery monitoring and maintenance program in Reference 3, Attachment 1, Section 4. The new program to be contained in the SSES TRM will contain the elements from the affected Technical Specification LCO's whose parameter values will continue to be controlled at their current level.

Enclosure to PLA-6080 Page 5 of 5 A copy of the battery monitoring and maintenance program (Draft) is provided in . The SSES TRM is considered a part of the SSES FSAR and as such is subject to the provisions of 10 CFR 50.59.

ATTACHMENT 1 TO PLA-6080 PPL SUSQUEHANNA BATTERY MONITORING AND MAINTENANCE PROGRAM (DRAFT)

LIJDAF Battery Monitoring and Maintenance Program 3.8.7 3.8.7 Battery Monitoring and Maintenance Program TRO 3.8.7 Battery cell parameters for the Class 1 E 250 V batteries and Class 1 E 125 V batteries shall be within limits.

APPLICABILITY: When associated DC electrical power subsystems are required to be OPERABLE.

ACTIONS


NOWr7 ---------------------------------------------------------

Separate Condition entry is allowed for each battery.

CONDITION REQUIRED ACTION COMPLETION TIME A. One or more batteries on A.1 Verify pilot cell electrolyte level 1 hour1.157407e-5 days <br />2.777778e-4 hours <br />1.653439e-6 weeks <br />3.805e-7 months <br /> one 125 VDC electrical and float voltage meet Table 3.8.7-1 power subsystem or on one Category C limits.

250 VDC electrical power subsystem for electrolyte level or float voltage not within Category A or B limits.

AND A.2 Verify battery cell parameters 8 hours9.259259e-5 days <br />0.00222 hours <br />1.322751e-5 weeks <br />3.044e-6 months <br /> meet Table 3.8.7-1 Category C limits for electrolyte level, cell AND temperature, and float voltage.

Once per 7 days thereafter AND A.3 Restore battery cell 31 Days parameters for electrolyte level, float voltage and Pilot Cell Specific Gravity to Category A and B limits of Table 3.8.7-1.

B. Required Action and B.1 Enter TS 3.8.6 Condition A, C Immediately associated Completion Time and/or D.

for Condition A.1 or A.2 not met.

C. Required Action and C.1 Declare associated battery Immediately associated Completion Time inoperable.

for Condition A.3 not met.

LIJDAF Battery Monitoring and Maintenance Program 3.8.7 D. One or more batteries on D.1 Restore in accordance with T.S 31 Days one 125 VDC electrical 3.8.6 C.3, apply equalizing charge power subsystem or on one to battery/or affected cell, and verify 250 VDC electrical power cell meets Table 3.8.7-1 Category C subsystem with one or more Limits for float voltage and cells electrolyte level less temperature.

than minimum established design limits.

E. One or more batteries on E.1 Restore battery average 24 Hours one 125 VDC electrical electrolyte temperature to greater power subsystem or on one than or equal to Table 3.8.7-1 250 VDC electrical power Category B Limits.

subsystem with average electrolyte temperature less the Table 3.8.7-1 Category B Limits.

Battery Monitoring and Maintenance Program ILRATJ 3.8.7 TECHNICAL REQUIREMENT SURVEILLANCE I

. SURVEILLANCE FREQUENCY 4-TRS 3.8.7.1 Verify for each terminal and connector: 92 Days No visible corrosion OR

a. < 50.OE-6 ohms; or
b. < 100.OE-6 ohms with the calculated average resistance for the battery < 50.OE-6 ohms.

TRS 3.8.7.2 Verify average electrolyte temperature (minimum of 10% 92 Days of cells) is within Table 3.8.7-1 Category B limits.

TRS 3.8.7.3 Verify battery cell parameters meet Table 3.8.7-1 2 Years Category B Limits for Specific Gravity.

TRS 3.8.7.4 Verify Battery cells, cell plates, and racks show no visual 2 Years indication of physical damage or abnormal deterioration that could potentially degrade battery performance.

TRS 3.8.7.5 Verify the battery connection resistance is: 2 Years

a. < 100.0 E-6 ohms for any single connection; and
b. The calculated average resistance for the battery is

< 50.0 E-6 ohms.

ILDZ Battery Monitoring and Maintenance Program 3.8.7 Table 3.8.7-1 (page 1 of 1)

Battery/Battery Cell Parameter Requirements Minimum Established > 129 VDC for the 125 V Batteries > 258 for the 250 V Batteries Battery Terminal Float Voltage:

CELL CATEGORY A: CATEGORY C:

PARAMETER LIMITS FOR EACH CATEGORY B: ALLOWABLE LIMITS DESIGNATED PILOT LIMITS FOR EACH FOR EACH CELL CONNECTED CELL CONNECTED CELL Electrolyte Level > Minimum level > Minimum level Above top of plates, indication mark, and indication mark, and and not overflowing

< % inch above < 1,%inch above maximum level maximum level indication mark(a) indication mark(a)

Float Voltage >2.13 V Ž2.13 V > 2.07 V Specific Gravity(b)(c) N/A Not more than 0.020 N/A below average of all connected cells AND Average of all connected cells

Ž1.195 Cell Temperature 60 Degrees F 60 Degrees F 60 Degrees F (a) It is acceptable for the electrolyte level to temporarily increase above the specified maximum level during and immediately following equalizing charges provided it is not overflowing.

(b) Corrected for cell temperature. Level correction is not required.

(c) A battery charging current of < 0.25 amp for Class 1 E 250 V batteries and

< 0.1 amp Class 1 E 125 V batteries when on float charge is acceptable for meeting specific gravity limits.

ATTACHMENT 2 TO PLA-6080 PPL SUSQUEHANNA Revised Markup to Proposed Units 1&2 Technical Specification Section 5.5.13

PPL Rev. 6 Programs and Manuals 5.5 5.5 Programs and Manuals (continued) 5.5.13 Battery Monitoring and Maintenance Program This program provides for battery restoration and maintenance, is licensee controlled, and includes the following:

a. Actions to restore battery cells with float voltage < 2.13 V, and
b. Actions to equalize and test battery cells that had been discovered with electrolyte level below the minimum established design limit.

SUSQUEHANNA - UNIT 1 TS / 5.0-18A Amendment

PPL Rev. 6 Programs and Manuals 5.5 5.5 Programs and Manuals (continued) 5.5.13 Battery Monitoring and Maintenance Program This program provides for battery restoration and maintenance, is licensee controlled, and includes the following:

a. Actions to restore battery cells with float voltage < 2.13 V, and
b. Actions to equalize and test battery cells that had been discovered with electrolyte level below the minimum established design limit.

SUSQUEHANNA - UNIT 2 TS / 5.0-18A Amendment