ML20042G048

Nonproprietary Rev 0 to WCAP-8587,Suppl 1 EQDP-ESE-69, Equipment Qualification Data Package,Eagle 21 Process Protection Sys (Environ & Seismic).

ML20042G048
Person / Time
Site:	Sequoyah
Issue date:	02/28/1990
From:	Channarasappa, Jabs R, Lyman J WESTINGHOUSE ELECTRIC COMPANY, DIV OF CBS CORP.
To:
Shared Package
ML19302E126	List: ML20042G044 ML20042G045 ML20042G047 ML20042G048 ML20042G049
References
EQDP-ESE-69, WCAP-8587-S01-0, WCAP-8587-S01-R00, WCAP-8587-S1, WCAP-8587-S1-R, NUDOCS 9005110029
Download: ML20042G048 (30)

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i i fmj: WCAP-8587 (E Supplement 1-E0DP-ESE-69 Rev. 0, 2/90 O Avg EQUIPMENT -0VALIFICATION DATA' PACKAGE I

l This document contains information re'ative to the Qf qualification of the equipment identified below in

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accordance with the methodology of WCAP-8587. "The 7 Specifications section (Section 1) defines' the assumed  ;

limits for the equipment qualification'and constitutes-interface requirements to the user.

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EAGLE.215 PRdCESS PROTECTION SYSTEM l-(Environmental and Seismic)

i-1 f Approved: M vff#1 D. E. Rygg, papagfr RCS Engineering s

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.l EQUIPMENT OVALIFICATION DATA' PACKAGE

^ EAGLE 21 PROCESS PROTECTION SYSTEM (ENVIRONMENTAL AND SEISMIC) ._

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V A Yl m '2 J. )r. Lyman, EngVieer

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'5. Channarasappa', Engineb'r 2 //+/10 Class _1E Systems Equipment Qualification & Testing Author Author 4

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.R. H. abs Engineer / / "J. Parello Engineer Class ~1s / stems / Equipment Qualification & Testing Reviewer Reviewer

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W ' $7 _Y ' 2.//f/* fd R..B. Miller, Engineer 5. Radomski, Engineer . . / /'

• Instrumentation and Control Systems Process Systems Engineering Licensing Reviewer '

Reviewer L

(V~h l$56 Approved:/

2 sbo Yf Approved:

A//S 90 C. G.. Modris, Manager W. V. Cesarski, Manager Class 1E Systems . Equipment Qualification & Testing l l

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, ,W SECTION-1 -- SPECIFICATIONS kI .

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, 11.0 PERFORMANCE SDECIFICATIONS l

- 1 7 1 n; -l.1 Electrical Requirements NY ,

_. 1.1.1- Voltage: 120 Vac.+/-10 percent

1.1.2 Frequency

60 542 +/-5 percent >

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1.1.3 Load:' N/A g):. . ..

1.1.4 ' RFI, Noise, Fault, Surge, Electromagnetic Interference:

WCAP-11733 (Reference.1) _,

1.1.5 Other

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1.2 Installation Requirements: Installation details for the EAGLE 21*

Process Protection System (PPS) are specified in Westinghouse drawing L 1870E16.

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1.3 Auxiliary Devices: None w fy

'1.4 Preventive Maintenance Schedule: Known age sensitive equipment may q l require special maintenance. procedures or replacement schedules to address

[ the thermal sensitive materials or mechanical. cycle limitations. The I L supporting Westinghouse design technical documentation will define the i known age sensitive equipment and recommended maintenance procedures. The utilities shall establish a surveillance / maintenance program that addres- :l ses general equipment aging / reliability. This preventive maintenance-L ' program shall not compromise the qualification status of the equipment. '!

L A i V 1.5 Design Life: The design life goal of the Eagle 21w PPS equipment is 40-years. The 40 yea,r design life goal (References 2 and 3) was selected based on expected plant life and is to be supported by periodic component

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replacement due to random failures, known age degradation and normal U plant surveillance / maintenance practices for class 1E equipment.

1.6_ Operating Cycles (Expected number of cycles during design life, including test): Continuous p/-

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.$ t.7 Perfornience Requirements for Function of Equipment: EAGLE 21" PPS k?-

8 ca y Conditions Contsiruusmt D6E Post-OttE 6, Parameter Morine1 Atmorma1 Test FtB/ stb LOCA Seismic f t B/St8 LOCA Ses sune o

1.7.i Y4me Requirement Continuous t2 hours N/A N/A N/A Note 8 M/A N/A Cent 1*vuous 1.7.2 Performence Note A Note A N/A N/A N/A No damage: N/A 94/A Note A Requirement Notes A, 8 1.8 Environmental Conditions for Same Function 1.8.1 Tenperature ('F) 60-80 82-120 N/A N/A N/A Ambient N/A N/A Ambient Notes C & D m

t.8.2 Pressure (psig) O O N/A N/A N/A Amet ent N/A N/A Ambient M i -4 w

1.8.3 Humidity (% RH) 30-50 95 N/A N/A N/A Anblent N/A N/A Ambient Z Note C y N O c

6.3.4 Radiation (R) 500 R (l) Nrme N/A N/A N/A None N/A N/A Norse (M Note E M n

Chemicals None None N/A 1.8.5 N/A N/A None N/A N/A None h to 1.8.6 Vibration None None N/A N/A N/A None N/A N/A None M tas 1.8.7 Acceleration (g) None None N/A N/A N/A Figures 2 & 3 N/A N/A None - ,

i Notes A: See Table 1.

B: Electronics required to function before, during and after a seismic event.

C: Figure 1. envelope 3. However, based on tfestinghouse ewportence, operation at low humidity is not an equipment operating concern.

The abnormal extreme for humidity shall be 95 percent relative humidity.

D: 140*F was used in Reference 4 which includes 20*F to simulate a fully loaded cabinet. The results from Reference $ supports the 20*F rise for internal cabinet tesperatures.

l E: The radiation dose requirement is based on and 14mited by the radiation qualification established for fes05 integrated circuits (IC's) used in the equipment electronics. The gamma radiation limit for s+ ..ts that are not fes05-type IC's is 10 Rads total integrated dose (TID).

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<- 1.9 Qualified Life: Westinghouse specifies the design life instead of the

'f qualified life for qualified equipment located in mild environments. The Westinghouse position on qualified life for mild environment equipment is 7

found in Reference 6.

- . 1.10 Remarks:.-None.

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SECTION 2 -- OVALIFICATION BY TEST L)  ;

2.0 TEST PLAN

[ A test program was performed on the EAGLE 21* PPS as documented in

• Reference 5. Additional component tests were performed as documented in Reference 4.

[ Environmental testing and seismic testing were performed at the Westinghouse Advanced Energy Systems (WAES) testing laboratory in large, Pennsylvania.

Environmental cycling was performed on the EAGLE 21* PPS in a temperature

- and humidity chamber. A microprocessor controls the chamber and maintains the temperature and humidity conditions desired. Seismic tests were performed at the WAES Seismic Laboratory. References 4 and 5 provides a more detailed description of the test facility.

2.1 Equipment

Description:

EAGLE 21w PPS cabinet and components (see O Tables 2, 3, and 4)

.Q 2.2 Number Tested: Minimum one of each item (equipment) listed in Tables 2 and 3

2.3 Mounting

Per Section 1.2

2.4 Connections

Standard plant wiring terminated with ring terminals in the back of the termination frame O) -

( 2.5 Aging Simulation Procedure: Thermal aging simulation is addressed in separate component aging test programs (see Section 2.10.3.3) and the Westinghouse position on mild environment given in Reference 6. Radiation qualification is addressed in Section 2.10.3.4. r

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= 2.6 Service Conditions to Be Simulated by Test : IEAGLE 21= PPS

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'5 Normal Abnormal Test Seismic HELB Post-HELB B:

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2.6.1 Tenperature (*F) Anbient Figure 4 N/A Ambient N/A N/A 2.6.2 Pressure (psig) ,,

Ambient Ambient N/A Ambient N/A N/A 2.6.3 Humidity (% RH) Ambient Figure 4 N/A Ambient N/A N/A

-M 2.6.4 Radiation (R) None None N/A None N/A N/A $

5 m 2.6.5 Chemicals None None N/A None N/A N/A 2.6.6 Vibration None None N/A None N/A N/A h w

w j 2.6.7 Acceleration (g) None None N/A RRS N/A N/A i

Figures 2 & 3 i

1 The generic tests completed by Westinghouse employ parameters designed to envelop a number of plant applications. Margin shall be demonstrated on plant specific applications by comparing the generic Westinghouse qualification parameters to plant-specific parameters.

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m 2.7 Measured Variables 1 Not 4 l 2.7.1 Category I -- Environment Required Required ,

(oj 2.7.1.1 Temperature A B 2.7.1.2 Pressure -

A,B 2.7.1.3 Moisture A B 2.7.1.4 Gas Composition -

A,B

( 2.7.1.5 Vibration B A i 2.7.1.6 Time A,B -

2.7.2 Category II -- Input Electrical Characteristics 2.7.2.1 Voltage A,B -

2.7.2.2 Current A B 2.7.2.3 Frequency A B 2.7.2.4 Power -

A,B 2.7.2.5 Other -

A,B 2.7.3 Category III -- Fluid Characteristics 2.7.3.1 Chemical Composition -

A,B

! 2.7.3.2 Flow Rate -

A,B ,

2.7.3.3 Spray -

A,B 2.7.3.4 Temperature -

A,B 1

2.7.4 Category IV -- Radiological Features -

2.7.4.1 Energy Type -

A,B 2.7.4.2 Energy Level -

A,B 2.7.4.3 Dose Rate -

A,B 2.7.4.4 Integrated' Dose -

A,B

. Note: A -- Operational test, normal / abnormal environment conditions B -- Seismic tests 8207R/640R900214;s0 6

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Not l Recuired Required 2.7.5 Category V -- Electrical Characteristics 2.7.5.1 Insulation Resistance -

A,B 2.7.5.2 Output Voltage A,B -

2.7.5.3 Output Current A,B -

2.7.5.4 Output Power -

A,B 2.7.5.5 Response Time -

A,B 2.7.5.6 Frequency Characteristics -

A,B ,

2.7.5.7 Simulated Load A,B -

2.7.6 Category VI -- Mechanical Characteristics 2.7.6.1 Thrust -

A,B 2.7.6.2 Torque -

A,B 2.7.6.3 Time -

A,B 2.7.6.4 Load Profile -

A,B 2.7.7 Category VII -- Auxiliary Equipment None Note: A -- Operational test, normal / abnormal environment conditions B -- Seismic tests O

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WESTINGHOUSE CLASS 3 2.8 Preferred Test Sequence

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L The preferred test sequence, as specified in IEEE Standard 323-1974, is supplemented by IEEE Standard 323-1983 as follows. The actual sequence employed is shown in Section 2.9, including justification for any deviations O

g from the preferred.

2.8.1 Inspection of Test Item 2.8.2 Operation (Normal Condition)

(~ 2.8.3 Operation.(Performance Specification Extremes, Section 1)

\-}> 2.8.4 Simulated Aging (for age sensitive materials) 2.8.5 Seismic Simulation / Vibration 2.8.6 Operation (Simulated High Energy Line Break (HELB) Conditions) .

2.8.7 Operation (Simulated Post-HELB Conditions) 2.8.8 Inspection '

2.9 Actual Test Sequence >

This section identifies the actual test sequence that constitutes the

'( qualification program for the EAGLE 21* PPS. A justification for other than

j. the preferred sequence is provided.

l The Westinghouse Short-Term Component Aging Test Program (Reference 7) and the Microprocessor and Supporting Electronic Components Aging Test Program (Reference 8) have identified no in-service age-related mechanisms that would cause degradation or result in a common-mode failure during the specified simulated life. Therefore, consistent with Reference 6, simulated aging is not included in the test sequence of the EAGLE 21$ PPS. The EAGLE 21* PPS '

( is required to be located so that it is not exposed to HELB or post-HELB

j. conditions. Therefore, simulated HELB and post-HELB conditions are not included in the test sequence. The single Design Basis Event (DBE) for the E

EAGLE 21* PPS is the seismic event.

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I Step Justification for Steps not Performed 2.9.1 Inspection of Test Item O

2.9.2 Operation (Normal Condition) 2.9.3 Operation (Performance Spec-ification Extremes, Section 1) 2.9.5 Seismic Simulation / Vibration h

2.9.8 Inspection 2.9.4 Simulated Aging Aging addressed in Section 2.5 h

2.9.6 Operation (Simulated HELB Conditions) N/A -- EAGLE 21* PPS is not required to operate in an HELB environment.

2.9.7 Operation (Simulated Post-HELB Conditions) N/A -- EAGLE 21* PPS is not required to operate in a post-HELB environment.

2.10 Type Test Data ,

2.10.1 Objective The objective of this test program is to demonstrate, employing the 4 recommended practices of Regulatory Guide 1.89 (IEEE Standard 323-1974 as supplemented by IEEE Standard 323-1983) and Regulatory Guide 1.100 (IEEE Standard.344-1975), the capability of the EAGLE 21* PPS to perform its safety-related functions, described in Section 1.7, while exposed to the applicable environments defined in Section 1.8. l 2.10.2 Equipment Teste,d The testing was performed on the EAGLE 21* PPS cabinet and components described in Tables 2 and 3. .

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The qualification units were functionally tested under normal environmental l conditions before the abnormal environment testing. The purpose of this test  !

was to verify that the Eagle 21* PPS components were operating within their Q rack calibration accuracy and that all test equipment, input and outputs were setup properly.

2.10.2.2 Abnormal Environment and Seismic Testing V

The EAGLE 21* PPS was assembled in a typical system configuration and I installed to simulate the standard plant mounting. The tests were designed to y provide electrical exercising of many of the system modules during the .

abnormal environment tests and seismic tests. '

2.10.2.3 Aging Evaluation Program ,

A representative sample of components from the systems electronics was O'd included in the Short-Term Component Aging Test Program (Reference 7) and the Microprocessor and Supporting Electronic Components Aging Test Program I

(Reference 8). These programs were conducted employing the methodology described in Appendix B of WCAP-8587 (Reference 9).

2.10.3 Test Summary 2.10.3.1 Environmental Tests ,

p Westinghouse requires that the EAGLE 21m PPS be located so that it does not

'd experience a consequent adverse environment when required to operate following an HELB. Therefore, the only testing required is to demonstrate equipment functionality under normal and abnormal service conditions (temperature, g humidity, ac voltage and frequency). Figure 4 shows the environmental test O] profile and Table 5 shows actual qualification test conditions. Irradiation e simulation is not required for this equipment.

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The environmental testing reported in References 4 and 5 is intended to j demonstrate the capability of the EAGLE 21w PPS to meet the safety-related I performance requirements specified in Section 1.7 when exposed to the variations in temperature, humidity, voltage, and frequency indicated in j Figure 4. The system components were installed in a typical / operating process l 4

channel design configuration. Cabinet heat rise was included in the component testing (Reference 4). The testing successfully demonstrated the safety-related performance requirements. Additional margin was included in this test by submitting the equipment to two additional cycles of electrical and environmental extremes, also described in Figure 4. These tests are considered to satisfactorily demonstrate the EAGLE 21* PPS' capability to meet its safety-related functional requirements when exposed to the specified abnormal environments (Section 1.7) and the permitted range of frequency and voltage variations (Section 1.1) meeting the intent of IEEE Standard 323-1974 as supplemented by IEEE Standard 323-1983, Section 6.3.2(2) and (3).

The methodology employed by Westinghouse for abnormal qualification testing is documented in WCAP 8587 (Reference 9).

2.10.3.2 Seismic Tests Following the abnormal environment testing, the EAGLE 21* PPS cabinet (Table 2) and components (Table 3) were subjected to multi-axis, multifrequency inputs in accordance with requirements of Regulatory Guide

, 1.100 (IEEE Standard 344-1975), as described in References 4 and 5. Figures 2 and 3 show the Operating Basis Earthquake (0BE) Required Response Spectrum (RRS) and the Safe Shutdown Earthquake (SSE) RRS for the cabinet tests.

In-equipment response spectra were developed from the testing in Reference 5.

EAGLE 21m PPS components (Table 3) were then tested to envelope this spectra.

g Each customer should compare their actual plant mounting location requirements to the principal axis SSE RRS shown in Figure 3 to ensure that sufficient g margin exists. W The methodology employed by Westinghouse for seismic qualification testing is documented in WCAP-9714 (Reference 10).

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, 2.10.3.3 Aging Evaluation f T~

The Westinghouse Aging Evaluation Program (Subprogram C of Reference 9) has incorporated a sample of components representative of those used in the EAGLE 21* PPS. The results are reported in the Short-Term Component Aging Test

[' Program (Reference 7) and the Microprocessor and Supporting Electronic Components Aging Test Program (Reference 8). Subprogram C demonstrated that during a specified simulated life there were no in-service aging mechanisms that will reduce the capability of the components to perform during or after a

/3 seismic event. Consistent with Reference 6, these results should be supplemented by the plant's surveillance / maintenance program.

2.10.3.4 Radiation Qualification Per WCAP 8587, Revision 6-A, Appendix C, common-mode failures will not arise in electrical equipment during or after a seismic event as a result of radiation-induced degradation for radiation doses up to 10 E+4 rads gamma.

-O A lower threshold of damage dose was determined for the electrical charac-teristicsofNMOS-typeintegratedcircuit(IC) chips. The design limitation to radiation exposure was determined by a test and analysis program (Reference 11). An neceptable total integrated dose (TID) of radiation was established as 500 rads gamma for the NMOS ICs.

Based on the above, the TID of radiation qualified for the EAGLE 21= PPS

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electronics is 500 rads gamma.

g 2.10.4 Conclusion V

Westinghouse specifies the design life instead of the qualified life for qualified equipment located in miM environments. The design life of the EAGLE 21* PPS is 40 years provided that the equipment: is located in a mild environment (Section 1.8), the design technical documentation defines known

(] age sensitive equipment and the plant's surveillance / maintenance program addresses general equipment aging / reliability. The EAGLE 21* PPS has V

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successfully passed abnormal' environmental testing and seismic testing. The  :

environmental and seismic testing, demonstrate the qualification of the EAGLE '

21$ PPS and the implementation of the plant's surveillance / maintenance ,

program should maintain the qualification status over the EAGLE 21* PPS's >

design life. The qualification conditions of the equipment are specified in .

Table 1.  !

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. WESTINGHOUSE CLASS 3 l SECTION 3 -- OVALIFICATION BY ANALYSIS

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.3.0 ANALYSIS PLAN j p

V Analysis was used +o demonstrate that design changes made to Table 4 components l did not impact their environmental and seismic performance. The qualification )

of these components is based on a combination of analysis and testing. 'l 7~3 References 4 and 5 document the testing performed. The analysis performed is i V described in the following sections and Reference 4.

3.1 Equipment Description The EAGLE 21* Process Protection System (PPS) components analyzed are identified in Table 4. i 3.2 Analysis Summary  ;

3.2.1 Abnormal Environment Analysis The EAGLE 21w PPS components (Table 4) were evaluated in Reference 4. The I analysis proved that the components were similar to tne previously tested  ;

components and no additional abnormal environment test were required for these components.

3.2.2 Seismic Analysis i The EAGLE 21* PPS components (Table 4) were evaluated in Reference 4. The l

\ analysis demonstrated that the components were similar to the previously ,

j tested components and no additional seismic tests were required for these components.

(C 3.2.3 Conclusion The abnormal environment and seismic analyses demonstrated that the l EAGLE 21* PPS components (Table 4) are qualified for EAGLE 21* PPS cabinet V applications for the parameters identified in Section 1.7.

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1. qualification program for the EAGLE 21V PPS.-

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l I c SECTION 5 -- REFERENCES l

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1. Doyle, J: " Noise, Fault, Surge and Radio Frequency Interference Test Report m for Westinghouse EAGLE 21w Process Protection Upgrade System," WCAP-11733  :

(v ) (Proprietary),

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2. " EAGLE 21* Process Protection System Design Requirements," 408A46 I Revision 0.

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e 3. " EAGLE 21* Process Protection System Design Specification " 408A61 (x Revision 0.

3 l 4. Lyman, J. M., and S. Channarasappa: " Equipment Oualification Test Report:

EAGLE 21S Process Protection System Components (Environmental and i Seismic),"WCAP-8687, Supplement 2-E69B(Proprietary). ,

5. Bauer, J. S., and S. Channarasappe: " Equipment Qualification Test Report:

EAGLE 21w Process Protection System (Environmental and Seismic Testing),"

WCAP-8687 Supplement 2-E69A (Proprietary). 7

6. Clark T. F., Bruschi, H. J., and Johnson, W. J.: " Westinghouse Position on Qualified Life for Mild Environment Equipment," ENG/1ES(88)10-732.

,- 3 7. Jabs, R., J. Parello, J. Huang, and M. Yalich: " Equipment Qualification Test Report: Short-Term Component Aging Test Program," WCAP-8687, Supplement (V) 2-APP.Al(Proprietary).

! 8. Jabs, R., and M. S. Chang: *Ecuipment Qualification Test Report:

l Microprocessor and Supporting Electronic Components Aging Test Program "

WCAP-8687, Supplement 2-APP.A5 (Proprietary).

9. Butterworth, G., and R. B. Miller: " Methodology for Qualifying Westinghouse 1-(WRD) Supplied NSSS Safety-Related Electrical Equipnient," WCAP-8587, Revision 6-A (Nonproprietary).

10. Kelly, R. E., and J. J. McInerney: " Methodology for the Seismic Qualification of Westin house WRD Supplied Equipment," WCAP-9714 (Proprietary) or WCAP-9750 (Nonpropretary).

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11. Gisoni, G., *Multibus Board Irradiation Test Report," CIES(90)-126 (Proprietary).

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- TABLE 1 EAGLE 21* PPS PERFORMANCE REQUIREMENTS

!. Condition Acceptance Criteria l Ambient o At ambient environmental conditions, the EAGLE 21* '

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process inputs and process outputs are required to 3 be within the Rack Calibration Accuracy (RCA) specified:

RCA  !

Board Type (% of Span)

RTOInputNarrowRange(ERINR) 0.250 AnalogInput(EAl) 0.126 0-10 Vdc Input (ERI WR 0-10 Vde) 0.159 Wide-Range RTD Input (ERI WR RTD Input) 0.150  ;

Analog Output (EAO) 0.174 O o The EAGLE 21* TAPS output voltages are required to D be within +/- 5% of the selected SV increments from 5-30 volts, o The EAGLE 21+ TAPS maximum power supplied to a tr&nsmitter shall be less than 3.55 watts for the normal operating range of.10-50 mA.

o The cabinet mounted pushbutton switch shall operate without any spurious outputs. -

Abnormal o, At abnormal environmental conditions, the EAGLE 21*

Environment system outputs are required to meet a system Rack Temperature Effect (RTE) allowance of +/-1.0 percent of span.

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..r TABLE 1 (cont)

EAGLE 21* PPS PERFC3MANCE REQUIREMENTS l gdition Acceptance Criteria o At abnormal environmental conditions, the EAGLE 21*

process setpoints are required to meet the RTE g

allowances specified:  ;

Setpoint Type (% of Span)

RTE h: ,

Typical: ERI NR 0.50 Typical: EA! 0.25 .

Typical: ERI WR (0-10 Vde) 0.25 ,

Typical: ERI WR (RTD Input) 0.25 Calculated (Delta T, OTSP, OPSP) 0.75 1 o At abnormal environmer,tal conditions, the EAGLE 21* g contact outputs and partial trips shall perform as W required by each test input condition.

o The EAGLE 21* TAPS output voltages are required to be within +/- 5% of the selected 5V increments from 5-30 volts.  ;

o The EAGLE 21* TAPS maximum power supplied to S transmitter chall be less than 3.55 watts for the normal operating range of 10-50 mA.

o The cabinet mounted pushbutton switch shall operate without any spurious outputs.

9-O 8207R/640R900214:s0 18

f J.h  !

WESTINGHOUSE CLASS 3

.4, -. '

V ..

, x TABLE 1(cont) j t EAGLE 21* PPS PERFORMANCE REQUIREMENTS I Condition Acceptance Criteria l i

I Seismic Tests o The EAGLE 21* PPS process inputs and system outputs shall not exhibit shifts beyond the accuracy ~

of the test measuring devices as a result of,the [

seismic tests. All contact outputs and partial I trips shall perform as required by each tett input condition. l i

o The EAGLE 21= TAPS output voltages are required to i be within +/- 5% of the selected SV increments from' I 5 30~ volts.  ;

i o The cabinet mounted pushbutton switch shall operate without any spurious outputs. i O i t

4 O ,

.v O

a207R/640R900214:50 19

. . ._ _ _ . . , . . _ .._.__..._ ._.-..~- _ _ . _ _ . _ . _ . . _ . . _. . . . _ - . . , I

s

• WESTINGHOUSE CLASS 3' .

TABLE 2 EAGLE 21* PPS EQUIPMENT TESTED Drawing Number Desetiption Revision i 956093 EAGLE 21* Baseline Design Document 0 ,

956073 EAGLE 21* Multibus and I/O Board Configuration H l 1870E97 EAGLE 21* Cabinet General Assembly and Detail 3  !

Subassemblies:

1871E36G01 1870E94G01 Cabinet Structure Assembly Card Cage Assembly 3

3 h,

2D33574G07 Power Supply 15-Mult 4 2033574G09 Power Supply 15-Mult 4 )

1871E34G01 Power Dist. Box Assy. 3  !

1' 1E17G01 Front Test Panel 1 i a f)241G01 Power Supply Conn. Panel 1 l

,,..0241G03 Power Supply Conn. Panel 1 i

!?0246G01 Terminal Block Assy. 2 l 1871E37G01 Wiring Channel Assy. 3 3D20245G01 Cable / Power Bus Cover Assy. 3 3020245G02 Cable / Power Bus Cover Assy. 3 i 1871E31G01 Power Bus Assy. 4 2033578G01 Blower w/ Filter, Grille 3 ,

1870E16 Cabinet Base Ntg. Assy. 2 i 5368C80 Cabinet / Door Latch & Stop Kit Details 2 i 1870E99G01 1/0 Framework Assembly 3  !

3020237G01 Rear Test Panel 2 1 5371C10G01 Analog Input Board, 10-50, 4-20 mA (EAI) 3 I

(Style #5367C57, rev. 4) 5371C15G01 Digital contact Output Board (ECO) 3 (Style #5367C61, rev. 2) 5371C11G02 Analog Output Board, 10-50 mA (EAO) 2 (Style #5367C60. rev. 3) j 5371024G01 Wide-Range RTD Input Board (ERI WR) 2 (Style #536BC29. rev. 2) 5371022G02 Narrow-Range RTO Input Board (ERI NR) 2 (Style #5368029, rev. 2) 4 5371022G01 Partial Trip Output Board (EPT) 1 l (Style #2D33786,rev.2)  !

l Ol 9'

a207R/640R900214.50 20  ;

rc j WESTINGHOUSE CLASS 3 7

TABLE 3  !

EAGLE 21* PPS COMPONENTS TESTED ABNORMAL ENVIRONMENT TEST  !

I Drawing L ( Number Description Revision l Transmitter Aux Power Supply PC Board '

3021608G01 1 r

2004E77G01 Transmitter Aux Power Supply Chassis Assembly I 5368029G02 RTO Input 1/0 Board (ERI) _

5 7 3D21703G01 Cabinet Mount Pushbutton Assembly 1  ;

ERI Shared Input Termination Module

( 2D27362G03 4 l

f

-SEISMIC TESTS ,

5368C29G02 RTO Input 1/0 Board (ER1 4 8242C76G02 RTD Input 1/0 Board (ERI 1  :

2033578G01 Blower (Kooltronics KPS2 A-33 Metal Wheel) 4  !

2027362G03 ERI Shared Input Termination Modulo 4 Transmitter Aux Power Supply PC Board 3D21608G01 1 2004E77G01 Transmitter Aux Power Supply Chassis Assembly 1 3021703G01 Cabinet Mount Pushbutton Switch Assembly 1 0 '

S 4

O

~

'O s20m/640meoo214:so - 21

3

_. - - _ _ , _ . - _ . . ~ . . _ . . _ . _ . . . - _ . . . . . , . . _ _- . .

.i WESTINGHOUSE CLASS 3 -

i

.4 i TABLE 4 ,

E0VIPMENT ANALYZED i

I l

\

\

l Included in included in Drawing Adnormal Environment Seismic Component Number Analysis Analysis  ;

!. i

. Front Test Panel 11 2000E18 Yes Yes )

l Blower (Metal) 2D33578 Yes Tested (See Table 3)

Contact input 2D27362 Yes Yes i Termination Module Rear Test Panel !! and 3021632 Yes Yes I Cable Modifications NV RAM Board 3D21637 Yes Yes ERI RTD Input Board (Relay) 5368029 Yes Tested (See Table 3) l TAPS 2004E77 Yes Tested (SeeTable3)

EPT Termination Module 2D33779 Yes Yes 1

9 I

b l

l l.

O O

O 8207R/640R900214:50 22 s

- - e s m ,~ <3 p ./- x .. <

'( .

E o T Aeu 5 x

ACTUAL QUALIFICATION TEST CONDITIONS o

g ABNORMAL /- EMvtROPSOENTAL EXTREMES QUAL o EQUIPMENT (1) LOCATION ' MANUFACTURER ACCIDENT OPERABILITY ACCURACY DESIGN QUAL QUAL PROGRAft O SYSTEM / CATEGORY STRt,CTURE/ AREA TYPE / MODE L PARAMETER SPECIFIED (2) CUAtiFIED REO DE M RE Q DER LIFE #E T P4M REF STATUS E AGLE 21" Centro 1 8viid- w

_PCD Temperature 120 F (3) 12 hr. Two Note Note 40 Seq. ESE- Com-PPS tru/ Control EAGLE 218 ' Pressure Atmos. 12-hr. 4- 4 years Test 69 pieted Category d Room PPS Rel. Humidity 95% cycles Note Sae Tables Padiation 500 rm+s (I) 6

2. 3 and 4 Note S

. - Chemistry None Seismic Figures 2 and 3

y. ..

m (n

--e Notes: *-*

Z 1: For a definition of the category letters. refer to NUREG 0588 " Interim Staff Position on Environmantoi Qualification of Safety-Related y m

(#

Electrical Equipment." Appendix E. Section 2. @

(n res 2: Plant-specific environmental parameters are to be inserted by the applicant. n t~

tn 3: Ambient room temperature of 120 F. M

(#

4: Acceptance criteria for equipment are shown in Tatsia 1. Test results demonstrated that the equipmant met the acceptance critecta.

5: The TID qualified for the EAGLE 21" PPS is based on and limited by the radiation qualification established for tN PeUS integrated circuit chips used in the EAGLE 21" PPS electronics, (See Section 2.10.3.4.) The gamme radiation 11mit for %~.ats that are not 98405-type IC's is 10 Rads TID.

6: Providad that the equipment is located in a et td environmant (Section 1.8). the design technical documantation defines known age sensitive equipment and the plant's surveillance / maintenance program addresses ganacal eqthipment aging / reliability.

2 5

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Required Response Spectrum (RRS)

Principal Axes

,/a \

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r .%

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Figure 3. Safe Shutdown Earthquake (SSE)

Required Response Spectrum (RRS)

Principal Axes n

f 1  !

. \s 8207R/640R900214:50 26 t

. . . . - - -- - .. , _ . - - . _ . . _ ~ . - . - . - . - . . . -.

WESTINGHOUSE CLASS 3 4

t TMAX'HMIN

TEMPERATURE /

HUMIDITY

- - - - - -T AT HMAX I

---

VMAX VOLTAGE

---

V ggy

---

f MAX FREQUENCY l l l ----f y l

• -12 -+ + 12 -* + 12 -+ +12 +

HOURS l

l l LO l figure 4. Environmental Test Profile L

O .

8207R/640R900214:50 27 u

n.

?

. _- - -_