ML20003F739
| ML20003F739 | |
| Person / Time | |
|---|---|
| Site: | Zimmer |
| Issue date: | 04/21/1981 |
| From: | SARGENT & LUNDY, INC. |
| To: | |
| Shared Package | |
| ML20003F733 | List: |
| References | |
| NUDOCS 8104230512 | |
| Download: ML20003F739 (300) | |
Text
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WM H. ZIMMER - UNIT 1 4130-00
SUMMARY
OF EQUIPMENT
, QUALIFICATION l
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TABLE OF CONTENTS TAB 1) ZIMMER EQUIPMENT QUALIFICATION PROGRAM A) INTRODUCTION B) BACKGROUND C) ASSESSMENT AND REQUALIFICATION PROCEDURES D) VERIFICATION TEST PROGRAM E) CONSERVATISMS TAB 2) OPERATINGPROCEDURESCkNARIOS A) SCENARIO FOR MAINTAINING COLD SHUTDOWN B) SCENARIO FOR MAINTAINING HOT STANDBY C) TABLE IDENTIFYING EQUIPMENT REQUIRED FOR O COLD SHUTDOWN, HOT STANDBY, AND POST LOCA TAB 3) COMPLETION SCHEDULE TAB 4)
SUMMARY
OF HARDWARE MODIFICATIONS RESULTING FROM REQUALIFICATION PROGRAM TAB 5)
SUMMARY
OF EQUIPMENT QUALIFICATION A) EQUIPMENT B) HVAC DAMPERS C) VALVES f
r D) INSTRUMENTATION I
t
CARGENT Q LUNDY E N GIN E E DS CHICAGO
(]) Introduction The purpose of this report is to briefly summarize-the philosophy, methodology, and procedures used in the dynamic qualification of the Zimmer balance of plant safety-related equipment. A more detailed presentation may be found in the Zimmer Formal Safety Analysis Report (FSAR) and in the Zimmer Design Assessment Report (DAR).
Background 3 s
The present Zimmer equipment qualification program has evolved through a period of eight years. The evolution has involved advancements in dynamic analysis and test methods, identifi -
cation and refinement of, additional dynamic loads to be considered, improvementsin industry standards, and increased regulatory requirements. The definition of the dynamic loads, having the greatest impact on equipment qualification, has evolved through four stages to its present level.
Initially the dynamic load definition included only seismic loads, however in late 1974 the existence of additional dynamic loads began to be recognized. These new loads were associated
(]} with extended SRV discharge into the suppression pool. In late 1975, as a result of the efforts of the Mark II owners group and the NRC staff,the loads associated with a postulated SRV discharge event were defined, and subsequently the Zimmer equipment qualification program was revised to incorporate these new loads.
The next development occurred as a result of changing the type of SRV discharge device used from the ramshead to the T-quencher.
j This change was made in order to accomplish be,tter heat transfer and thermal mixing in the suppression pool,butalso resulted in changing the structural response of the Containment. In order to accomodate this change, the dynamic load definition for the Zimmer equipment qualification program was again revised to include this new SRV load definition. Also at this time the dynamic loads associated with a Loss Of Coolant Accident (LOCA) were incorporated into the load definition.
The final state in the evolution of the dynamic load definition occurred in mid 1980 when the spectra defining the dynamic loads were regenerated to incorporate refinements made by General Electric in their definition of the Mark II hydrodynamic loads.
As each new generation dynamic load definition was incorporated
{} into the Zimmer equipment qualification program , an assessment e- - , r - , - - - -, ,,e - - - - , , , , - - ,,p ,-,-g-n-,- w- --n, -, ,-,,-a--<,,y,~- ,ae-v,.,-~ ,w---- , sn
CARGENT & LUNDY E N G1N E E RS CHICAGO O was made of the equipment previously qualified. Where the assessment determined there were inadequacies the equipment was requalified and hardware modifications were made as required. For new equipment or equipment where the qualifi-cation had not been completed, the qualification was performed using the latest load definition. In addition, each stage of this asessment and qualification effort was performed using the, latest industry standards and regulatory requirements.
Design Load Combinations ,
Itemized below are the load combinations used in the Zimmer equipment qualification program. Also identified are the appropriate damping values, service levels and the method used to combihe the individual loads. -
w Drping Service Cctrbination a
Ioad Cmbination Value Invel Method
- 1) N + OBE % B* ABS
- 2) N + SSE 1% C* ABS
/ 3) N + OBE + Envelope (SRVg_ SRVg_ ) 1% B ABS
+ SRVgyy_g)+ N 2% C E
2% C ABS
+ 0.6 SRVAll-M) + col
+ SRVgyy_g) + T2 2% C E 2 2
- these service levels reflect that combinations 1 and 2 are used for equipment not affected by the SRV and LOCA loads (equipment located outside of reactor building). Combinations 3 through 7 are used for equipment located in the primary containment and reactor building.
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SARGENT & LUNDY EN GIN E E RS CHICAGO O Assessment and Requalification Procedures
- 1) General Approach The procedure used to assess the existing qualification documentation to determine the equipment adequacy for the additional hydrodynamic loads, consists of three steps.
Step 1: 'Uheck the original qualification method to insure that all important issues have been addressed and that the ogiginal qualification is still in accordance with the lates.t applicable codes and standards.
Step 2:- Det~ ermine if the input used in the original qualification.is sufficient to properly include the additional hydrodynamic loads.
This includes both the increased frequency content and amplitude.
Step 3: If the frequency range considered in the original qualification ~is less than
. the frequency content of the additional Os hydrodynamic loads, determine if there is sufficient margin in the input accelera-tion to account for the effect of the
. higher frequencies.
If the assessment demonstrated that the equipment is adequate for the additional hydrodynamic loads and that the qualification documentation is in proper order, then the component was considered qualified. If the assess-ment determined deficiencies or that further investigation was required, then the component was requalified.
The method of requalification was generally dictated by the original qualification method. In most cases this involved simply supplementing the original qualification.
However, a significant number of cases required complete re-analysis or retesting.
- 2) Procedure for Equipment Originally Qualified by Test Basically there were four major concerns involving qualifi-cation by testing that have been addressed by the Zimmer equipment qualification program. These concerns are:
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CARGErn' O LUNDY ENGINCCRS CHICAGO
() a) the increased frequency content and b) increased acceleration levels-associated with the hydrodynamic loads c) the effect of cross-coupling and .
d) multimode response when the original qualification was single axis or single frequency.
A brief summary describing how these concerns have been addressed is provided below.
a) For multiple frequency tests the increased frequency content was addressed by first determining whether the test response spectra (TRS) enveloped the requi, red response spectra (RRS). In cases where the TRS did not envelope the RRS, the. natural frequencies were compared against the exceedances.
If no natural frequencies were found in the areas not enveloped, the component was considered qualified.
However, in some- cases the TRS was not plotted after 33 Hz or natural frequencies greater than 33 Hz were not deterimined. For these cases, the criterion for determining adequacy was: did the test input
() include sufficiently high acceleration levels to account for possible high frequency effects, or, based upon qualification of similar equipment, is this component sensitive to high frequencies. This criterion is to be verified by the Zimmer verification test program.
For single frequency tests the increased fraquency content concern was addressed by determining if the test input included sufficiently high acceleration levels to account for possible high frequency effects, or by determining the sensitivity of the equipment to high frequencies. This determination was generally based upon the qualification results of similar equipment. The basis for making these determinations l will be confirmed by the Zimmer verification test l program.
b) The increased acceleration levels associated with the hydrodynamic loads were addressed by determining if the test input acceleration bounded the increased
- acceleration levels, c) The cross-coupling concern for equipment qualified by single axis testing was addressed by determining whether the test input included sufficient margin to
([') account for cross-coupling effects. The amount of margin required was based upon previous testing
SARGENT & LUNDY ENGINEERS CHICA20
{} experience and found to be dependent upon:
- the relative rigidity of the equipment
- eccentricity of the center of gravity from the centroid of the mounting. This includes the '
eccentricity of locally mounted devices in the equipment as well as overall equipment eccentricity
- the sensitivity of mechanical linkages to cross-coupling d) The effects of multi-mode response for' single frequency testing was addressed by determining if there was sufficient margin in the test input acceleration to account for the participation of multiple modes. The amount of margin required was determined by examining the m'odal participation factors of similar equipment.
) Procedure for Equipment' Originally Qualified by Analysis For equipment originally qualified by analysis there were two major concerns, the increased frequency content and the increased acceleration levels associated with the hydro-(~' ' dynamic loads. These concerns were addressed by extending
\ the analysis to include the effect of the higher frequencies, and when the additional hydrodynamic loads resulted in combined loads exceeding the design basis loads, the analy is was repeated using the new combined loads, j 4) Use of SRSS The above discussion summarizes the supplemental qualifica-tion efforts implemented on equipment identified by the assessment as either having qualification deficiencies or as requiring further investigation. As a result of these efforts one of the following actions has,been or will be
, implemented:
a) equipment classified as qualified f b) equipment retested or reanaly zed c) hardware modifications made d) equipment replaced _
However before hardwale modifications were made or replace-ment was initiated the ccmbining of the seismic and hydro-l (N) x- dynamic loads by the sc wre root of'the sum of the squares (SRSS) method was consi9nred. If sufficient load reduction l
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.w as obtained, then' modifications or replacement were not t- necessary. If the load reduction was not sufficient.then' ~
+ the modifications made were-based upon loads combined by-
, the absolute sum (ABS) method.-
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CHICAGO O VERIFICATION TEST PROGRAMS I. In-situ Test Programs A. In-situ Impendcr..e Test Program The purpose of this test program is to obtain the equip-ment natural frequencies in the range of 1-100 Hz, associated mode shapes and modal participation factors as well as damping and cross coupling parameters. It is intended to use these results to verify analytical techniques used for the equipment qualification and to supplement existing test qualification as needed. Nine pieces of equipment were chosen for tne. test program with the concurrence of the NRC-SQRT. These nine pieces comprise a representative sample of the types of equip-
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( )/ ment used in the Zimmer plant.
These pieces of equipment are:
- 1) lE51C001 Reactor Core Isolation Cooling Pump
- 2) lE51C002 Reactor Core Isolation Cooling Steam Turbine Assembly
- 3) lH22P017 Reactor Core Isolation Cooling Instrument Panel
- 4) lE51F010 6" Motor Operated Reactor Core Isolation Cooling Gate Valve
- 5) lE12B001 Residual Heat Removal Heat Exchanger
- 6) lE12F014A 16" Motor Operated Residual Heat Removal Butterfly Valve
- 7) lVG05SA Standby Gas Treatment System Equipment Train
- 8) 1AP15EA 480 volt Reactor Building Motor Control Center lA l 9) LWR 0lPA Reactor Building Closed Cooling
! Water Pump r The test was completed using different methods of excita-1 l tions such as a hydraulic shaker, electromagnetic shaker l . . - . - . . --- -- - - .- . - _ _ _ . . . _- - -
, ' - CARGENT.C2 LUNDY EN GIN EE R9 ,
CHICAGO O
(_j and calibrated hammers. The dynamic input was in the-form of white noise - (Plat spectra) , shaped spectra and impact. The points of measuring response were selected
~
to construct a test model capable of detecting global and local modes.
B. In-Plant SRV Test Program
-The purpose of this test 1 program is to verify the predicted forcing function, structural response, the nature of the input to equipment and the accuracy of predicted equipment response during a safety relief valve discharge event.
Seven pieces of equipment have been chosen to be monitored during the test. They are:
,_ 1) lE22C001 High Pressure Core Spray Pump k) 2) lH22P017 Reactor Core Isolation Cooling Instrument Rack
- 3) lE22F015 20" Motor Operated High Pressure Core Spray Gate Valve
- 4) 1APlSEE 480 Volt Reactor Building Motor Control Center lE
- 5) 1B33C001B Reactor Recirculation Pump
- 6) lH22P027 Reactor Vessel Level and Pressure Instrument Rack
- 7) 1C41F001 3" Motor Operated Standby Liquid Control Globe Valve .
II. Fatigue Evaluation The impact of the extended duration of the hydrodynamic SRV and LOCA loads is asse's sed by analytical and testing tech-niques.
A. Analytical Approach O
a Two pieces of mechanical equipr.ent which have been qualified by analysis will be selected and a detailed
SARGENT & LUNDY' EN GIN EERS CHICAGO
) fatigue analysi,s will be performed to calculate the cumulative usage factor.
B. Testing Approach Selected pieces of equipment and instrumentation'which are scheduled to be requalified by test are.to be fatigue tested. This test will be conducted after the completion of qualification testing and will consist of extended duration segments debigned to represent the hydrodynamic loads associated with the S/R valve actuation and LOCA events. The test duration is conservatively estimated from the equivalent number of cycles for each event, and the test input is taken as the envelope of the combined loads associated with
. each postulated loading combination. These tests are being performed by Southwest Research, and when completed the results will be summarized and presented to the NRC.
}- It is intended to use these results to draw generic conclusions about the impact of the extended nature of the hydrodynamic loads on equipment and instrumentation.
III. Sensitivity Testing of Relays The purpose of this testing program is to determine the sensitivity of relays and similar electrical devices and instrumentation to the input frequency of the dynamic loads.
The test will be conducted in three phases using four relays.
In the phase one the relays will be tested using a dynamic input consisting of frequencies from 51 to 100 Hz only, and amplitude which shall be incrementally increased until failure occurs. Phase two will be identical to phase one except the dynamic input will consist of frequencies from 1 to 50 Hz. Finally, in phase three the dynamic input will consist of frequencies from 1 to 100 Hz. The results will
- be used to draw generic conclysion's about the effect of frequency upon performance of rg, lays and similar type devices.
. SARGENT & LUNDY
- ENGINEERS CHICA2O
) Conservatisms The following conservatisms have been incorporated into the Zimmer equipment qualification programs:
- 1) Lower damping values than those recommended in Regulatory Guide 1.61 were used.
- 2) The loads were combined by the absolute sum (ABS) method rather then the square root of the sum of the squares, (SRSS) method. J 4
- 3) The response spectrum method was used rather than the time history method.
- 4) Peaks of'the hydrodynamic load response spectra have been widened by 20%.-
- 5) The primary containment and reactor building response spectra consist of a resultant (radial) horizontal and a vertical curve. However, this resultant horizontal was applied in each individual (N-S and E-W) horizontal direction simultaneously with the
. vertical direction.
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- 6) The load combinations use the envelope of SRVALL and SRVggy in all directions while SRVALL is maximum in the vertical direction while SRVA sy is maximum in the horicontal direction.
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ZIMMER NUCLEAR STATION UNIT 1 BOP EQUIPMENT QUALIFICATION
SUMMARY
USING T-QUENCHER HYDRODYilAMIC LOADS EQUIPMENT NAME:
EQUJPMENT NO.: SPEC. NO.:
I LOCATION:
l EQUIPMENT CLASSIFICATION: C ACTIVE CPASSIVE QUALIFICATION METHOD:
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l QUALIFICATION DOCUMENT
REFERENCES:
O LOAD COMBINATIONS CONSIDERED IN QUALIFICATION:
i 1. N + OBE + ENV SRVASY-TQ + SRVEL-TQ
& SRV ADS-TQ
+
ASY-TQ
- 5. N+ )SSE2 , gp2 QUALIFICATION:
l PREPARED BY: DATE:
REVIEWED BY: DATE: PROJECT NO. 4130-15 l APPROVED BY: DATE: EMD FILE NO.
SARGENT& LUNDY
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O OUALIFICATION SUMARY SEISMIC QUALIFICATION METHOD:
T-00ENCHER REQUALIFICATION METHOD:
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Reference:
EMD File No. l; SARGENT5LUNDY Il
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w QUALIFICATION
SUMMARY
OF EQUIPMENT
. I. PLANT NAME: ZIMMER - Unit 1 TYPE:
- 1. Utility: Cincinnati Gas & Electric PWR []
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(, 2. NSSS: General Electric BWR
- 3. A-E: Sargent & Lundy II. COMPONENT NAME:
- 2. Model Number: Quantity:
l 3. Vendor:
l 4. If the component is a cabinet or panel, name and model No.
of the devices included:
- 5. Physical Description Appearance:
Dimensions: Weight:
- 6. Location: Building: Elev.:
- 7. Field Mounting Conditions:
Bolting: Number: Size:
[] Welding: Weld Type:
( Leg: Length: Pitch:
- 8. Natural Frequencies in Each Direction:
Hl:
H2:
V:
- 9. (a) Functional Description (b) Equipment required for:
[] Hot Standby Cold Shutdown Both
- 10. Pertinent Reference Design Specifications:
III. IS EQUIPMENT AVAILABLE FOR INSPECTION IN THE PLANT: [] Yes []No Comments:
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Reference:
EMD File No. SARGENT&LUNDY
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IV. EQUIPMENT QUALIFICATION METHOD: Test
[] Analysis Combination of Test b3and Analysis
(^)
(_ 1. Test and/or Analysis by (Name of Ccrapany or laboratory & Report tb.)
- 2. If Qualification by combination of test and analysis state which components were tested and which were analyzed:
V. VIBRATION INPUT: ,
- 1. Loads considered: Seismic Hydrodynamic Explosive Other (Specify) :
- 2. Required Response Spectra (attach the graphs):
- 3. Method of combining Requiring Response Spectra:
[] Absolute Sum SRSS x
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- 4. Required Acceleration in Each Direction (if Required):
H1 H2 V
- 5. Damping OBE: Basis for damping:
SSE:
VI. IF QUALIFICATION BY TEST, THEN COMPLETE:
- 1. Test Method: [] Single Frequency
[] Multiple Frequency
[] Random Motion
[] Sine Beat O
- 2. Input Motion: [] Single Axis Multi Axis
- 4. Frequency Range:
b d
Reference:
EMD File No. ..~. .....
C MC AGO r
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No [] Yes (attach TRS graphs)
- 6. Input g-level Test at Hl= H2= V=
e- 7. Laboratory Mounting:
[] Bolting: Number Size
[] Welding: Weld Type:
Leg Length Pitch
- 8. Functional operability verified: 0 Yes O No O Not Applicable
- 9. Other tests performed VII. IF QUALIFICATION BY ANALYSIS, THEN COMPLETE:
- 1. Type of Analysis
[] Static Analysis
[] Equivalent Static Analysis
[] Dynamic Analysis: Response Spectrum
[] Time History
- 2. Model Type:
[] l-Dimensional [] Finite Element 2-Dimensional [] Closed Form Solution
(~ [] 3-Dimensional []
- 3. Method of Analysis:
Computer b3Programs-Aidedused: Calculation Hand Calculations O
- 4. Have equipment supports been adequately considered in analysis? [] Yes [] No
- 5. Stress Evaluation at Critical Structural Elements:
Element ac Allow Stress stress l
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Reference:
EMD File No. OY
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- 6. Deflection Evaluation at Critical Structural Elements (Active Equipment Only) ac Allow Element Deflec. Deflec.
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VIII. ADDITIONAL COMMENTS:
O O SARGENT &LUNDY
Reference:
EMD File No. . ~ ~ . . . . .
C M eC AGO
ZIMMER NUCLEAR STATION UNIT-1
(])-
4130-00/4130-15 BOP VALVE QUALIFICATION
SUMMARY
UTILITY : CINCINNATI GAS & ELECTRIC CO.
NSSS : GENERAL ELECTRIC CO. TYPE: BWR AE : SARGENT & LUNDY SPEC NO.:
VALVE MANUFACTURER:
VALVE SIZE (S) & RATING (S):
VALVE GdAL. METHOD:
l QUALIFICA~. ION DOCUMENT
REFERENCES:
1.
2.
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4.
5.
PREPARED BY: DATE:
REVIEWED BY: DATE:
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l-II. MOUNTING:
On pipe Weld Type [] Flange Type Any other support? (describe bricfly)
III. IF QUALIFICATION SY ANALYSIS:
- 1. Method of analysis:
[] Finite element Computer aided (Program)
[] Closed form Hand calculations
[] Other
- 2. For active valves, operability of the valve was addressed by:
O Limitins deflections
[] Limiting stress to within design allowables Both
- 3. Stress in the critical elements:
CcLevel in axis
- Calculated Allowable stress (ksi)
Element a b c Stress (kci) Upset Emergency n
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- 4. Deflections, for active valves only:
Calculated Allowable 3-Level h1 axis * ,
Deflection Element Deflection a b c in in
- Axis a - Along outlet pipe run b - Perpendicular to axis 'a' and in the plane of axis 'a' and valve stem axis c - Perpendicular to both 'a' and 'b'
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, IV. IF THE QUALIFICATION IS BY TEST:
, a-i 1. Laboratory mounting:
- Ci ' 2. Normal operating loads input'by
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- 3. Resonance search test:
i a) Input axes: -
Single [] Biaxial i b) Frequency range to Hz.
l c) Sweep rate octaves / min.
l d)- Input acceleration: ___
- 4. Qualification test:
l
! a) Input axes: Single Biaxial _ Pseudo-biaxial
{ b) Frequency range: Hz.
I. c) No. of tests in each crientation:
I Upset: Emergency:
l d)' Test' method f [] Sine beat (single frequency) :
! No. of beats , No. of cycles / beat
~
Beats at Input acceleration Upset: a ,b ,c Emergency: a ,b ,c Sine Dwell (single frequency) : Duration:
Dwells at Input acceleration Upset: a ,b ,c Emergency: a ,b ,c Random motion (multi frequency) : Duration:
Damping: Upset: Emergency:
e) Other tests performed and comments:
SARGENT&LUNDY
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V. RESULTS OF QUALIFICATION:
O aESoN^Nr raeoUEnc1ES Nax1=M AnnownStE 'G' vitUE AePLIsn S1=tTANEoUstr UPSET EMERGENCY a b c a b c a b c VI. LOADS FROM PIPING ANALYSIS:
pyp N N ERATION IN 'G'S' SUBSYSTEM IDADS VALVE UPSET N ANAL.DATE WITHIN TAG & VALVE NO. DD FILE ALLOW.
a b c a b c O
l ADDITIONAL CONSIDERATIONS:
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-s- SARGENT&LUNDY c w sC AGO t
THE CINCIT.NATI GAS & ELECTRIC COMPANY '
WM. H. ZIMMEr. NUCLEAR POWER STATION - UNIT 1 SCENARIO FOR ACCOMPLISHING HOT OR COLD SHUTDO.J
(
, Several success paths are available for safely shutting the reactor to a cold shutdown condition or maintaining an interim condition, assuming the following initiating events:
- 2) Loss of Off-Site Power s
- 3) Single Failure #
For purposes of selecting one success path for accomplishing cold shutdown, RHR 1A pump, lE12C002A, is assumed as the single failure. The following seismic Category I equipment are available for reactor scram, RPV depressurization and decay heat removal:
- 1. ESS Relay Panel senses loss of off-site power bnd O. initiates diesel generators and load sequencing.
- 2. CRD Hydraulic Units insert the control rods and shutdown the core (SCRAM) .
- 3. Diesel Generators are started and reach rated speed and accept auxiliary load.
- 4. RHR 1B and 1C pumps are started and operate on minimum flow recirculation.
- 5. The following electrical equipment is energized during and following load sequencing:
- a. 4.16 kV Switchgear
- b. 480-V ESS Substation O
SCENARIO FOR ACCOMPoIS!!ING COLD S!!UTDOWN PAGE 2 OF 3
{} c4 480-V MCC.'s
- i d. Dattories e.
24-V, 125-V, 250-V DC Distribution Panels / Cubicles f.
120-V AC Distribution Panels .
g.
Electrical Penetration Assemblies 6.
The following equipment is automatically started during a
load sequencing:
Service Water Pumps (lWS System) c.
Control Room Air Conditioning (lVC System)
- d. Switchgear Heat Removal (lVX System)
- e. CSCS Room Coolers (lVY System) f.
SW Pump Structure Room Coolers (lVH System) 9 CSCS Water Leg Pumps 7.
Cooling Water becomes available for'the following heat exchangers:
, a. DG Hx
- b. RBCCW Hx c.
RBCCW Expansion Tank provides suction head on RBCCW i
pumps.
9.
Safety Relief Valves provide RPV pressure control for
- depressurizing RPV to permit RHR initiation. Once the RHR System begins operation (below 135 psig vessel pressure),
the reactor can be maintained at any desired temperature or pressure, or cooldown may be continued.
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SCENARIO FOR ACCOMPLISHING i' AGE 3 OF 3 COLD S!!UTDOWU 10.
{ MiscellaneousSection III tanks provide high presseru
.! air for closing the MSIV's and opening the SRV's from the main control room.
11.
The following valves are cycled to line up piping to permit DG cooling and decay heat removal:
lE12F003B IWS037A/D-lE12F004B lWS033 4 lE12F047B IE12F042C lE12F048B lE12F006B See attached table IE12F008-1E12F009 for valve functions lE12F053B lE12F068B
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lE12F014B
)
( %* 1B21F013A-D, E-H, K, L, P, R, S '(GE Furnished) 1B21F022A/D (GE Furnished) 1B21F028A/D (GE Furnished The above equipment therefore provides on-site power, instrumentation, decay heat removal, auxiliary equipment cooling and main control room habitability to safely shut down the reactor from power operation to cold 1
shutdown.
- i. The attached list of BOP and MSSS equipment noted by an asterick denotes in detail the equipment required for accomplishing the above success path.
RJ Pru sk i /m.:
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VALVE DESCRIPTION & FUNCTION e
by lE12F003B RHR HX(B) Disch. to RPV lE12F047B Inlet to RHR HX(B) lE12F048B Bypass RHR HX(B) lE12F006B) lE12F008 ) " Suction to RHR(B) lE12F009 ) ,
From Recirc. Suction Pipe lE12F053B Return to RPV from RHR HX(B) lE12F068B Service Water Discharge from RHR HX(B) lE12F014B Service Water Inlet to RHR HX(B) lE12F004B Suction to RHR Pump (B) from Suppression Pool lE12F042C Discharge from RHR Pump (C) to RPV
() lE12F004C Suction to RHR Pump (C) from Suppression Pool (Not required to stroke - normally open) 1B21F013A-D,E-H,
, K,L,P,R,S Safety Valve Main Steam System 1B21F022A/D Inboard MSIV 1B21F028A/D Outboard MSIV 1WS037A/D Service Water Dish from D.G. HX lWS 033)' Service Water Essential -
1WS034), Loop Iso. Valves O
. .O. .
'O .
o.
Pete t .
TABLE 110.6 3 SE15Mic Q"ALIFICAT101 SLNMARY OF CATECr*Y ! PECitANICAL AND ELECTRICAL EQUtfHEWT 4
. I Methad Pettied ;
Eqvftwent of Equtpoent inspect!an Equip.*ent Equip ent of Equipeent tnerestten .
Equ! punt Function **
Naae Func t ion ** Avattability tsumtie r Name Qualificetton** Avattability Eve.Se r Qvattf tcation** ,
j AD 250 V tattery Test (3) C, D tes
- 8t A104.9 A/C 4.16 KV Switet. gear Test ($) Yes *1(M.01E A
- .N t
" *tt)CllEA/C 123 V Battery Test ($) C, D tare.i ti/e. f,.9 KV $witchgear Test (3) A, E . .
- 14t"a".E 410 V 155 Substation , Test (5) AD " - *LDC2 tE A/S 24/49 V Dettery Test ($) C, O 1 Alv..r *
! sfer.r .
- Fattery Rachs Analy sis (?) C. D, E "
t tt* tor S lAtt3L
- tA*2ilA/C 480 V PCC Test (3) Ae D
.A Battery Nonitore Test ($) C, D 141559A/S t Atl'.t A/G .
- tte07fA/c ofesel ott Day Tantt Analysts (7) C,D E "
IDCO2EA/B 250 V Battery Charger Test (5) A, C D Analysta(8) C, D " 1DC12tA/C 115 Y Battery Charger
- Test (S) A,C D .
e t tvA14 /C Diesel cen.
- 1 Pt.10J A/C D. C, Cneitrol Fanet Test (3) C, D ..
- !!!9 TEA /S 120 Y AC Dist. renete Test (5) A, D C,D,E " t ilts.1r. .
all#/s2.u/D D. C. tttet Exetienger . Analy s t s (9) l'WJO AU S
, lit 94E lt/M A A/ S C, D "
- tt<:04EA 250 V DC tilst. Cuttetes Test (S)
Itt.0%rA/C e t ty/1'.r,A/C D. C. Enhaust $ttencer Analysts (8) CDE "
It..owA/C
- 1DG14EA/C 123 V DC Pist. Cubietes Test (S) C, D
- ttic2 t.l:A/S 24/48 Y DC Dist. Cubittes Test (S) CD elf 4;17t A/' 1% Cyttndar Esp. Joint Analysts (8) ! "
- 14r$0t Aft 1 Electtical Penettetton Analyste(7) C, D E Itt.tetA/c ,
LAP 50FJ/N A9sembites IAr50EP
" IAr50tR
- ils;!rl4/C 12 Cylinder Esp. Joint Analysts (8) E lt,;28tA/C IN226.A/C I'iO kVA Transforcer Test (1) A, D aoquip in'.~tegst rid f ar cold al.utdown based on scenetto at tact.ed (1 success path for accomp!!shing shutdown). IU P/e.k
'6*the key to inferinetton referenced nueaertcally appears on the last page of this table. _
l
[
l- l O )
C-
~
- TAttt 110,4 Pese 2 1
SE!S"!C TJAf.tFICAf t01 St* NARY OF CAYECORT I MECMANICAL AND tttCTRICAC t?JtrMtter 1 1
Method Itat r-ent Equ!poent of Equipment M thed tete r in9pretton Equireent '
I;4ae qualification ** Equipment of FunctLon** Avallability 18vmtre r Name Equipment inspection
- Qua t tit e e t t on*
- Function ** Avattanttity
- ttMitJ t in Control Beard Analysts (8)
!!?Of f A ssembt te s C. 13 E Yes IV0030A/S st.T5 Coottag fan I
- Anotysts (1) D Yes II M .JJ ~
tl *** 1 . * .
IVG0554/h scT5 Equip. Train I t !*ts ?J
. Analysts (8) D " g Strnt IVC 04A4/5 St45 lleating Colt Analysts (A) D. E ".
instruments for Meta Test (3) C.D- " '
t'entret hards .
3;'.;T5 Temperature 1At021 # Transmitter Test (6) E
- Misc. Auto Centret Cabinet Analysts (8) E. " '
4
- tW ntrA/D ttfrC Water rumps and Pfotors Analyste (7) fieluge te==l Controttler ,
A. D " Test (S) E "
- ts 21 t.tel ttts Water Ieg Pveps a fac toge Valve MDL-370DCT t ! 21.'.001 A " Test (3) E
- ti l:-ot) l*ressure Trans. . Test (3) E "
4 1110.f 4/8 rrt. Cnnt. saaptint System. [
- D " Detoge riping Analyste (7) "
g t.s s. Cont. Pfon. systers E tvC03Ya/8 sClu
- tW;.08 tA/D 3crvice Water Pumpo & Motors (VC04YA Anotysts (9) -
D "
- Analysts (7) A. D * .
. t IV .'*4 A/S Traveling Vater Screens Analyets (7) Solenold Valee E " Test (2) D "
tW .'s21 A/R Satvite Water Strainers Ane!yste (8) E "
Actuator Analyste (7) D *
- tt?t*4AA/C -
h flCCW ffuat Factienger *1Yt!OtCA/D Vent Pens Analysts (8) A. D "
tVfntC Analyste (?) A. D *
- lit.12S s.2 Cy!!nder p.ack tYt01C
- I
. Analysts (8) D. E "
iMt 34 tVv03C IVYO4t'.
esp' .WitA/D Misc. Tanks section !!! tYt.04CA/B '
Analyste (7) A, D *
- tilP e A'es'A/n !YGnttA/n InU .4etth/c IVhttetA/F ,
t h2 8. *tM II /C IVXHCA/C f p!!. A"Injn:/t. IVAO)C i f* s I = A*t % 1/t* ,
Restlient Isolators Analyste (?) E "
t u t A' net.
Motors Apelyste (9)
- p2:.4. , it
- A. D
- 1VC02CA/B C.R. Condensing Unit Analysts (7) A. D *
- tV101CA/F $witekseer Condenstng Unit
. Anetysta (7)(8) A. D "
St.ptga nt sep.tred for told shutdow.i based on scenerlo attacteed (1 success patte for accomp!!shing shutdown).
- th MJB/gk k y to inforratten referenced nwmetcally apreers on ttie test page of trils table. * '
I.. l L _ _ _ . _ _ . _ _ _ _ _ _ _ _ _ _ __ _ _ _ _ _ _ _ _
. i
-( - .
.l dp p
V TABLE 's10.6 j St!5MIC C'JAf !FICAT!C9 StM4ARY OF CAf tConf 1 PECI'ANICAt. AND ELECTRICAt. EQt IPMElff l
Metfied fee thod Fqstr-ent Etv!pmnt of Equipment Inspection Equirm at Equipment of Equipment Inspettlen V,e r lia-o quattffcation** t unc t i on *
- Avattability Numbe r Ne se, Quatt!tcation64 Functioneo Avette%tilty titr.51 Contret ranets Test (!) A, D Yes *tVX06AA/F l'ttter for $pecial Cett Analysta (7) A, E yes Irt PU Ca bine t s IfvAC Da*rers Test (4) t tu ttXA/S IfVA". Duct 5ttencers Anetysts (9) E
" Refrigeretten $pettettlee == . A, D gee titter Dryer in.'AC cravity shutters Test (2) .
- 1VC095A/S resenttet Fachese Fttter Anotyste (8) A, t 9,e
- I'.T.P tA/9 flw tienent s
- E No tVC103 units .
tvth)2A/8 lit t f. Pressure Indleating Test (2) E IttitJ __ t!vAC repels Analysts (8) A, D fes 'wltch Mut.2414859
. l .'1 M J
- li t *p)J Damptng Framing Analyste (7) E #
1 trf163A/S ten Motor Analyste (7) A, D a I?v4C te.st r. A, D We Mpuntinit peachete . Analyste (?) E =
Amonte Montoring Systes = A a
, riesswee Transattter Test (5) t netage Velves = 1 po temperature Transmittere = t =
', ?.ssenttet riessure Couges = A, O *
- !fr.!!TA/C Coottag W ter Reservett Tank' Analyste (7) C, D, t Tde and Thermometers lif.13T A/C . ,,
,. . *1 plt!JA/C kss. Relay renets Test (3) C, D ve's
- !Mit T A /r e..W. Enransion Tank ,Analyste (7) C, D, t 1PL67JA/S itasuste $hutdown renete Test (1) D
- ltrrttTA/C 0.0. $gerar,e Tank . Anetysts (7) C, D, C tire tutingutslitng System Test (3) C, D =
Anetyste (6) "
- t WitTA/P ithCf.V ispsneton Tank A. D. t ,
- tt:002rA/D ruet 011 Tiensfer r eps Analysts (7) C, 0 a
- lhf.l! A /C tir Pecetwer Tank Anotysts (7) C, 0, t Analysts (4) A, D "
Iso. Trans. & Sensere .
spectet Colt Cabinete Analysts (7) A, D ' " Analyste (7) *
- t'.*f;t m/8 . *tVt03CA/8 Wentitetton Ferie A, 9 t vtis A /O typotCA/C fVr.liA/r Essenttet ruessure and A, D "
t V v4'.1 Test (1) t V'e Wi .
t'teperature Evitches
- tv e4%
s- a es.nty..v. regutted for cold shutdown based on estnert attached (1 ovecess path for eccomplishing st utdown). -
pejli/gk es T he key to informetton referenced numericatty appears en the test rage of this table, .
Page 4 TABLE 110.6 SttSMIC Q'JALIFICAf t01
SUMMARY
CF CATECORY t HECttANICAt, AND ELECTRICAt. EQUINEy Pet 504 Equ!paent Nethed
- ttatraemt of tquipment Inspection Eqwtpaent Equ t raent N s*tt r N8*e Funttlen*
of Equirent fairectlen Qualtftcatten* Avattability Nebe r Name QualtittatteM* Function
- Availability
!:VAC Cont re,1* Da= pet s Analysts (1) E Yes Arttyt VArves Freese Protection Equipment
- D. E IF.12F008 Cate Valve No Analysts (7) C Tee lyr.Q l1 A /R tes '!setation Dampers Analysts (7) A. D Yes IF.!!F009 Cete Valve Analyste (7) C I'.*f 8.Y A/ S 1Dri!VA/S ILt2F04SA/B Angle Valve tYJe4TA/S
, , Analysis (7) A t rui*'v a / s
. Ib 8.8s t')Y a / S .
IVW)V . *
,,. %*per Operaters N1190 Settee Test (4) A. D "
- Aeteater ,
- itte. Centret renets . .
IfstFJ = D. E "
, IIN t t! -
A. D. E "
1PL79J
- A. E "
=
Switchr. car for pecir. t.TNG 4tt.0V and e,ticV Test (3)
- A. E "
resentir t Centret Room ' Analysts (7) A. D "
Iestation Ef>eck Dempers
- Limiter 19e Motnr Operators Test (4) A, D "
- *< ti. 4 0 Wh.! * *
$Mn.2
- f
- M. l l
Pve t Accide nt Pvt. Coit. Test (3) D "
r,t.a. R.edto-activity Montters Systtm N, -
N i *
'tain Content Rewi Radletten ,. Dg fee .
tientters .
=
\- .
. NSU
- !6e ter to infor*sttom referenced numericatty erpears og the last page of this table. -
) .
k
g
- g .
n Q
o -
Page 3 TASLt 110.6 k
SE!S*f tC QUALIFICATIC't SLMARY CF CATECCRV 1 NECffANICAL AND ELECTRICAL EQUIPfCNT
- L Methed {
Equipeent Equip *ent Pethed of Equipment inspection Equirment Equipment j Num.4 r f:4me quatifiention** Function *e
=f. Equipaent tespectlen Ace t telet tit y punt.c r Na+e quattficatten+e runstte..** AvattabLtity _
ltt!>o21 Rf!M Clote Valve 10" Anotysts (F) A, D 1es li t.'6 3 24 A /S IV900!A/B Primary Centatnm nt flVAC Analysis (7) ivy 002A/B A. D Ves ttI2FC49 Butterfly Vatve t.'" ' ,
- Ivgou1A/3 IFStt022 - RCtc Clobe Valve 4" ," ivy 904A/8 Analysts (7) A. D tu',014. A/ l) service llater Clobe valve 3" " !W W 4A/D Service Water Butterft', Analysis (8)
- An,alysts (7) luso0>A/n Vatre 24" A, p If.4tl001A/A sten.ity Liquid Contret Analysts (7) " , *IWa03)A/D AD ],
cleS* Valve 1" * $ 1W:.0 34 A/3 i
lilltollA/S WI'R Cste Velve 4" Analysta (7) " *1V.03?A/D service V.ter pattently Analysta (8) L Ittitr%A/s A. D Valve 8" A. D "
g IF ill n27.a/8 trt2t049 " " "
3" Analysts (7) AD " IttituStA/S RifR Clote Valve 6" A, D itt2106SA/5 "
2.5" * '
It*D109 LPCs Cate Valve 14" Analysts (7) "
A. D ttN012 Inst. N2 Supply Clobe
- Test (3) and A, D
- II)lt010 BCIC Cate Valve 6* Analysis (7) A, D "
Valve .73* '
16 16'l82 !!%013 " "
2.3" Analysts (7) .
ItSIF911 *
- IRi tn S Equip. Drain to Radweste Test (S) and "
ItS tinti 5 1Rt049 A. D y l'Ctc Cate Va tre 8" Analysts (7) A. O " Clobe Valve 2.5" Analysts (71 . -
ti r.C IS Fuel Poet Coottng and Clean- . tRt001 Floar Drain to Redweste A, 17 "
tutpo2 Test (5) and A, D "
II t 0 3 '. up Cat, Valve 12" Clotie Valve 2.5" Analysts (7)
IWJ% RPCCV Cate Valve 6" Analysts (7)
~'
IW5020 service Water Clebe Test (3) and "
100% A. D A. O Valve 10" Analysts (7)
!Ws023 "
12"
- I V*.003 Service W ter Cate Valve 30" Analyste (7) " tus030 A. D ,
le.ht2A/S service Wette Cate Velve 4" spi 2fon3A/S kitR Cate valve 14" Analysts (7) A, O g" ep.128 tt04A/C " " " Analysts (?) A. D "
- 8. Al lA/B '
20"
- sle:1Il 004A/S tb" IW'.0 7 3 A /O *trvice Wter Clebe Valve 3" Analysts (7) " IFl21014A/S 14" .
A. O 10121017A/3 14" aIll2tolsA/a Rmt autten tly Velve 16" Analysis (8) A, O i
~lF121047A/B 14" all.1210t. A/B "
14" Analysts (8) "
ti.12It 001 LPCS Cate Valve 20* A, D "
IVH001 A'l Pact. house Ventilation Analysts (8)
- A, D tym.024/B hutterity valve 12" IF.12l012 f.PCS Ctabe Valve 12" IVi m jA/S Analrata (7) A. D "
t vir*04 A / 3
- 16.1260874/5 RitR Clebe Valve 3" .
it5tr043 " " Analysis (7) A. D
- RCtc 4" 1pjjrogv Recirculation Diaphram e .o u . a r t
- n t ve _75"
. A, D pe IVS0064/5 Service Water Butterfly Analysts (7) "
tu m0FA/n Valve 30" A. D etquis4ent required ter cold shutdown teased on scenario atta.;Ied (1 success path for accompitshing shutdown).
PUS /A 2*The key to infer,arton referenced numerically appears en the test page of this table.
- CARGENT & LUNDY . ..
G. a r. A".O . i .
l.- ,' ,
,m NOTES: ' ' -
(_) -
The folicwing referenced numerical key applies to the Method of Qualification column:
1, Muktifrequency random motion biaxial testing with Test Response Spectrum (TRS) enveloping the Required Response Spectrum (RRS).
- 2, Test input to specimen based on single axis and single ,
frequency excitation. .
3, Test input to specimen based on biaxial and single frequency excitacion.
4, Test input to specimen based on single axis and multi-frequency excitation.
5, Test input to specinen based on biaxial and multifrequency
, excitation. .
6, Test input to specimen based on fragility level excitation, 7,
Analysisofspecimenbasedonsta7.icanalysis.
S, Analysis of specimen based on dynamic analysis.
.')
C"? .9, Analysis of specimen based on static coefficient analysis.
l The following referenced alphabetical key applies to the Equip-ment Function column.
l A, Hot Standby and Cold Shutdown E, liot Standby C, cold Shutdown .
l 'p, Post LOCA . . .
i E, Passive. -
l The list of all the active valves and the method of qualification is included in table 110.6. There are approximately 1400 passive valves which are not listed in the above table but were qualified to the same requirements.
l (E)
I 1
SARGENT Q LUNDY Naco g Balance of Plant Equipment Qualification Progress Assessment Requali-g fication Carplete Complete Equipment 100. 85.
Valves 100. 80.
~
Instrumentation 100. 50.
C's Balance of Plant Equipment Qualification Schedule a o 7 e >. $ $ $
s t 5 9 F & t
< x n o < m o Equipment HVAC Dampers Valves Instrumentation Engineering Effort Implementation of Hardware Modifications o _
V Testing 4
J
O O d Um. H. Zimmar
SUMMARY
OF Page ! of I Project Na. 4130-00 EQUIPMENT MODIFICATIONS pey, 6C Date 4~M~S/
Equipment Description Modification Description Number IVG02CA Standby Gas Treatment System Vibration Isolators & Mounting Bolts Fan lh Strengthened 1VG02CB Standby Gas Treatment System Vibration Isolators & Mounting Bolts Fan 1B Strengthened -
lVG03CA Standby Gas Treatment System Vibration Isolators Strengthened Cooling Fan lA lVG03CB Standby Gas Treatment System Vibration Isolators Strengthened Cooling Fan 1B IVG04AA Standby Gas Treatment System Reinforcement of Coil Support Heating Coil lA lVG04AB Standby Gas Treatment System Reinforcement of Coil Support Heating Coil 1B .
IVCllXA Control Room HVAC Return Fan Providing Anchorage to Foundation Silencer lA lVCllXB Control Room HVAC Return Fan Providing Anchorage to Foundation Silencer 1B .
L
O O O Wm. II. Zimmer
SUMMARY
OF Page E of I Project No. 4130-00 EQUIPMENT MODIFICATIONS Rev. 00 Date U #- 8/
Equipment Description Modification Description Number IVY 01C CSCS-RilR Equipment Room Cooling Fan Vibratiori Isolators Strengthened IVYO2C CSCS-LPCS/RilR Equipment Room Cooling Vibration Isolators Strengthened Pan IVYO3C CSCS-RCIC Equipment Room Cooling Vibration Isolators Strengthened Fan IVYO4C CSCS-IIPCS Equipment Room Cooling Vibration Isolators Strengthened Fan IVYO5A CSCS-RIIR Equipment Room !! cat Additiohal Cabinet Anchorage & Coil Exchanger Reinforcement IVYO6S CSCS-LPCS/RilR Equipment Room Coil Additional Cabinet Anchorage & Coil Cabinet (lVYO7AA, IVYO7AB) Reinforcement IVYO8A CSCS-RCIC Equipment Room IIcat Additional Cabinet Anchorage & Coil Exchanger Reinforcement IVYO9A CSCS-IIPCS Equipment Room IIcat Additional Cabinet Anchorage & Coil Exchanger Reinforcement
t' O ~~%
( L/ (d Wm. H. Zimmer
SUMMARY
OF Page of 7 Project No. 4130-00 EQUIPMENT MODIFICATIONS Rev. OO Date U/f-8/
Equipment Description Modification Description 1PL30JB Off-Gas Instrument Panel 1B Mounting Welds Provided 1PL65JB Station Ventilation Purge and Additional Anchorage Provided Prim. Cont. HVAC Panel 1C41-A002 Standby Liquid Control Test Tank Providing Nozzle Reinforcing Pads LWR 02AA Reactor Bldg. Closed Cooling Saddle Supports Modified and Additional Water Heat Exchanger lA Anchorage Provided LWR 02AB Reactor Bldg. Closed Cooling Saddle Suppor'ts Modified and Additional Water Heat Exchanger 1B Anchorage Provided LWR 02AC Reactor Bldg. Closed Cooling Saddle Supports Modified and Additional Water Heat Exchanger 1C Anchorage Provided Detail AA (1) Rack For Locally Mounted Additional Anchorage Provided Instruments Detail DD (3) Racks For Locally Mounted Additional Anchorage Provided Instruments Detail JJ (2) Racks For Locally Mounted Additional Anchorage Provided Instruments -
L
()
r'x p)
(.
f's O
SUMMARY
OF Page of 7 Wm. H. Zimmer Project No. 4130-00 EQUIPMENT MODIFICATIONS Rev. OO Date Y-#~N Equipment Description Modification Description Number 1RE0lT Reactor Bldg. Equip. Drain Tank Additional Mounting Provided 1PS10S Sample Station 1PL50J Chiller Anchorage Grouting Provided lH13-P659 Rod Sequence Control System Mounting Welding Provided 1FC02AA Fuel Pool Heat Exchanger 1A Additional Bracing Provided, Reinforcing Saddle Supports, and Additional Anchorage Provided 1FC02AB Fuel Pool Heat Exchanger 1B Additional Bracing Provided, Reinforcing Saddle Supports, and Additional Anchorage Provided 1FWO2AA High Pressure Feedwater Heater Reinforcing Lower Supports lA-6 1FWO2AB High Pressure Feedwater Heater Reinforcing Lower Supports 1B-6
O O O Wm. H. Zimmer
SUMMARY
OF Page of 7 Project No. 4130-00 EQUIPMENT MODIFICATIONS Rev. dd Date V~l?~ Al Equipment
' Description Modification Description Number IVC 08SA Control Room HVAC Air Handling Additional Anchorage Provided Unit 1A lVC08SB Control Room HVAC Air Handling Additional Anchorage Provided Unit lE ,
LINO 3DA Drywell Pneumatic Sys. Dryer lA Anchorage Reinforcement Provided Skid (lIN07FA , B; lINllFA,B)
LINO 3DB Drywell Pneumatic Sys. Dryer 1B Anchorage Reinforcement Provided Skid (lIN07FC,D; IIN11FC,D)
LAP 05E 480V ESS Substation lA-1 Additional Anchorage Provided LAP 06E 480V ESS Substati ' 1A-2 Additional Anchorage Provided LAP 07EA 400V ESS Substation lA-3A Additional Anchorage Provided 1AP08EA 480V ESS Substation lA-4A Additional Anchorage Provided 1AP09E 480V ESS Substation 1B-1 Additional Anchorage Provided
(
O O O bb. H. Zimmer
SUMMARY
OF Project No. 4130-00 Page of 7 EQUIPMENT MODIFICATIONS Rev._OO Date V -/[- 3l Equipment Description Number Modification Description LAP 10E 480V ESS Substation IB-2 Additional Ancherage Provided 1APllEA 480V ESS Substation 1B-3A Additional Anchorage Provided 1AP12EA 480V ESS Substation IB-4A Additional Anchorage Provided LAP 13E 480V ESS Substation IC-1 Additional Anchorage Provided 1AP14EA 480V ESS Substation IC-2A Additional Anchorage Provided lVG0lYB Essential Recirculation Fan Isolation Damper Modification Hangers of Operator Mounting and/or IVQOlY Primary Containment Purge Isolation Damper Modification Hangers of Operator Mounting and/or IVQO2Y Primary Containment Purge Isolation Damper e Modification Hangers of Operator Mounting and/or P
O O O Mn. H. Zimmer
SUMMARY
OF Page 7 of 7 Proj ect No. 4130-00 EQUIPMENT MODIFICATIONS Rev. 60 Date V -l[- 8l Equipment Description Modification Description Number IVP0lYA Primary Containment HVAC Modification of Operator Mounting and/or Isolation Damper !! angers lVP0lYB Primary Containment HVAC Modification of Operator Mounting and/or Isolation Damper Hangers lVP10YA Primary Containment HVAC Modification of Operator Mounting and/or Isolation Damper Hangers IVPllYA Primary Containment HVAC Modification of Operator Mounting and/or Isolation Damper Hangers IVPllYB Primary Containment HVAC Modification of Operator Mounting and/or Isolation Damper Hangers D'
ANALYTICAL METHODS O Static Analysis: an analysis procedure used for equipment which has been demonstrated to be rigid (i.e. equipment has no natural frequencies in the frequency range of concern). This procedure evaluates the stresses and deflections.resulting from steady forces acting through the center of gravity. These steady forces are the maximum forces input at the equipment base.
They are determined from 'the zero period acceleration (ZPA) of the appropriate response spectra.
Equivalent Static Analysis: an analysis procedure used for ,
equipment whose dynamic characteristics have not been completely defined. This procedure evaluates the stresses and deflections resulting from steady forces acting through the center of gravity. The steady forces are the maximum forces associated with the peak response of any single degree of freedom system. They are deter-mined from the peak acceleration of the appropriate response spectra multiplied by an appropriate amplifica-tion factor to account for the possibility of multi-node response.
O Simplified Dynamic Analysis: an analysis procedure.used for equipment which can easily be modeled and whose dynamic characteristics are known. This procedure evaluates the stresses and deflections resulting from steady forces acting through the center of gravity. These steady forces are the maximum forces associated with equipment resonance. They are determined from the acceleration i associated with the equipment's natural frequency multi-l plied by an appropriate amplification factor to account I for the possible participation of higher modes.
l Detail Dynamic Analysis: a finite element analysis procedure
- for multi-degree-of-freedom systems where the responses are determined for each mode and then combined to deter-mine the true response and associated stresses and
! deflections resulting from any forcing function.
l i
0
O '
v
)
Specification No. 11 2156._
SUMMARY
OF PageIll of G'I .
Vendor: Tw imrerint EQUIPMENT QUALIFICATION Rev. f>O Wm. 11 . Zimmer Date ' l -l 5'- 81 Project No. 4130-00 Equipment
<2ncription h$
- i. Location Qualification llesults Number Method
,_ _. --- e.3 . . , _ . _. . :
4.16 IN Switch Group A Auxiliary Pesonance Search 1-5011z Natural Frequencies:
lAPO4EA Front to Back: 18 Itz lAPO4EB Side to Side: 27 !!z 1AP04DC Randan mtion Blaxial Test TRS envelopes RRS FB/V and SS/V, 1-50 !!z Functional Ogurability Verified lAPO4ED 6.9 KV Switch Group A Auxiliary Pesonance Search 1-5011z Natural Fruluencies: ;
Front to Back: 10, 14, 18, 1AP045'E 21 !!z '
Side to Sides 10, 19, 24, 30 !!z l' Harxken Motion Diaxial Tests TRS envelopes RRS l FD/V and SS/V,1-5011z Functional Operability l Verified L
y -- - - - , . . . - -
O O O Specification No. 11-2157
SUMMARY
OF Page !D. of O'?
Vendor: ITE Imperial Rev. 00 EQUIPMENT QUALIFICATION .
Wm. 11 . Zimmer Pro],ect No. 4130-00 Date 'l - l 6 - Yil Equipment Description hf ia Location Qualification Results Nuber Method
- s __ -
1AP05E 480 V Substation. A Aux. Bldg. Random Motion Biaxial Test. Principal resonant frequen-1AP06E EMD-000606 cies were determined to be:
1AP09E A resonance search test FB/V: 6,8,11,19,23 & 3 3 IIz .
LAP 10E was performed from 0.5 to SS/V: 4.5,13,18,23,30 &
1AP13E 50 IIz. This was followed 43 IIz. TRS envelopes RRS by Random Motion Tests from Functional Operability 0.5 IIz to 50 IIz Verified lAPOSE 750 KVA Transformer A Aux. Bldg. Random Motion Biaxial Test. Principal Resonant frequen-1AP06E (Associated with 480V EMD-001235 cies were determined to be:
LAP 09E Substation). EMD-001802 FB/V: 2,7,9,12,15,17.5,21 LAP 10E A resonance search test was & 30 IIz. SS/V: 4.4,7,8.5, LAP 13E performed from 2 to 30 IIz. 12,17 & 20 IIz . The TPS This was followed by Random envelopes the RRS Motion Tests from 0. 'i to Functional Operability 100 IIz Verified W
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O O b O U
Specification No. 11 - 2158
SUMMARY
OF Fage II,3 of b[ .
Vendor: Tw Tmnorini EQUIPMENT QUALIFICATION Rev. OS Wm. II . Zinnmer Project No. 4130-00 Date Lk - l#.5 I I Equipment h jI Qualification Description i a Location Results Number Method -
_s_ _
1AP15EA 480 V Motor Control Center A Reactor Pseudo-Biaxial Sino Sweep Natural Frequencie's:
1AP15EB Resonance Scarch 1-35 !!z Front to Back: 7-8 .75, 35 Itz Side to Side: 8-10, 35 IIz Pseudo-Biaxial Sine Dwell Input Accelerations greater for 1-26 I!z range. Narrow than ZPA and TRS envelopes B(uxl Pseudo-Biaxial Randan RRS, Ibnctional Operability Motion Test for 3.94-10.26 II: Verified for Original range. Sine Beat Psotrio- ' Oualification Criteria.
Biaxial Tests at 8.75,10 Requalification to T-Quencher and 35 liz. Criteria tbt Carpleted.
1APl6EA 480 V Motor Control Center A Auxiliary Pseudo-Biaxial Sine Sweep Natural Frequencies:
1APl6EB Resonance Scarch 1-35 112 Pront to Back: 7-8.75, 35 lfz 1AP16EC Side to Side: 8-10, 35 !!z 1AP16ED 1AP16EE Pseudo-Biaxial Sine Dwell for Input Accelerations greater IAP16EF 1-26 IIz range. Narrow Band than ZPA and TRS envelopes Pseudo-Biaxial Randan Motion RRS. Functional Operability Test for 3.94-10.2611z range. Verified.
Sine Deat Pseudo-Biaxial -
Test at 8.75, 10 and 35 Ilz.
L
O O O Specification No. 11- 2158
SUMMARY
OF Page A'{ of C .
" #* ^
EQUIPMENT QUALIFICATION Rev. do Mn , II . Zimmer Project No. 4130-00 Date N ~I C ~ 2l Equipment Description hk ia Location Qualification Results Method -
a ___ ,
1AP20EA 480 V Motor Control Center A WS Bldg. Pseud & Biaxial Sine Sweep Natural Frequencie's:
1AP20EB Resonance Search 1-35 112 Front to Back: 7-8.75, 35 fiz 1AP20EC Side to Side: 8-10, 35 IIz Pseudo-Biaxial Sine Dwell for Input Accelerations greater 1-26 IIz range. Narrow Band than ZPA and TRS envelopes Pseudo-Biaxial Pandan Motion RRS. Functional Operability Test for 3.94-10.26 IIz range. Verified.
Sine Beat Pseudo-Biaxial Test at 8.75,10 and 3511z.
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O O O Specification No. H- 2159
SUMMARY
OF Page li d of 67 Vendor: Stewart & Stevenson Rev. (R)
EQUIPMENT QUALIFICATION Wm. H. Zimmer Lg--le.91 Date . <.
Project No. 4130-00 Equipment Description ia Location Qualification Results Number Method
- S 1DG0lKA Diesel Generator A Aux. Bldg. Finite Element Dynamic The lowest frequency 1DG0lKB Units Analysis. obtained from the program 1DG0lKC EMD-002581 is 15 Hz. Element stresses EMD-012939 representing the various
. A finite element Dynamic parts of the DG are within 1DG02AA Diesel Generator Analysis and Static Analy- allowable limits as are 1DG02AB Heat Exchangers sis were performed using bolt stresses. Deflection 1DG02AC the computer program ANSYS. of the generator shaft is 1DG03AA A value of 1% damping was calculated to be 0.005 1DG03AB used. The maximum inch compared to an actual 1DG04AA stresses in the component air gap of 0.392 inch.
1DG04AB parts of the assembly and bolts are determined. The maxi:aum generator shaf t .
deflection is also computed .
1DG05KA DG Exhaust Silencer P Aux. Bldg. Finite Element Dynamic The lowest frequency 1DG05KB 1A, 1B, 1C, lA, 1B, Analysis. obtained from the program 1DG05KC 1C EMD-002581 is 30.11 Hz. Stresses 1DG06KA A finite element Dynamic within allowable limits.
1DG06KB Analysis and Static Analy-1DG06KC sis were performed using ANSYS with 1% damping.
Stresses in the equipment were calculated.
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O O O Specification No. H-2163
SUMMARY
OF Page NU of gr7 Vendor: Gould Rev. DO EQUIPMENT QUALIFICATION -,
Mn. H. Zimmer Date # k ' h_a - f I Project No. 4130-00 Equipment gC1 Qualification Description i a Location Results N mber Method n
1DC01EA 250V Battery lA A Aux. Bldg. Random Motion Bi' axial Test TRS envelopes RRS. The 1DCllEA 125V Battery lA,lB,1C EMD-003689 equipment passed the test 1DCllEB A random motion biaxial without compromise of 1DCllEC type test was performed structure or electrical 1DC21EA 24/48 V Battery lA,lB from 1 to 40 Hz. 5 OBE function.
1DC21EB tests were followed by 1 SSE test in each of two orientations. The tests were of 30 second duration each and were all analyzed at 2% damping.'
1DC01EA Battery Racks P Aux. Bldg. Static Analysis. Natural frequencies in each 1DCllEA (equipment number EMD-004697 direction: h y=48.59 Hz 1DCllEB same as battery). Fundamental Natural Fre- h 2 =43.43 Hz 1DCllEC quencies were determined V=46.60 Hz 1DC21EA in each direction. A (rigid). Stresses within 1DC21EB static analysis was then allowable limits.
performed using ZPA val es Structrual Integrity from 1/2% OBE and 1% L >_ Demonstrated.
- urves . Accelerations:
OBE / DBE hl=0.20/0.32 h2=0.18/0.28 v=0.20/0.30 e- - - - - - . - - - - - - - - - - - _ - - - - - - - . - - - - - - _ - - - - _ - - - -
7 v~ t e pm O O O Specification No. H-2164
SUMMARY
OF Page A 9 of 6')
Vendor: Power Conversion Products Rev. 00 EQUIPMENT QUALIFICATION .
H. Zimmer Wm.
Date # k l , ? 7. k Proicct No. 4130-00 Equipment Description hS Qualification Results g Location i
Number Method
_ -a 1DC02EA, 250V Battery Charger A Aux. Bldg. Random Motion Bi' axial Test TRS envelopes RRS. The EB 1A EMD-003274 equipment passed the test 1DCl2EA, 125V Battery Charger A random motion biaxial without compromise of EB, EC 1A, 1B, 1C type test was performed structure or electrical 1DCl3EA 125V Battery Charger from 1 to 33 HC. 5 OBE func tion .
Spare tests were followed by 1
.lDC22EA, 24V Battery Charger SSE test in each of two EB,EC,ED lA, 1B, 1C, ID orientations. The tests were of 30 second duration each and were analyzed at 1/2% OBE and 1% DBE.
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O O O Specification No. 11-2165
SUMMARY
OF Page }\ li of i '7 .
Vendor: ITE Ig1ppgifL pg p
Wm. !! . Zinuner Project tio. 4130-00 Date 'I I,. > ,(*.l _
s Equipment b C{ Qualification Denc r i pt. ion i I.oca t i on Ilesults Number .
Method
- u ,
IIP 01EA 120 VAC Distribution A Aux.nldg. Pacudo-Bia::ial Sine Sweep Natural Frequencies:
LIP 01En Panel Resonance Search 1-35 112 Front to Back: 7-8.75, 35 !!z IIP 03E 120 VAC Distribution W Side to Side: 8-10, 35 Itz IIP 04E Panel Pseudo-Blaxial Sine Dwell Input Accelerationn for 1-26 11z range, Narrow greater than ZPA and TRS Dand Pneudo-Ulaxial Randorn envelopen RitS. Functional Motion Tout for 3.94-10.2t operability verified.
!!z range. Sine Dent Pseudo-Biaxial Test at 8.75, 10 and 35 11z .
, s -
O O O Specification No. 11-2166
SUMMARY
OF Page jEI i of ,f/ .
Vendor: ITE Imperial EQUIPMENT QUALIFICATION Rev. l'O Wm. II . Zimmer , ,
Project No. 4130-00 Date ll lU 1I Equipment Description h$
ia Location Qualification Results N mber Method *
- S 1DC04EA 250 VDC Main A Aux. Bldg. . Pseudo-Biaxial Sine Sweep Natural Frequencies:
Distribution Panel lA Resonance Search 1-35 IIz Front to Back: 7-8.75, 35 IIz Side to Side: 8-10, 35 liz.
Pseudo-Biaxial Sine Dwell Input Accelerations for 1-26 llz range.. Narrow greater than ZPA and TRS Band Pseudo-Biaxial Randon envelopes RRS. Functional Motion Test for 3.94- operability verified.
10.26 Ilz range. Sine Beat Pseudo-Biaxial Test at 8.7 5,10 and 35 IIz .
1DC05EB 250 VDC Motor Control A RX.Blde. Pseudo Biaxial Sine Sweep Natural Frequencies IDC05EC' Centers Resonance Search 1-35 liz Front to Back: 7-8.75,35 IIz Side to Side: 8-10, 35 112 Psuedo-Biaxial Sine Dwell Input Accelerations greate :
for 1-26 IIz range. Narrow than ZPA and TRS envelope: ,
Band Pseudo-Biaxial Randon RRS, function operability
, Motion Test for 3.94- verified for original 10.26 112 range. Sine Beat qualification criteria.
Psuedo-Biaxial Test at Requalifications to T-8.7 5,10 and 3 5 IIz . Quencher Criteria not completed.
w Y v v Specification No. 11-2166
SUMMARY
OF Page [s 1. of Cf /
Vendor: ITE Imperial EQUIPMENT QUALIFICATION Rev. M Mn. II. Zimmer '
Project No. 4130-00 Date II I .: 'l Equipment 5j Qualification Number Description i. Location Method Results
--i U , _ _ _ _ _ _ _ _ . .
1DCl4EA 125 VDC Distribution A Aux. Bldg. Pseudo-Biaxial Sine Sweep Natural Frequencies:
1DCl4EB Panels lA,1B,1C Resonance Search 1-35 IIz Front to Back:'7-8.75,35 !!z 1DCl4EC Side To Side: 8-10, 35 !!z Pseudo-Biaxial Sine Dwell Input Accelerations for 1-26 11z range. Narrow greater than ZPA and TRS Band Pseudo-Biaxial Randon envelopes RRS. Functional Motion Test for 3.94- Operability Verified.
10.26 112 range. Sine Beat Pseudo-Biaxial Test at 8.75,10 and 35 Itz.
1DCMEA 24/48 VDC Distributior A Aux. Bldg. Pseudo-Biaxial Sine Sweep Natural Frequencies:
1DC26EB' Panels Resonance Search 1-35 I!z Front to Back: 7-8.75, 35 11:
Side to Side: 8-10, 35 IIz Pseudo-Biaxial Sine Dwell Input Accelerations for 1-26 112 range. Narrow greater than ZPA and TRS Band Pseudo-Biaxial Randat envelopes RRS. Functional Motion Test for 3.94- Operability Verified.
10.26 IIz range. Sine Beat Pseudo-Biaxial Test at 8.75,10 and 35 IIz .
O O O Specification No. 11-2167
SUMMARY
OF Page [lI$ of C '[
Vendor: Conax Corporation . . c' EQUIPMENT QUALIFICATION Rev. '
Wm. II . Zimmer Date M
Lv r-g Project No. 4130-00 Equipment I sc Qualification e 1 Number Description i a Location Method Results s_ _
LAP 50EA, Low Voltage Power P Rx. Bldg. Static Analysis' The natural frequencies EM Elec. Penetration EMD-000549 calculated rere:
Assembly E-1, E-16 EMD- O 1 P "T.* h 14 3 11z -
1AP50EP L.V. Control Elec. P Rx. Bldg. Natural frequency calcula- h12== 900 Itz EJ Penetration Assembly tions were performed to V = 143 IIz E-8, E-12 justify a static analysis. Stresses were within the
, LAP 50ED, L.V. Instrument Service P Rx. Bldg. The required acceleration allowable limits.
EL, ES, Elec. Penetration in each direction was:
ET, EU Assembly E-5, E-15, (OBE/DBE): Functional Integrity E-3, E-ll, E-14. h1 = 0.34/0.48 Verified for original 1AP50EB, L.V. Neutron Monitor P Rx. Bldg. h2 = 0.44/0.50 qualification criteria.
EE, EG, Elec. Penetration Requalification to V = 0.37/0.45. T-Quencher criteria not EK Assembly E-2, E-6, E-9, E-13 completed, LAP 50EC, Control Rod Position P Rx. Bldg. -
EII, EN Indicator L.V. Elec.
Penetration E-4, E-10, E-17.
LAP 50EP Medium Voltage Power P Rx. Bldg.
ER Elec. Penetration Assembly E-18, E-19.
t L
O O O Specification No. 11-2175
SUMMARY
OF Page l$19 of @)
Vendor: United Electric Controls Rev. oO EQUIPMENT QUALIFICATION ,_.
Wm. II . Zimmer Project No. 4130-00 Date N-\B~2}
Equipment Description hI ia Location Qualification Results Number Method
- S 1PM0lJ Genetator and Station A Aux. Bldg. Finite Element Dynamic There were a total of 21 Auxiliary Control Analysis. mode.x considered in the 73;d. EMD-004798 analysis. The lowest fre-1PM02J Tu. Jne - Condenser P Aux. Bldg. EMD-004845 quency obtained was 9.59 arr wxiliaries Control EMD-018429 Hz. The resulting stresses F. ed. A dynamic analysis was at all locations were with-1PM03J F. er Heaters and P Aux. Bldg. performed by the Engineer- in allotrable limits for Aar.iliaries Control ing Mechanics Division on both assembly #1 and Board, two " assemblies". Assembly assembly #2. Structural 1PM04J Generator and Trans- P Aux. Bldg. #1 included panels 1PM0lJ, Integrity Demonstrated.
former Recorder Pnael 02J, and 03J. Assembly 1PM05J Station Totalizing P Aux. Bldg. #2 included 1PM07J and Panel. 1PM08J. Remaining Panels 1PM06J Leak Detection Panel P Aux. Bldg. qualified by similarity.
1P^407J HVAC and SGTS Panel P Aux. Bldg.
IPM08J Station Services Panel P Aux. Bldg.
..PM09J Fire Protection and P Aux. Bldg.
Deluge Valve Control Panel. '
1PM13J Excess Flow Check P Aux. Bldg.
Valves Status Panel.
1PM16J 345KV Switchyard P Aux. Bldg.
Mimic Bus Panel.
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, t- , r- -
O O O Specification No. 11-2177
SUMMARY
OF Page Al6 [,f 67 .
Vendor: Fisher Controls U, V
. EQUIPMENT QUALIFICATION Rev.
Mn. ii . Zimmer Project No. 4130-00 Date 11 ~ \ r,_,. -e,. , f Equipment Description h$
ia Location Qualification Results er Method s _ _ __ . . _ , - - - , _ _ _ _ . : _- -
1PA02J Misc. Auto. Control P Aux. Bldg. Finite Element Dynamic Natural frequencies were Panel. Analysis. found to be:
- EMD-003796 18.74 IIz EMD-004328 18. 87 11z A finite element dynamic 21.28 I!z
. analysis was performed 23.73 112 using the program 28.32 IIz STARDYNE to determine The stresses calculated the natural frequencies by the program are within of the panel. An equiva- the allowable limits.
lent static analysis was Structural Integrity then done to determine Demono' ated.
stresses in the panel.
The peak value of the response spectrum curves at 2% damping was applied in each direction. OBE/
DDE values of accelera-tion were:
h1 = 1.0/1.5 h2 = 1.0/1.5 V = 1.2/1.75 Stress's from each load case were auded using absolute sum method.
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O O O Specification No. 11- 2185
SUMMARY
OF Page AIL of 6'l .
Vendor:_Dingham Willamitte__ OO EQUIPMENT QUALIFICATION Rev.
W:n . II . Zimmer ,
gI-Ib..'(l Project No. 4130-00 Date Equipment Description 5$
ia Location Qualification P.esults Msber Method -
m -
LWR 0lPA RDCCW Pumps A Pcactor Static Analysis Acceleration levels used:
LWR 0lPB Building Ioacst fn N U* U1 = 0.Mg, H2 = 0.369 ,
LWR 0lPC IWR0lPD y ,o,709 Critical stress = 17,380 psi (allowable = 17,500 psi)
Critical def1cetion= 0.0075" (allowable = 0.011")
Analysis Vendor requalification not cm pleted.
lE12C003 CSCS Water Leg Pumps A Pcactor Static Analysis Acceleration levels used:
lE21C002- Building Pump freq.: 49.7 IIz 111 = 0.2 g, 112 a 0.28 g, 1E22C003 Driver freq.: 252 I!z y = 0.14 9 lE51C003 Critical stress = 31,975 psi (allowable = 70,000 psi)
Operability stated to be not effected even should contact occur on rotating parts.
Analysis Vendor requal. not empleted.
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7 .,- . , ,
O O O Specification No. !!- 2233B
SUMMARY
OF Page ft !7 of b '/ .
kb. II . Z2mmer h71fc IiE do. tors) EQUIPMENT QUALIFICATION Rev. UO Project No. 4130-00 Date .. <,
-t . ... l Equipment Description ia Location Qualification er Method Results
- S . - _ _ _ - ._'
lhS0lPA Service Water Pumps & A Service Static Analysis, Pump Acceleration levels used:
lhS0lPD Pump bbtors Water Natural frequency: 45.9 IIz 111
= H = 0.909 , V = 0.659 2
1hS0lPC Pump Critical stress = 24,573 psi lhS0lPD Structure . (allowable = 26,250 psi)
Deflection = 0.0067" (Allow. = 0.011")
Static Analysis, Motor Acceleration levels used:
Natural frequency: 32 IIz lil"U2 = 1.10g, V = 0.78g Critical stress = 11,250 psi (allowable = 40,000 psi)
Deflection = 0.00202" (Allowable = 0.024" max.)
y I " "
, y O O O Specification No. 11- 2237 Venclor:Ax_[hnitizaltlq^--
SUMMARY
OF P89" IIIE f E1 '
EQUIPMENT QUALIF1 CATION ROV- O hw . II . Zimmer , ,
Project No. 4130-00 Date il I > 'i I Equiprent Description 5$
ia I,oca t i on Qualification Number s s Method ,
,dL lhS03FA Traveling water nereens W Service Detailed dynamic analysis Analysis by restonso spectnn 1WS03!.3 hhter Ptmp Natural fral. 17 112 Critical stress = 26.26 ksi lhG04FA Structure (Allowablo = 38.1 kni) lhS041B l- _ _-
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- f Y T O O O Specification No. 11- 2245
SUMMARY
OF Page / of 9/ -
Vendor: Yuba IIcat Transfer Co.
EQUIPMENT QUALIFICATION Rev. 00 Mn. !! . Zimmer Project No. 4130-00 Date ' f ' l '.b Y I Equipment Description ia Location Qualification g Flethod Results
- a lhE02AA RIXUV lleat ExchanGor P Reactor Simplified Dyna:nic Arnlysis Acceleration levels-used:
lhE02AB Building Natural freq.: 11y = 0.569 , 11 3 = 0.469, lhE02AC II1= Rigid, II =V=29.1, 2 32.6 IIz.
- y,g Critical stress = 29,343 psi
. (Allowable = 35,000 Imi)
Stnictural Integrity Dmonstra-tcxl for original qualification criteria. Requalification to T-Quencher criteria not conpleted.
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O O O Specification No. 11- 2273
SUMMARY
OF Page A99 of 69 .
ndor: Graver M EQUIPMENT QUALIFICATION Rev. AO Wm. H. Zimmer Project no. 4130-00 Date N-lb'N}
Equipment Description 5$
ia Location Qualification Results Number Method '
_ _ _ _z_= _
L_S .
1B21-A001A MSIV Accumulator tank P Prim. Static analysis Accel. levels used:
1B21-A001B Cont. Natural freq.: Hy = 0.55g, H2 = 0.55g, 1B21-A001C Hy =H 2
= V = 34.6 Hz V = 1.20g 1 1-A00E Critical stress = 16,955 psi I
(Allowable = 21,600 psi)
Static analysis Accel. levels used:
Natural freq.: IIy = 2.1 g , 112 = 0.6 g, Hy = 52 Hz, H2 '122 Hz, V = 2.8 g V = 36 IIz Critical stress = 7,977 psi (Allowable = 9,020 psi) 1B21-A002A MSIV Accumulator tanks P Prim. Static analysis Accel, levels used:
1B21-A002B Cont. Natural freq.: 111 = 0.55g, H2 = 0.55g, 1B21-A002C I!y = H2 = V = 34.6 Hz V = 1.20g 1B21-A002D Critical stress = 16,955 psi (Allowable = 21,600 psi)
Static analysis Accel. levels used:
Natural freq.: 111 = 0.36g, H2 9 Hy = 390 Hz, H2 = 1,725 Hz V = 0.50g V = 107 Hz Critical stress = 5366 psi (Allowable = 9020 psi) i
V
- V m r s U ( d Specification No. 11-2273
SUMMARY
OF. Page ?,l r4 M of *; I9 -
Vendor: Graver Tank Rev. OO EQUIPMENT QUALIF1 CATION Mn. II . Zimmer Date # $- ! P ~
Project No. 4130-00 Equipment Description 5S ia Location Qualification Method ,
1 -
1B21-A003B MSIN Accumulator tanks P Prim. Static analysis Accel. levels used: ~
1B21-A003C Cont. Natural freq.: 111
= 0.559 ,112=0.55g 1B21-A003F Ily=H2 = V = 35 llz 1B21-A003G -
V= 1.209 1B21-A003K cal suess = M,2R psi 1B21-A003L 1 1 = 1,600 ps0 Illuivalent static analysis Accel. levels used:
Natural freq.: 111
= 1.0 g, II 2= 1.0g 11 = 19.7 IIz, H = 35 IIz, 1 2 v= 1.0g V= 44.5 IIz Critical stress = 22,800 psi (Allowable = 29,500 psi) 1B,21-A004A/II MSIN accumulator tanks P Prim. Static analysis Accel. levels used:
1B21-A004K Cont. Natural freq.: 11 = 0.559, !! = 0.55g 1 2 1B21-A004L
~
111=H2 = V = 34.6 IIz v= 1.20g
_ g Critical stress = 14,892 psi 1B21-A004S (All wable = 16,440 psi)
D]uivalent static analysis Accol. IcVels used:
Natural freq.: 11 = 1.2 g, H = 1.2 g 1 2 Ill = 854 IIz,112 = 398 IIz, y= 2.3g V = 76 IIz Critical stress = 29,238 psi
- (Allowable = 29,520 psi)
L
/ ^
( bp bf Specification No. 11- 2288
SUMMARY
OF Page [W/ of 6T) .
Vendor: Refer to Equip. Status Sheets EQUIPMENT QUALIFICATION Rev. Ad Wm. !! . Zimmer ,_,
Project No. 4130-00 Date #-f-lW-El Equipment Description 5k ia Location Qualification Results Number Method
- 3- __ _ _ _ _ __'
IVG05SA SGTS equipnent trains A Reactor Detailed dynamic analysis Max. stresses well within IVC 05SB Building Natural freq.: allowable limits at critical 14.64 IIz, 31.9 IIz, 40.4 IIz sections.
Deflection analysis demon-strates operability of units.
lVG02CA SGIS primary supply Fans A Reactor Static analysis (fan-motor- Accel. levels used:
lVG02CB Building shaft assembly) Il y=9.45g,II =V=9.0g 2
(Assem. )
Natural freq.: 229 IIz gg1=1,gg,jg2 =3.2g, V=1.29 (obtor)
Min. margin of safety (motor shaft) = 3.16 Min. margin of safety (founda-
- tion bolts) = 1.1 Min. margin of safety (base angle) = 1.0 Max. rotor assembly def;= 0.002" (Allowable = 0.025")
, Fan-motor assembly subjected to limiting-load analysis; assembly capable of withstanding 8.10 g's i
1
___.7_ ,
__--__.r--_ , ,. _ _ _ __
o O -
O Specification No. H-2288
SUMMARY
OF Page I)A$of 69 -
Vendor: Rerer to cauip. status, sheets Rev. ),
EQUIPMENT QUALIFICATION Rn. H. Zimmer ;; . e' p/
Project No. 4130-00 Date .
Equipment Description hk ia Location Qualification Results er Method '
.:. 9 -
lVG03CA SGIS cooling fans A Reactor Static analysis (fan-motor Accel levels used:-
lVG03CB H1=H Building assembly) 2 =9.45 g, V=9.0 g (Assen. )
Natural freq.: 182 Hz H1 =1.9 g, H 2=3.2g, V=1.2g (Motor )
Min. nnrgin of safety = 1.3 Max. rotor deflection = 0.00243" (Allowable = 0.013")
Fan-notor assembly subjected
, to limiting-load analysis; Assembly capable of withstand-ing 39 g's lVG04AA SGTS heating coils A Reactor Detailed Dynamic Analysis Accel. levels used:
lVG04AB Building H = 1.0 g, H =1.2 g, 1 2 Natural freq.:
Hy = 37.7 Hz, H2= 11.1 Hz' V= 0.9 g Critical stress = 18,300 psi V= 14.3 Hz (Allowable = 38,800 psi)
(System freq. = 56.6 Hz) Operability demonstrated for original qualification criteria.
Requalification to T-Quencher criteria not canpleted.
,4 \ -#-F>
U n./ C/
Specification No. 11- 2288 Vendor: Refer to equin, status sheets
SUMMARY
OF Page i of . f.
hti. I! . Zimmer EQUIPMENT QUALIFICATION Rev. '
Project No. 4130-00 1 e t
Date :t -
Equipment Nunber Description hf 1 a Qualification Location
- a. m.
Method Results
-_ . _ _ _ _ _. _ _ _ . L _% __u . - . -.
IVGllYA Backdraft dampers A Reactor lVGllYB Fquivalent static analysis Required acceleration levels:
Building Natural freq.: 90 IIz (min.) IIy=II2 = 1.12 g, V = 1.28 g Acceleration levels used:
Ily=II2 =V= 10.0 g Critical stress = 1,570 psi
. (Allowable = 20,000 psi)
Equivalent static analysis Accol. levels used:
Natural freq.: IIy= 10 g, 112 = 10 g, IIy=V= 90.6 g, H2 " #i 9id V= 10 g Critical stress = 17,985 psi (A1,lowable = 18,000 psi)
Critical deflection = 0.0025" (Allowable = 0.03")
1VG12YA Backdraft Dampers A lVG12YD Reactor Static analysis Required acceleration levels:
Building Natural freq.: 90 Hz (min.) 11 y =11 2 = 0.42 g, V = 0.65 g Acceleration levels used:
II (Result.) = 1.0 g, V = 1.0 g Critical stress = 10,333 psi (Allowable = 20,000 psi) c4
O O O Specification No. II-2288 Vendor: Pcfer to ecTuip. status sheets SUMMAlY OF Page ll. "J o f !#'/ -
,c' EQUIPMENT QUALIFICATION Rev. '
kb. II . Zimmer -
Project :;o. 4130-00 Date .
.E . iq Equipment scription h$
ia Location Qualification Number Method Results
- u. . _ . - - - _ ___ : ), _ _ _.
_ a. ._ _____ , _ _ _ _ _
lVG12YA Equivalent static analysis Accel. levels used:
lVG12YB Natural freq. : 70 IIz. 11 = 1. 0 g, 11 = .0 g, (cont'd) 1 2 1
v= 1.0 g Critical stress = 12,686 psi (allowable = 21,600 psi)
Critical deflection = 0.006" (allowable = 0.021")
IIepa filter banks P lVG05SA Static analysis Accel. levels used:
lVG05SB Natural freq.: Ily= 0.52g,11 2=0.70 g, II "II = 33.3 IIz, V = rigid 1 2 v= 0.90g Min.
- margin of safety = 2.17 Max. relative displacanent =
0.043" which will not cause leakage past gasket interface.
,, , i . --
O O O Specification No. 11-2288
SUMMARY
OF Page l}c,( of (?7 -
Vendor: Arcrican Air Filter EQUIPMENT QUALIFICATION Rev.
Mn . H. Zimmer ~
Project No. 4130-00 Date &'t I
'- fl Equipment Description h k' ia Locatiori Qualification Number Method Results
- i . . _. _ . , _ _ _ _ _ _ _ .
IIepa filters P lVG05SA Uniaxial sinusoidal test Operability (structural lVG05SB 2-8 Hz, 3.0 g input integrity) verified.
8-600 IIz, 2.0 g input Natural freq. :
Ily=H2 = 33.3 IIz V = rigid SGIS pre-filters P lVG05SA Statis analysis Limit-load analysis performed lVG05SB Natural freq.: 226 Hz and indicates failure at 366 g's Allowable stress = 22,000 psi Min. deflection nurgin of safety = 2.62 Solenoid valve & piping A lVG05SA Uniaxial sine sweep No resonances found IVG05SB l-35 Hz; input: Ily =H 2 = 4.5 g, V = 3.0 g; Sweep: 15 sec./ cycle Pseudo biaxial sine dwell Require acceleration levels:
@ 5,10,15, 21, 27, 31, 33 IIz Ily =H 2 =1.12 g, V = 1.28 g Input: Hy=H2 =4.5 g, V = 3.0 g Structural integrity and operability demonstrated.
l
- w. _ _ _ _
nv O. O Specification No. 11-2288
SUMMARY
OF Page Elik j of 7'/ -
Vendor: American Air Filter
EQUIPMENT QUALIFICATION Rev.
Wm. H. Zimmer ; -
Project No. 4130-00 Date .. .}
Equipment Description hk ia Location Qualification Results er Method '
O _S. ___ . . _ _
Solenoid Valve & Piping A lVG05SA Uniaxial Sine Sweep No resonances found.
IVGOSSB l-35 Hz; Input: Il =H y 2 = 4.5 g
, V = 3.0 g; Sweep: 15 sec/ cycle Pseudo Biaxial Sine Dwell Require acceleration levels:
@ 5, 10, 15, 21, 27, 31, 32 Hz Il y=H 2 = 1.12 g, V = 1.28 g Inpute: H y=H2 = 4.5 g V= 3.0 g Structural integrity and opera-bility denonstrated.
Moisture Separator P 1VG05SA Uniaxial Sine Sweep Natural frequencies: 26 Hz
~
IVG05SB 2-33 liz (double sweep); .
Input: Hy =H 2 = 0.2g, V = 0.lg Biaxial Randarn Motion Horiz. TRS Envelops RRS 1.25 - 31.5 Hz, 1/3 Octave Vert. TRS does not. Conserva-tive analysis at critical locations showed stresses to be within allowables:
Critical stress = 10,560 psi (allowable = 22,000 psi)
Based on equivalent static analysis.
Structural integrity verified.
Specification No. 11-2290
SUMMARY
OF Page :4 30 of I' l -
Vendor: Buffalo Forge Co.
EQUIPMENT QUALIFICATION Rev.
Wm. II . Zimmer -
Project No. 4130-00 Date -
r}
Equipment Description h$ Qualification g Location i
er Method Results
.n -
IVC 04CA Control Roxt IIVAC A Aux. Bldg. Equivalent Statis Analysis Accelerations levels used:
lVC04CB Return Fans (Peak x 1.5):
Hy =Il 2 = 11.6 g, V= 4.4 g Critical stress = 43,440 psi (allowable = 45,000 psi)
Critical deflection = 0.0044" (allowable deflection = 0.0184")
lVG01CA Reactor Building A Aux. Bldg. Sinplified Dynan c Analysis Required acceleration levels:
lVG01CB Recirculation Fans II1=II3 = 5.0 g, V= 2.0 g Critical stress = 31,537 psi (allowable = 45,000 psi Critical deflection = 0.01752" (allowable deflection = 0.0288")
lVII0lCA Service Water Punp A Service Equivalent Static Analysis Acceleration levels used (Peak IV1101CB Cooling Fan Water Pump Natural frequencies: >36 IIz x 1.5): I1)=112 =3.0g, V = 3.3g 1 'I CC Structure Critical stress = 13,560 psi (allowabic = 28,800 psi)
Critical Chflection = 0.00467" (allowable deflection = 0.062" L
q , , r 0v VJ .
O u
Specification No. 11- 2290
SUMMARY
OF. Page I h of 9/ .
Vendor:J ffalo Fo M Q. EQUIPMENT QUALIFICATION Rev.
Wm. II . ZirrJner *
/!
Project No. 4130-00 Date '
Equipment Description hI ia Location Qualification Results Number Method
__s _
IVX02CA SWGR IIcat Remval Fans A Aux. Bldg. Equivalent Static Analysis Acceleratien levels used:
lVX02CC Natural frequencies: >79 IIz !!1 = 3.0 g, 112 = 3.0 g, IVX02CC V= 3. 2 g
. Critical Stress = 5,641 psi (Allwable Stress = 32,400 psi)
Critical deflection = 0.0094" (Allowable Deflection = 0.093")
lVX04CA SWGR IIeat Rcmoval Fans A Aux. Bldg. Equivalent Static Analysis Acceleration levels used:
lVX04CB Natural frequencies: >31.4 IIz (Peak x 1.5):
lVX04CC 111 =11 2 =3.0g, V= 3.3g lVXO4CD Critical Stress = 19,022 psi 1FX04CE. (Allwable = 28,000 psi) 1VX04CF Critical deflection = 0.0281" (Allwable deflection = 0.14")
lVY01C CSCS Equip. Rocm Cooling A. Reactor Equivalent Static Analysis Acceleration levels used:
lVY02C Fans Building Natural fregrncies: >36 IIz (Peak x 1.5):
lVYO4C 111 =I1 2 =3.09, V = 3.3g Critical stress = 13,560 psi (Allowable = 28,800 psi)
Critical deflection = 0.00467" (Allwable deficction = 0.062")
Equivalent Static Analysis Acceleration levels used:
Natural frequencies: >36 IIz (Peak x 1.5):
!!1=II2=3.09, V = 3.3g Critical stress = 21,874 psi (Allwable = 28,800 psi)
Critical deficction = 0.0047" (Allwable deflection = 0.015")
m
r Specification No. 11- 2290
SUMMARY
OF Page f)(R of . - ' ' .
Vendor: Buffalo Fome__Co. P FI W W Rev. u' Mn. II . Zimmer ,i '
Project No. 4130-00 Date - f - j ' , p- l Equipment 5j Qualification N eber Description ia Location Method Results S, ..
IWO3C CSCS Equip. Rocm Cooling A Reactor Equivalent Static Analysis Acceleration levels used:
Fan Building Natural frequencies: >75 IIz (Peak x 1.5): -
111 =11 2 =3.0g, V = 3.3g
. Critical stress = 11,417 psi (Allowable = 28,B00 psi)
Critical deflection = 0.0044" (Allowable deflection = 0.038")
Vibration Isolators A Fans Equivalent Static Analysis Aodeleration levels used:
(II-2290) 111=!!2=2. 2g , V = 2.3g Critical stress = 15,762 pai (Allowable = 28,800 psi)
- Fans are to be hard mounted u
O .
O O SPecification No. 11-2293
" Vendor: Trane Co.
SUMMARY
OF Page /k " !o f :. ' l -
Mn. !! . Zimmer EQUIPMENT QUALI'FICATION Rev. .3 Project No. 4130-00 ,
Date '
. i . :- ? l Equipment Number Description hk ia Location Qualification Method Results
_ . J _ %, _ _ . _ _ _ _ _ . . . . . . . , . _ . _
IVC 02CA Control Rocm Condensing A Aux. Bldg. Detailed Dynamic Analysis IVC 02CB Units Critical stress = 3,500 psi (Allcreable = 3,500 psi)
Critical deflection = 0.0039" (Allowable deflection = 0.0352")
lVX01CA SWGR IIcat Ranoval A Aux. Bldg. Detai. led Dynamic Analysis IVX01CB Condensing Units Critical stress = 33,986 psi lVX01CC (Allowable = 34,000 psi) lVX01CD Critical deflection = 0.00198" IVX01CE (Allowable deflection = 0.0317")
IVX01CF 1Pw3J llVAC Condensing Unit A Aux. Bldg. Biaxial Randcm Motion Test IPLB4J, Control Panels for TRS envelops RRS. Structural 1PLB57 1-40 IIz integrity and operability lVC02CA/F IPLB6J verified.
IPLB7J Fragility Test Min. fragility level (randan IPLB8J wave): 11 1 =5.0g, II2=V=3.0g IPLB9J IPIrlJ
ex o r~
U d #)
(
Specification No. 11-2298
SUMMARY
OF Page lI::'fof 9/ .
Vendor: Refer to Fauip. Status Sht's.
EQUIPMENT GUALIFICATION Rev. /hi hh. II . Zimmer Project No. 4130-00 Date # ! - ['[" f } ,
Equipment Description h$
i Location Qualification Number Method Results
-a ..
IVCllX7s Control Rocm IUAC Return A Aux. Bldg. R1uivalent Static Analysis Acceleration levels used:
lVCllXB Fan Silencers (Peak x 1.5):
111 =5.7g,11 2 =11.4g, V = 4.2g Critical stress = 1,349 psi (Allwable = 1,721 psi)
Structural intergrity verified.
1FEVG001A Air Flow Monitors A Reactor Sinplified Dynamic Analysis Acceleration levels used:(Rcq'd)
IFEVG001B Building Natural frequencies: 117,405 !!z (Pcquired) :
Ily=H2 =1.09, V = 1.59 Critical stress = 3,113 psi (Allowable = 22,500 psi)
No critical deflections.
IFEVG002A Air Flow Monitors A Aux. Bldg. Sinplified Dynamic Analysis Acceleration levels used:
IFEVG002B Natural frequencies: 15,75.3, (required) :
438 IIz II1=H2=1.0g, V = 1.5g Critical stress = 13,444 psi (Allowable = 26,400 psi)
Critical deflection = 0.0831" No offect on operability.
t_
S O O
~
Specification No. 11- 2299 isuMMARY OE Page [} M" of Eg -
Vendor: Powers Regulator Co.
EQUIPMENT QUALIFICATION Rev. 60 Mn . H. Zimmer Project No. 4130-00 Date #l-l{$^O)
Equipment Description 5$
ia Location Qualification Results Number Method
- _ . . . _ _ . . _ _ _ _ z_ S -
1PLl4JA Control Rocm Vent and Air A Aux. Blgd. Simplified Dynamic Analysis / Vibration test to deternune 1PLl4JB Cond. Equipment Control Detailed Dynamic Analysis / resonant freq: 8.7, 122, 15.7, Panel Uniaxial Sine Sweep Test / 16.2 Hz. (Sweep: 0-35 IIz, 3
. Uniaxial Sine Dwell Test modes), cross-coupling noted.
Structural integrity and opera-bility demonstrated by finite elenent analysis (response spectrum) . Iland calculations supplemented the analysis:
Critical stress = 12,920 psi (Allowable = 21,600 psi deflections were insignificant.
1PM19JA Control Roan Ionization A Aux. Bldg. Simplified Dynamic Analysis / Vibration test for resonance 1PM19JB Detection Relay Panels Detailed Dynamic Analysis / search: f >35Hz.
n IPL60JA and Uniaxial Sine Sweep Test /
IPL60JB Diesel Generator Rocm Uniaxial Sine Dwell Test Structural integrity and opera-IPL60JC HVAC Control Panels bility demonstrated by finite elenent analysis (response spectrum) hand calculations supplanented the analysis (H1=H2 =1.5, V = 2.5g):
Critical stress = 9,800 psi (Allowable = 25,200 psi)
No critical deflections.
O O O Specification No. II- 2299
SUMMARY
OF. Page (D 's o f ED7 .
Vendor: Pcwers Reculator Co.
EQUIPMENT QUALIFICATION Rev. 40 Wm. II . Zimmer [ [ .1, O<t!
Project No. 4130-00 Date S C Equipment e 1 Qualification Number Descript. ion i a Location Method Results A l ._ . .. _ _ ._ __
_ _ . _ _ _ _ _2 __
1PL61JA Service Water Pump Cooling A Service Uniaxial Sine Sweep Test Closed-door case: Icwest lPL61JB Panels Water Pump 0-35 IIz fn>35 IIz response - 0.03 g's.
Structure Open-door case:
frequency = 12.2 and 17.9 IIz (Damping of 2.9 & 2.5)
Response - 0.10 and 0.23g's.
Static Analysis Acceleration levels used:
II1=0.20g, II 2=0.20g, V = 0.14g Critical section: factor of safety = 15 (min.), based on ZPA + 10% nnrgin acceleration levelo.
Operability not effected.
1PL69JA SGIS Control Panels A Reactor Uniaxial Sine Sweep Test No resonant frequencies below IPL69JB Building 0-40 IIz 35 Hz.
. Static Analysis Acceleration levels used:
11 =0.81g,11 =0.74g, V = 4.5g 1 2 (Critical stress = 36,000 psi)
Structnral integrity verified.
IPL91J SNGR IIeat Rmoval Control A Aux. Bldg. Uniaxial Sine Sweep Test Panel frequency: >33 IIz (Open or closed door case)
Door Frequency: 31.2, 31.9 112 (Damping: 2.9, 2.5%)
Response - 15h's.
L
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O Specification No. 11-2805
SUMMARY
OF Page i'i t 7, of 5'/
Vendor: Bishopric Rev. A ~ ~3 .
ht . II . Zimmer Pro 3cct No. 4130-00 Date 2f f.r Fl Equipment Description hk ia Location Qualification Results Number Method
- S 1DG07TA Diesel Oil Day Tanks P Aux. Bldg. Static Analysis Natural Freq.
1DC07TB 1A, 1B, 1C OBE/SSE Input: Hz H =H =33 2
Hy =0.2g/0.41g
- 82. l!*
, H"*
2 E!
- E Worst Stresses:
V=0.35g/0.55g Shell Bending for 1.0g Damping: 1.0% ksi o -
.65 calc ksi
cale" allow
= 2.6 24.7 Anchor Bolts o = 9.99 13.07 cale S,77,y= 63. 84.
1DG12TA Diesel Generator Cooling P Aux. Bldg. Static Analysis Natural Freq.
1DG12TB Water Reservoir Tanks SSE Input: H y =0.5g 11 - 8 7 . 5 "
- 1DB12TC 11 =0.5g 2 H2=195.
V=0.55g V=95.3 Damping: 1.0%
Worst Stresses: OBE SSE Saddle /Shell ksi ksi calc = 10.l 8.l S g y, = 24.0 29.1 t_
O O o 4
Specification No. II- 2805
SUMMARY
OF Page / - if of 69 Vendor: Bishopric EQUIPMENT QUALIFICATION Rev. 06 .
Wm. 11 . Zimmer Pro],ect No. 4130-00 Date f-/ 6- El Equipment S C e i Qualification Description i g Location Results Number fiethod
. p IDG12TA (Continued from previous Anchor Bolts
' O S
gg
=- 24.9 Tcale" - I'0 S = 13.3 ailow Nozzle /Shell o
cale
= 14.1 25.2 S
yyg = 22.6 27.4
O O O specification No. H- 2805
SUMMARY
OF Page /l4d of '5 ' /
Vendor: Bishopri EQUIPMENT QUALIFICATION Rev. dI -
Wm. H. Zimmer Project No. 4130-00 Date 'l I i" El Equipment Description l5iaS Location Qualification Number Method Results S
LWR 03TA RBCCW Expansion Tanks P Rx. Bldg. Static Analysis Natural Freq.
LWR 03TB OBE/SSE Input Hy =0.36g/0.53g("8) -Hy =14.8 H2=67.9 V-65.4U
- H =1.125g/0.9g(EO 2 Worst Stresses:
V=0.9/0.9g Anchor Bolts g , g Damping 1.0% calc S
g9 = 63.0 Tcalc "
! o = 0.97 21.8 calc S,y g = 22'.6 24.7 1DG13TA Diesel Generator Cooling P Aux. Bldg. Static Analysis Natural Freq.
1DG13TB Water Reservoir Tanks H y=H SSE Input: 2 -0.5g H1=68.Hz H2 =169.
1DG13TC V=0.55g V=239.
Damping: 1.0%
Worst Stresses: OBE SSE Saddle o, = 5.67 6.92 S =24.7 29.1 alh Nozzle /Shell o -ll.58 20.7 calc S
gygy =22.6 27.4
O O O Specification No. 11-2805
SUMMARY
OF Page I M l o f 5' 9 vendor: Bishopri EQUIPMENT QUALIFICATION Rev. 00 .
Wm. 11 . Zimmer Project No. 4130-00 Date 'l- l6 E i Equipment Description 5$ Qualification g Location i Results Number Method
g
=
- 24.9 T
eale
= 1.754 S
y
= - 13.3 1DG14TA Diesel Generator Cooling P Aux. Bldg. Static Analysis Natural Freq.
1DG14TB Water Expansion Tanks SSE Input: 11 = 0.5g 7
11 =28.6 7
H2=227. v=259.
1DCl4TC 1DGl4TD N = 0.46g 2 Worst Stresses: OBE SSE IDG14TE V = 0.7g Shell Saddle o 15.7 1DG14TF Damping: 1.0% cale=
allow"
- o cale
= 9.63 13.67 Sgg = 12.6 18.9 Anchor Bolts o = 6.03 9.57 cale S
gg = 12.6 18.9 Nozzle c e97e
= 34.1 S
allow
= 34.1 L
O O O Specification No. 11- 2805
SUMMARY
OF Page filllof @/
Vendor: Bishopri EQUIPMENT QUALIFICATION Rev. .) 0 .
Wm. II . Zimmer Project No. 4130-00 Date 2I-I~ "d' !
Equipment Description h$
1 a Location Qualification Results Number Method 1DGISTA Air Receiver Tanks P Aux. Bldg. Static Analysis Natural Freq.
1DCISTB Input: 11 =11 =0.41g ilz 1DGl5TC 1 2 11 =11 -81.1 V-297.Itz 1DG15TD V-0.55g W rat Stresses:
1D015TE Damping 1.0%
1D F lloop Stress a = 8.26 ksi S -13.70 1DC15T11 allo 1DG15TI Beam Stress a calc = 4.13 1DG15TJ ,
IDG15TK S
313ay =13.70 1DCISTL Skid Bolt (SSE) ocalc"
- S =12.60 dlow 1D00lTA Diesel Oil Storage Tanks P Aux. Bldg. Static Analysis Natural Freq.
1D001TB Input: 11 =ll -0.30g 2
1t= 49. 3 V-49.3 lbO0lTC V=0.70g Worst Stresses: SSE
{ Damping 1.0% si At Support T Ic
=13.20 S,g , -15.00 Tank is Buried In Sand L
O O O i Specification No. 11-2812
SUMMARY
OF Page lf:l3 of I.RI Vendor: C&D Batteries Co.
EQUIPMErlT QUALIFICATI0tj R e'. A1 -
ICn . II . Zimmer .? e Projoct No. 4130-00 Date +-5 .
.', l Equipment S C e 1 Qualification Number Description i a Location Res uts Method
- S _
l 1DCl3EB 125-V Battery Chargers A Aux. Bldg. Biaxial Test, Randoi:n Motion TRS Graph envclv pes required IDCl3EC Resonance Search 1-35Hz respc,ase spectra.
l Test require:: ents exceeded
! specs.
Post-Testing functional operability verifled.
J l
I J
O o O Ppecification 110. 11- 2151 1 ._
SUMMARY
OF Page ph'}of'.**
Vendor :Ealmon cn- mpe munmm Rw.
Mii . II . Z irruite r Project No. 4130-00 Date ,! 4 e I:quipment h'i C1 Qua1ification Descript. ion 1 . I,oca t ion enults N r ,
Method ca __ . __ .m - _ _ _
IVC 08SA Control Room IIVAC Air A Aux. Bldg. Static Analysin Natural Frequencies:
IVC 08Sn llandling Units Finite Element Analysis Coils: fn = 57.5tiz I"P"C Coil Support: f n"33*"
IVC 13AA Control Room IIVAC Cooling . Cabinet & Colls lit -il 2 -0.62g Coil Fin Crush Press:
IVC 13An Coils v=1.7g Damping: 1.0% ocale= 3.43P81 Sailow= 6.5P"i Nozzle Bolts acalc" 2 29 S yyjoy=20.
,Tealc= 0.81 Sa11ow=10.0 CabinetNayZ. Freq.
f n=36.I Cab. tlorat Stresses:
ksi o cate= 5.02 S,ggoy=21.6 t enic= 0.67 Sallow =10.8 Anchor Bolts:
ksi ocale"17.95 S311oy=40.0 T
cale= 5.24 So yjo,f2L.6
O)
O\_) O)
Specification No. II- 2816 Page (l'f S of G' r a
SUMMARY
OF Vendor: Bahnson .
Wm. H. Zimmer EQUIPMENT QUALIFICATION Rev. i.'
d Project No. 4130-00 Date Ii '> 7I Equipment Description hY ia I,ocation Qualification Number Method Results
_ <.-.-,n-- . . - _ - _ - - _ _ .. _ _ - -
_.,S.__ _ n __.
IVCl3YA Air Foil Dampers A Aux. Bldg. Biaxial Test, Random Motion Natural Freq.
IVCl3YB In Equipm't Freq. Range 1-40.II* Damper Blade fn"ll 3 IVCl4YA No. Reg'd Input: H1=Il2=0.62g IVC 14YB Multi-Zone Damper Blade IVC 08SA,B V=0.68g IVC 15YA
' f n=13.H2 Test Response / Input: fn*14 "
IVC 15YB IVC 16YA n .n,=20g/5g
' Functionally Operable IVC 16YB V=15g/5g IVH03AA Service Water Pump Cooling A Service Static Analysis Natural Freq.
IVH03AB System Heat Exchangers & Water Pump Finite Element Analysis Coil Bank: f n=35.4Hz IVH03AC Cooling Coils Structure Reg'd Input: II =ll =0.2g Ileader Assembly: fn"33' IVH03AD 1 2 V=0.14g Coil Support: fn=43.5H3 Damping: 1.0%
Worst Stresses: SSE Anchor Bolts:
Ocale= 9.29k Sailow= 40.
Teale" 3*09 g
Sa llow= 21.6 Nozzle Pipe:
ocale= 13.15k si Sallow = 32.4 Coil Perimeter Bolts:
ocale= 7.42 ksi Sallow = 20.0 ksi Teale = 5.64k si Sallow = 10.0 ksi L-
O O O Specification No. 11- 2816
SUMMARY
OF Page jifl0 of Ct / .
Vendor: Bahnson EQUIPMENT GUALIFICATION Rev. */
Mn. II . Zimmer
Project No. 4130-00 Date ,!
Equipment hj Qualification Number Description ia Location Method Results
- - - . = , - - - - _. Zj,_ , _ _ _ _ _
IVXO3SA SWCR IIcat Removal Air A Aux. Bldg. Static Analysis Natural Freq.
IVXO3SB Ilandling Units Finite Element Analysis Tube: fn= 60.II*
IVXO3SC Reg'd Input: Coil Support: f n=33.D IVX03SD li y=H2 =0.4 6g Worst Stresses IVXO3SE V-0.95g 1VX03SF Damping: 1.0%
Nozzle o
Bolt:
=2.96 ksi Sallow =20.0 T cale=1.045
. Sallow =10.0 IVX05AA SWCR IIcat Removal Cooling A IVXO3SA Static Analysis Natural Freq.
IVX05AB Coils IVX03SB Reg'd Input: Coils: f n=51.5U*
IVX05AC IVXO3SC li t -il =2 0. 4 6g fn =75.7 IVX05AD IVXO3SD V-0.55g Worst Stresses IVX05AE IVX03SE Damping: 1.0% Anchor Bolts IVX05AF IVXO3SF si Ucalc= 6.01 Sallow = 40.0 Tcalc= 2.47 Sallow = 21.6 IVXO6FA Air IIandling Unit Filters A IVXO3SA Plant Usage Experience and The frame and keeper slot are IVXO6FB IVXO3SB Engineering Judgement adequate to hold the light IVXO6FC IVXO3SC weight filter elements at pres-IVX06FD LVXO3SD sures much higher than an IVXO6FE IVXO3SE anticipated seismic event' in IVXO6FF IVX03SF combination with normal opera-tion.
L
O O O Specification No. 11- 2816
SUMMARY
OF Page id'/ of U/> .
EQUIPMENT QUALIFICATION Rev.
Mn. II . Zimmer -
Project No. 4130-00 Date
- Equipment Descriytion b$
ia Location Qualification Number Method Results
_S..______ , m4__. _
1WOSA CSCll-RilR Equip. Room IIeat A Rx. Bldg. Static Analysis Natural Freq.
J lWO6S Exchanger and Cooling Finite Element Analysis Coils: fn =35.211 5 IWO8A Coil Reg'd Input: fn =36.0 IWO9A =112 =0. 67g Il l Tube: fn=43.0 V=1.2g Support: f n=53.0 11eader Assembly: fn=33.
k'orst Stresses:
Beam acalc= 6.92k si Sallow = 21.6 T eale= 3.47 Sallow =10.8 Anchor Bolts Ocalc= 36.9k si Sallow = 48.6 i
teale = 11.82 Sallow = 24.3 Nozzle Pipe Stress Ocale= 13.5k si
, Sallow = 35.0 Structural Integrity Demon-strated for original qualifi-cation criteria.
Requalification to T-Quencher criteria not completed.
s
O O O Specification No. H-2816 Vendor: Bahnson
SUMMARY
OF Page N 'i'l of h!/ .
EQUIPMENT QUALIFICATION Rev. .)3 h H. Zimer #'
Project No. 4130-00 Date '. 7I Equipment Description h$
ia Location Qualification h ber Method Results 1RG10M Angle Line Strainer P Aux. Bldg. Uniaxial Sine Sweep & Multi- g-Level Qualification By 1RG20M Axis Testing:
1-33nz Sine Dwell H 2 =9.2g Octave / Minute Sweep V=6.4g Required Input: Structural Integrity (Peak x 1.5) Demonstrated Ily=H 2 =4.2g V=2.85g 1RGllMA Filter Drier P Aux. Bldg. Uniaxial Sine Sweep & g-Level Qualification By 1RGllMB Multi-Axis Sine Dwell Tes t.ing:
1RG21Md 1-33HZ H =8.8g 1RG21MB H 2 =9.2g 1RG21MC Required Input: V=6.4g 1RG21MD (Peak x 1.5) Structural Integrity 1RG21ME Hy=H2 =4.2g Demonstrated 1RG21MF V-2.85g 1RG12M Moisture-Liquid Indicator P Aux. Bldg. Pseudo-Biaxial, Sine Dwell and g-Level Qualification By 1RG22M Sine Sweep Testing:
1-33 Hz H1=4.8g H 2 =9.2g Required Input:
V=5.0g Hi"H2 M .2g Structural Integrity Demonstrated L_ .
O b J w
)
Specification No. H-2817 Page N'H of 8 '7
SUMMARY
OF EQUIPMENT QUALIFICATION Rev. OO Wm. H. Zimmer Project No. 4130-00 Date :. ; ., 4Ior' rj
(.
Equipment Description ia Location Qualification Number Method Results
. x -
IVC 05CA Control Room HVAC Standby A Aux. Bldg. Static Analysis Natural Freq.
IVC 05CB Make-Up Fan Accelerations OBE/SSE H =8 Horizontal: .37g/.62g H2 -89.HZ Vertical: 1.95g/2.70g V=115.5 Worst Stresses Motor Hold-Down Bolts: OBE/SSE Damping: 1.0% Calc. Stresses:
0.40 /0*73k si Rigid Support Considerations in the model. Allow. Stresses:
k 13.1 si/21.8k si Foundation Bolts:
Calc. Stresses:ksij 0.40 Allow. Stresses:
k 20.5 sif34.2k si Deflection: 5.5(10)-3 in.
No effect on functional opera-tion.
Fan Shaft: OBE/SSE Shear Stress: 618/838 psi Allowable: 9660/13110 psi Tensile Stress: 1207/1655 psi Allowable: 16100/21850 psi L.
.---__r _
O O O Specification No. H- 2817
SUMMARY
OF Page flEC of 91 -
Vendor: Cv1 Co.
EQUIPMENT QUALIFICATION Rev. U Mn . H. Zimmer Project No. 4130-00 Date 'l- I C- $ I Equipment Description N$
ia Location Qualification Number Method Results
_- s _
IVC 09SA Control Room HVAC Filter A Aux. Bldg. Static Analysis Natural Freq. .
IVC 09SB Packages Accelerations OBE/SSE Hy=20.3 Hz IVC 10S H: 0.5g/0.75g H2 =20.3, 35.5"*
l y,19*3 Hz 11 2: 0.34g/0.5g V: 1.9g/2.2g W rst Stresses Charcoal Screen:
Calc Avg a = 28.O ksi Damping: 1%, 2% Peak o= 48.7 Rigid Support Conditions Allow S= 60.0 Anchor Bolts:
ocale= ll.21ksi
-rcale= 2.33 Sallow = 32.4 HEPA Mount. Frame Ocale= 26.3k si Sallow = 28.2 Fan Struct. Anchor Brackets Ocale== 31.9k si S
allow 32.4 No critical deflections Structural Integrity Demon-strated t
O O O Specification No. H- 2817
" ' ^
SUMMARY
OF Page h' I of 6 ' ~/
EQUIPMENT QUALIFICATION Rev. A0 Wm. H. Zimmer ,, . -
Project No. 4130-00 Date *t d '. 'I Equipment Description h$
ia Location Qualification Number Method Results
_ _ _ _ __ M -
IVCl2AA Filter Package Heat Coils A Aux. Bldg. Uniaxial & Multi-Axis Natural Freq. .
IVC 12AB Weight: 39. bs Sine Sweep Hz Mounted w/6-3/8"O Bolts 2-50 H1 =10*N*
- 14*Il2 H2 =5.,38.
V=4., 13., 22.
g-Level Qualification By Testing:
H1=H2 =V-0.55g Structural Integrity Demonstratel IVC 93Y Filter Package Backflow A Aux. Bldg. Equivalent Static Analysis Natural Freq.
IVC 94Y Dampers Rigid Support Conditions f =22.2 D n
Damping: 0.5%, 1% Worst Stresses Blade / Shaft: ksi Accelerations OBE/SSE oc ,1c= 4.56 Horizontal: 7.3g/7.2g Sallow =24.0 2.9g/2.6g T Vertical: eale= 3.67 Sallow =14.5 Support Angle o
k calc = 25.4 si M
Sallow = 28.6 L
O O O Specification No. 11- 2834
SUMMARY
OF Page flE ' of f t .
Vendor: Automation Industries, Vitro Labs Div.
Trh . II . Zimmer EQUIPMENT QUALIFICATION Rev. '9 Projoct No. 4130-00 S C' Date #
f - [ '. II _
Equipment e 1 Qualification Number Description i Location Results Method a _
1PL12JA Essential Relay Panels A Aux. Bldg. Biaxial Random Motion 3 Freq. Natural Freq. -
1PL12JB 1A, 1B, 1C Range: 111 =12. 5,12. 7 5,12. 8,19. 5,2 0.Hz IPL12JC 1-35.UZ II -4.9,5.0,5.lIIZ 2
V=20.5,23.0,25.dIt TRS Graphs Envelope Required Response Spectra - Functional Opera-bility Verified L
O O O Specification No. 11- 2835
~
SUMMARY
OF Page [tf.3 of 6') .
Vendor: Unit Elect. Control
. EQd?.PMENT QUALIFICATION Rev. t h. '
hb. H. Zimmer ll ' ! - / }
Project No. 4130-00 Date Equipment Description NI i Location Qualification Results Number Method
= - -
- S . _ _ - - - . . _ . . . _
__ _ 1 _ _
IPL67JA Remote Shutdown Panels A Aux. Bldg. Biaxial Random Motion Test TRS Graphs ,
1PL67JB 1A, 1B Freq. Range: 1-4 0Hz Envelope Required Response Spectra - Functional Opera-bility Verified.
Natural Frequencies:
Front to Back: 8,40,80 11z Side to Side: 12.5,40 Hz O
L
O O O
-m j Specification No. 11-2836
SUMMARY
OF Page /l(3} of ,[l., i.
Vendor: Chentron Coro. .J' C EQUIPMENT QUALIFICATION Rev.
Rn. 11 . Zimmer ,,_ l..
Project No. 4130-00 Date ..; . r:c}
Equipment Description h$
ia Location Qualification Results Ilumber Method '
i - ._ ._ _ _z
_ m_. _ . _ - ._ _1-- S,- - _ _ _ _ _ - - - _ _ _ _ _ _ _
i 1PLC7JA CO2 Fire Protection Panelo P Aux. Bldg. Biaxial Random flotion Test TRS Graphs .
IPLC7JB Freq. Range: 1-4 0HZ Envelope Required Response 1PLC7JC Spectra - Functional Opera-1PLC7JD bility Verified
]
. Natural Frequencies: None in 1-100 liz range
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O o o Specification No. Il-2861
SUMMARY
OF Page ji ^ f- of 1 .
Vendor: Joy Manufacturing p , s .3 Wm. II . Zimmer Project No. 4130-00 Date '. -l Equipment Description hk ia Location Qualification Results N er Method v !L -
IVC 03CA Control Room llVAC Fans A Aux. Bldg. Statis Analysis Natural Freq. '
IVC 03CB lt. , 1B Required Input: 111 = 2775.IIZ WT = 1.96k 3;t , 3,98 112= 425.
112 = 7.88 V= 200, V = 2.9g Worst Stress Damping: 1/2% OBE Anchor Bolt (Isolator To Fan):
o calc k
" 47 4 si S,11oy = 55.0 Deflections of Shaft Acalc = 0.0062" dallow '= 0.100" IVD01CA DG Room Vent. Fan A Aux. Bldg. Static Analysis Natural Freq.
IVD01CB Wt = 2.46K Required Input: 111 = 1866.112 IVD01CC 111 = 1.6g !!2" 379-112 = 2.0g V= 146.
V = 2.2g Worst Stresses Damping: 1/2% OBE Anchor Boit (Isolator To Fan):
k O
calc = 23.6 si Sallow = 55.0 Deflection of Shaft Acalc = 0.0025 Aallow = 0.160
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o Specification No. !!-2289
SUMMARY
OF Page (2;\ of -73?. .
Vendor: Refer Below Rev. (* 0 EQUIPMENT QUALIFICATION kb. II . Zimmer Project No. 4130-00 Date 4 - \ G - T,1 Equipment S C e 1 Qualification Description i Location Results Number Method
= s. _ -
IVG03YA/B Isolation Dampers A Aux. Bldg. Equivalent Static Analysit Acceleration Levels Used:
(Pacific Power (Damper) Method fly =H2*V"77 9 Controlmatics (M.Oper) critical stress = 30,251 psi Namco (Limit Switches)) (Allowable = 34,200 psi)
Simplified Dynamic Analysis Lowest f n = 18 llz Max. Calc. Acceleration:
111= .48g, 112= .61g V = 2.4g Therefore, past analysis
( Above)by equivalent static
- ana-lysis method applies ,
lVG04YA/B Isolation Dampers A Aux. Bldg. Equivalent Static Analysis Acceleration Levels'Used:
(Pacific Power (Damper) Method !!1 = 112 " Y " 7*7 9 Controlmatics (M.Oper) Critical Stress = 30,251 psi Namco (Limit Switches)) (Allowable = 34,200 psi)
Simplified Dynamic Analysit Lowest f n = 18 11z Max. Calc. Acceleration:
11 .66g, H2" *9 V=7 =1.7 9 Therefore, past analysis (Above) by equivalent static analysis method applies. ,,,,;,
y l I Y g~ g r~s N/ %
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Specification No. 11-2298
SUMMARY
OF Page fJ of 93 Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. Co Wm . 11. Zimmer Proj,ect No. 4130-00 Date 'l - 1 "5 2 )
Equipment Description 5S ia Location Qualification Results Number Method '
1_? _ _ _ . -
lVC07Y Backdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: f y=
Damper (AIR Balance, 5-50 IIz, Input: 111 = 25 g , 33 liz, f 3 = 30 liz, Model: SND-ll6) 112 = 4.5 g, V = 2.0 g f y
= 33 Uz Uniaxial Sine Dwell @ Response: 25 g, 9.5 g, Resonant Freq. and 20 g, respectively.
Operability (Structural integrity) Demonstrated.
IVC 18YA/B Backdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: f y=
Damper (AIR Balance, 5-50 Hz, Input: Hy = 15 g , 33 liz, f 3 = 3 0 11 z ,
Modal: SND-ll6) 112 = 4.5 g, V = 2.0 g f y
= 33 Hz Uniaxial Sine Dwell @ Response: 25 g, 9.5 g, 4
Resonant Freq. and 20 g, respectively.
Operability (Structural integrity) Demonstrated.
.lVC19YA/B Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 II:
Type (AIR Balance, 5-60 liz , Input 0.4 g Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 IIz integrity) demonstrated during and after test.
No weld defects.
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Specification No. 11-2298
SUMMARY
OF Page $3 of E vendor: Refer Below EQUIPMENT QUALIFICATION RcV- 60 Wm. II . Zimmer Ll - 1 C,"
Project No. 4130-00 Date /. [
1:quipment Deucription 5$
ia 1.ocation Qualification R sults Method ,
J. -
IVC 21YA/Il llackdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: f y=
Damper (AIR Balance, 5-50 IIz, Input: 11 7 = 275 g, 33 Itz, f. = 30 liz, Model: SND-ll6) 112 = 4.5 g, V= 2.0 g. f = 3 3 f,iz .
y Uniaxial Sine Dwell Response: 25 g, 9.5 g,
, O Resonant Freq. and 20 g, respectively.
Operability (Structural integrity) Demonstrated.
IVC 22YA/B Fire Damper, Curtain P Auxi1.iary Uniaxial Sine Sweep Nat. Frequency: 37 Itz Type (AIR llalance, 5-60 11z , Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Itz integrity) Demonstrated during & after test.
No weld defects.
IVC 23YA/B Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Itz Type (AIR Balance, 5-60 liz, Input 0.4 9 Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Itz integrity) Demonstrated during & after test.
No weld defects.
IVC 25YA/B Backdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: f y=
Damper (AIR Balance, 5-50 Ilz, Input: !!y = 25 g, 3 3 112 , f ., = 3 0 11 z ,
= 3 3 fiz .
Model: SND-ll6) !!.j =4.5g, V= 2.0 g, f y
Uniaxial Sine Dwell Response: 25 g, 9.5 g, O Resonant Freq. res and 20 <lity-(pectivelEl Qperabi otructur snennr4eys nmmn c + r n t g_i_
L
O O O ;
I Specification No. 11-2298
SUMMARY
OF Page bi of 9,3 .
Vendor: Refer Below Wm. II . Zimmer EQUIPMENT 00ALIFICATION Rev. & -
Project No. 4130-00 Date N-l6-9,'
Equipment Description hk ia Location Qualification Results Number Method
_ ? _1 IVC 28Y Opposed Blade Balancin< r P Auxiliary Static Analysis Lowest f = 24.8 llz Damper (Waldinger) Acceleration Levels Used:
11 1. 0 0 g , 112 = l.00 g, V=1 =1.25 g.
Simplifled Dynamic, Analysis Lowest f = 10 5 11z AcceleraEion Levels Used:
5.0 g in all directions critical stress =
26,615 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
- Il -
.78 g, li, = .76 g, V=y = 68 g.
IVC 30YA/B Backdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: f y =
Damper (AIR Balance, 5-50 liz , Input: 111 = 2,5 g, 3 3 IIz , f = 30 IIz, 2
Model: SND-ll6) 112 = 4.5 g, V = 2.0 g. f y = 33 liz.
- Uniaxial Sine Dwell Response
- 25 g, 9.5 g,
@ Resonant Freq. and 20 g, respectively.
Operability (Structural integrity) Demonstrated.
e 9
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O O O '
4 i
Specification No. 11-2298
SUMMARY
OF Page [d of $3 Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 00 Wm. II . Zimmer Project No. 4130-00 Date Lf -l 6-Sl Equipment S C e 1 Qualification Description i a Location Results Number Method
- s _
IVC 32YA/B Backdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: f y=
Damper (AIR Balance, 5-50 Hz, Input: 11 = 2.5 g, 33 Hz, f 7 = 30 IIz ,
1 Model: SND-ll6) H2 = 4.5 g, V = 2.0 g. f y
= 33 Hz.
Uniaxial Sine Dwell Response: 25 g, 9.5 g,
@ Resonant Freq. and 20 g, respectively.
Operability (Structural 4 integrity) Demonstrated.
IVC 33YA Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 llz Balancing Damper AcceleraElon Levels Used:
(Waldinger) H 1.00 g, 11 = 1.00 g, 2
V=y =1.25 g.
Simplified Dynamic Analysh Lowest f = 29 IIz AcceleraEion Levels Used:
5.0 g in all directions critical stress =
26,615 psiX Allow.=32,000 psi)
Max. Calc. Accelerations:
11 =
.48 g, H2 = 4.82 g, V 7= 2.36 g.
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O .
O O Specification No. li-2298
SUMMARY
OF Page 8lo of 83 -
Vendor: _ n n ro ,- nninw p g p g Wm. !! . Zimmer cr Project No. 4130-00 Date 'l-\kD-o[
Equipment Description 5$
- i. Location Qualification Results Number Method '
__9 lVC33YB Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 IIz Balancing Damper AcceleraEion Levels Used:
(Waldinger) 11 = 1.00 g, 11 = 1.00 g, 7 2 V= 1.25 g.
Simplified Dynamic- Lowest f =.29 Itz Analysis AcceleraEion Levels Used:
5.0 g in all directionn
. Critical stress = 26,615 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
11 .48 g, 11 , = 1.96 g, V=7 = 62 g. '
IVC 34Y Pire Damper (AIR P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Itz Balance, Curtain Type: 5-60 liz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 IIz integrity) Demonstrated during & after Test.
No weld defects.
IVC 35Y Pire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 !!z Type (AIR Balance, 5-60 liz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 11z. integrity) Demonstrated during & after test.
No weld defects.
O O O !
Specification No. !!-2298
SUMMARY
OF Page f$ rl of $(3 -
Vendor: Refer nelow EQUIPMENT 00ALIFICATION Rev. 60 Wm. II . Zimmer Project No. 4130-00 Date 9 -l E5- E l Equipment Description hh ia Location Qualification Results Number Method, S,
lVC38Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz Type (AIR Balance, 5-60 liz, Input 0.4 g. Response: 3.50 g.
Model: 319)
- Uniaxial Sine Dwell Operability (Structural Dwell at 20 IIz Integrity) demonstrated
. during and after test.
No weld defects.
IVC 39Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Freauency: 37 IIz Type (AIR Balance, 5-60 IIz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 I!z. integrity) demonstrated during and after test.
No weld defects.
IVC 40Y Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 IIz Balancing Damper AcceleraEion Levels Used:
(Waldinger) 11 1. 0 0 g , 112 = 1.00 g, V=1 =1.25 g.
Simplified Dynamic Lowest f = 62 llz Analysis AcceleraEion Levels Used:
5.0 g in all directions Critical stress = 26,615 psi (Allowable = 32,000 psi)
Max, Calc. Accelerations:
11 7
=
.77 g, 112= .64 g, V= .87 g.
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O O .
Specification No. 11--2298
SUMMARY
OF Page B<? of '/ 3 -
Vendor: nnfor noinw EQUIPMENT QUALIFICATION Rev. GQ Mn. II. Zimmer Project No. 4130-G0 Date Af - l 6-3 \
Lquipment escdption 5$
ia Location Qualification Results Number Me dod ,
- s IVC 41Y Opposed Blade Balmicinc P Auxiliary Static Analysis Lowest f = 24.8 IIz Damper (Waldinger) AcceleraElon Levels Used:
11
- 1. 0 0 g , 112 = 1.00 g, V=1 =1.25 g.
Simplified Dynamic,Analysi Lowest f = 7 3 IIz AcceleraEion Levels Used:
5.0g in all directions Critical Stress = 26,615 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations :
11
.51g.g, 112= .62 g, V=7 = 68 IVC 42Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 IIz Type (AIR Balance, 5-60 IIz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 !!z Integrity) demonstrated during and after test.
No weld defects.
IVC 43Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 !!z Type (AIR Balance, 5-6 0 11z , Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 IIz integrity) demonstrated during and after test.
No veld defects.
L
T I 'Y y 1 I O O O Specification No. 11-2298
SUMMARY
OF Page 6Cf of $13 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 60 wm. II . Zimmer Project No. 4130-00 Date *f -l $-8f Equipment 5y Qualification Number Description ia Location Method Results IVC 44Y Opposed Blade Balanc- P Auxiliary Static Analysis Lowest f = 24.8 IIz ing Damper (Waldinger) AcceleraEion Levels Used:
11 = 1.00 g, 11 = 1.00 g, 2
V I = 1.25 g.
Simplified Dynamic, Lowest f = 17 11z Analysis AcceleraElon' Levels Used:
5.0 g in all directions.
. Critical stress = 26,615 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
.70 g, 11 .82 g,
!!y V= =3.27 g. 2=
IVC 45Y Opposed Blade P Auxiliary Static Analysis Lowest f = 24. 8 !!z .
Balancing Damper AcceleraElon Levels Used:
(Waldinger) 1. 0 g.
!!y =1.25 0 g , !!2 = 1.00 g,
, V=
Simplified Dynamic Lowest f = 17 liz.
Analysis 5.0 g in"all directions.
Critical stress = 26,615 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
.70 g, 112= .90 g, V 1=
11
, = 3.45 g.
--y------- a i i 7 i
.J v ,
1 Specification No. 11-2298
SUMMARY
OF Page 9)O og 'g3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 60 Wm. II . Zimmer Project No. 4130-00 Date N-lG-El Equipment Description
!$ Qualification g Location i Results er Method ,
' Th IVC 46Y Opposed Blade Balan- P Auxiliary Static Analysis Lowest f = 24.8 Hz cing Damper (Waldinger) AcceleraEion Levels Used:
IIy = 1.00 g, H 2 = 1.00 g, V = 1.25 g.
Simplified Dynamic. Lowest f = .7 3 IIz Analysis AcceleraElon Levels Used:
5.0 g lia all direction:, .
Critical stress = 26,615 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
11 S .82 g, II., = .79 g, 1 '
V= .95 g.
IVC 47Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 !!z Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 11 2 integrity) demonstrated during and after test.
, No weld defects.
a
- y. , ,
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Specification No. H-229 8
SUMMARY
OF Page 6 \ l of S'S .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 60 Wm. H. Zimmer Pro],ect No. 4130_00 Date N-l 6-2l Equipment escription 5$a Location Qualification Results Number Method
- S _
IVC 48Y Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 Hz Balancing Damper AcceleraEion Levels Used:
(Waldinger) H 1.00 g, H, = 1.00 g, V=y =1.25 g.
Simplified Dynamic Lowest f = 47 Hz Analysis AcceleraEion Levels Used:
5.0g in all directions Critical Stress = 26,615 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
H 1.14
- g. g, H2 = .46 g, V=y = 58 IVC 49Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) demonstrated during and after test.
No weld defects.
IVC 50Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) demonstrated during and after test.
No weld defects.
y
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O V
Specification No. II-9 2 9JL_
SUMMARY
OF Page 8ld of S Vendor: Refer B6107 EQUIPMENT QUALIFICATION Rev. dO Wm . !! . Zimmer Project No. 4130-00 Date 9-16 #$f Equipment Description 5$
ia Location Qualification Results Number Method n
. s -
IVC 51Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Itz Type (AIR Balance, S-60 11z, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 !!z integrity) demonstrated
, during and after test.
No weld defects.
IVC 52Y Opposed Blade P Auxiliary Static Analysia Lowest f = 24.8 liz Balancing Damper AcceleraEion Levels Used:
(Waldinger) 11 1.00 g, 11 = 1.00 g, V=7 =1.25 g.
2 Simplified Dynanic Lowest f = 10 5 112 Analysis AcceleraElon Levels Used:
5.0 g in all directions.
Critical stress = 26,615 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
11 .38g.g, 112= .46 g, V=7 = 81 IVC 53Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 llz Type (AIR Balance, 5-60 liz, Input 0.4 g. Response: 3.50 g.,
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 11z integrity) demonstrated during and after test.
No weld defects, t
y 7 7 ; . _ . .
g Specification No. H-2 2 9 8_ Page bl3 of 33
SUMMARY
OF vendor: Refer Below EQUIPMENT QUALIFICATION Rev. (}O Wm. H. Zimmer Project No. 4130-00 Date N -l Eb -3l !>
Equipment escription k$a Location Qualification Results
- i, Number Method '
- S lVC54Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) Demonstrated during and after test.
No weld defects.
lVC55Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz.
Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) Demonstrated during and after test.
No weld defects.
IVC 56Y Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 Hz Balancing Damper AcceleraEion Levels Used:
(Waldinger) H y = 1.00 g, H = 1.00 g, 2
V = 1.25 g.
Simplified Dynamic Lowest f = 105 Hz Analysis AcceleraEion Levels Used:
5.0 g in all directions.
Critical Stress = 26,615 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
H .38 g, H2* '40<9' V=y = 55
. g.
1
.4 i L
O O O Specification No. 11-2298
SUMMARY
OF Page @dN of 55 3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. OO Wm. H. Zimmer Project No. 4130-00 Date N -I b-3 k Equipment hj Qualification Description i Location Results Number Method e , ,
- S .
lVC57Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz. integrity) Demonstrated during and after test.
No weld defe' cts.
IVC 58Y Fird Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 'liz Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
~~
Uniaxial Sine Dwell Operability (Structural Dwell at 20 112, integrity) Demonstrated during and after test.
No weld defects.
IVC 59Y Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 Hz Balancing Damper AcceleraEion Levels Used:
(Waldinger) Hy = 1.00 g, H2 = 1.00 g, V = 1.25 g.
Simplified Dynamic Lowest f = 17 Hz Analysis AcceleraEion Levels Used:
5.0 g in all directions Critical stress = 26,615 psi. -
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
H .49 g, H 2= .75 g, V=y =2.54 g.
m
O O O i Specification No. H-2 29 8
SUMMARY
OF Page Sl50e S3 .
Vendor: Refor nnlow EQUIPMENT QUALIFICATION Rev. dO oj c t IJ 130-00 Date Ll-l 6 -M i Equipment escription hka Location Qualification Results Number Method
.s -
1 lVC61Y Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz Fire Damper, Curtain P Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) Demonstrated during and after test.
No weld defects.
IVC 62Y Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 Hz Balancing Damper AcceleraEion Levels Used:
(Waldinger) H y = 1.00 g, H2 = 1.00 g, V= 1.25 g.
Simplified Dynamic Lowest f = 47 Hz Analysis AcceleraEion Levels Used:
5.0 g in all directions Critical Stress = 26,615 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
H = .32 g, H V=
1
.58 g.
2= .40 g, IVC 63Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz.
Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz. integrity) Demonstrated during and after test.
No weld defects.
t
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Specification No. H-2298
SUMMARY
.0F Page 8lL, of i3 s Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. OO W H. Zimmer Project No. 4130 00 Date d - l 4.-9 l Equipment Description hk ia Location Qualification Results
,g N ber Method -
. s lVC64Y Opposed Blade Balanc- P Auxiliary Static Analysis Lbwest f = 24.8 Hz ing Damper (Waldinger) AcceleraEion Levels Used:
H 1.00 g, H 2 = 1.00 ~g, V=y =1.25 g.
Simplified Dynamic. Lowest f = 47 Hz Analysis AcceleraEion Levels Used:
5.0 g in all directions Critical Stress = 26,615 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
H y = .36 g, H V= .76 g.
2" '49 9' IVC 65Y Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 Hz Balancing Damper AcceleraEion Levels Used:
(Waldinger) Hy = 1.00 g, H2 = 1.00 g, V = 1.25 g.
Simplified Dynamic Lowest' f = 47 Hz Analysis AcceleraEion Levels Used:
5.0 g in all directions Critical Stress = 26,615 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
H y = .61 g, H = .93 g, 2
V= .58 g.
c t s ,
1 y
O O O .
Specification No. H-2 29 8
SUMMARY
OF Page @l1 of $3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer Project No. 4130-00 Date N -153-N k Equipment escription 5fa Location Qualification Number Method Results
.s -
IVC 66Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) Demonstrated during and after test.
No weld defe' cts.
IVC 67Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural
. Dwell at 20 Hz integrity) Demonstrated during and after test.
No wcld dofocta.
IVC 68Y Fire Damber, Curteln P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz.
Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) Demonstrated during and after test.
No weld defects. ,
IVCG9Y Backdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: f y=
Damper (AIR Balance, 5-50 Hz, Input: H 1= 25 g, 33Hz, f2 = 30 Hz, Model: SND-ll6) H2 = 4.5 g, V = 2 0 g. f y
= 33 gz Uniaxial Sine Dwell Response: 25 9, 9.5'g,and
@ Resonant Freq. 20 g, respectively.
Operability (Structural integrity) Demonstrated.
L
' F V f V O O O Specification No. H-2298
SUMMARY
OF Page 8l9 of 63 -
Vendor: Refer Below '
EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer Project No. 4130-00 Date k SI Equipment 5y Qualification Description i Location Results Number Method
.J IVC 70Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) Demonstrated during and a.fter test.
No weld defects.
IVC 71Y Fire Damper, Curtain P Auxiliary Uniaxial Sine. Sweep Nat. Frequency: 37 Hz Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) Demonstrated during and after test.
No weld defects. '
IVC 72Y Backdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: Hy=
Damper (AIR Balance, 5-50 Hz, Input H
= 4.5 g, V = i 2.
15 g,
=0 g. 33 Hz, H2 = 30 Hz, Model: SND-ll6 H V = 33 Hz 2
Uniaxial Sine Dwell Response: 25 g, 9,5 g,
@ Resonant Freg. and 20 g, respectively.
Operability (Structural integrity) Demonstrated.
o o o j
__}
Specification No. 11-2298
SUMMARY
OF Page @({ 9 of 'N3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer Project No. 4130-00 Date 4-15-81
- S C Equipment e 1 Qualification Description i a Location Results Number Method '
- s __
lVC73Y Opposed Blade P Auxiliary Static Analysis Lowest f = 24. 8 liz Balancing Damper AcceleraEion Levels Used:
(Waldinger) 11 = 1.00 g,11 2 = 1.00 g, V 7= 1.25 g.
Simplified Dyanmic- Lowest f = 87 llz Analysis AcceleraEion Levels Used:
5.0 g in all directions.
Critical stress = 26,615 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
7 .' .48 g, !!2= .62 g, 11 =
V= .68 g. ,
IVC 74Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 liz Type (AIR Balance, 5-60 IIz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 liz integrity) Demonstrated during and after test.
No weld defects.
IVC 75Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 IIz Type (AIR Balance, 5-60 Hz, I n ,;nt 0 . 4 g . Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Ilz integri ty) Demonstrated during and after test.
No weld defects.
a
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O O O Specification No. 11-2298
SUMMARY
OF Page fQ) of T3 Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 00 Mn. II . Zimmer
_'roject No. 4130-00 Date N-l 6- 31 Eqtipment Description h$
ia Location Qualification Results N wou r Method -
3 IVC 79Y Opposed Blade P Auxiliary Static Analysis Lowest f = 2 4 . 8 11z Balancing Damper AcceleraEion Levels Used:
(Waldinner) Hy = 1.00 g, H2= 1.00 g, V= 1.25 g.
Simplified Dynamic Lowest f = 13 0 !!z Analysis AcceleraEion' Levels Used:
5.0 g in all directions Critical Stress = 26,615 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
.48 g.g, 112 = .62 g, 117= =
V .72 IVC 80Y Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 Itz Balancing Damper AcceleraElon Levels Used:
(Waldinger) 11 1.00 g, II , = 1.00 g, V=1 =1.25 g.
~
Simplified Dynamic Lowest f = 87 liz Analysis AcceleraElon Levels Used:
5.0 g in all directions Critical stress = 26,615 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
11 =
.66 g, 112= .84 g, V=7 1.52 g.
O O O Specification No. 11-2298
SUMMARY
OF Page 6 M of 9,3 -
Vendor: Refer Below Rev. M Wm. H. Zimmer Project No. 4130-00 Date d-l6- Ef!
Equipment Description hk ia Location Qualification Results Number Method ,
- S lVC83Y Backdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: f y =
Damper (AIR Balance, 5-50 IIz, Input: H y = 25 g, 33 Hz, f 2 = 30 IIz, Model: SND-ll6) H 2
= 4.5 g, V = 2.0 g. f y = 33 Hz.
Uniaxial Sine Dwell Response: 25 g, 9.5 g,
@ Resonant Freq. and 20 g, respectively.
Operability (Structural integrity) demonstrated.
IVC 84Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 IIz Type (AIR Balance, 5-60 IIz, Input 0.4 g. Response: 3.50 g.
Model: 319) .
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Ilz integrity) Demonstrated during and after test.
No weld defects.
IVC 85Y Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 liz Balancing Damper AcceleraEion Levels Used:
(Waldinger) 11 = 1.00 g, 11 = 1.00 g, 2
V 7= 1.25 g.
Simplified Dyanmic Lowest f = 215 IIz Analysis AcceleraEion Levels Used:
5.0 g in all directions Critical Stress = 26,615 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
li y
= .48 g, 11 = .62 g, 2
V = 1.1 9
_f.._---- , _ _
i Specification No. H-2298
SUMMARY
OF Page [$3 of T3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 6D Wm. H. Zimmer Project No. 4130-00 Date 4-lhb Equipment Description kf ia Location Qualification Results Number Method
.5 . _ _ _ . _ . _
IVC 96Y Fire Damper, Curtain P Auxiliary Biaxial Random Motion TRS Envelopes RRS Type (Ruskin, Model: 1-40 Hz, spaced at 1/3 Structural integrity and NIBD-23) octave, operability verified Biaxial Sine Beat Structural integrity and 1-32 Hz, Input 3.0.g, operability verified.
Beats at 1/2 octave.
IVC 97Y Fire Damper, Curtain P Auxiliary Biaxial Random Motion TRS Envelopes RRS Type (Ruskin, Model: 1-40 Hz, spaced at 1/3 Structural integrity and NIBD-23) octave. operability verified.
Biaxial Sine Beat Structural integrity and 1-32 Hz, Input 3.0 g, operability verified beats at 1/2 octave.
IVC 98Y Fire Damper, Curtain P Auxiliary Biaxial Random Motion TRS Envelopes RRS Type (Ruskin, Model: 1-40 Hz, spaced at 1/3 Structural integrity and NIBD-23) octave. operability verified.
Biaxial Sine Beat Structural integrity and 1-32 Hz, Input 3.0 g, operability verified.
beats at 1/2 octave.
lVD04YA/B/ Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz C Typ'e (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) Demonstrated during and after test.
No weld defects.
u
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V n
s/
I Specification No. 11-2298
SUMMARY
OF Page hc7d of 33 -
Vendor: nnfor nninw EQUIPMENT QUALIFICATION Rev. 6d Wm . II . Zimmer Project No. 4130-00 Date 4-l5 El Equipment 5 Qualification Description i Location Results Number Method
- 3 _ . _ _ __'
IVD05YA/B Backdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: 31.7 IIz Damper (AIR Balance, 5-50 IIz, Input 4.0 g,(Ibrz) 3 2. 0 11z , 32. 7 IIz .
Model: SNB:116 ,
2.0 g. (Vertical)
Uniaxial Sine Dwell Response: 20 g, 20 g, 189,
@ Resonant Preg. respectively. Operability (Structural integrity) demonstrated.
'iVD06YA/B/C Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 liz l Type (AIR Balance, 5-60 liz, Input 0.4 g. . Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 !!z integrity) Demonstrated during and aster test.
No weld defects, lVD09YA/B/C External Counter P Auxiliary Static Analysis Currently being relocated.
Balance Gravity Shutta Qualification pending.
(Ruskin, Model:CBS-7) h
O O ul Specification No. 11-2298 vendor: Refer Below
SUMMARY
OF Page [$96 of T?, ,
Wm. 11 . Zimmer p R 00 Pro-j ect No. 4130-00 Date 'f - } 6- S l Equipment Description 5$
i Location Qualification Number Method Results 3 .
IVG05YA/B Backdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: 31.7 IIz Damper (AIR Balance, 5-50 liz, Input 4.0 g.(IIorz) 32.0 IIz, 32.7 IIz Model: SND-116) 2.0 g. (Vert.)
Uniaxial Sine Dwell Response: 20 g, 20 g,18 g,
@ Resonant Freq. respectively.
Operability (Structural integrity) demonstrated.
IVX0lYA/B/C Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 !!z Type (AIR Balance, 5-60 IIz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Itz integrity) Demonstrated during and after test.
No weld defects.
IVX02YA/B/C Backdraft Isolation P Auxiliary Uniaxial Sine Sweep Nat. Frequencies: 31.7 liz, Damper (AIR Balance, 5-50 IIz, Inpu t 4 . 0 g , (IIorz) 32.0 IIz, 32.7 liz.
Model: SND-116) 2.0 g. (Vert.)
Uniaxial Sine Dwell Response: 20 g, 20 g, 18g,
@ Resonant Freq. respectively.
Operability (Structural integrity) demonstrated.
y l' ! i 1 .
j O O O Specification No. 11-2298
SUMMARY
OF Page 39/o of 'A3 vendor: Refnr Below EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer Project No. 4130-00 Date 'l-I6*b'l Equipment Description 5$
ia Location Qualification Results N d er Method,
__s. -- - - - _ _ .
1VX03YA/B Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 liz.
Type (AIR Balence, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural
, Dwell at 20 IIz integrity) Demonstrated i
during and after test.
No weld defects.
IVXO4YA Opposed Blade P Auxiliary Statilc Analysis Lowest f = 24.8 112.
Balancing Damper AcceleraEion Levels Used:
(Waldinger) 11 1.00 g, H 2= .00 g, V=1 =1.25 g.
Simplified Dynamic Lowest f = 215 Hz ~
Analysis AcceleraEion Levels Used:
5.0 g in all directions Critical Stress = 26,615 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
11
.48g.g, H2= .62 g, V=1 = 68
3r-O O O ,
i
__ a Specification No. H-2 29 8
SUMMARY
OF Page F%r7 of 75 Vendor: nnfar noinw Rev. 60 EQUIPMENT QUALIFICATION Wm. H. Zimmer Project No. 4130-00 Date 'f- l 53- b!
Equipment Description hk ia Location Qualification Results ber Method
. s __
IVX04YB Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 Hz.
Balancing Damper AcceleraEion Levels Used:
(Waldinger) H y = 1.00 g, H = 1.00 g, 2
V= 1.25 g.
Simplified Dynamic Lowest f = 215 Hz.
Analysis '
AcceleraEion Levels Used:
5.0 g's, in all directions Critical stress = 26,615 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
H y = .37 g, H = .43 g, 2
. Vw .55 g.
x ,
y ,
o
@ U Cm.J
(
Specification No. H-2 2 9 8
SUMMARY
OF Page $$8 of EN3 .
Vendor: Refer Below Rev. CO EQUIPMENT QUALIFICATION Wm. H. Zimmer Project No. 4130-00 Date N l k3- 2 l Equipment Description hk i Location Qualification Results Number Method
.= .-- --
il . . __ .~. . __ __'_ __
IVX05YA/B Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz l Type (AIR Balance, 5-60 Hz, Input 0.4 g Response: 3.50 g.
Model: 319) l Uniaxial Sine Dwell Operability (Structural l Dwell at 20 Hz integrity) Demonstrated during and after test.
No weld defects, lVX06YA/B/ Fire Damper, Curtain P Auxiliary Uniaxial Sine. Sweep Nat. Frequency: 37 Hz.
C Type (AIR Balance, Md1 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) Demonstrated during and after test.
No weld defects.
IVX07Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 37 Hz Type (AIR Balance, 5-60 Hz, Input 0.4 g. Response: 3.50 g.
Model: 319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) Demonstrated during and after test.
No weld defects.
IVX09Y Fire Damper, Curtain P Auxiliary Uniaxial Sine Sweep Nat. Frequency: 27 Hz.
Type (AIR Balance, Md3 5-60 Hz, Input 0.4 g. Response: 3.50 g.
319)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) Demonstrated during and after test.
No weld defects.
/~ - /- rx
(
C ',
. -1 Specification No. H- 2298
SUMMARY
OF Page bEi of 93 .
Vendor: Refer Below EQUIPMENT QUALIFICATI0fJ Rev. OO Wm. H. Zimmer Project No. 4130-00 Date 'f - l bd Equipment Description hk ia Location Qualification Results Number Method S .. _
lVX11Y Fire Damper (Ruskin, P Auxiliary Biaxial Random Motion TRS Envelopes RRS Curtain Type, Model: 2 , 1-40 Hz, spaced at 1/3 Structural integrity and NIBD-23) octave, operability verified Biaxial Sine Beat Structural integrity and 1-32 Hz, Input 3.0 g, operability verified.
beats at 1/2 octave.
IVX12Y Fir Damper (Ruskin, P Auxiliary Biaxial Random Motion TRS Envelopes RRS Cur ain Type, Model: 1-40 Hz, spaced at 1/3 Structural integrity and NIBD-23) octave. operability verified.
Biaxial Sine Beat Structural integrity and 1-32 Hz, Input 3.0 g. operability verified.
beats at 1/2 octave.
lVYO3Y Opposed Blade Balanc- P Reactor Uniaxial Sine Sweep Nat. Frequency: 36 Hz.
ing Damper (Waldinger) 5-60 Hz, Input 0.4 g. Response: 2.78 g.
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz. integrity) Demonstrated during and after test.
No weld defects.
IVY 05Y Opposed Blade P Reactor Uniaxial Sine Sweep Nat. Frequency: 26 Hz.
Balancing Damper 5-60 Hz, Input 0.4 g. Response: 2.78 g.
(Waldinger)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz integrity) demonstrated during and after test.
No weld defects.
T 8 i i 7 v O O O Specification No. H-2298
SUMMARY
OF *Page B BS of 73 3 -
Vendor: nnfor nolnw EQUIPMENT QUALIFICATION Rev. CO Wm. H. Zimmer Project No. 4130-00 Date 4-l5 'd)
Equipment !$ Qualification Number Description gg Location Method , Results
/_ _1 lVYO7Y Opposed Blade P Reactor Uniaxial Sine Sweep Nat. Frequency: 36 Hz.
Balancing Damper 5-60 Hz, Input 0.4 g. Response: 2.78 g.
(Waldinger)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz. integrity) Demonstrated during and after test.
No weld defects.
IVY 10Y Opposed Blade P Reactor Uniaxial Sine Sweep Nat. Frequency: 36 Hz.
Balancing Damper 5-60 Hz, Input 0.4 g. Response: 2.78 g.
(Waldinger)
Uniaxial Sine Dwell Operability (Structural Dwell at 20 Hz. integrity) Demonstrated during and after test.
No weld defects.
l l
L
y- 1 1 1 r i y O O O .
Specification No. 11-2868
SUMMARY
OF Page 63) of S3 .
Vendor: nefer Below_
EQUIPMENT QUALIFICATION Rev. DO Wm . !! . Zimmer Project No. 4130-00 Date 4 ?> l Equipment 5j Qualification Number Description ia Location Method Results
- -_P _
IVA0lY Opposed Blade Bal- W/S Auxiliary Static Analysis Nat. Freq.> 33 liz.
ancing Damper (AWV Acceleration Levels Used:
Oamper), ITT (M.Oper.) 117 = 1. 0 g , 112 = 1.0 g, Namco (L. Switch)) -
V = 3.0 g.
Simplified Dynamic. Lowest f = 4 3 IIz .
Analysis AcceleraEion' Levels Used:
5 g's in all directions.
Max. Stress = 17.269 psi (Allowable = 19,200 psi) 1VA02Y Opposed Blade Bal- W/S Auxiliary Static Analysis Lowest f = 24. 8 IIz .
. ancing Damper (AWV AcceleraEion Levels Used:
Camper), ITT (M.Oper.) 11 1.00 g, 11 = 1.00 g, Namco (L. Switch)) V=1 =1.25 g's 2 Simplified Dynamic Lowest f t 4 0 IIz . Limit Analysis Load Ana2ysis performed with a resulting allow.>
5.0 g as compared to a ma> .
calc. acceleration of 0.95 g.
IVC 0lYA/B Butterfly Isolation A Auxiliary Static Analysis Nat. Freq. > 3 3 IIz .
Damper (AWV (Damper), Acc. Levels Used:
ITT (M. Oper.), Namco 11 1.0 g, 11 (L. Switch)) V=7 =1.25 g's 2= 1.0 g, Static Analysis Lowest f = 83.7 liz Acc. Lev 01s Used:
11 1 = 1.0 g, II2 = 1.0 g, s E 58.4 Mi?('A110#."U1 f.YRat)
fs /~'N (T V V V l
+
Specification No. 11-2868
SUMMARY
OF Page !33.D of 9 ?> -
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. OC Wm. II . Zimmer Project No. 4130-00 Date 4-15 's1 Equipment sedpdon hka Location Qualification Results Number Method L L _ __ __ _ _ _ _ _ _' _
lVC02YA Butterfly Isolation A Auxiliary Static Analysis Nat. Freq. > 33 Itz.
Damper (AWV (Damper) Acceleration Levels Used:
ITT (M.Oper), Namco if = 1.0 g, 112 = 1.0 g, 1
(L. Switch)) V= 1.25 g.
- Simplified Dynamic Lowest f = 111 11z .
Analysis AcceleraEion Levels Used:
11 = 1.0 g, 117 = 1.0 g, 7
V= 1.25 g.
Critical stress = 18,467 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration 11 = .66 g, II,, = .52 g, V 1=.67 g.
lVC02YB Butterfly Isolation A Auxiliary Static Analysis Nat. Preg. > 33 Ilz.
Damper (AWV (Damper) Acceleration Levels Used:
ITT (M.Oper.), Namco 117 = 1.0 g, !!2 = 1.0 g, (L. Switch)) V = 1.25 g.
Simplified Dynamic Lowest f > = 111 112 Analysis AcceleraElon Levels Used:
11 1.0 g, H 2 = 1.0 g, V=1 =1.25 g.
Critical stress = 18,467 psi. (Allow. = 19,200 psi)
Max. Calc. Acceleration:
!!y = 67.66g.g, 112= .85 g, V= .
J r I I : I r~~
O O O ,
Specification No. H-2968
SUMMARY
OF Page h33) of $6 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. CO wm. H. Zimmer Project No. 4130-00 Date #f-l 6- 7l Equipment Description 5$
ia Location Qualification Results Number Method
- S, IVC 05Y Butterfly Isolation A Auxiliary Static Analysis Nat. Freq . > 33 Hz .-
Damper (AWV (Damper) Acceleration Levels Used:
ITT (M. Oper), Namco H 1.0 g, H 2 = 1.0 g,-
(L. Switch)) V=y =1.25 g.
Simplified Dynamic, Lowest f = 58 Hz Analysis AcceleraEion' Levels Used:
H y = 1.0 g, H = 1.0 g, 2
V = 1.25 g.
Critical stress = 18,467 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
H y = .50 g, H = .42 g, 2
V= .47 g.
IVC 06Y Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 33 Hz Balancing Damper (AWV Acceleratbn Levels Used:
(Damper), ITT (M.Oper) Hi = 1.0 g, H2 = 1.0 g, Namco (L. Switches)) V= 3.0 g.
. Simplified Dynamic Lowest f = 43 Hz Analysis AcceleraEion Levels Used:
5.0 g in all directions.
Critical stress = 17,269 psi. (Allow. = 19,200 psi)
Max. Calc. Accelerations:
H 2.3g.g, H2 " 1*49 9' V=y = 75 r
y y t i O O O St. .cificgtign be.yl-2868
SUMMARY
OF Page 8,39 of IS -
Vendor:
EQUIPMENT QUALIFICATION Rev. DO Wm. II. Zimmer Project No. 4130-00 Date ll- k h 7I Equipment Description 5$ Qualification g Location i sults er Method ,
._p. _ _ .
IVC 08YA Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 33 Itz.
Balancing Damper (AWV, Acceleration Levels Used:
(Damper), ITT (M.Oper) 117 = 1.0 g, 112 = 1.0 g, Namco (L. Switches)) V = 3.0 g.
Simplified Dynamic, Lowest f = 4 3 IIz .
Analysis AcceleraEion i.evels Used:
5.0 g in all directions.
Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
. 11 7
= 1. 4 g , 11 2 = 2.38 g, V= .68 g.
IVC 08YB Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 3 3 !!z .
Balancing Damper (AWV Acceleration Levels Used:
(Damper) ITT (M. Oper) 11
= 1.0 g, H2= 1.0 g, Namco (L. Switches)) V 7= 3.0 g.
Simplified Dynamic Lowest f = 4 3 11z .
Analysis AcceleraElon Levels Used:
5.0 g in all directions.
Critical stress = 17,269 psi.
'(Allowable = 19,200 psi)
Max. Calc. accelerations:
11 .95 g, H 2 = 1.37 g, V= 1 = . 68 g.
l
y I i , . t ;
p) c p N d Specification No. 11-2868
SUMMARY
OF Page fj{$ of -{3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer m
,l-IC~Ol Project No. 4130-00 Date Equipment Description h$
ia Location Qualification Results Number Method
- s __
1VC09YA/B/ Opposed Blade P Auxiliary Static Analysis L6 west f = 2 4 . 8 IIz .
C/D Balancing Damper (AWV AcceleraEion Levels Used:
(Damper), ITT (M.Oper) IIy= 112 = 1.00 g,V =1.25 g.
Namco (L. Swi tches ) )
Simplified Dynamic Analysh Lowest f = 36 liz.
AcceleraEion Levels Used:
11 (Result.) = 3.3 g, V= 5.0 g.
Critical Stress = 13,330 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
11 1= .48 g, 112 =.85 g, V =.85 g.
IVC 10YA Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 IIz Balancing Damper (AWV AcceleraEion Levels Used:
(Damper), ITT (M.Oper) 11 = 11 = 1.00 g, V =
Namco (L. Switches) lh25 g.2 Simplified Dynamic Lowest f = 213 IIz Analysis AcceleraEion Levels Used:
II (Result.) = 3.0 g, V = 5.0 g.
Critical stress = 13,330 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
11 1
=
.67 g, H2 * *0 9
V= .85 g.
1 O O O t L
i Specification No. H-2868
SUMMARY
OF Page 63G of i3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 06 Wm. H. Zimmer Project No. 4130-00 Date '}-f6-2l Equipment Description h$
ia Location Qualification Results Number Method -
9 ,, __ -
lVC10YB Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (AWV Acceleration Levels Used:
(Damper) ITT (M.Oper), Hy = 1.0 g, H2 = 1.0 g, Namco (L. Switch)) V = 3.0 g.
Simplified Dynamic - Lowest f = 43 Hz.
Analysis AcceleraEion Levels Used:
5.0 g in all directions.
- Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
Hy =
.66 g, H2 " 1*17 9' V= .69 g.
IVC 10YC Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 Hz.
l . Balancing Damper (AWV AcceleraEion Levels Used:
- (Damper) ITT (M.Oper), H y =H2 = 1.00 g, V =1.25g Namco (L. Switch))
Simplified Dynamic Lowest f = 213 Hz.
Analysis AcceleraEion Levels Used:
H(Result.) = 3.0 g, V = 5.0 g.
Critical Stress = 13,330 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
H .67 g, H 3 = 1.13 g, V=y = 85 g. '
3
y T i . , 1 r-O O O a
Specification No. 11- 2868
SUMMARY
OF Page B 3'7 of 23 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. OO Wm . II . Zimmer '
Project No. 4130-00 Date 'l-l 5- 8)
Equipment hj Qualification ^~
Number Description ia Location Results
. s Method.
IVC 10YD Opposed Blade P Auxiliary Static Analysis Lowest f = 2 4 . 8 liz .
Balancing Damper (100/ . I AcceleraEion Levels Used:
(Damper) ITT (M.Oper.) II y = 11 = 1.00 g, V=1.'25g.
2 Namco (L. Switch))
Simplified Dynamic Lowest f = 213 liz.
AcceleraEion. Levels Used:
II (Result . ) = 3.0 g, V = 5.0 g.
Critical stress = 13,330 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
II = .67 g, 11 = .85 g, I 2 V= .85 g.
IVCllYA Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 33 liz .
Balancing Damper (AWV Acceleration Levels Used:
(Damper) ITT (M.Oper) 111 = 1.0 g, !!2 = 1.0 g, Namco (L. Switch)) V = 3.0 g.
Simplified Dynamic Lowest f = 4 3 IIz .
Analysis AcceleraEion Levels Used:
5.0 g in all directions.
Cri tical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
11 .66 g, 112= .84 g, V=1 = 68 g.
e
y r- 1 1 1 ,
r--
O O O Specification No. H-2 8 6 8
SUMMARY
OF Page 63X of $2 vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 60 W. U- ZiMMGE Proj,ect No. 4130-00 Date 'l-l $- R$
Equipment 5y Qualification Number Description ia Location Method
- Results
. s IVCllVB Opposed Blade A Auxiliary Static Analysis Nat. Freq.> 33 Hz.
Balancing Damper (ANV Acceleration Levels Used:
(Damper) ITT (M.Oper) Hy = 1.0 g, H 2 = 1.0 g, Namco (L. Switch) V = 3.0 g.
, Simplified Dynamic Lowest f = 43 Hz.
Analysis 3.cceleraEion' Levels Used:
5.0 g in all directions.
Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Acc.mlerations:
H 1.5 g, H = 2.09 g, V=y =1.17 g.
2 lVC17YA Opposed Blade A Auxiliary Static Analysis Nat. f req . > 33 Hz.
Balancing Damper (AWV El . 591'--7" Acceleration Levels Used:
(Damper) ITT (M.Oper) H y = 1.0 g, H = 1.0 g, 2
Namco (L. Switch)) V = 3.0 g.
Simplified Dynamic Lowest f = 43 Hz.
Analysis AcceleraEion Levels Used:
5.0 g in all directions.
Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
H y = 2.93 g, H 2 = 1.8 g, V= 1.2 g.
n
1 O O O ,
- - i Specification No. H-2868
SUMMARY
OF Page 639 of 7,3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 60 Wm. H. Zimmer 4 .
Project No. 4130-00 Date N -l EE- 87 Equipment Description 5{
ia Location Qualification Results Number Method . .
. ____ s IVC 17YB Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (ANV Acceleration Levels Used:
(Damper) ITT (M.Oper) H y = 1.0 g, H = 1.0 g, 2
Namco (L. Switch)) V = 3.0 g.
Simplified Dynamic. Lewest f = 43 Hz.
Analysis AcceleraEion Levels Used:
5.0 g in all directions.
Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
- Hy = 2.93 g, H2 = 1.8 g, V= .68 g.
IVC 20YA Opposed Blade A Auxiliary Static Analysis Nat. Freq.> 33 Hz.
Balancing Damper (AWV Acceleration Levels Used:
r amper) ITT (M.Oper),
Hy = 1.0 g, H2 = 1.0 g, Namco (L. Switch)) V = 3.0 g.
Simplified Dynamic Lowest f = 43 Hz.
Analysis AcceleraEion Levels Used:
5.0 g, in all directions Critical stress = 17,269 l psi.
l (Allowable = 19,200 psi)
Max. Calc. Accelerations:
l Hy =
.66 g, H2" '84 9' V= .66 g.
I L
y i 1 , r- ,
y i
O O O i I
- - i Specification No. H-2868
SUMMARY
OF Page @'lO of Y33 .
Vendor: Refer nelow EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer Project No. 4130-00 Date '[-f $- fl Equipment Description hk ia Location Qualification Results Number Method '
- L. __.
lVC24YB Opposed Blade A Auxiliary Static Attalysis Nat. Freq. > 33 Hz.
Balancing Damper (AW/ Acceleration Levels Used:
(Damper) ITT (E.Oper.) Hy = 1.0 g, H2 = 1.0 g, Namco (L. Switch) V = 3.0 g.
Simplified Dynamic. Lowest f = 4.3 Hz Analysis AcceleraEion Levels Used:
5.0 g in all directions.
- Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
H 1.54 g, H = .84 g, V=y = 68 g.
2 IVC 26Y Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (ANV Acceleration Levels Used:
(Damper) ITT (M.Oper), Hy = 1.0 g, H2 = 1.0 g, Namco (L. Switch)) V = 3.0 g.
Simplified Dynamic Lowest f = 43 Hz.
Analysis AcceleraEion Levels Used:
5.0 g in all directions.
Critical stress = 17,269 psi. {
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
U .64g.g, H2= .62 g, V=1 = 95
y ,
y O O O Specification No. 11-2868
SUMMARY
OF Page hkfof f53 .
Vendor: Refer Below Rew M Wm. II . Zimmer Pro],ect No. 4130-00 Date 'l -l 6 ~ NI Equipment Description h$
ia Location Qualification Number Method Results
. s .
IVC 20YB Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (AWV Acceleration Levels Used:
(Damper) ITT (M.Oper)
Namco (L. Switch))
- 11 V=1 1.0g.g, H2 = 1.0 g,
=3.0 Simplified Dynamic. Lowest f = 4 3 IIz ,
Analysis AcceleraEion Levels Used:
5.0 g in all directions.
Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
11 1. 5 4 g , 11 = .84 g, V= 1 = 68 g.
2 IVC 24YA Opposed Blade Balan- A Auxiliary Static Analysis Nat. Freq. > 33 Hz.
cing Damper (AWV, Acceleration Levels Used:
(Damper) ITT (M.Oper.) H 1.0g.g, H2 = 1.0 g,
, Namco (L. Switch)) V=y =3.0 Simplified Dynamic Lowest f = 43 Hz.
Analysis AcceleraEion Levels Used:
5.0 g in all directions.
2 Critical stress = 17,269 psi.
(Allouable = 19,200 psi)
Max. Calc. Accelerations:
11 .66 g, H *
- 9' V=1 = 66 g.
2
__7-____ , ,
O O O Specification No. H-2868
SUMMARY
OF Page Ba'[r0 of 'r$ 3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer Project No. 4130-00 Date d - f 97- E* l Equipment Description h$
ia Location Qualification Results Number Method -
. 3 IVC 27Y Opposed Blade A Auxiliary Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV AcceleraEion Levels Used:
(Damper) ITT (M.Oper) H y =H = 1.00 g, V=1.25g 2
Namco (L. Switch))
Simplified Dynamic Lowest f = 173 Hz.
Analysis ,
AcceleraEion Levels Used:
H(Result.) = 3.0 g, V = 5.0 g.
, Critical stress = 13,330 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
H .67g.g, H2= .85 g, V=y = 85 i
IVC 29YA/B Opposed Blade A Auxiliary Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV AcceleraElon Levels Used:
(Damper) ITT (M.Oper), Hy=H2 = 1.00 g,V=1.25g.
- Namco (L. Switch))
Simplified Dynamic Lowest f = 173 Hz.
Analysis AcceleraEion Levels Used:
H ( Result . ) = 3.0 g, V = 5.0 g.
Critical stress = 13,330 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
H y = .67 g, H = .85 g, 2
V= .85 g.
y- r 1 ; r -
y i
, O O O i
. .._J Specification No. H-2 8 6 8
SUMMARY
OF Page (18lSof 93 .
Vendor: Rnfor nelow EQUIPMENT CUALIFICATION Rev. 60 Wm. H. Zimmer .2 Project No. 4130 00 Date 4 -l 6- El Equipment hj Qualification .
Ibunber Description ia Location Method Results s, ._
IVC 31YA Opposed Blade A Auxiliary Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV AcceleraEion Levels Used:
(Damper) ITT (M.Oper) Hy=H2 = 1.00 g, V=1.25g, Namco (L. Switch))
Simplified Dynamic Lowest f = 173 Hz.
Analysis . AcceleraEion Levels Used:
H (Result. ) = 3.0 g, V = 5.0 g.
Critical stress = 13,330 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
H y = .48 g, H = .62 g, 2
V= .85 g.
IVC 31YB Opposed Blade A Auxiliary Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV AcceleraEion Levels Used:
( Dai..per ) ITT (M.Oper.) H y =H2 = 1.00 g, V=1.25g, Namco (L. Switch))
Simplified Dynamic Lowest f = 48 Hz.
Analysis AcceleraEion Levels Used:
H(Result.) = 3.0 g, V = 5.0 g.
Critical stress = 13,330 psi.
Allowable = 19,200 psi)
Max. Calc. Accelerations:
H .48g.g, H2= .62 g, V=y = 85 a
~~~~
i $ 1 s T y O O O Specification No. II-2868
SUMMARY
OF Page 84 N of '$3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 60 wm. II. Zimmer Prolect No. 4130-00 Date 'l - l 5- Rl Equipment Description 5$
ia Location Qualification Results Namber Method
. s -
IVC 36Y Opposed Blade A Auxiliary Static Analysis Lowest f = 24. 8 !!z . i Balancing Damper (AWV AcceleraEion Levels Used:
7 = 112 = 1.00 g, V=1.25g (Damper) ITT (M.Oper) 11 Namco (L. Switch))
Simplified Dynamic Lowest f = 39 liz .
Analysis AcceleraEion Levels Used:
II ( Resul t . ) = 3'.0 g, V= 5.0 g.
Critical stress = 13,330 psi (Allowable = 19,200 psi)
Max. Calc. Accelerations: i 11 =
. 6 7 g , 112= .85 g, V=7 .85 g.
IVC 37Y Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 3 3 IIz .
Balancing Damper (AWV Acceleration Levels Used: -
(Damper) ITT (M.Oper), 11 = 1.0 g, 11 = 1.0_g, ;
2 Namco (L. Switch) V 1= 3.0 g.
Simplified Dynamic Lowest f = 43 liz.
Analysis AcceleraEion Levels Used:
5.0 g in all directions.
Critical stress = 17,269 psi.
(Allowabic = 19,200 psi)
Max. Calc. Accelerations:
11 .86 g, 11 2 = 1.83 g, V=7 =1.12 g.
q r c . . q O O O i Specification No. 11- 2868
SUMMARY
OF Page @d3of VNs -
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. OD h .11.
Zimmer q q -, g g Pro]ect No. 4130 00 Equipment Description hI ia Location Qualification Results 7
Number Method '
- S IVC 82Y Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 33 112.
Balancing Damper (AWV Acceleration Levels Used:
(Damper) ITT (M.Oper), H y = 1.0 g, 11 = 1.0 g, 2
Namco (L. Switch)) V = 3.0 g.
Simplified Dynamic. Lowest f = 4 3 IIz .
Analysis AcceleraEion Levels Used:
5.0 g, in all directions.
Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max . Calc. Accelerations :
11 =
.83 g, 112 = 1.24 g, V=7 1.65 g.
IVC 86Y Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 3 3 IIz .
Balancing Damper (AWV Acceleration Levels Used:
(Damper) ITT (M.Oper) Hy = 1.0 g, H2 = 1.0 g, Namco (L. Switch)) V = 3.0 g.
Simplified Dynamic Lowest f = 4 3 IIz .
Analysis AcceleraEion Levels Used:
5.0 g.in all directions.
Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
II y = 1.50 g, 11 2 = 1.59 g, V= .75 g.
t!
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V x ,
Specification No. 11-2868
SUMMARY
OF Page f% b of $3 .
Vendor: nnfor nelow Mn. II . Zimmer UFmg Rev. d'k Proj,ect No. 4130-00 DM YkY'l /
Equipment Description h$
ia Location Qualification Results N d er Method
- 9 .
IVC 87Y Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 liz.
Balancing Damper (AWV AcceleraEion Levels Used:
(Damper) ITT (M.Oper.) 11 = 11 2 = 1.00 g, V=1.25g.
' 1 Namco (L. Switch))
Simplified Dynamic Lowest f = 119 liz.
Analysis ,
AcceleraEion Levels Used:
II(Result.) = 3.0 g, V = 5.0 g.
Critical stress = 13,330 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
II .43 g, 112= .41 g, V=y = 95 g.
IVC 88Y Opposed Blade P Auxiliary Static Analysis Lowest f = 2 4 . 8 li z .
Balancing Damper (AWV El.525'-7" AcceleraEion Levels Used:
(Damper) ITT (M.Oper), 11 =H .00 g, V=1.25g.
1 2 Namco (L. f$ witch))
Simplified Dynamic Lowest f = 17 2 IIz .
Analysis AcceleraEion Levels Used:
II(Result ) = 3.0 g, V = 5.0 g.
Critical stress = 13,330 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
11 .42 g, 11 2
~41 9' V=7 = 95 g.
y i- 1 : 1 y
O O O Specification No. 11--2868
SUMMARY
OF Page (dN9 of 5f 3 Vendor: Refer Below F Rev. M Mn. II . Zimmer Project No. 4130-00 Date b-l6"b Equipment Description 5$ Qualification Number ig Location Method
- Results
- S IVD0lYA/B/ Opposed Blade A Auxiliary Static Analysis Lowest f = 24.8 Itz.
C/D/E/F Balancing Damper (AWV AcceleraEion Levels Used:
(Damper), ITT (M.Oper) 111 = 112 = 1.00 g, V=1.25g.
Namco (L. Switch))
Simplified Dynamic Lowest f = 41 liz Analysis AcceleraEion. Levels Used:
II ( Result . ) = 3.0 g, V = 5.0 g.
Critical Stress = 13,330
. psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
. II .36g.g, 112= .48 g, V=y = 95 lVD02YA/B/ Opposed Blade A Auxiliary Static Analysis Nat. Freq. > 3 3 IIz .
D/E/F Balancing Damper (AWV Acceleration Levels Used:
(Damper), ITT (M.Oper) 11 = 1.0 g, !! = 1.0 g, 7 2 Namco (L. Switch)) V = 3.0 g.
Simplified Dynamic Lowest f = 4 3 IIz Analysis AcceleraEion Levels Used:
5.0 g in all directions Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
11 .36, 11 = .46 g, V=1 = 55 g.
2
. y , , , -
y O A p C/ U V Specification No. H-2 8 6 8
SUMMARY
OF Page @ QY of 93 Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. CO Wm. H. Zimmer Project No. 4130-00 Date 'f - l 6-S l Equipment Description h$
i Location Qualification Results Number Method -
.s 1VD03YA/B/ Opposed Blade A Auxiliary Static Analysis Lowest f = 24.8 Hz.
C/D/E/P/G Balancing Damper (AWV AcceleraEion Levels Used:
/H/J/K/L/ (Damper), ITT (M.Oper) H y =H2 = 1.00 g, V=1.25g.
M Namco (L. Switch))
Simplified Dynamic Lowest f = 39 Hz.
Analysis '
AcceleraEion Levels Used:
H ( Result . ) = 3.0 g.
V = 5.0 g.
Critical Stress = 13,330 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
H .36g.g, H2= .48 g, V=y = 95 lVD07YA Opposed Blade P Auxiliary Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (AWV Acceleration Levels Used:
(Damper) ITT (M.Oper) H y = 1.0 g, H = 1.0 g, 2
Namco (L. Switch)) V = 3.0 g.
Simplified Dynamic Lowest f = 4' .n z .
Analysis AcceleraEion Levels Used:
5.0 g in all directions.
Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
Hy = .4 g, H = .46 g, 2
V= .55 g.
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O O O i Specification No. Il-2 8 6 8
SUMMARY
OF Page 69@ of $3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. OO
- Wm. H. Zimmer Project No. 4130-00 Date d-l6-8\
Equipment 5$ Location Qualification Number
" E "
h$s Method -
Results IVD07YB Opposed Blade P Auxiliary Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (AWV Acceleration Levels Used:
(Damper) ITT (M.Oper) H y = 1.0 g, H = 1.0 g, 2
Namco (L. Switch)) V=30g.
Simplified Dynamic- Lowest f = 43 Hz Analysis AcceleraElon Levels Used:
5.0 g in all directions.
Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
H y = .66 g, H = .46 g, 2
V= .55 g.
lVD07YC Opposed Blade P Auxiliary Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (AWV Acceleration Levels Used:
(Damper) ITT (M.Oper), Hy = 1.0 g, H2 = 1.0 g, Namco (L. Switch))
Simplified Dynamic Lowest f = 43 Hz.
Analysis AcceleraEion Levels Used:
5.0 g in all directions.
Critical stress = 17,.269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
H y = .36 g, H = .46 g, 2
V= .55 g.
1
^
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O O O Specification No. 11-2868
SUMMARY
OF Page 8 of */>.E .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. sO Wm. II . Zimmer Date N
- I b' bf Project No. 4130-00 Equipment Description hS ia Location Qualification Results Number Method -
. s IVQ05YA Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 IIz.
Balancing Damper (AWV AcceleraEion Levels Used:
(Damper) ITT (M.Oper) 11 =H = .00 g, V=1.25g 7 2 Namco (L. Switch)) *
< Simplified Dynamic Lowest f = 4 3 112 .
Analysis AcceleraEion Levels Used:
II ( Result . ) = 3.0 g, b = 5.0 g.
Critical stress = 13,330 psi.
(Allowable = 19,200 psi)-
Max. Calc. Acceleration:
- 11 = .80 g, II = .80 g, 1 2 V= .95 g.
IVQOSYB Opposed Blade P Auxiliary Static Analysis Nat. Freq. > 3 3 112 .
Balancing Damper (AWV Acceleration Levels Used:
(Damper) ITT (M.Oper) 117 = 1. 0 g , 112 = 1.0 g.
Namco (L. Switch)) V = 3.0 g.
Simplified Dynamic Lowest f = 43 Hz Analysis AcceleraElon Levels Used:
5.0 g in all directions.
Critical stress = 17,269 psi.
(Allowable = 19,200 psi)
Max. Calc. Accelerations:
II . 5 6g.g , II2* ~79 9' V=1 =1.15
t- , i .
]
O O O -1
.--a Specification No. H- 2 8 6 8
SUMMARY
OF Page 'p 5 ) of ./F Vendor: Refer Below EQUIPMENT QUALI-FICATION Rev. 60 -
Wm. H. Zimmer Project No. 4130-00 Date N l6-% l Equipment Description hk ia Location Qualification Results Number Method
~
l IVQ06YA Opposed Blade P Auxiliary Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, AcceleraEion Levels Used:
(Damper) ITT (M.Oper) Hy=H2 = 1.00g, V=1.259 Namco (L. Switch)) ~
Simplified Dynamic Lowest f = 53 Hz.
! Analysis '
AcceleraEion Levels Used:
H(Result.) = 3.0g, V = 5.0g.
Critical Stress = 13,330 psi
( Allowable = 19,200 psi)
Max. Calc. Accelerations:
111 .= .34g, H2= .709, V= .95g.
IVQ06YB Opposed' Blade P Auxiliary Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, AcceleraElon Levels Used:
(Damper) ITT (M.Oper), Hy=H2 = 1.00g, V = 1.25g.
Namco (L. Switch))
Simplified Dynamic Lowest f = 53 Hz.
Analysis AcceleraEion Levels Used:
H(Result.) = 3.0g, V=5.0g Critical Stress = 13,330 psi (Allowable = 19,200 psi)
Max. Calc. Accelerations:
U .70g, H 2 = .459, -
V=l = 95g.
l i i
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- i O O O t
. . _ . . _. _ i Specification No. 11- 2868
SUMMARY
OF Page OSR of $3 .
Vendor: Refer Below Rev. 00 Mn. II . Zimmer t{ , g g_ g Project No. 4130-00 Date Equipment Description hf Qualification g Location i Results Neber Method ,
- S lVR0lYA Butterfly Isolation W/S Auxiliary Simplified Dynamic Lowest f = 8 6 IIz .
Damper (AWV (Damper) Analysis AcceleraEion Levels Used:
Bettis (Model: 721C- 111 = 112 = V = 1.0g SR, M.Oper.) Namco Critical Stress = 9,907
( L.. Switches)) psi
. (Allowable = 28,700 psi)
Max. Calc. Acceleration:
=
11 7 . 4 8 g , 112 = .62g,
- V= .70g.
IVR0lYB/C Butterfly Isolation W/S Auxiliary Simplified Dynamic Lowest f = 8 6 112.
Damper (AWV (Damper) Analysis AcceleraEion Levels Used:
Bettis (Model: 721C- 11 = 11 = V = 1.0g 7 2 SR, M.Oper), Namco Critical Stress = 9,907 (L. Switches)) psi (Allowable = 28,700 psi)
Max. Calc. Acceleration:
11 7
=
.51g, 112 = .62g,
- V= .70g.
1 c r y i
O O O
_ . . a. ;
Specification No. II- 2 8 6 8
SUMMARY
OF Page @$3 of y ,R .
Vendor: pnfor nelow -
EQUIPMENT QUALIFICATION Rev. dC Wm . h. . Zimmer Project No. 4130-00 Date N - l 6- 7l Equipment Description 5{
ia Location Oualification Results Number Method 8- .% i IVR02YA Butterfly Isolation W/S Auxiliary Simplified Dynamic Lowest f = 8 6 112.
Damper (AWV, (Damper) Analysis AcceleraEion Levels Used:
Bettis (Model: 721C- 11 = 11 = V = 1.0g.
SR M.Oper.) Namco Chitic$1 Stress = 9,907 (L. Switches)) psi (Allowable = 28,700 psi)
Max. Calc. Acceleration:
11 .34g, 112* '419'
- V=7 = 55g.
IVR02YB Butterfly Isolation W/S Auxiliary Simplified Dynamic Lowest f = 86 liz.
Damper (AWV (Damper) Analysis AcceleraElon Levels Used:
Bettis (Model: 721C- 7 = 112 = V = 1.0g 11 SR M.Oper) Namco Critical Stress = 9,907 (L. Switches)) psi (Allowable = 28,700 psi)
Max. Calc. Acceleration:
!! .38g, H2"
- 9' V=1 = 86g.
I i 7 i n--
O O '
O ,
. .s Specification No. 11- 2868
SUMMARY
OF Page HTid of Id$ .
Vendor: nefer Below -
EQUIPMENT QUALIFICATION Rev. OO Wm . II . Zimmer '
Project No. 4130-00 Date N -- l 5 4 1 Equipment escr p n hka L cation Qualification Results Number Method -
9 IVR02YC Butterfly Isolation W/S Auxiliary Simplified Dynamic Lowest f = 8 6 112 .
Damper (AWV (Damper) Analysis AcceleraEion Levels Used:
Bettis (Model: 721C- H y =H =V= 1.0g 2
SR M.Oper.) Namco Critical Stress = 9,907 (L. Switches)) psi (Allowable = 28,700 psi)
Max. Calc. Acceleration:
= .47g, 11 11 7 2" '4l9'
- V= .559 IVR03YA/B Cpposed Blade W/S Auxiliary Static Analysis Nat. Freq . = 2 3 3 112.
Balancing Damper (AWV, Acceleration Levels Used:
(Damper) Powers 11 = 1.09 , 11 = 1.0g, 2
(M.Oper.) Namco V 7 = 3.0g.
(L. Switch))
Simplified Dynamic Lowest f = 81. 5 IIz .
Analysis AcceleraEion Levels Used:
11 = 1 . 0 g , 11 2 = 1.09, 7
V = 2.0g.
Critical Stress = 12,142 psi (Allowable = 31,600 psi)
Max. Calc. Acceleration:
IIy = 0.629, H = 0.379, 2
V = 1.79
7 ,
O O O !
.--..J Specification No. H- 2868 Vendor: Refer Below
SUMMARY
OF Page , T'f:$ of 93 -
UIPMENT QUALIFICATION Rev. 9D -
b'm . H. Zimmer Project No. 4130-00 Date N l Y5-2k -
Equipment Description hk i Location Qualification Number Method Results
_s, _ _ J __-
IVR09Y Opposed Blade W/S Auxiliary Static Analysis Nat. Preg. = 233 Hz.
Balancing Damper (AWV, Acceleration Levels Used:
(Damper) Powers Hy = 1.0g, H2 = 1.0g, (M.Oper.) Namco V = 3.0g.
(L. Switch))
Simplified Dynamic. Lowest f > 75 Hz.
Analysis AcceleraEion Levels Used:
Hy = 1.0g, H2 = 1.0g, V = 3.0g Critical Stress = 14,006 psi (Allowable = 31,600 psi)
Max. Calc. Acceleration:
H y = 0.6g, H = 0.44g, 2
V = 0.98g.
IVP0lYA/B Opposed Blade W/S Re ctor Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, Accele.raEion Levels Used:
(Damper) ITT (M.Oper.) H = 1.00g, H2 = 1.00g, 1
Namco (L. Switches)) V = 1.25g.
Simplified Dynamic Lowest f n = 40 Hz.
Analysis Limit analysis performed with resulting accelerations found to be above tolerable level.
Damper system is subject to modification. -
4 m.
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O O O :
Specification No. H- 2868
SUMMARY
OF Page Q6of y, ?,
vendor: Refer Below
- EQUIPMENT QUALIFICATION Rev. 00
- h. H. Zimmer Proj,ect No. 4130-00 Date d-lb- 6k ,
Equipment Description h$
ia Location Qualification Results Number Method ,
n IVP10YA/B Opposed Blade W/S Reactor Tcatic Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, AcceleraEion Levels Used:
(Damper) ITT (M.Oper.) Hy = 1.00g, H2 = 1.00g, Namco (L. Switches)) V = 1.25g Simplified. Dynamic Lowest f n 40 Hz.
Analysis , Limit analysis performed
, with resulting accelerations found to be above tolerable level.
Damper system is subject to modification.
IVPllYA/B Opposed Blade W/S Reactor Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, AcceleraEion Levels Used:
(Damper) ITT (M.Oper), H1 = 1.00g, H2= 1.009, Namco (L. Switches))' V = 1.25g Simplified Dynamic Lowest f n = 40 Hz.
Analysis Limit analysis performed with resulting accelerations found to be above tolerable level.
Damper system is subject to modification.
_ _ . - _ 7 _ . - _ ,
^x, O)
\m Specification No. H- 2 8 6 8
SUMMARY
OF Page Sf 7 of 7'S -
Vendor: nnfor nninw 00 l
EQUIPMENT QUALIFICATION Rev.
Wm. H. Zimmer Project No. 4130-00 Date d'lb-hf Equipment Description h{
ia Location Qualification Results Number Method '
S- . _ _ . _ _ _ _
IVQOlY Butterfly Isolation W/S Reactor Static Analysis L'owest f = 98.7 Hz.
Damper (AWV, (Damper), AcceleraEion Levels Used:
ITT (M.Oper.), Namco H =H = 1.0g, V = 3.0g (L. Switches)) Cbitical 2
Stress = 2,895 psi (Allowable = 23,400 psi)
Simplified Dynamic Lowest f n > 40 Hz.
Analysis Limit load analysis performed which found acceleration levels beyonc a tolerable level.
Damper system is subject j to modification.
, IVQO2Y Butterfly Isolation W/S Reactor Static Analysis Lowest f > 98.7 Hz.
Damper (AWV, (Damper), AcceleraEion Levels Used:
ITT (M.Oper.), Namco Hy=H2 = 1.09, V = 3.0g (L. Switches)) Critical Stress = 2,895 psi (Allowable = 23,400 psi)
Simplified Dynamic Lowest f & 40 Hz.
Analysis Limit lo0d analysis
- performed which found acceleration levels beyond a tolerable level.
Damper system is subject to modification.
i f
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O O- u -
i Specification No. 11- 2868
SUMMARY
OF Page $ $~ % of 46 3 .
Vendor: nnfor noinw .
EQUIPMENT QUALIFICATION Rev. On Wm. II . Zimmer af- [I 'Cl
~
Project No. 4130-00 Date b
Equipment $ Qualification Description i g Location Results Number Method '
- 8 IVQO3Y Butterfly Isolation W/S Reactor Static Analysis Lowest f = 98. 7 Itz.
Damper (AWV, (Damper), AcceleraEion Levels Used: -
ITT (M.Oper.), Namco 117 = 112 = 1.09, V = 3.09 (L. Switches)) Critical Stress = 2,895 psi
- (Allowable = 23,400 psi)
Simplified Dynamic Lowest f Analysis Limit loSd->analysis 4 0 liz .
performed with Max. Calc.
acceleration level of 1.49 as compared to an allowable of 5.49 IVQllY Butterfly Isolation W/S Reactor Static Analysis Lowest f = 98.7 liz.
Damper (AWV, (Damper), AcceleraEion Levels Used:
1 = 112 = 1.09, V= 3.0g ITT (M.Oper.), Namco 11 (L. Switches)) Critical Stress = 2,895 psi (Allowable = 23,400 psi)
Simplified Dynntic Lowest f n 40 Hz.
Analysis Limit load analysis performed with Max. Calc.
acceleration level of 1.4g as compared to an allowable of 5.49 I
-y O O O Specification No. 11- 2 8 6 8
SUMMARY
OF Page h 6t of f3 .
Vendor: Refer Below_ g ggy, 30 Wm. II . Zimmer . [ - l d. p'l Proicct No. 4130-00 Date -
Equipment D scripti n h$
ia L ation Qualification Results Number Method
- s.. ,
IVQ13Y Butterfly Isolation W/S Reactor Static Analysis Lowest f = 233 liz.
Damper (AWV, (Damper), AcceleraEion Levels Used:
Powerc (M.Oper.), 11 = 11 = 1.0g, V = 3.0g Namco (L. Switches)) Cbitic31 Stress = 22,410 psi (Allowable = 32,400 psi)
Simplified Dynamic Lowest i > 75 Ilz.
Analysis AcceleraEion Levels Used:
11 = 11 =V = 1.4g Cbitic$1 Stress = 319 psi (Allowable = 18,000 psi)
Max. Calc. Acceleration:
11 7 = 112 " V " 1*49 lVQ14Y Opposed Blade P Reactor Static Analysis Nat. Freq. > 3 3 112.
Balancing Dampers Acceleration Levels Used:
!!y = 1.0g, !! 2 = 1.09, (AWV, (Damper) Powers (M.Oper.), Namco V = 3.0g (L. Switches))
Simplified Dynamic Lowest f = 283 Itz.
Analysis AcceleraEion Levels Used:
6.0g's in all directions Critical Stress = 23,412 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
1.059, H, = .609,
!!y V= = 81 9
7-O ,
O O :
i . . L .; : l Specification No. H- 2868
SUMMARY
OF Page 800 of $3 ,
vendor: Refer Below
' EQUIPMENT QUALIFICATION
. Rev. o t) -
H. Zimmer Wm.
Project No. 4130-00 Date d'\6 b!
Equipment U f P hf^ U Qualification Results
- Number Method '
- s. ._
IVQ15Y Opposed Blade P Reactor Static Analysis Nat. Freq. > 33 Hz.
Balancing Dampers Acceleration Levels Used:
(AWV, (Damper) Powers H = 1.09, H 1.0g, (M.Oper.), Namco 2 V= 3.09
~
(L. Switches))
Simplified Dynamic Lowest f = 36 Hz.
Analysis AcceleraEion Levels Used:
6.0g's in all directions.
Critical Stress = 23,412 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
H y = .48g, H = .379, 2
V = 1.15g.
IVQ16YA/B Opposed Blade P Reactor Static Analysis Nat. Freq. > 33 Hz.
Balancing Dampers Acceleration Levels Used:
(ANV, (Damper) Powers H 1.0g, H 2 = 1.0g, (M.Oper.), Namco V=y =3.0 9 (L. Switches))
Simplified Dynamic Lowest f = 50 Hz.
Analysis AcceleraEion Levels Used:
6.0g's in all directions Critical Stress = 23,412 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
H .949, H = .879, 2
V=y =1.03g.
e .
.s
l Specification No. H- 2 868
SUMMARY
OF Page f.(yl of f3 Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer N-l(- 7[
Date Pro 3ect No. 4130-00 Equipment Description hf ia Location Qualification Results
{
Number Method,
_- _S - - - - - -- -
IVQl7Y Butterfly Isolation W/S Reactor Static Analysis Lowest f = 233 Hz.
Damper ( AWV, (Damper) AcceleraEion Levels Used:
Powers (M.Oper.), H y =H 2
= .09, V= 3.09 Namco (L. Switches)) Critical Stress = 22,410 psi (Allowable =.32,400 psi)
Simplified Dynamic Lowest f > 75 Hz.
Analysis AcceleraEion Levels Used:
H3 =H 3
= V = 1.4g.
Critical Stress = 319 psi (Allowable = 18,000 psi)
M a'x . Calc. Acceleration:.
H y =H 2
=
V = 1.49 IVQ18Y Opposed Blade P Reactor Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (AWV, Acceleration Levels Used:
(Damper), Powers H y = 1.0g, H = 1.09, '
2 (M.Oper.), Namco V = 3.0g.
(L. Switches))
Simplified Dynamic Lowest f = 76 Hz.
Analysis AcceleraEion Levels Used:
6.0g's in all directions.
Critical Stress = 23,412 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
H y = 5.78g, H = 5.'789~1 ,
2 V = 3.04g.
')9 h
0 1 Y I f *
,m.
(~ .
U \._,/ C) j Specification No. H- 28 68
SUMMARY
OF Page 64-2 of (,2 Vendor: Refer Below Rev. CD EQUIPMENT GUALIFICATION .
Wm. H. Zimmer Date 4 - I Ch - 6 l Pro],ect No. 4130-00 -
Equipment hf Qualification Results Description g Location i
Number Method ,
. _- *1 . _ . . - - .. _ _ - _ .- -- - .r. _ -__ - - - _
lVR10Y Opposed Blade W/S Reactor Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (AWV, Acceleration Levels Used:
(Damper) Powers H 1.0g, H 2 = 1.09, (M.Oper.), Namco V= y =3.0g. ~
(L. Switches))
Simplified Dynamic Lowest f = 44 Hz.
Analysis AcceleraEion Levels Used:
6.0g's in all directions.
Critical Stress = 23,412 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
11 .749, H 2 * ~749' V= 1 = .74g.
IVRllY Opposed Blade W/S Reactor Static Analysis Nat. Freq. > 3 3 IIz .
Balancing Damper (AWV, Acceleration Levels Used:
(Damper) Powers !!y 1.09, 112 = 1.0g, (M.Oper.), Namco V= =3. 09 (L. Switches))
Simplified Dynamic Lowost f = 44 Hz.
Analysis AcceleraEion Levels Used:
6.0g's in all directions.
Critical Stress = 23,412 psi (Allowable = 32,000 psi)
- 4a x . Calc. Accelerations:
.74g, H2" '749'
!!y u= = 74g.
4
O O O Specification No. II- 2 8 6 8
SUMMARY
OF Page f%3 of $ ?. .
Vendor: Refer Below s EQUIPMENT QUALIFICATION Rev. L9 '
Wm. H. Zimmer
'f- f 6-TI Project No. 4130-00 Date Equipment Description hk i Location Qualification Results Number Method -
- _n _ . _ _ _
lVR15Y Opposed Blade W/S Reactor Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (AWV, Acceleration Levels Used:
(Damper) Powers Hy = 1.0g, H2 = 1.09, (M.Oper.), Namco V = 3.0g.
(L. Switches))
Simplified Dynamic Lowest f = 44 liz.
Analysis AcceleraEion Levels Used:
6.0g's in all directions.
Critical Stress = 23,412 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
H y .74g, 112" ~749'
= 74g.
V= .
IVR16Y Opposed Blade W/S Reactor Static Analysis Nat. Freq. > 33 liz.
Balancing Damper (AWV, Acceleration Levels Used:
(Damper) Powers Hy = 1.0g, 112 = 1.0g, (M.Oper.), Namco V = 3.09 (L. Switches))
Simplified Dynamic Lowest f = 44 Itz.
Analysis AcceleraEion Levels Used:
6.0g's in all directions Critical Stress = 23,412 psi -
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
11 1 .74g, 112 " '749'
= 74g.
V= .
r i i i i ->
O O i O :
. __i Specification No. H 2868
SUMMARY
OF Page Ob8{ of %3 -
Vendor: Refer Below EQUIPMENT QUAL"IFICATION Rev. OJ D ,H. Zimmer Date N-15-81 Pro]ect un. 4130-00 Equipment Description h$
ia Location Qualification Results N er Method ,
S, IVR21Y Opposed Blade W/S Reactor Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (AWV, Acceleration Levels Used:
(Damper), Powers H1 = 1.0g, H2 = 1.09, (M.Oper.), Namco V = 3.Og.
(L. Switches))
Simplified Dynamic. Lowest f = 44 Hz.
Analysis AcceleraEion Levels Used:
6.0g's in all directions.
Critical Stress = 23,412 psi (Allowable = 32,000 psi)
Max. Calc. Accelerations:
Hy =
.74g, H2" '749' V= .74g. .
b
. v i
. . v y _
O O O Specification No. H-2868
SUMMARY
OF Page !! ';F of r3 .
Vendor: Refer Below
' EQUIPMENT QUALIFICATION Rev. 20 Wm. H. Zimmer Project No. 4130-00 Date -(- g g, gl Equipment Description hk ia Location Qualificatian Results i
Number Method
_- s IVR22Y Opposed Blade W/S Reactor Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (AWV, Acceleration Levels Used:
(Damper) Powers (M. H y = 1.0 g, H = 1.0 g, Oper), Namco (L. 2 V = 3.0 g.
Switches))
Simplified Dynamic Lowest f = 44 Hz.
I Analysis AcceleraEion Levels Used:
6.0 g's in all directions.
Critical stress = 23,412 psi.
(Allowable = 32,000 psi)
Max. Calc. Accel.erations:
H .74 g, H2* ~74 9' V=y = . 74 g.
IVR23Y Opposed Blade W/S Reactor Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (AWV, Acceleration Levels Used:
(Damper), Powers (M.Oper.), Namco
, Hy = 1.0 g, H2 = 1.0 g, V = 3.0 g.
(L. Switches))
Simplified Dynamic Lowest f = 44 Hz.
Analysis AcceleraEion Levels Used:
6.0 g's in all directions.
Critical stress = 23,412 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
H .74 g, H 2* '74 9' V=y = 74 9
-y --
r
,,, 1 O A p
'd U d Specification No. H 2868
SUMMARY
OF Pagc [ G6 of $3 .
Vendor: Refer 65~1ow go EQUIPMENT QUALIFICATION Rev.
Wm. II . Zimmer Proj,ect No. 4130-00 Date 5/-l 6- Yl Equipment Description 5$
ia Location Qualification Results Namber Method
__ -y IVR24Y Opposed Blade W/S Reactor Static Analysis Nat. Freq. > 33 liz.
Balancing Damper (AWV, Acceleration Levels Used:
(Damper), Powers fly = 1.0 g, H2 = 1.0 g, (M.Oper.), Namco (L. V = 3.0 g.
Switches))
Simplified Dynamic Analysk Lowest f = 44 Hz.
AcceleraEion Levels Used:
6.0 g's in all directions.
Critical stress = 23,412 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
H .74 g,!!2* *74 9' V=y = . 74 g.
IVR31Y Opposed Blade. W/S Reactor Static Analysis Nat. Freq. > 33 Hz.
Balancing Damper (ANV, Acceleration Levels Used:
(Damper), Powers (M. 11 = 1.0 g , !! = 1.0 g, 7 2 Oper.), Namco V = 3.0 g.
(L. Switches))
Simplified Dynamic Lowest f = 4 4 112.
Analysis AcceleraEion Levels Used:
6.0 g's in all directions.
Critical stress = 23,412 psi.
(Allowable = 32,000 psi)
Max. Calc. Accelerations:
11 =
. 7 4 g , 112" '74 9' V=7 .74 g.
O O O
~
Specification No. H-2 8 6 8
SUMMARY
OF Page c'. W o f 92 ?> .
Vendor: pofor noinw p g .
p 39 7
Wm. H. Zimmer Date :! . l gg geg-Project No. 4130-00 Equipment escription hIa Location Qualification Results Number Method
.s -
lVY0lY Opposed Blade A Reactor Static Analysis Lowest f = 24.8 Hz Balancing Damper (AWV, AcceleraEion Levels Used:
(Damper) ITT (M.Oper.) Hy = 1.00 g, H2 = 1.00 g, Namco (L. Switches)) V= 1.25 g.
Simplified Dynamic . Lowest f = 53 Hz Analysis AcceleraElon Levels Used:
H(Result.) = 3.0 g,
. V = 5.0 g.
- Critical stress = 12,467 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
H y = .83 g, H 2 ** O 9' V = 2.15 g. i IVYO2Y Opposed Blade A Reactor Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, AcceleraEion Levels Used: l (Damper), ITT (M.Oper) H y = 1.00 g, H 2 m 1.00 g.
Namco (L. Switches)) V = 1.25 g.
Simplified Dynamic Lowest f = 39 Hz.
Analysis AcceleraEion Levels Used:
5.0 g's in all directions.
Critical stress = 18,701 psi.
(Allowable = 19,200 psi) j Max. Calc. Acceleration:
H y = .30 g, H V= .64 g.
2* '44 9' ;
~
O O O Specification No. 11-2868
SUMMARY
OF Page fl,6 of f3 -
Vendor:, ne fer nelow EQUIPMENT QUALIFICATION Rev. CO wm. II . Zimmer Project No. 4130-00 Date N-l65 8f Equipment Description 5k ia Location Qualification Results Number Method.
. 3 __
IVY 04Y Opposed Blade A Reactor Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, AcceleraEion Levels Used:
(Damper), ITT (M.Oper) Hy = 1.00 g, H2 = 1.00 g, Namco (L. Switches)) V = 1.25 g.
Simplified Dynamio Lowest f = 53 Hz.
Analysis AcceleraEion Levels Used:
5.0 g's in all directions.
- Critical stress = 18,701 psi.
(Allowable = 19,200 ps1)
Max. Calc. Acceleration:
11
.70 g, H2" '7b 9' V=7 = 78 g.
IVYO6YA/B Opposed Blade A Reactor Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, AcceleraElon Levels Used:
(Damper), ITT (M.Oper) 11 = 1.00 g, 11 = 1.00 g, 2
Namco, (L. Switches)) V 7= 1.25 g.
Simplified Dynamic Analy- Lowest f = 4 3 11z .
sis AcceleraEion Levels Used:
II ( Result. ) = 3.0 g, V = 5.0 g.
Critical stress = 12,467 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
11 =
. 3 7 g , !!2= .37 g, V 7= 1.1 g.
, - , t :
- m
- O O T LJ V J
. :. J Specification No. H-2 8 6 8
SUMMARY
OF Page[3G'iof 5/,3 -
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer Pro],ect No. 4130-00 Date 4[-l 6- Yl -
Equipment e rp on h$a Location Qualification Results Number Method ,
-=*s IVY 08Y Opposed Blade W/S Reactor Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, AcceleraEion Levels Used:
(Damper), ITT (M.Oper) H y = 1.00 g, H = 1.00 g, 2
Namco (L. Switches)) V = 1.25 g.
Simplified Dynamic- Lowest f = 39 Hz.
Analysis AcceleraEion Levels Used:
5.0 g's in all directions.
Critical stress = 18,701 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
H y = .30 g, H 2 * '44 9' V= .64 g.
IVYO9Y Opposed Blade A Reactor Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, ,
AcceleraEion Levels Used:
(Damper) ITT (M.Oper), Hy =
1.00 g, H2 = 1.00 g, Namco (L. Switches)) V = 1.25 g.
Simplified Dynamic Lowest f = 53 Hz.
Analysis AcceleraEion Levels Used:
H (Result . ) = 3.0 g, V = 5.0g.
Critical stress = 12,467 psi. .
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
H y = .50 g, H 2 = .85 g, V= .80 g.
- c
' * *% f
i ,
O O i O I Specification No. H-2 8 6 8
SUMMARY
OF Page 876 of 63 -
Vendor: nnfor noinw gg p _
Wm. H. Zimmer i Project No. 4130-00 Date 'f - l 3 - T }
Equipment h Qualification Number Descript?on ia Location Results Method *
= S IVYllY Opposed Blade A Reactor Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, AcceleraEion Levels Used:
(Damper) ITT (M.Oper) H y = 1.00 g, H 1.00 g, 2
Namco (L. Switches)) V= 1.25 g.
Simplified Dynamic- Lowest f = 76 Hz.
Analysis AcceleraEion Levels Used:
5.0 g's in all directions.
Critical stress = 18.701 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
Hy = 1.26 g, H2 " l*73 9' V = 2.14 g.
IVY 12Y Opposed Blade A Reactor Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, AcceleraEion Levels Used:
(Damper) ITT (M.Oper) H1 = 1.00 g, H 2 = 1,00 g, Namco (L. Switch)) V = 1.25 g.
Simplified Dynamic Lowest f = 53 Hz.
Analysis AcceleraEion Levels Used:
5.0 g's in all directions.
Critical stress = 18.701 psi.
(Allowable - 19,200 psi)
Max. Calc. Acceleration:
H, = 1.25 g, H 2 = 43 g, V'= .60 g.
t
- 1 - -
-y T
, 1 b o .
Specification No. II- 2 8 6 8 SUMMNRY OF Page f"Ji of j [
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 00 kb. H. Zimmer Project No. 4130-00 Date 4 - l 6-Tl Eauipment Description 5$
ia Location Qualification Results N ber Method ,
- S l IVY 13YA/B Opposed Blade A Reactor Static Analysis Lowest f = 24.8 Uz.
Balancing Damper (AWV, AcceleraEion Levels Used:
(Damper) ITT (M.Oper) H y = 1.00 g, H 2 = 1.00 g, Namco (L. Switch)) V= 1.25 g.
Simplified Dynamic Lowest f = 53 Hz.
Analysis AcceleraEion Levels Used:
5.0 g's in all directions.
Critical stress = 18,701 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
H y = .32 g, H 2 = .38 g, V= .62 g.
IVYl4Y Opposed Blade A Reactor Static Analysis Lowest f = 24.8 Hz.
Balancing Damper (AWV, AcceleraEion Levels Used:
Damper) ITT (M.Oper.) H = 1.00 g, H 1.00 g, 2
Namco (L. Switch)) V= 1.25 g.
Simplified Dynamic Lowest f = 39 liz.
Analysis AcceleraEion Levels Used:
5.0 g's in all directions.
Critical stress = 18,701 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
H y = .44 g, H = 1.35 g, 2
V= 1.1 g.
(^}
LJ ("A s
Specification No. 11-2868
SUMMARY
OF Page PG2 of VR -
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. OO Wm. II . Zimmer tl-l $, 3 k Project No. 4130-00 Date l
Equipment Qualification Description i Location Results Number Method IVY 15Y Opposed Blade A Reactor Static Analysis Lowest f = 2 4 . 8 II: .
Balancing Damper (AWV, Accelera$ ion Levels Used:
(Damper) ITT (M.Oper) H y = 1.00 g, 11 2
= 1.00 g, Namco (L. Switch)) V= 1.25 g.
Simplified Dynamic. Lowest f Analysis AcceleraN.ion = 53 liz.
Levels Used:
II (Result... ) ~ = 3.0 g, V = 5.0 c Critica] ' stress = 12,467 psi.
(Allowable = 19,200 psi)
. Max. Calc. Acceleration:
11 = .75 g, 11 = .58 g, 1 2 V= .80 g.
p 1 r . .
(]
u.-
IO N.J Specification No. 11-2874
SUMMARY
OF Page Ps 73 of f.B Vendor: Refer Below Rev. O)
EQUIPMENT GUALIFICATION Wm. II . Zimmer ,
Project No. 4130-00 Date di3 6I Equipment Description 5$
ia Location Qualification Results Number Method s ._ _ _ _ _
lVG0lYA Butterfly Isolation A Reactor Static Analysis Lowest f = 33 Hz.
Damper (AWV, (Damper), AcceleraSion Levels Used:
ITT (M.Oper.), Namco H y = 0.60 g, H = 0.60 g, V = 0.65 g. 2 (L. Switches)) Critical stress = 7,002 psi.
(Allowable = 36,000 psi)
Simplified Dy,namic Lowest f = 70.3 Hz.
Analysis AcceleraEion Levels Used:
11 = 1.07 g, H 2 = 1.07 g.
1 V= 1.05 g.
Critical stress = 18,771 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
H y =H 9 = 1.07 g, V= 1.05 g.
y 3 t , ,
l O
v O v
Specification No. 11 2874
SUMMARY
OF Page S7tl of '[ 3 .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. CO Wm. II . Zimmer Project No. 4130-00 Date '[- [ C-f[
Equipment , ,
hj Qualification escription 1 a Location Results Number Method
- L ___ __ _ ._ _ __..__ _' _ _,
IVG0lYB Butterfly Isolation A Reactor Static Analysis Lowest f = 33 liz.
Damper (AWV (Damper) AcceleraEion Levels Used:
ITT (M.Oper.) Namco 111 = 0.60 g, H2 = 0.60 g, (L. Switches)) V = 0.65 g.
Critical stress = 7,002 psi.
(Allowable = 36,000 psi)
Simplified Dynamic Lowest f = 70.3 IIz.
Analysis AcceleraEion Levels Used:
11 1.07 g, 112= 1.07 g, V=7 =1.05 g.
. Cri-tical stress = 18,771 psi.
(Allowable = 19,200 psi)-
Max. Calc. Acceleration:
II = 11 2 = 1.07 g, V=1.05g.
Ddmper is subject to modifications.
~
% 8 6 I e
O O O
.W-+ 6 w Specification No. 11-2874
SUMMARY
OF Page 876 of yf3 i vendor: Refer nelow CG EQUIPMENT QUALIFICATION Rev.
Wm. II . Zimmer Project No. 4130-00 Date 'I- l.( Ni Equipment Description hk ia Location Qualification Results er Method, lVG06YA/B Butterfly Isolation A Reactor Static Analysis Lowest f = 340 11z .
Damper (AWV, (Damper), AcceleraEion Levels Used:
ITT (M.Oper.), Namco 111 = 1.5 g, 2 = 1.5 g,11 (L. Switches)) V = 2.0 g.
Critical stress = 6,077 psi.
(Allowable = 26,000 psi)
Simplified Dynamic Lowest f = 340 IIz.
Analysis AcceleraEion Levels Used:
111 = 1.5 g , II2 = 1.5 g, V = 2.0 g.
Critical stress = 18,771 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
11 = 0.42 g, 11 2 = 0.33 g, V 1= 0.75 g.
O O O Specification No. 112874
SUMMARY
OF Page @/b of 75 -
1 Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. CO h5. II . Zimmer Proj,ect No. 4130-00 Date 1l- } $' b Equipment 5$ Qualification Description ja Number Location Results Method *
! - S IVG07YA Butterfly Isolation A Reactor Static Analysis Lowest f = 3 4 7 IIz .
Damper (AWV, (Damper) AcceleraEion Levels Use.d:
ITT (M.Oper.), Namco 11 1 = 1.5 g, II2 = 1.5 g, (L. Switches)) V = 2.0 g.
Critical stress = 6452 psi.
(Allowable = 26,000 psi)
Simplified Dynamic Lowest f = 3 4 7 IIz .
Analysis AcceleraEion Levels Used:
11 = 1.5 g, 11 = 1.5 g, 2
V 7= 2.0 g.
Crit. stress = 18,771 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
IIy = 0.34 g, 11 2 = 0136'g, V = 0.75 g.
{
u 1 r ,
7 o ; o o Specification No. 11-2874
SUMMARY
OF Page f.~/~/ o f $3 Vendor: Refer Below .-
v,9 EQUIPMENT QUALIFICATION Rev.
Wm. H. Zimmer Project No. 4130-00 Date d - I #5 - hf Equipment cripdon 5Sa Locadon Qualification Number Method Results
.s -
lVG07YB Butterfly Isolation A Reactor Static Analysis Lowest f = 340 Hz.
Damper (AWV (Damper) AcceleraEion Levels Used:
ITT (M.Oper.), Namco H y = 3.91 g, H2 = 3. 91 g ;
(L. Switches)) V = 0.66 g.
Crit. stress = 6257 psi (Allowable = 26,000 psi)
Simplified Dyanmic Lowest f = 340 Hz.
Analysis AcceleraEion Levels Used:
111 = 3.91 g, H2 = 3.91 g, V = 0.66 g.
Critical stress = 18,771 psi.
(Allowable = 19,200 psi)
Max. Calc. Acceleration:
111 = . 4 2 g , H = 0.38 g, V = 0.25 g.2 L
b n e 4
w i i O :O i
O ;
Specification No. H 2874
SUMMARY
OF Page PQ'<?of M- .
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. DO Wm. H. Zimmer Project No. 4130-00 Date N - l $- T31 Equipment Description hk ia Location Qualification Results Number Method
"_1________.-
lVG08YA/B Butterfly Isolation A Reactor Static Analysis Lowest f = 347 Hz.
Damper (AWV, (Damper), AcceleraEion Levels Used:
ITT (M.Oper.), Namco H = 1.5 g, H2 = 1.5 g,-
(L. Switches)) V=1 1.0 g.
Critical stress = 6452 psi (Allowable = 26,000 psi)
Simplified Dynamic Lowest f = 347 Hz.
Analysis Accelera9 ion Levels Used:
H1 = 1.5 g, H2 = 1.5 g, V = 2.0 g.
Critical stress = 18,771
, psi..
(Allowable = 19,200 psi)
Max. Calc. Acceleration':
H1 = 0 . 3 4 g , II2 = 0.36 g, V = 0.75 g.
O O O l Specification No. 11-2874
SUMMARY
OF Page {$79 of $N Vendor: Refer Below p g Wm. !! . Zimmer Project No. 4130-00 Date L{-lb31 Equipment Description h$
ia Location Qualification Results Number Method
- S _
IVG09YA/B Butterfly Isolation A Reactor Static Analysis Lowest f = 347 Itz.
Damper (AWV, (Damper) AcceleraEion Levels Used:
ITT (M.Oper), Namco 11 7 = 1.5 g. !!2 = 1.5 g, (L. Switches)) V= 2.0 g.
Critical stress = 6452 psi (Allowable = 26,000 psi.
Simplified Dynamic Lowest f = 3 4 7 11 z .
Analysis AcceleraEion Levels Used:
11 = 1. 5 g , 11 = 1.5 g, 2
V 7 = 2.0 g.
Critical' stress = 18,771 psi (Allowable = 19,200 psi)
Max. Calc. Acceleration:
11 = 0 . 3 4 g , 11 2 = 0.36 g, V 7 = 0.75 g.
-W
, _ _ _ __--.__.------ - _ _. - r-- r 4 i ~
,1 O O O Specification No. H-2874
SUMMARY
OF Page P.80 of 73 Vendor: Refer Below Rev. OK)
EQUIPMENT QUALIFICATION .
- Wm. H. Zimmer Project No. 4130-00 Date 'l' l b- Il Equipment hf Qualification Results Description g Location i
ber Method
.S IVG10YA/B Butterfly Isolation A Reactor Static Analysis Lowest f = 1859 Hz.
Damper (AWV, (Damper), AcceleraEion Levels Used:
ITT (M.Oper.), Namco Hy = 1.0 g, H 2 = 1.0 g, (L. Switches)) V = 0.63 g.
Critical stress = 696 psi (Allowable = 3 6,000 psi)
Simplified Dynamic Lowest f = 1859 Hz.
Analysis AcceleraEion Levels Used:
- = 1.0 g, H y = 1.0 g, H 2
V = 0.63 g.
Critical stress = 18,771 psi.
(Allowable = 19,200 psi)
Max. Calc. acceleration H y = 0.42 g, H = 0.38 g, 2~
V = 0.75 g.
7 O O O Specification No. H- 3874
SUMMARY
OF Page $81 of $3 Vendor: Refer Below Rev. CK3 EQUIPMENT QUALIFICATION Wm. H. Zimmer Project No. 4130-00 Date 9- l 5- $ }
Equipment Description h$
ia Location Qualification Results Number Method
- S IVQ10Y Butterfly Isolation A Reactor Static Analysis Lowest f = 193 Hz Damper (AWV, (Damper) AcceleraEion Levels Used:
ITT (M.Oper.), Namco H y = 0.35 g, H = 0.35 g, 2
(L. Switches)) V = 0.65 g.
Critical stress = 5216 psi (Allowable = 36,000 psi)
Simplified Dynamic' Lowest f = 193 Hz.
Analysis AcceleraEion Levels Used:
H y = 0.35 g, H = 0.35 g, 2
V = 0.65 g.
Critical stress = 10,409 psi (Allowable = 19,200 psi)
Max. Calc. Acceleration:
Hy = 0.32 g, H2"
- N' V = 0.65 g.
. i i >
O O O Specification No. H-2 8 8 3
SUMMARY
OF Page (579 of 73 Vendor: Refer Below Rev. 60 EQUIPMENT QUALIFICATION Wm. H. Zimmer Date '\ - k 'b 'I l Project No. 4130-00 Equipment Description hf ia Location Qualification Results ber Method
- 8 IVC 89Y Essential Isolation P Auxiliary Simplified Dynamic Analysis Lowest f = 3.21 Hz.
Check Damper (Techno (Remaining f > 353 Hz)
Corp (Damper) Miller Acceleration"L8vels Used (M.Oper.), Namco and Reg'd. per H-2883):
(L. Switch)) H =H =V= 2.0 g.
Chitic$1 stress = 37,399 ps-(Allowabic = 41,990 psi)
Simplified Dynamic Max. Calc. Acceleration:
Analysis fl y = .87 g, H-= .95 g, 2
V= 1.31 g.
Therefore, past analysis (above) applies.
IVC 90Y Essential Isolation P Auxili ary Simplified Dynamic Lowest f = 3.21 Hz.
Check Damper (Techno Analysis (Remaining f > 353 Hz)
Corp (Damper) Miller Accel. LevelE,Bsed(and reg'e (M.Oper.), Namco per H-2883):
(L. Switch)) !! , =H 2 =V= 3.0 g.
Cfit. stress = 37,399 psi
( Allowable = 41,990 psi)
Simplified Dynamic Max. Calc. Acceleration:
11 1= .87 g, H2= .95 g, V = 1.31 g.
Therefore, past analysis (above) applies.
Specification No. H-2 8 8 3
SUMMARY
OF Page ON8of 83 Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. 80 .
Wm. H. Zimmer Project No. 4130-00 Date Y-/d-9I Equipment escdpdon hfa Location Qualification Results Number Method
. : _ .2 lVC91Y Essential Isolation P Auxiliary Simplified Dynamic Lowest f = 3. 21 !!z .
Check Damper (Techno Analysis (RemainiEg f n > 3 53 Hz .)
Corp (Damper) Miller Acceleration {5vels Used (M.Oper.), Namco (And req'd per H-2883):
(L. Switch)) H =H = V = 3.0 g.
Chit. ktress = 37,399 psi (Allowable = 41,990 psi)
Simplified Dynamic Max. Calc. Acceleration:
Analysis
!!y 1.15
= 88 g. g, H2* '78 9' V= .
Therefore, past analysis (above) applies.
IVC 92Y Essential Isolation P Auxiliary Simplified Dynamic AnalysisLowest f = 3.21 Hz.
Check Damper (Techno (RemainiRg f > 353 Hz)
Corp (Damper) Miller Acceleration,L5vels used (M.Oper), Namco (and reg'd. per H-2883)
(L. Switch)) ll =H = V = 3.0 g.
Chit. $ tress = 37,399 psi (Allowable = 41,990 psi)
Simplified Dynamic Analysis :4ax . Calc. Acceleration:
1.15 g, H 3 = .78 g,
!!y 1= = 88 g Therefore, past analysis (above) applies.
- O .
O O Specification No. 11-2191 Vendor: Rockwell International
SUMMARY
OF Page e.} of 45 Wm. II. Zimmer EQUIPMENT QUALIFICATION Rev. oo Proj,ect No. 4130-00 Date %-IS-81 Equipment Description 5k ia Location Qualification Number Method Results
. s ,
lE51F065 6" Non-Slam Check A Reactor No extended part Rigid in all directions Valve Building Stresa evaluation for No limiting accelerations operability under nozzle Obtained allowable loads Nozzle loads to assure operability
)
lE22F024 14" Non-Slam Check A Reactor No extended part Rigid in all directions valve Building Stress evaluation for No limiting accelerations operability under nozzle Obtained maximum nozzle loads loads for operability 1B21F010A/B 18" Non-Slam Check Primary No extended part Rigid in all directions Valve Cont. Stress evaluation for No limiting accelerations A operability under nozzle Obtained maximum nozzle 1B21F032A/B Reactor loads loads for operability Building k
y i 1 r v v O O O Specification No. 11- 2194
SUMMARY
OF Page d.2 of 45 .
Vendor: GPE Control EQUIPMENT QUALIFICATION Rev. oo Wm. II . Zimmer Project No. 4130-00 Date #t 31 Equipment Description h$ Qualification g Location i Results er Method
.s -
lE12F103A/B 1 5" Vacuum Relief A Reactor Natural Frequency Estimate Minimum Natural Frequenc3 Valve Building Static Analysis of all = 8045 !!z critical ccnponents. Stresses Qualified for Upset 3'g' limital to design allowables Emergency 5 'g '
LE51F082 2" Vacuum Relief P Reactor Natural Frequency Estimate Minimum Natural Frequency lE51F084 Valve Building Static Analysis = 7985 Ilz Qualified for Upset 3'g' Emergency 5 'g '
1PC005A, B, 20" Vacuum Relief A Reactor Natural Frequency Analysis Minimum Natural Frequency C, D Valve Buildit Static Analysis of all = 967 Hz 1PC006A, B, critical cmponents. Qualified for Upset 3 'g '
C, D Stresses limited to design Emergency 5 'g '
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O O O Specification No. 11- 2263
SUMMARY
OF PageOS of I6 t .
Vendor:11n. Pow 11 cb.
EQUIPMENT QUALIFICATI,0N Rev. oo wm. II . Zimmer Project No. 4130-00 Date At . ) 6 - f?I Equipment 5j Oualification Number Description i g Location Results Method '
'1__
lhR018 21",
s M, Globe Valve P React. Bldg Qualification in progress lhE029 with the vendor lhE035A, B Aux. Bldg.
lhE037A, B Ibact. Bldg LWR 047A, B React. Bldg LWR 067A, B Prim. Cont.
lIN061 3"-150#, FQ Globe Valves A React. Bldg Qualification in progress lWS076A, B P- with vendor IC41F001A, B P lE12F040 3"-400# bb, Globe Valves A y Finite clonent method Natural frequencies 40!!z,77 !!z Natural frequencies Qualified acceleration level Simplified dynamic analysis. Upset & Dnexgency Stresses linited to design a = 5.0 'g', b = 5.0 'g', ~
allowables c = 3.5 'g' lWS117A, B 3", M, Globe Valves P Service Qualification in progress C, D dater Pump with vendor house lE51F022 4", Mo, Globe Valves A React. Bldg Otmlification in progress with vendor lhE038A, B 4", M, Globe Valves P Tux. Bldg. Qualification in progress with vendor 1WE040A, B, 6", M, Globe Valves P Diesel Qualification in progress u-C,D,E,F, Generator with vendot -
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U i- I ! ! i O O O Specification No. 11- 2264
SUMMARY
OF PageC 7 of 45 -
Vendor: Mn. H. Powell Co.
EQUIPMENT QUALIFICATION Rev. oo Wm. H. Zimmer Proj,ect No. 4130-00 Date #t S l Equipment Description hk i Location Qualification Results ber Method
.s -
1B21F501A, B 2 ", bb Gate Valves P Turbine Qualification in progress Bldg. with vendor 1CY045 2 ", M, Gate Valves P React. Bldg Qualification in progress 1CYO47 Prim. Cont with verdor LWR 017 React . Bldg lhE027 lhm040A, B Aux. Bldg.
LWR 041A, B "
lhE045A, B React. Bldg LWR 066A,B lWS073A, B 3"-150#, bb, Gate Valves A React. Bldg Finite element analysis Minimum natural frequercies Natural frequency evaluation 74.5 Hz, 61.6 Hz Static analysis Qualified acceleration level Upset & Emergency tw4.82'g', b=4.82'g', c=5.82'g' lE12F049 3"-300#, Mo, Gate Valves A React. Bldg Finite elcmant analysis Minimtm natural frequencies Natural frequency evaluation 46.8 Hz, 79.4 Hz Simplificd dynamic analysis Qualified acceleration level Stresses limitcd to design a =3.78 'g ' , b=3.78 'g ' , c=2.89 tf allowables 1B21F326 3"-600# Fb, Gate Valves P Aux. Bldg Qualification in progress with vendor 1B21F016 3"-900# bb, Gate Valves A Prim. Cont Qualification in progress 1B21F019 React. Bldg with vendor 1CllF082 React. Bldg
, ________________7- ,
O O O Specification No. 11-2264
SUMMARY
OF Page d.8 of 45 .
Vendor: Mn.11. Powell Co. '
Rev. oo EQUIPMENT QUALIFICATION Wm. 11 . Zimmer Proj,ect No. 4130-00 Date #t - 1 Ei - S I Equipment Description h$
ia Location Qualification Results er Method
. s .
1RE047A, B 3", M, Gate Valves P React. Bldg Qualification in progress lhR025A, B React. Bldg with vendor B Service lhSll8A' C, D .
m ter pump house lhS122A, B React'. Bldg 1CllF087 Prim. Cont.
1C41F002A, B React. Bldg IC41F031 lE12F007 1E12F063A,B,C
. lE12F071A, B lE12F072A, B -
lE12F082 i lE12F086 l lE12F303 i lE12F308
! lE12F314
[ lE21F004 l lE21F008 lE21F025 lE22F003 1E22F019 lE22F026 ,
lE22F031 9 lWS011A, B 4"-150 lbs., m , A Service Finite elenent analysis Natural frequencies 55.6 IIz, Gate Valve water ptrnp Natural frequency evaluation 80.4 IIz house Static analysis Qualified acceleration level Upset & Dnergency -
a=4 . 4 ' g ' , b=4 .4 ' g ' , c=6.72 ' g '
t O O O ,
_ . _ _ +
Specification No. 11- 2264 Vendor: Wn. II. Powell Co.
SUMMARY
OF Page dFJ o f ,,h EQUIPMENT QUALIFICATION Rev. oo Wm. II . Zimmer Pro],ect No. 4130-00 Date /t-f5 -8I Equipment h 1 Qualification g
Description i g Location Results Method *
- s. . _ . ,. __
lWS012A, B 4"-150# , Fb, Gate Valves A React. Bldg Finite elenent amlysis Natural frequencies 55.6 IIz, Natural frequency evaluation 80.4 IIz Simplified dynamic analysis Qualified acceleration level Stresses limited to design Upset & Emergency allowabies a = 5 'g ' , b = 5 'g' ,c = 4. 25 'g '
lE12F064A,B,C 4"-300#, Mo, Gate Valves A React. Bldg Qualification in progress lE21F0ll React. Bldg with vendor lE51F059 4"-600# , Fb, Gate Valves A React Bldg Qualification in progress 1B21F020 P with vendor 1B21F500A, B P Turb. Bldg. -
lE51F008 4"-900#, Mo, Gate Valves A React. Bldg Finite elanent method Natural frequencies 49.6 Hz, 1G33F100 P Prim. Cont. Natural frequency evaluation 81.1 llz 1G33F101 p Simplified dynamic analysis. Qualification acx:elerationlevel 1G33F106 P o Stresses limited to design allombles g E k19g y, W a-
---,N- 'g_', c=5.62'g' 1G33F040 4"-1500#, Mo, Gate Valves A React. Bldg Qualification in progress with verrlor LWR 042A, B 4", M, Gate Valves P Aux. Bldg. Qualification in progress lE12F018A,B,C React. Bldg with vendor lE21F302 LWR 073 6", Ao, Gate Valves A React. Bldg Qualification in progress LWR 074 with vendor 7
, 7 ;
O O O Specification No. 11- 2264 Vendor: Wn. H. Powell Co.
SUMMARY
OF Page d.lo of k63 ,
EQUIPMENT QUALIFICATION Rev. oo Wm. H. Zimmer 2t. Is _ p t Project No. 4130-00 Date b
Equipment Description f
1 a Location Qualification Results N d er Method -
s, _
lhE054 6"-150#, Mo, Gate Valves P React. Bldg Finite elanent method Natural frequencies 55.8 Hz, lhE055 P Natural frequency evaluation 96.8 Hz lE51F010 A Simplified dynamic analysis Otulification acceleration-lE51F031 P V Stresses limited to design level, Upset & Buergency
, allovabloc a =4.l'g', b =4.1'g' c =3.05'g' lE51F012 6"-600#, Mo, Gate Valves P React. Bldg Qualification in progress with vendor lE51F013 6"-900#, Fb, Gate Valves A React. Bldg Qualification in progress 1G33F001 A Prim. Cont, with vendor 1G33F004 A React. Bldg lE51-F016 6", M, Gate Valves P React. Bldg Qualification in progress i with vendor lE51F068 8"-150#, Mo, Gate Valves A React. Bldg Finite elanent analysis Natural frequencies 38.1 Hz, l Natural frequency ciraluation 71.6 Hr.
! Simplified dynamic analysis Qualification acceleration Stresses limited to design level Upset & Brergency -
allowables a = 3 'g' , b = 3 'g' , c = 3.5 'g '
lE51F063 8"-900#, Me, Gate Valves A Prim. Cont. Finite elanent analysis Natural frequencies 73.3 Hz, lE51F064 React. Eldg Natural frequency evalulation 86.6 Hz Static aralysis Qualification acceleration Stresr.es limited to design level Upset & Bnergerry -
allowables a = 5 'g' , b = 5 'g ' , c = 6 'g '
1B21F310A, B 10"-600#, Mo, Gate Valves P Turb. Bldy Qualifi, cation in progress with vendor
O O O
- u. . -
- Specification No. 11- 2264
SUMMARY
OF Paged l l of kB -
vendor: Wn. II. Powell Co.
EQUIPMENT QUALIFICATION Rev. oo Wm. H. Zimmer Project No. 4130-00 Date 4 8 1 Equipment Description h$
ia Location Qualification Results Number Method
__S
_x __
lE12F042A,B,C 10"-900#, Mo, Gate Valves A React. Bldg Finite elonent analysis Natural frequencies 74.2 IIz, lE21F005 Natural frequency evaluation 83.3 IIz
. Static Analysis Qualification acceleration Stresses limited to design level Upset & Bnergency -
allowables a = 5 'g' , b = 5 'g ' , c = 6 'g '
1FC029 12"-300#, M, Gate Valves P React. Bldg Qualification in progress 1FC034 with vendor 1FC035 IE12F335 lE21F309 Y lE22F301' 14", M, Gate Valve P React. Bldg Qualification'in progress with vendor 1821F065A, B 18"-900#, Mo, Gate Valves A React. Bldg Finite element metixxl Natural frequencies 59.1 Hz, lE12F008 Natural frequency evaluation 81.9 112 lE12F009 Prim. Cont. Static analysis Qualification acceleration Stresses limited to design level Upset & Bnergency allowables a = 5 'g ' , b = 5 'g' , c = 3.5 'g '
1B21F011A, B 18"-900#, M, Gate Valves P Prim. Cont. Qualification in progress lE12F306 with vendor lWS005 30"-150#, Mo, Gate Valves P Service Finite elanent method Natural frequencies 20.2 Hz, Ltter Pump Natural frequency evaluation 33.3 liz llouse Equivalent dynamic analysis Qualification acceleration level Upset & Bnergencv a = 5 ' g ' , b = 5 'g ' , c = 4.5 .'g '
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O O O Specification No. 11- 2265
SUMMARY
OF Page d.l3 of M .
Vendor: Jamesbury (brp.
- Ren oo Wm. 11 . Zimmer Pro],ect No. 4130-00 Date k \S-21 Equipment Description h$
ia Location Qualification Results er Method
- S lWS036A to 11 6", M, Butterfly Valve P Diesel Gen. Finite elment analysis Minnum natural frequency Room Natural frequency evaluation = 118 Hz Qualification acceleration Static amlysis level Upset - a=3 'g ' , b=3 'g' , c-4 'g '
Bnerg.- a=5'g', b=5'g', c=6'g' 1%S037A to D 8", Mo, Butterfly Valve P Diesel Gen. Finite elment analysis Mimmum mtural frequency Roam Natural frequency evalulation = 41.6 Hz Static analysis Qualification acceleration level Upset - a=3'g', b=3'g', c=4'g' Dnerg .- a=5 'g ' , b=5 'g ' , c=6 'g '
lVH001A, B 12", Ao, Butterfly Valves P Service Dynamic analysis using finite Minimtm natural fre quency -
IVH002A, B Ltiter Ptmp elenent nodel = 24.1 IIz IVH003A, B lbuse Frequency evaluation Qualified to the response IVH004A, B Response spectra analysis spectra lE12F068A, B 14", Mo, Butterfly Valve P React. Bldg In progress lhS017 14", M, Butterfly Valve P React. Bldg In progress lhS018 lhS019 lhS021
- lE12F014A, B 16", Mo, Butterfly Valve P React. Bldg, In pregress lhS027 16", M, Butterfly Valve P React. Bldg. In progress lWS032
1 I I I i Y .
O O O '" c
.ii_ . I Specification No. 11- 2265 Vendor: Jamesbury Corp.
SUMMARY
OF Page d k of /3t .
EQUIPMENT QUALIFICATION Rev. cc k'm . !! . Zimmer Project No. 4130-00 Date k 81 Equipment Description hk ia Location Qualification Results Method Number
. g IVQ001A, B 18", Ao, Butterfly Valvu P React. Bldg In progress IVQ002A, B IVQ003A, B 1 lVQ004A, B 1hS016 18", M, Butterfly Valve P React. Bldg In progesss -
IV5023 lhS024 IIG028 IVS029 193031 1hS026 lhS004A,B,C,0 24", N , Butterfly Valve A Servicethter Finite elanent amlysis Minimum mtsral frequercy lhS008A,B, Pump flouso Natural frequency evaluation = 49.8 IIz ltE033A, B Aux. Bldg. Static amlysis Qualification acceleration 1%5034A, B Aux. Bldg. level Upset - a=3 'g ' , b=3 'g' , c=4 'g' Dnerg .- a=5 'g ' , b=5 'g ' , c=6 ' g '
1CY008A, B 16", M, Butterfly Valve P Outside Finite elenent amlysis Minimtm mtural frequency Natural frequency evaluation = 82.2 112 Static analysis Qualification acceleration level Upset - a=3'g', b=3'g', c=4'g' D erg.- a=5'g', b=5'g', c=6'g' 1hS070 18", M, Butterfly Valve P Service Finite clanent analysis Minimum mtural frequency Phter Pump Natural frequercy evaluation = 38 liz Ibuse Static analysis Qualification acceleration level M .2 s k [ $ $ 0 ', N 8
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Specification No. 11- 2266
SUMMARY
OF PageC,16 of 45 .
Vendor: Fisch r Controls (brp.
EQUIPMENT QUALIFICATION Rev. 00 Mn. II . Zimmer Project No. 4130-00 Date 4 16 - S I Equipment 5 Qualification Number Description ia Location Method Results S
l- -
lE51F004 1", 26, Globe Valve P React. Bldg Finite Element Method Minimum natural frequem y lE51F005 Natural frequency evaluation = 35.05 Hz Equivalent dymmic amlysis Qualified to actml accelera-tions obtained fran piping amlysis lE51F025 1", Ao, Globe Valve A React. Bldg Minimum natural frequency lE51F026 = 35.19 Hz y Qualified to actual accelera-tions obtained fran piping amlysis 1B33F07 6 ,B 2", M, 3-Way Valve P Prim. Cont. Finite Elonent Method MiniInum mtural frequency Natural frequency evaluation = 89.7 Hz Static amlysis Qualification accelerations level for Upset & Dmrgency a=5'g', b=5'g', c=5'g' lIN012 -
2 ", Ao, Globe Valve A React. Bldg Finite clanent method Minimun mtural frequency IIF013 Na'tural frequency evaluation = 34.63 Hz aquivalent dynamic analysis Qualification acceleration Stresses limited to design level Upset & Bnergency Allombles to assure a=2.5'g', b=2.5'g', c=2.5'g' operability 1RE048 2 ", Ao, Globe Valve A Peact. Bldg Minimum natural frequency LEE 049 A = 35.48 Hz IIF001 P Qualification acceleration 1RF002 P level Upset & Bnergency Y a=3. 25 ' g ' , b=3 . 25 'g ' , c=3. 25 ' q '
m
O O O Specification No. 11- 2266
SUMMARY
OF, Page Cl'7 of h6 ,
vendor: Fischer Controls Corp. Rev. oo '
EQUIPMENT QUALIFICATION Wm. II . Zimmer Date 4 15 -f 1
- Project No. 4130-00 Equipment hj Qualification Results Description 1 Location Method Number
= S .
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React. Bldg Finite elcuent method Minimum natural frequency lE12F065A,B 2 ", Ao, Globe Valve A Natural frequency evaluation = 34.77 11z Equivalent dynamic analysis Qualification acceleration Stresses limital to design level Upset & Dnergency allowables to assure a=2.5'g', b=2.5'g', c=2.5'g' operability Minimum natural frequency lE12F051A,B 6", Ao, Globe Valve A
= 31.7 !!z Otnlified to accelerations ob*h fran piping amlysis Minirtun natural frequency lWS020 10", Ao, Globe Valve A
=27.1 IIz Qualified to accelerations obtained fran piping analysis Muumun natural frequency 1WS025 12", Ao, Globe Valve A
= 28.45 Itz Qualified to accelerations obtainal fran piping analysis
" Mirunum natural frequercy lWs030 12", Ao, Globe valve A p
= 28.3 IIz Qualified to accelerations
. obtained fran pipiry analysis 1
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Specification No. II- 2268 Vendor: J. E. Iomm
SUMMARY
OF Page C,l S of 45 - -
EQUIPMENT QUALIFICATION Rev. Oo Mn. II . Zimmer It Project No. 4130-00 Date t 5 -S 1 Equipment $ Qualification .
N er Description ga Location Method Results
- s -
1DG017A to L 3/4" x 1", Relief Valve P Aux. Bldg. Spring frequency Spring frequency - 191 IIz 1DG018A to F D.G. Static analysis Valve body is stronger than pip (
Ccriparison of area and section tb limitation on acceleratiors nodulus of valves to connected tbzzle loads limitcd by con-Pi ping nected piping lE22F014 3/4" x 1", Relief Valve P React. Blds Spring frequency - 47 Itz Valve body is stronger than pipc tb limitation on accelerations Nozzle loads limitcd by con-nected piping IC41F029A, B 1" x 1", Relief Valves P React. Bldy SprirYJ frequency - 47112 Valve body is stronger than pipe No limitation on accelerations Nozzle loads limited by con-nccted piping IIN005A, B -
1" x l\", Relief Valves P React. Bldg Spring frequency - 191 IIz valve body is stronger than pipe tb limitation on accelerations
- bzzle loads limited by con-aected piping lE12F005 1" x 1 ", Relief Valve P React. Bldg i Spring frequency - 191 IIz
/alve bcdy is stronger than pipe tblimitation on accelerations
!bzzle loads limited by con-nected pipin] *""b J
r -- i e
O O O Specification No. 11- 2268
SUMMARY
OF PageC.l9 of h .
Vendor: J. E. Ionergan EQUIPMENT QUALIFICATION Rev. oo Wm. H. Zimmer Project No. 4130-00 Date 4 81 Equipment Description h$
ia Location Qualification Results Number Method n_ __ _
lE12F030 1" x 2", Relief Valves P React. Bldg Spring frequency Sprirs frequency - 151 liz lE21F031 Static analysis Valve body is stronger thanpipe lE51F017 Ccxnparison of area and section No limitation on accelerations modulus of valves to conmated Nozzle loads limited by con-piping ,
nected piping ID0005B,D,P 1 " x 2", Relief Valves P D. G. Spring frequency evaluation Spring frequency - 181 IIz LWR 077 React. Bldg Static analysis for stresses Valve body is strorger thin pipc lE12F025A,B,C React. Bldg and deflections No limitation on accelerations lE22F035 React. Bldg Comparison of area and section Nozzle loads limited by piping modulus of valves to connected piping .
lE51F018 1 " x 3", Relief Valve P React. Bldg \ Spriry frequercy - 178 Hz -
Valve body is stronger than pipe No limitation on accelerations Nozzle loads limited by piping lE21F018 2" x 3", Relief Valve P DNict. Bldg Spring frequency - 196 Hz Valve body is .c'ronger than pipe No limitation ( accelerations Nozzle loads limited by piping lE12F036 3" x 4", Relief Valve P React. Bldg h Spring frequency - 191 Hz Valve body is stronger than pipe No limitation on accelerations Nozzle loads limited by piping
n NY p
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Specification No. 11- 2804
SUMMARY
OF PageC,2 o of 45 -
Vendor: Dresser Irflustries, Inc.
EQUIPMENT QUALIFICATION B r.v - oo Mn. H. Zimmer Project No. 4130-00 Date k-\o,. -8)
Equipment Description hk ia Locatic.,
Qualification Results Number Method ,
_t __.
_w All "
, M, Gate Valves P All Bldgs. No extended part Rigid in all directions Valves shown to be stronger Ib limitation on accelerations than pipe Nozzle loads lirrited by piping All h", M, Globe Valves P All 3/4", M, Gate Valve P All 3/4", M, Globe Valve P r p t 1B33F013A/B 3/4", Check Valves A Prim. Cont. No extended part Rigid in all directions 1B33F017A/B a Valves shown to be strorger No limitation: on accelerations lE32F010 React. Bldg than pipe Allowable rozzle loads obtaina3 lE32F0ll Valve stresses limited to to assure, operability design allowables All other 3/4", Check Valves P All Bldgs. No extended part Rigid in all directions Valves shown to be stronger Ib limitation on accelerations than pipe Nozzle loads lirrital by piping All 1", M, Gate Valve P All 1", M, Globe Valve P All 1", Check Valve P All 1 ", M, Gate Valves P '
,n All 1 ", M, Globe Valves P ,
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Specification No. 11- 2804
SUMMARY
OF Page C2 ) of 45 .
Vendor: Dressor Trvhmtries. Inc. Rev. on EQUIPMENT QUALIFICATION Wm. H. Zimmer Project No. 4130-00 Date k-\6-2l Equipment b Description hk ia Location Qualification Results Nmber Method '
.L_ -. __-
1C41F006 1 ", Check Valves A React. Bldg No extended part Rigid in all directions 1C41F007 = Valves shown to be stronger No limitation on acce1ersLiens lC41F033A/B Prim. Cont. pipe Allowable nozzle loads obtained Valve stresses limited to to assure operability
, design allowables All Other 1 ", Check Valves P All Bldgs. No extended part Rigid in all directions Valves shown to be Stronger No limitation on accelerations than connected pipe Nozzle loads limited by piping All 2", M, Gate Valves P All 2", M, Globe Valves P 1' b b lE12F084A,B,C 2", Check Valves A React. Bldg No extended part Rigid in all directions lE21F033A,B,C Valves shown to be stronger No limitation on accelerations lE531021 than pipe Allowable nozzle loads obtained lE5LF028 Valve stresses limited to to assure operability lE51F061 l' design allnwables lE22F007 All Other 2", Osck Valves P All Bldgs. No exteru part Rigid in all directions Valves shown to be stronger Ib limitation on accelerations than pipe Nozzle loads limited by piping
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_--_---_7 7 O O O Specification No. 11- 2811
SUMMARY
OF Page C2 3 of 9-5 .
Vendor: Anchor thrling valve Co.
EQUIPMENT QUALIFICATION ReV- O k%. II . Zimmer Project No. 4130-00 Date 2} - \ 6 - 3 I Equipment Description
! Qualification i a Location
- Number s s Method ,
S 1DG003A,B,C 2 ", M, Gate Valves P Diesel Effect of exteM(xl portion Rigid in all directions 1DG004A,B,C Gen. Rocm negligible on frequencies Qualification accelerat-lon 1DG007A,B,C Static arnlysis level Upset & Bnergency lDG008A,B,C *t y a=ll'g', b=10'g', c=10'g' 1T49F304 4", M, Gate Valve P React. Bldg P 1B21F527 6", Mo, Gate Valve P Turbine Natural frequency evaluation Minimun natural frequencies Bldg. Static analysis a are 160 112, 178 112.
Qualification acceleration level Upset & Bnergency a=6'g', b=5'g', c=5'g' lhR134 6", M, Gate Valve P React. Bldg Effect of valve extended Rigid in all directions Portion is negligible on Qualification acceleration frequencies level Upset & Bnergency Static analysis a=ll'g', b=10'g', c=10'g' lVP006A,B 8", Ib, Gate Valves A React. Bldg Natural frequency evaluation Minimun natural frequencies lVP012A,B
- Static analysis are 73.3 Itz & 161 IIz IVP045A,B Prim. Cont. Qualification acceleration level Upset & Bnergency a=6'g', b=5'g', c=5'g' lhE133A,B 8" M, Gate Valve P React. Bldg Effect of extended part is Rigid in all directions negligible on frequencies Qualification acceleration Static analysis level Upset & Bnergency a=ll'g ' , b=10 'g ' , c=10 'g '
V y r i- v v y r
\
O C <
O J Specification No. II- 2811
SUMMARY
OF Page C,7l of. h 5 .
Vendor: Anchor Darlim Valve Co. Rev. 60 EQUIPMENT QUALIFICATION W ,11. Zit iner Project No. 4130-00 Date 4 15-8i Equipment Description h$ Qualification g Location 1 Results g Method
_ _s , __
lE12F391 12", M, Gate Valve P React. Bldg Natural frequency evaluation Minimum natural frequencies Static analysis are 160 IIz and 179 112 Qualif"ation acceleration level Upset & Ibergency a=6'g', b=5'g', c=5'g' lE12F003A,B 14", bb, Gate Valves A React. Bldg Minimum natural frequerries lE12F016A,B are 71.9 IIz and 126 Itz lE12F017A,B U' Qualification acceleration lE12F047A,B y level Upset & Emergency a=6'g', b=5'g', c=5'g' lE12F307 14", M, Gate Valve P React. Bldg Effect of valve extendcd Rigid in all directions portion on frequencies Valve body stronger than pipe negligible Qualification acceleration Static analysis level Upset & Dacrgency Comparison of valve area arx1 a=5'g', 6 5'g', c=5'g' section modulus with pipe lE]2F006A,B 16", bb, Gate Valve A React. Bldg Natural frequency evaluation Minimun natural frequencies simplified dyrumic analysis 54.4 Hz ard 80.5 Hz for stresses and deflections Qualification acceleration of all critical cmponents to level Upset & Bnergency assure operability and strtr- a=6'g', b=5'g', c=5'g' tural integrity 4
( ,
O O O Specification No., 11- 2811
SUMMARY
OF Page Q 5 of 45 .
Vendor: Anchor / Darling Co.
EQUIPMENT QUALIFICATION Rev. co Wm. II . Zimmer \,3 - 3 I Project No. 4130-00 Date k -
Equipment Description hf Qualification g Location i Results N d er Method *
- S _
lE12F067 16", M, Gate Valve P React. Bldg Natural frequency evaluazion Minuum mtural frequency =
lE12F302A, Static analysis 158 IIz B,C Canparison of valve area and Valve body straonger than pipe section modulus with pipe Qualification accelerationlevel
, Upset & Dmrgency a=5'g', b=5'g', c=5'g' lE21F001 20", 150#, Mo, Gate Valve A Natural frequency evaluation Minimum natural frequencies are Simplifial dynantic amlysis 28.5 IIz and 35.1 IIz Qualification accelerationlevel Upset & Bnergency a=.83'g', b=2.3'g', c=2.17'g' lE12F004A,B 20", 300#, Mo, Gate Valve A ,7 Ilard prepared static analysis Minimum natural frequencies C Natural frequency evaluation 37.2 IIz and 63.911z Simplified dynamic analysis Qualification accelerationlevel Upset:
a=4.0'g', b=3.0'g', c=3.0'g' Bnergency:
a-4.5'g', b=3.5'g', c=3.5'g' l
O O O Specification No. II- 2816
SUMMARY
OF Paged)f of 45 ,
" #* " Rev. oo EQUIPMENT QUALIFICATION P oj c t t1 130-00 Date h F] l Equipment Description 5$
ia Location Qualification Results Number Method
. s y ___ m 1RG071A to F 3/8", M, Globe Valve P Aux. Bldg All valves tested at same Resonances 26.5 liz, 27.5 Hz llE081A,B time Pseudo-biaxial Test Qualification acceleration-Resonance Search 1-33 Hz level Upset & Bnergency Sine Sweep Input a=4.0'g', b=4.8'g', c=4.0'g' 1 to 10'g' llorizontal 0.5 to 5'g' Vertical Sine dwell at each restraint frequency Four orientatioris of O', 90',
180 and 270*
Duration of dwell in each orientation 240 sec. (min) 1RG041A,B 3/8", M, Angle Globe 1RG047A,B Valve 1RG051A,B,D, E,F 1RG057A to F 1RG050A to G 1", M, Relief Valve IRG070A to F 1-1/8" , M, Globe Valve V 1RG072A to F 1RG046A to II 1-1/8" , M, Expansion E Y J to N, P Valve 1RG056A to F, Y u li,J,N, P
O O O
! Specification No. II- 2816
SUMMARY
OF PageC.S 7 of 45
- Vendor: Bannson Rev. oo EQUIPMENT QUALIFICATION Wm. II . Zimmer Date k -- l 6 - g l Project No. 4130-00 Equipment hj Qualification Number Description ia Location Method Results
. s .
1RG048A 1-1/8" , M, Relief Valve P Aux. Bldg All valves tested at same Resonances 26.5 Hz, 27.5 llz time Pseudo-biaxial Test Qualification acceleration Resonance Smrch 1-33 Hz level Upset & Dnergency Sino Sweep Input a=4 . 0 ' g ' , b=4 .8 'g ' , c-4. 0 'g '
1 to 10'g' Ihrizontal O.5 to 5'g' Vertical' Sine dwell at each restraint freqdency Four orientations of O', 90',
180 and 270" Duration of dwell in each orientation 240 sec. (min) 1-3/8" , Solenoid 1RG055A to H, A J to N,P Operated Globe Valve 1RG059A to H 1-3/8" , Solenoid Operated Bypass Valve lRG045A to H 1-5/8" , Solenoid Operated Globe Valve 1RG049A to D l-5/8" , Solenoid Operated Bypass Valve 1RG052A to F 1-5/8", M, Globe Valve P 3, 1RG053A to F 'r 1RG054A to F
O O O Specification No. 11- 2816
SUMMARY
OF Page d g of 45 .
"d #* Rev. oo EQUIPMENT QUALIFICATION Wm. H. Zimmer Date 4_ ]$ -gi Project No. 4130-00 Equipment Description h$
ia Location Qualification Results Number Method
- s .
t 1FG080A,B 2-1/8", M, Globe Valve P Aux. Bldg. All valves tested at sane Resonances 26.5 Hz, 27.5 Hz 1RG082A,B time, Pseudo-biaxial Test Qualification acceleration Resonance Search 1-33 Hz level Upset & Btergency '
Sine Sweep-Input a=4. 0 'g ' , b=4 .8 ' g ' , c=4 .0 ' g '
1 to 10'g' lbrizontal, r 0.5 to 5'g' Vertical Sine dwell at each resonant frequency Four orientations of 0*, 90*,
180 and 270*
Duration of dwell in each orientation 240 sec. (min)
IBG042A,B 2-5/8", M, Globe Valve "~
1RG043A,B q k
1PG044A,B 1RG060A,B ,
l l l
l
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O O O Specification No. 11-2819
SUMMARY
OF Page (',_2 9 of L5t .
Vendor: Anchor Darlina Valve Co.
EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer Project No. 4130-00 Date jl - I S - 8 1 Equipment Description h$
ia Location Qualification Results Number Method
- S Rigid in all directions 1DG005A,B,C 2 ", M, Globe Valves P Aux. Bldg.l Effect of valve extendal Qualif.i 7 tion acceleration 1DG006A,B,C Aux. Bldg. portion on frequencies level 1SA079 React. Bldc negligible Upset &
1SA081 React. Blds Static analysis Dnerg. a=ll'g' , b=10'g' , c=10'g '
lE32F012 3", M, Globe Valve P React. 111dg lE32F013 4", M, Globe Valve P React. Bldg 4 9
lE21F012 12", m , Globe Valve P React. Bldg Natural frequencies evaluation Minim a natural frequencies Equivalent dynamic analysis are 42.1 Hz & 51.011z Qualification acceleration level Upset - a=1.35 'g' , b=1.35'g ' ,
c=1.35'g' Dnerg = a=1.5'g', b=1.5'g',
c=1.5'g'
Y eT ~3 V b7 a Specification No. 11- 2820
SUMMARY
OF P a g e "<' 3 o of 45 -
Vendor: Rockwell International Rev. oo EQUIPMENT QUALIFICATION Mn. H. Zimmer Project No. 4130-00 Date 4 - \5 - R I Equipment hj Qualification Number Description ia Location Method Results 9 ._
lE12F087A,B 3", bb, globe valve A lbactor Natural frequency evaluation Minunum natural frequencies Building Static analysis for stresses are 69.4 liz & 17911z.
and deflections Qualification Acceleration level upset & anergency a-5'g', b-5'g', c-5'g' lE51F045 4", Mo, globe valve A Reack.or Natural frequency evaluation Minunum natural frequencies Building simplified dynamic analysis 46 liz, 61 Hz Qualification acceleration 1cvel Upset: a-1.86'g', b-1.86'g',
c-1.86'g' Emergency: a-2.0'g', b-2.0'g',
c-2.0'g' lE12F023 6", Mo, globe valve P Peactor In progress Build.ing 1G33F102 6", Mo, globe valve P Prim. In progress Cont.
lE12F052A,B 8", Mo, glove valve A Reactor In progress Building o
1E12F053A,B 10", Mo, globe valve A Heactor la progress Building 1E12F048A,B 14, bb, globe valve A Reactor In progress Building
a O O O Specification No. 11-2821
SUMMARY
OF. Page (13 ] of 4-5 .
Vendor: Mission nmufacturing Co. Rev. oo EQUIPMENT QUALIFICATION Wm . 11. Zimmer Proj,ect No. 4130-00 Date h \ C7- S\
Equipment Description hki Location Qualification Results Number Method
.S .
1CY046 2b", check valve P Beactor In progress Building 1SA080 .
lIN063 3", check valve P Reactor In progress Building .
lWS074A,B CW.P.IIS lWS077A,B Reactor Building lE21F303. 4", check valve P Reactor In progress Building LWR 136 6", check valve P Prim. In progress Cont.
lE51F0ll Reactor Building lE51F030 6", check valve A Beactor -
Buildir.g IVP046A,B 8", check valve P Prim. In progress Cont.
lE51F040 8", check valve A Reactor In progress Buil.c ing
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Specification No. ,11-2822
SUMMARY
OF Page(.3a of 45 -
Vendor: Anchor Darling Valve Co.
EQUIPMENT QUALIFICATION Rev. oo Mn . II . Zimmer Date k_ \$ - 81 Project No. 4130-00 Equipment Description hk Qualification Results g Location i
N e er Method
- S . .
lE21F003 l'2", Non-Slam Check Valve A Reac. Bldg. No extended part Rigid Valve body analysis for No limitation on accelerations
- maximun nozzle loads to Allowable nozzle loads obtainec
' assure operability to assure operability lE12F031A,B, 14", Non-Slam Check Valve A Reac. Bldg. y , ,
o O
y i i y r O O O Specification No. H- 2823
SUMMARY
OF PageOMIf- of 45 -
Vendor: Mn. H. Powell Co.
P FI m g Rev. o o Mn. H. Zimmer '
Project No. 4130-00 Date -t -- l 9
- RI Equipment Description hk ia Location Qualification Results Method
. s
- lE12F039A,B 3", Check Valves P React. Bldg. No extended part Rigid C,D Ccrparison of Valve body Valve body shown to be stronger lE12F304 Area and section nxxlulus than connectcd piping lE12F305 Nozzle lmds li lnitcd by piping lE12F306 lE12F054A,B 4", Check Valves P lE51F023 & n u
lE12F046A,B, 4", Check Valves A u No extended part Rigid .
C Static amlysis for maxinun No limitation on accelerations lE12F089 nozzle loads to assure Allowable nozzle loads cbtained operability to a'ssure operability 4
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y v i i r 1 O O O Specification No. H-2852
SUMMARY
OF Paged.3 6 of k$ .
Vendor: Kerotest Manufacturing Corp.
EQUIPMENT QUALIFICATION Rev. oo Mn. H. Zimmer Project No. 4130-00 Date k-16-R1 Equipment Description hk ia Location Qualification Results N uber Method
- s '
101005 , Ao, Globe Valves A React. Bldg Qualification in progress 101006 with Vendor 101012 ,
101014 1CM025 1CM026 y < -
91 Valves "
, M, T-Type, Globe P All Bldgs. No considerable valve Rigid Valves extended part No limitation on accelerations Valve body shown to be Nozzle loads limited by stronger than pipe connected pipe 25 Valv'es "
, M, Y 'Iype, Globe P <r Valves 9 101003 3/4", Ao, Globe Valves A Reacs. Bldg Qualification in progess 101004 with Vendor 1B33F019 1B33F020 Prim. Cont.
lE12F060A,B React. Bldg lE12F075A,B 4 "
lE12F338A,B,C 3/4", Mo, Globe Valves P Prim. Cont.
1E21F330 1E22F314 .
lE51F317 i
~
& y O O O Specification No. !!-2852 .
SUMMARY
OF Paged 3 7 of k$ -
Vendor: Kerotest 2nufactur.tng Cbrp.
EQUIPMENT QUALIFICATION Rev. oo wm. II . Zimmer Project No. 4130-00 Date 4 S t Equipment Description h$
ia Location Qualification Results Number Method s -
574 Valves 3/4", M, Globe Valves P All Bldgs. Ib considerable valve Rigid Extended part No limitation on accelerations Valve body shtsn to be stronger Ibzzle loads limited by than connected pipe connected pipe 1.IN008A,B 1", bb, Globe Valves P React. Bldg Qualification in progress 1E12F099A,B A Prim. (bnt. with Vendor iE51F076 A Prim. Cont.
IVQOl6A to H, 1", M, Globe Valves P All Bldgs. No considerable valve : Rigid J to N, P Exterxled position ?b limitation on accelerations LWR 152 Valve body shown to be stronger Nozzle loads limito-1 by pipe lhT1153 than pipe 1C41F015 1C41F018 1C41F019 1C41F020 1C41F024 1C41F025 lE12F076A,B ,
lE12F077A,B lE12F078A,B lE12F079A,B lE12F326A,B lE12F327A,B .
lE51F334 lE51F335 u
O O O Specification No. 11- 2852 Vendor: Kerotest Manufacturirg Corp.
SUMMARY
OF PageC%8 of 4.5 .
p p . ION Rev. oo Vb. H. Zimmer Project No. 4130-00 Date k i5-8i Equipment Description h$
ia Location Qualification Results N aber Method
- S -
- . = . . -
]WR158A,B 1 ", bb, Glom Valves A React. Bldg Qualification in progress
- lLR160A,B React. Bldg with Vendor 1B21F067A,B, Atoc. Bldg.
C,E lE12F073A,B React. Bldg lE12F074A,B -
lE32F001A,B C,D lE32F002A,B C,D 1E32F003A,B C,D lWS160 1 ", M, Globe Valves P All Bldgs. No considerable valve Rigid lWS161 Extended part No limitation on accelerations 1tc162 Valve bcxty shown to be Nozzle loads limited by lWS163 stronger than pipe connected pipe IC41F003A,B lC41F008 1C41F016 lC41F037 lE12F080A,B lE12F081A,B v
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O O O Specification No. H- 2832
SUMMARY
OF Page0301 of L-5 i .
Vendor: kerotest mnufacturing Corp.
EQUIPMENT QUALIFICATION Rev. CO H. h er Date 9 8 )
- Project No. 4130-00 Equipment Description 5$
ia Location Qualification Results Number Method '
IVS014A,B 2", bb, Globe Valves A React. Bldg Qualification in progress 1B21F001 P Prim. Cont with Vendor 1B21F002 P Prim. Cont 1B21F005 o Prim. Cont lE32F006 A React. Bldg lE32F007 -
lE32F008 lE32F009 lE51F019 lE51F046 lE51F069 lE51F080 "
lE51F086 ,
. P 4 1T008A,B 2", M, Globe Valves P All Bldgs. No considerable valve Rigid IVC 009A,B Extended part No limitation on accelerations IVC 010A,B Valve body shown to be Nozzle loads limited by IVC 0llA,B stronger than pipe connected pipe IVC 012A,B IVC 013A,B IVC 014A,B IVC 015A,B IVC 016A,B IVQ021 .
IVQ024 lhR161 1B21F077A,B C,D 1B33F029 1B33F030 "
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1 y , 1 1 Specification No. 11- 2853
SUMMARY
OF Page C. /+.1 of 2t5 -
Vendor: Anderson, Grecrrexl & Co.
EQUIPMEt4T QUALIFICATIO?1 Rev. oo Wm. II . Zimmer Project !!o. 4130-00 Date k \ 5 - 3 \_
Equipment Description hk i Location Qualification Results Number Method ,
lIA155A,B ", Check Valves P Prim. Cont. Ib valve extended part Rigid 1B21F036A Valve body shown to be No limitation on accelerations to II, K, L, strorrJer than pipe Ibzzle loads limited by piping P,R,S 1B21F0408, "
, Check Valves A fb valve extended par't Rigid C,F,G,K,L Valve body stresses limited No limitation on accelerations to design allowables Allomble nozzle loads pro-vided to assure operability 1B21F024A,B, 3/4", Check Valves A y C,D 9 IB21F029A,B 3
C,D lIN006A,B 1", Check Valves P React. Bldg tb valve exterried part Rigid Valve body shown to be Ib limit on eccelerations stroryjer than pipe Ibzzle loads limited by pipirrj
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O O O Specification No. H- 2862
SUMMARY
OF Pageh/+l+ of h3 .
Vendor: Taroet Rock Corp.
EQUIPMENT QUALIFICATION Rev. Oo Wm. H. Zimmer /.
Project No. 4130-00 Date 4 L.
Equipment Description h$
ia Location Qualification Results Nder Method
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1 01019
, Solenoid Operated A React. Bldg Frequency evaluation Minimum natural frequency =
101020 Globe Valves Static analysis for stressen 158 Hz 1 01021 and deflections Qualification acceleration level 101022 Upset & Bnergency 1B33F355B,C a=5'g', b=5'g', c=5'g' 1B33F356B,C 0 101007 3/4", Solenoid Operated A React. Bldg 101008 Globe Valves 4 101009 10110 10111 10113 10123 10124 1B33F355A,D 1B33F356? L 1 1T49F305A,B p IIN170 1 ", Solenoid Operated lIN171 Globe Valves .
IVQ005A,B 2", Solenoid Operated IVQ008A,B Globe Valve lIN004A,B 1", Pressure Reg. Valves y lE53F015 2", Pressure Reg. Valves A y I'
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Specification No. 11-2156
SUMMARY
OF Page OI of 54 Vendor:ITE Imperial Corp.
EQUIPMENT QUALIFICATION Rev. OO Wm. II . Zimmer Project No. 4130-00 Date 4-l6-8I Equipment escdpdon h$a Location Qualification Results Number s Method s '
GE A Aux. Bldg. Instruments were qualified All' essential instruments Potential Transformer lAPO4EA with switchgear unit. See were monitored. There Model: JVM-3-643-93 lAPO4EB equipment qualification were no structural or lAPO4EC for details. functional abnormalities AG detected.
. Time Delay Relay Model: 7012-PB IR Motor Differential Relay Model GRD-202D0541 WE Ammeter / Voltmeter Model: KA-241 ID Auxiliary Relay Model: J13 P3012 GE Lockout Relay Model: 12HEA61C233 MS Test Switch Model: DPDT-DB-RH2 GE Indicating Light y V y y Model: ET-16 L - - --
V F'~ V ' i 1 v V
O., O O 3 Specification No., 11-2156
SUMMARY
OF Page D) of 66 .
Vendor:ITE Imperial Corp.
EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer Project No. 4130-00 Date S/ - / dI- 8 /
Equipment Description hk i Location Qualification Results Number Method -
.,- s_ _
IS A Aux. Bldg Instruments were qualified All essential instruments Ground Relay LAP 04EA with switchgear unit. See were monitored. There Model: GR-5 202D6141 1APO4EB equipment qualification were no structural or lAPO4EC for details. functional abnormalities IS detected.
Ground Sencor Model: GS-05 IS ,
Current Transformer Models:
MCS-21-40ll53-T2 MCS-21-40ll53-T3 MCS-21-40ll53-T4 MCB-5A-401024-T5 MCS-21-40ll53-T5 MCS-21-40ll53-T6 MCS-21-40ll56-T6 MCS-21-40ll53-T7 MCB-5A-401024-T7 MC/B-5A-401024-T7 MC-5-400862-T8 MC-5-400862-Tll MC-5-400862-T13 MC/5-Al-40ll60-T14 v v MC-SS-400898-T20 y ,e w
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Specification No. H- 2157
SUMMARY
OF Page D /t of 56 Vendor: ITE Impreial p F Rev. N .
l Wm. II . Zimmer Date #/ ~ /8- f /
Pro],ect No. 4130-00 Equipment Description h$
ia Location Qualification Results Number -
Method
- S GE Aux. Bldg.
Indicating Lamp A lAPOSE Instruments were qualified All essential instruments Model: ET-16 1AP06E with sub-station unit. See were monitored. There were 1AP07EA/B equipment qualification no structural or functiona]
i IR 1AP08EA/B for details, abnormalities detected.
I Neutral Sensor LAP 09E Model: 609301-K1 1AP10E lAPllEA/B IR 1AP12EA/B Neutral Sensor lAPl3E ,
Model: 609301-K2 LAP 14EA/B IL Potential Transformer Model: PT-6 400765-K3 IL Potential Transformer Model: PT-16 400765-K3 IL Control Switch Model: C77 1001 1CCl 0002 IL Current Sensor Model: TKM-1 4C1181-T24 sr q v
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l rm y n V ~J U Specification No. H- 2157
SUMMARY
OF Page D3 of $(;
vendor: ITE Imperial Rev' . OO Wm. H. Zimmer Date '/- / f- f /
Pro],ect No. 4130-00 Equipment Description hf ia Location Qualification Results Number Method
- S IL Aux. Bldg.
Current Transformer A 1AP05E Instruments were qualified All essential instruments Model: TKM-1 40ll81-T21 1AP06E with sub-station unit. See were monitored. There wer(
LAP 07EA/B equipment qualification no structural or functiona]
IL 1AP08EA/B for details, abnormalities detected.
Current Transformer LAP 09E Model: TEM-1 40ll81-T22 LAP 10E lAPllEA/B IL LAP 12EA/B Current Transformer LAP 13E Model: TKM-1 4Cll81-T23 1AP14EA/B IL -
Ground Sensor TL-2 Model: 400 799 K6 ID Auxiliary Relay Model: J13P3012 IR Neutral Sensor Model: 609301-K2 IL Control Power Trans-former
! Model: CP-6 401566-K1 GE Ground Relay Model: 12IAC53A803 s/ s/ V
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O O O Specification No. H-2159
SUMMARY
OF Page D8 of $4 -
Vendor: Stewart & Stevenson EQUIPMENT QUALIFICATION Rev. 00 Wm. H. Zimmer Project No. 4130-00 Date Y ~ /dI " 8 /
Equipment Description h$
ia Location Qualification Results Number Method ,
S Square D Pressure P Aux. Bldg. Qualification Tests Essential equipment is switch 1DG10CD Biaxial random motion monitored. No abnormali-Model: 9012 ACW-22 1DG10CA frequency range: 1-40 Hz ties were deducted during 1DG106E TRS enveloped RRS. and after the test.
1DG10CB Model: 9012-ACW-21 GE Control Switch 1PL10JA Model: CR2940 1PL10JB 1PL10JC se EMD Temp. Switch s'
Qualification in Progress Model: 8447100 EMD Temp. Switch Model: 7447102 H.O. TRERICE 1DGlSTA Pressure Gauge +
1DG15TL Marshaltown Pressure 1PLG6JA,B Gauge 1PLG7JA,B s/ IPLG8JA,B Y
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O O O Specification No. 11- 2175
SUMMARY
OF Page BF of $ (, .
Vendor: Unit Electric Controls, INc.
Wm. H. Zimmer EQUIPMENT QUALIFICATION Rev. Q Project No. 4130-00 Date Y-/.$*f/
Equipment Description hk ia Location Qualification Results Number Method 3 __ _'
G Electrical Indicator A Aux. Bldg. Resonance Search Tests All essential equipmnt were Type 180. Vertical Edge- 1PM07J Pseudo Biaxial Sire Sweep nonitored. No abnormalities wise DC/AC. 1PM08J Freq. range: 1-33 IIz were deducted during and after 1PM06J Qualification Test the test.
Pseudo Biaxial Sine Beat Tests Natural frequencies:
at one-half octave freq. inter- 1st SS/V: 23 IIz vals between 1-33 IIz. 2nd FB/V: 28 IIz Resulting max. acc.: 4.97 g 2nd SS/V: 30 IIz in all directions.
E Indicating Light 1PM07J No Natural Frequency in the Type ET-16 y 1PM08J the. testing Range G Control Switches A 1PM01J bbdel SB-1 1PM07J 1PM08J G Aux. Relays P 1PM08J Model: 12NG A15AS1 V
Autanatic Timing & Control P 1PM08J y Natural Frequency:
Inc. Auxiliary Relay 1st SS/V: 22,26,30 liz bbdel: 305D007L20P lst FB/V: 31 112 2nd SS/V: 26 Ilz
I I I i : 4 O O O Specification No. 11- 2175 "9" -U '
Vendor: Unit Electric Controls, Inc.
EQUIPMENT QUALIFICATION Rev. 6o Wm. II . Zimmer Project No. 4130-00 Date #/-/f-8/
Equipment Description h$
ia Location Qualification Results Method,
- s _ _ _ _ _ _ _ .. -
Transmation Signal Con-Aux. Bldg. Resonance Search: Resonance frequency are found
{ Unlaxlal Sine Sweep in the horizontal direction verters Frequency Range .5 to 35 llz at 8 and 19 liz, 3.5 and 17 liz.
el: 600 A 1m08J Qualification Test; 610TS 1PM07J All essential equipnent were 650TS Uniaxial Sine Dwell 1PM06J Frequency Range .5 to 35 IIz monitored. No abnornnlities Input acceleration = '3.0g in were detected during and after ,
all directions. the test.
Iceds & Northrup Pen IIIP13-P601 Qualification Tests All essential equipnent were Recorder Type: Speedomax 1PM06J Biaxial RandcIn bbtion monitored throughout the test.
M Mark III 1PM07J Frequency Range 1-4011z. No abnormalities were detected bbdel: 831 TRS enveloped RRS during and after the test.
832 833 i
Electro Switch Corp. 1PM07J Seismic Qualification Report Control Switch Type 1PM08J is presently being evaluated.
Series 40 y 1PM06J l
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O O O Specification No. II- 22 6 5
SUMMARY
OF Page D l'l- of g .
Vendor: Jamesbury Corp. '
EQUIPMENT QUALIFICATION Rev. 00 Mn. II . Zimmer Project No. 4130-00 Date U /f"[/
Equipment Description hk ia Location Qualification Results Number Method
,I s ,
Bettis Air Operator P Rx. Bldg. Static Analysis Natural frequency = 37.2 Hz Air Op.rator IVQ001A,B Input: x=5g; y=5g;x=5g Stress T312B-SR3-12 1VQ002A,0 Max. Max.
IVQ003A,B Spring Cartridge Ca1 0. Allow 3r IVQ004A,B Connection 19.1 105 Tensile stress ksi 19.1 105.
, Piston assembly tie bar 33.6 105.
Rx. Bldg.
NAMCO P lVH001A,B Qualification Test No abnormalties or struc-Limit Switch IVH002A,B Pseudo Biaxial sine sweep tural failure were EA-170 lVH003A,B Frequency range: 1-35 Hz detected after the test.
v IVII004 A, B Input: from 3-79 in all directions ASCO A lVH001A,B Qualification Test Operability was demon-Solenoid Valve IVH002A,B Uniaxial Sine Sweep strated. No abnormalities Model: 831655 lVH003A,B Frequency Range 10-40 IIz were detected. Structural gg IVII004 A, B Max. input acceleration integrity satisfied.
= 7.5 g Model: IITX8321 A 1VQ001A,B Qualification Test IVQ002A,B Uniaxial Sine Sweep IVQ003 A ,B Frequency Range 10-40 IIz V 1VQ004A,B Max. input acceleration
= 12.2 g V
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SUMMARY
OF -
Page D 14 of 54 -
Vendor: American Air Filter EQUIPMENT QUALIFICATION Rev. OC kb. II . Zimmer Project No. 4130-00 Date 9 - /S- 8/
Equipment Description h fl I,ocation i
Qualification Results Number Method '
M __
Mercoid Temperature A Reactor Resonance Search No resonances found in Switch DAW Bldg Uniaxial Sine Sweep the frequency range. All DAW-7036-804-S2 lVG05SA/B Frequency range: 1-35 IIz essential equipment were Qualification Test detected during and after Uniaxial Sine Dwell the test.
Frequency range: 1-35 liz Input: horiz. = 3.0g #
vert.. ,- 2.0g Barton Differential P Resonance Search Natural Frequencies Pressure Transmittal Uniaxial Sine Sweep determined Model: 385 Frequency Renge: 1-35 IIz IIoriz . (1) 4,12,17,21,28,33 Qualification Test Uniaxia' lloriz. (2) 9,15,18, 22, 30 Sine Dwell at resonant Vert. = 8, 13, 29 frequencies.
Input Acceleration: Instrument was monitored IIoriz . 2.09 throughout the test. No Vert. 1.5g abnormalities were recorded.
ITT Motor Operator A Qualification Test All essential equipment Model: NII-9 5 p Biaxial Random Motion were actuated. No ab-Frequency range: 1-33 IIz normalities were detected TRS enveloped RRS up during and after the tect.
to 100 IIz a
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O O O Specification No. H-2288
SUMMARY
OF Page b I5 of 54 -
Vendor: American Air Filter Rev. OO EQUIPMENT QUALIFICATION Wm. H. Zimmer Project No. 4130-00 Date Y' /I- 8 /
Equipment Description h$
ia Location Qualification Results er Method ,
- -_ _ _ E Dwyer Magnehelic Diff. Reactor B
Resonance Search No natural frequencies Press. Gage 9' Uniaxial Sine Sweep found in the test fre-Model #2002 P lVG05SA Frequency range: 1-40 Hz quency range. All 2003 lVG05SB Qualification Test essential equipment were 2010 Biaxial Random Motion inspected. No abnormali-Frequency Range: 1-40 Hz ties were detected during TRS enveloped RRS and after the test.
Mercoid Liq. Level A Resonance Search Test No resonances found in Switch 20lNT-9806-S2 Uniaxial Sine Sweep the frequency range.
Frequency range: 2-33 Hz All essential equipment Qualification Test were monitored. No ab-Uniaxial Sine Dwell normalities were detected Frequency Range 2-33 Hz during and after test.
Input accel. 2g in all directions.
ATkomatic Deluge Valve A Resonance Search No resonances found.
Model: 5700GX Y Pseudo Biaxial Sine Sweep All essential equipment Frequency Range 2-33 Hz were monitored. No ab-Qualification Test Pseudo normaities were detected Biaxial Sine Dwell Input: during and after the test.
4.5g Horizontal 3.0g Vertical Frequency range: 2-33 Hz h
y 1 ~l i ~! !
O O O Specification No. II- 2 2 8 8
SUMMARY
OF Page D16 of 5/, .
Vendor: American Air Filter EQUIPMENT QUALIFICATION Rev. Oo hb. H. Zimmer I'rolect No. 4130-00 Date '/- /I' I /
S C Equipment e 1 Qualification D scription i a Location Results er Method
_s __ --
Alison Temp. Sensor P RX. Bldg. Resonance Search No resonances found in the Model: 1052 lVG05SA/B Uniaxial Sine Sweep frequency range'. All Frequency range: 2-35 Hz essential parts were Input acceleration = 5 g detected during and after in all directions. the test.
Qualification Test' Uniaxial Sine Sweep Frequency Range: 2-35 Hz Input acceleration = Sg in all directions.
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O O O Specification No. 11-2289
SUMMARY
OF Page D18 of 64 .
Vendor: Pacific Air Products EQUIPMENT QUALIFICATION Rev. CO Wm. II . Zimmer Project No. 4130-00 Date #/~/[ I/
S C Equipment e 1 Qualification ber Description i a Location Results Method S. _ _ .
Contromatics Damper A Aux. Bldg. Static Analysis No ndtural frequency bekk Operator Model:500-SR IVG03YA, Input resultant accelera- 33 11z. Operability was YB tion = 4.5g demonstrated by showing lVG04YA, that the operating forces V YB are higher than the
. seismic forces.
--y i : i r ;
i O O O Specification No. 11-2289
~
SUMMARY
OF Page p1tC of 5 /, -
Vendor: Pacific Air Products EQUIPMENT QUALIFICATION Rev. OO h ,H. Zimmer Date #/- / [- $ /
Pro]ect No. 4130-00 Equipment Ds ription hS ia Location Qualification N d er Method Results
- - := S .
Asco Solenoid Valve A Reactor Seismic qualification of .
Model IIT-8 30 2-B-2 5-RF Bldg. instruments are in progres3 lVG05SA lVG05SB Aux. Bldg.
lVG03YA lVG03 YB IVG04YA ,
y IVG04.YB Namco Limit Switches P Aux. Bldg.
Model: D-1200-6 lVG03YA lVG03YB IVG04YA y IVG04YB
O O O Specification No. II- 2 293
SUMMARY
OF. Page D2o of g .
Vendor: Trane Company EQUIPMENT QUALIFICATION Rev. On Wm. II . Zimmer Proj,ect No. 4130-00 Date //- / S-8/
Equipment es p n h$a ocadon Qualification Results Number Method L? _____.n . . - - -
GE Control Relay A Aux. Bldg. Qualitication Tests All essential equipment .
CR-2810-414C2 , 1PLB4J Biaxial Random Motion were monitore6. No ab-1PLB5J Frequency range: 1-40 Hz normalities were detected 1PLB6J TRS enveloped RRS during and after the test.
1PLB7J 1PLB8J .
IPLB9J GE Control Switch 1PLClJ CR-2940 1PLB3J AGASTAT Time Delay Relay 7012 GE Time Delay Relay CR-2820-B11744-2 PENN-Pressure Switch P-45NC4-43 P-45NC4-20 P-70MA-20 ' U Y II f
@ 1P s
__7 ,.
O m
(..) U I Specification No. 11- 2299 Page 02t of 64
SUMMARY
OF -
Vendor: b g Powers EQUIPMENT QUALIFICATION Rev. OO D* II
- Zi"* #
Proj.ect No. 4130-00 Date '/" /S " 8/
Equipment S C e 1 Qualification er Description i a Location Results
. S Method ,
a .
Transmation Current P Auxiliary Pesonance Search: All essential equiptents Relay & Reactor Uniaxial Sine Swep were nonitored. No Model: 210A Building Frequency Range .5 to 35 IIz abnormalities were detected.
l Fesonance found only in Qualification Test: the horizontal direction at Uniaxial Sine Dwell 8 and 19 IIz.
Frequency Range .5 to 35 IIz Input acceleration = 3.0g in all directions GE Indicating Lights P 1PM07J Resonance Search Tests All essential equignent.wcre ET-16 4 1PM08J Pseudo Biaxial Sine Sweep monitored. No abnormalities Freq. Range: 1-33 Hz were deducted during and after the test.
Qualification Test No Natural Frequency in the Pseudo Biaxial Sine Beat Tests testing range.
at one-half octave freq.
intervals between 1-33 Hz.
Resulting Max. Acc.: 4.97g in all directions.
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O O O Specification No. II- 2299
SUMMARY
OF Page D2_2 of g (, .
Vendor: K C Powers EQUIPMENT QUALIFICATION Rev. CO Wm. H. Zimmer Project No. 4130-00 Date Y" /S" N Equipment Description hk ia Location Qualification Results Number Method
- s -
~
Dwyer Differential P Aux . Bldg. Resonance Searen: No rasonances found below Pressure Indicator lWOlC Uniaxial Sine Sweep 40 Hz Model: 2010 1WO2C Frequenc,' nge 1-40 Hz 2003 lWO3C 2005 lWO4C Qualifit.m ion Test: All essential instruments 2001 lWOSA Biaxial Raadan Motion were monitored. No 2015 lWO7AA Frequency Range 1-40 IIz abnormalities were detected lWO8A TRS enveloped RRS during and after the test.
V 1WO9A UE Temperature Switch A 1VC08SA Resonance Search: Resonance was determined Series 300 lVC08SB Uniaxial Sine Sweep in the horizontal direction F303D-5AS lVX01CA Frequency Range 1-40 Hz at 38 Hz F302D-5AS 1VX01CB F300-6AS lVX01CC Qualification Test: All essential instruments IVX01CD Biaxial Random Motion were monitored. No IVX01CE Frequency Range 1-40 Hz abnormalities were detected
below 4-6 Hz Input acceleration up to 12g.
q u i 1 , ^l -
i b b_-
Specification No. 11- 2299
SUMMARY
OF Page D 2_3 of $ r, .
Vendor: FCC Powers EQUIPMENT QUALIFICATION Rev. CO Wm. II . Zimmer Proicct No. 4130-00 Date #/ ~ /I"[/
Equipment 5 , Qualification N aber Description ia Location Method Results s _ _
.1
~
Iove Controls Current A Reactor & Resonance Search: No resonance found in the Relay Aux.. Bldg. Uniaxial Sine Sweep test frequency range. All Model: 54 1PLl4JA,B Frequency Range 1-40 Itz essential equipmnts were 56 1PL60JA,B monitored. No abnormalities 1PL61JA,B 48 Qualification Test: were deducted during and 1PL69JA,B Biaxial Randcm Motion after the test.
G Transfer Switch A IPL91J Frequency range 1-40 IIz Model: SB-1 1PL92J TRS envelopcxl RIE except 1PL93J below 4-6 I!z GE Relay llMA llBll A lIN07J Input acceleration up to 1PM19JA,B 12g.
G Relay 12IIFA 51A4911 A 1211FA 51A4211 Agastat TDR A Model: 7022 7012 7000 7032 Kepco Power Supply P PCX72-0.3 ASCO 3-way Solenoid Valve A Y V Y IIBX8320-Al
O O Q 1 Specification No. 11- 2299 Vendor: MCC Powers
SUMMARY
OF P"9" Cl.D f .51
- EQUIPMENT QUALIFICATION RcV- Od Wm. II . Zimmer Project No. 4130-00 Date #/~/S-8/
Equipment Description 5$
ia Location Qua1ification Method ,
3 -
Solon Pressure Switch A Ibactor & Ibr.onance Search: Ibsonance was found during 7P11NM, SPS111EW Auxiliary Uniaxial Sine s u r a vertical swep at 21 Itz lluilding Frequency Rango 1-40 !!r only on SPS111 MEW.
All essential .instrunents Qualification Test: w re monitoral. No 131 axial Randan Motion abnornalities wro detected Frequency Range 1-40 !!z during and after the test.
Tits envelolol RRS except lelow 4-6 Itz Input acceleration up to 129 .
W&T Q11orine Detector A Ibsonanco found at 18 Ilz 50-125 in the horizontal sweep W&T Chloring Detector A y y Resonance found:
50-125D horizontal 27, 30 vertical 33, 37
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1 Specification No. Il- 2299
SUMMARY
OF Page D2 5 of 64 .
Vendor: tw pmnr n EQUIPMENT QUALIFICATION Rev. OO hTa. H. Zimmer Project No. 4130-00 Date '/ - / [ ~ 8 /
Equipment 5 Qualification Number Description ia Location Method Results
- S, c .
Delaval Level Switch A Reactor & Resonance Search: All essential instruments 36497 Auxiliary Uniaxial Sine Sweep were nonitored. No Building Frequency Range 1-40 Hz abnormalities were detected during and after the test.
Qualification Test:
Biaxial Randan bbtion Frequency Range 1-40 Hz
, TRS enveloped RIG except below 4-6 Hz Input acceleration up to i 12g.
Dwyer DP Switch A 1638-0 Pyrotronics DIS 3/5A A DIA-ll A CTZ-2 A DIA-10 A y ESC-1 P V V
O O O, !
Specification No. 11-2299
SUMMARY
OF Page b 2,6, of g .
EQUIPMENT QUALIFICATION Rev. CO Wm. II . Zimmer Project No. 4130-00 Date #/ " /f " 8 /
Equipment Description 5k Qualification g Location i Results er Method '
S. _.
Ilays Flow Transmitter A Aux. Bldg. Seismic Qualification in
- 252:A1252:0 lVG05SA progress IVG05SB l\C82Y Eagle Tiner P 1PLl4JA IIK410A6 1PLl4JB FDT Scientific Amuonia A IPLl4JA Detector 7060-Fan iloffman Smoke Detector P A-42N3609 Penn Transformer P 1PL60JA Y64AL-2 1PL60JB l Moore Signal Converter IVC 10S j bbdel: CC-65, 7800 series l
l shcroit Thornoneter P 1PL93J i' 6435-DG 1PL92J 1PL91J Ihers Reg. Co. Fbtal P lWO65 ,
Thermometer 894-2780 lWOSA 1WO9A lWO8A Ashcroft Pressure Gauge P 1PLl43JA 1009AXPR-X46 1PLl4JB q
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Specification No. II- 2 8 0 9
SUMMARY
OF Page[>J1 of SC -
Vendor: Rosemount,Inc.
F Rev. OO W. 11 . Zimmer Pro 7ect No. 4130-00 Date Y- /f- 8/
Equipment Description 5$
ia Location Qualification R sults er Method ,
- S i
Rosemount Diff. Reactor Resonance Search Reso' nance was found at Pressure Transmitter Bldg. Uniaxial Sine Sweep Horiz. = 22,24,61, Model: ll52DP7A22PB Frequency Range 1-100 Hz 69,78 IIz
^
ll52GP4A22PB Qualification Test Vert. = 68 Hz 4
Uniaxial dine Dwell 5 6 Frequency Range 1-100 Hz Instrument was monitored i
ll52GP9A22PB npu agceleradon: houghout de test.
ll52GP6A22PB . g na ecdon. No abnorma h es were detected.
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O O O l
Specification No. 11 7809_
SUMMARY
OF Page D3o of 5,f .
Vendor:__ibsmmnt- T ne- EQUIPMENT QUALIFICATION Rev. OO
- II - ZI**"#
Proj.ect No. 4130-00 Date e/-/f-f/ l Equipment Description hk ia Location Qualification R sults j
j er Method
__ mm . _..
- M -
Ibsemount Temperature P Peactor Resonance Search: Natwal Frequencies D2tector Assembly Bldg. Biaxial Sine Sweep FB/V = 7.4, 24 11z btxlel: 88-14 Wall Frequency Range: 1-35 IIz FB/V = 7.6,11, 25 IIz Bulel : 183-108-1 bbunted SS/V = 7.7, 24, !!z bhlel: 183-105-1 tulel: 183-106-1 Qualification Test: No abnormalities detected l
Biaxial Sine Sweep after the test.
at resonant frcgtencies Input: 3.09 in all l directions
O O O Specification No. 11-2816
SUMMARY
OF Page D3)
' of $(' ,
Vendor: Powers Regulator EQUIPMENT QUALIFICATION Rev. 60 Wm. 11 . Zimmer Project No. 4130-00 Date 9- /f-[/
Equipment hj Qualification Number Description ia Location Method Results
-- . :s _ -_
ITT Damper Operator A Aux. Bldg. Resonance Search Resonance detected at 42, Model: Nil-91 lVC15YA Uniaxial Sine Sweep 48 112.
IVC 15YB Frequency Range 1-50 Itz lVCl4YA Qual. Test Biaxial Random Operators were actuated IVCl3YB Motion. Frequency Range during the test. No IVC 16YA 1-50 Itz abnormalities were detec-IVCl4YB TRS enveloped RRS ted during and after test .
IVCl3YA Nr IVC 16YB .
1
a r- -i :
4 (3 (~ ("\
L/ V) V Specification No. 11-2817
SUMMARY
OF Page D31 of gg. -
Vendor: CV.:
EQUIPMENT QUALIFICATION Rev- 6O Wm . II . Zimmer Project No. 4130-00 Date ^/'/f"[/
Equipment Description 5$
ia Location Qualification
""ID8 ber Method,
- il Dwyer Differential P Aux. Bldg. Resonance Search Uniaxial No resonances below 40 11z Pressure Indicator, IVC 09SA/B Sine Sweep Model
- 2000 ,
lVC103 Frequency Range 1-40 llz Qualification Test All essential instruments Diaxial Random Motion were monitored. No abnor-Frequency Range 1-40 IIz malities were detected TRS enveloped RRS during and after the Lost Namco Limit Switch P Aux. Bldg Qualification Test No abnormalities or Model: EA170-ll302 lVCl2YA Psuedo-Biaxial Sine Sweep structural failure were 1VCl2YC Frequency Range 1-35 !!z detected after the test.
IVC 81YA, Input from 3-79 in all YB directions.
ITT Barton Dif ferentia lP Aux. Bldg. Resonance Search Uniaxial Resonant frequencies found :
Pressure indicating IVC 09SA,B Sine Sweep.Frecuency Rangt FB = 1, 12, 18, 3 2 , 3 5112 switch Model: 289A 1-35 Ilz. SS = 5,7,11,17,22,25, 30 liz.
Qualification Test Uniaxia . Vert.= 5,7,11,34,35 liz.
Sine Dwell Frequency Range 1-35 IIz Instrument was monitored Input acceleration during the test.No abnor-llori z .= 4.0g malities were recorded.
Vert. = 2.67g Rosemount Differentia] Aux. Bldg. Qualification Test Instrument was monitored Pressure Transmitter P lVC09SA Biaxial Random Motion during the test. No ab-ll51DP-3-A-22. P IVC 09SB Frequency range: 1-35 Ilz.. ormalities were recorded P lVC10S TRS enveloped RRS during and after the test, I
, r 3 ., _,..
O O O Specification No. !!-2817
SUMMARY
OF Page D $2.of _6_, -
Vendor: CVI EQUIPMENT QUALIFICATION Itev . 00 Wm . 'II . Zimmer Project No. 4130-00 Date #/ * /J - 8[
Equipment Description h$
i Location Qualification Results Number Method ,
- A ITT Damper Motor Aux. Bldg. Resonance Search Uniaxial Resonance detected at 42, Operator NII-95 P IVC 12YA Sine Sweep Frequency Rangt - 48 !!z A lVC212YC 1-50 IIz.
A IVC 81YA A lVC81YB Qualification Test Biaxial Operators were actuated A 1VC82Y Random Motion during the test. No ab-Frequency Range 1-50 Itz normalities were detected TilS enveloped RRS during and after the test ASCO Solenoid Valve A Aux. Bldg. Resonance Search No resonance found in the Model: IIB 8 320 A-1 Uniaxial Sine Sweep test frequency range. Al Freq. Range 1-4 0 !!z . essential instruments weri -
monitored. No abnormaliti. s Qualification Test were detected during and Biaxial Random Motion after the test.
Frequency Range 1-40 Itz TRS enveloped RRS except below 4-6 !!z
. Input accel. up to 129 t
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O O O Specification No. 11-2835
SUMMARY
OF Page D3 (, of Sg Vendor: Unit Electric Controls, Inc. Rev. () C' EQUIPMENT QUALIFICATION Wm. 11 . Zimmer Date (/-/f-I/
Proj,ect No. 4130-00 Equipment Description hk ia Location Qualification Results er Method S. .
Aux. Bldg.
GE Control Switches A 1PL67JA . Instrunnnts were qualified All essential equipnent were CR2940 Selector 1PL67JB with equipment. See equipnent nonitored. No abnoimalities qualification for details. were detected during and after the test.
Cuttler iia:mer Push button switches 10250T t Electro Switch Control switches Series 40 i
GE Electrical Indicators 180 Vertical Edgewise DC Transmation Signal Converters Model: 610TS GE Control Switches '
SBM GC Control Switches "
SB-1
- N' V
/
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O O O Specification No. 11-2868
SUMMARY
OF Page D3g of S r' .
Vendor: Powers Regulator EQUIPMENT QUALIFICATION Rev. SC Wm. !! . Zimmer Project No. 4130-00 Date #/"/f .f/
1:quipment 5j Qualification Number Description i. Location Method Results
. _ R. __ _ , _ _
ITT Damper Operator Aux. Bldg. Resonance Search Test Resonance detected at 42 Model # Nil-95 RX. Bldg. Uniaxial Sine Sweep and 48 IIz.
Nil-91 All ele- Freq. Range 1-50 IIz.
Nil-95-3 vation Qualification Test operators were actuated Binxial Random Motion during the test. No ab-Frequency Range 1-50 !!z normalities were detected TRS enveloped RRS during and after the test.
GE Control Relay Model A Aux. Bldg. Resonance Search Test No resonance found in the
- 1211FA51A49 1PLl4JA Uniaxial Sine Sweep test frequency range. All Frequency Range 1-4 0 11z essential instruments were .
Qual. Test Biaxial Random monitored. No abnormalitit .s Motion , were detected during and Frequency Range 1-4 0 11z. after the test.
TRS enveloped RRS except below 4-6 IIz .
Input accel.up to 129 Namco Limit Switch A Aux. Bldg. Seismic qualification is Model: EA-750-20100 RX.Blu, . in progress.
All Elevation:
O O O ,
Specification No. !!-2874
SUMMARY
OF. Page D 3 of of 5g .
Vendor: American Narming & Vent.Co.
EQUIPMEf1T QUALIFICATI0t1 Rev. 60 Wm. H. Zimmer -
'/- /3 "p Project No. 4130-00 Date I' qui pment Description 5$
ia Location Qualification Results Number Method ,
- _ 3 Namco Limit Siwtch Aux. Bldg. Seismic Qualification is Model: EA-740-70100 A lVG06YA/ in progress YB IVG07YA/
YB lVG09YA/
YB lVG10YA/
YB IVG0lYA/
YB IVG08YA/ ,
u YB ITT Motor Operators A Aux. Bldg .
Model: Nil . -9 5 ,91 lVG06YA/B IVG07YA/B IVG08YA/A IVG09YA/B lVG10YA/B IVG0lYA/B Y v IVQ10Y
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Specification No. Il-2 8 81
SUMMARY
OF. Page D4o of 54 .
Vendor: Reliance Electric Co.
EQUIPMENT QUALIFICATION Rev. 66 Wm. II . Zimmer Pro],ect No. 4130-00 Date 9*/["[/
Equipment 5$ " "
Qualification Results
< Number $ Method s __ _
GE Indicating Light A Aux. Bldg. Resonance Search Tests All essential equipment ET-16 RX. Bldg. Pseudo Biaxial Sine Sweep were monitored. No abnorm-
, IPL79.T Preg, range: 1-33 IIz allties were deducted IPM18J Qualification Test during and af ter the test.
Pseudo Blaxial Sine Beat No natural frequency in Tests at one-half octave the testing range.
freq. intervals between 1-33 IIz Resulting max.acc. 4.979 in all directions.
GE Test Switch A Aux. Bldg. Qualification Test All essential equipment CR2940 1PM18J Biaxial Random Motion. were monitored. No abnorm- 1 Prequency range 1-40 IIz aliites were detected TRS enveloped RRS. during and after the tcst.
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O O O Specification No. 11-2881
SUMMARY
OF Page D41 of 54 ,
Vendor: Reliance Electric Co. p Ren CC Wm . II . Zimmer Pro],ect No. 4130-00 Date #[~~/I-8/
Equipment Description 5$
ia Location Qualification Results Number Method r.r . _ . - . __ _ . - ._____- __
GE Auxiliary Relay A Aux. Bldg. Resonance Search No resonance found in the Model: 12ilFA51A4911, RX. Bldg. Uniaxial Sine Sweep test frequency ' range.
1211MAllBll LPM 18J Frequency range 1-40 !!z All essential equipment 1PL79J Qualification Test: were monitored. No abnor-Biaxial Random Motion malities were deducte Frequency range 1-40 liz during and after the test TRS enveloped RRS except below 4-6 liz Input acceleration up to '
12g.
WE Test Switches A Aux. Bldg. See seismic qualification No resonances found below Type FT-1 1PM18J of siwtch gear unit under the test frequency.
Specification 11-2156 for All essential instruments details, were monitored. No abnor-malities were detected.
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O O O Specification No. C-135 Vendor: Electro Switnh_forp.
SUMMARY
OF Page Dk3 of 1 .
EQUIPMENT QUALIFICATION Rev- 60 wm. II . Zimmer Project No. 4130-00 Date '/- /f- 8/
Equipment Description lh {
i Location Qualification Results Nuber Method ,
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Electro Switch A Aux. Bldg Seismic qualification are
!!and swi tch 1PM08J being presently evaluated Series 40 4
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Specification No. C-442
SUMMARY
OF Page D/t 4 of g_g_ .
Vendor: Electro Switch Corp.
EQUIPMENT QUALIFICATION Rev. 66 Wm. II . Zimmer Project No. 4130-00 Date Y- /f- 8/
Equipment Description h$ Qualification g Location i
Number Method R sults 1 _ -- . .
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GE Iland Switch SB-1 A Aux.Dldg. Resonance Search. No resonance fo.und in the 1PM065 Uniaxial Sine Sweep test frequency range.All Frequency Range 1-40 112 essential equipments were Qualification Test: monitored. No abnormali-niaxial Random Motion ties were deducted during Prequency range 1-4 0 IIz and after the test.
TRS enveloped RRS cxcept below 4-6 !!z Input acceleration up to 129 9
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4 l Specification No. C-444
SUMMARY
OF Page D4r of 54 .
Vendor: General Electro Co. Rev. 6d EQUIPMENT QUALIFICATION bb. H. Zimmer Y- / 6 - 3/
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. Project No. 4130-00 Date 3
Equipment Description h$
1 a Location Qualification Results Number Method s -
GE A Aux. Bldg. Qualification Tests All' essential equipment Selector Switch 1H13-P601 Biaxial Random Motion were monitored. No
- CR2940 Frequency range
- 1-40 Hz abnormalities were i
TRS enveloped RRS detected during and after the test.
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Specification No. C-445
SUMMARY
OF Page DZt 1 of S<C .
Vendor: General Electri EQUIPMENT QUtLIFICATION Rev. C6 Mn. II. Zimmer Pro),cct No. 4130-00 Date P/ f~ 8/
i Equipment escription h$a Location Qualification Results Number Method ,
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GE Control Switch A Aux. Bldg. Resonance Search: hu resonance found in the
- Model: SBM 11Il2-P60 3 Uniaxial Sine Sweep test frequency range. Al Freq. Range 1-40 Hz essential equipments were Qualificatior Test: monitored. No abnormali-Biaxial Random Motion ties were deducted during Frequency Range 1-4 Hz and after the test.
TRS enveloped RRS except below 4-6 IIz.
Input acceleration up to 12g.
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Specification No. P0272H
SUMMARY
OF Page D 49 of $4 vendor: E hn % E w pter_i") EQUIPMENT QUALIFICATION Rev. SC i Wm. II . Zimmer Project No. 4130-00 Date '/ ~ /f" [/
I Equipment escripdon N$a Location Qualification Number Mo'chod Results
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$ Elma Engineering P Aux. Bldg Seismic qualification 24VDC Power Supply 1PM08J in progress 1.
Model: 164C5261-1 s
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O O O Specification No. PO-2876
SUMMARY
OF Page D5o of 5 / -
Vendor: Transmation EQUIPMENT QUALIFICATION Rev. OC Mn. H. Zimmer Project No. 4130-00 Date @'- /.5'- 8/
Equipment Description 5$
ia Location Qualification Results Number Method -
s Transmation Thermo- A Aux. Bldg. Resonance Search Resonance frequency couple A1:ams 1PM08J Uniaxial Sine Sweep are found in the i Model: 610 A-E ( A-X- 5 ) - 1PM07J Frequency Range . 5-35 IIz horizontal direction 235 1PM06J at 8,16,19 Hz Qualification Test Transmation Signal A 1T49-P865 Uniaxial Sine Dwell All essential were Converter 1T49-P866 Frequency range .5-35 Hz monitored. No abnormali-Model: SS20A-243, 1PL67J Input acceleration = 3.0g ties were detected during 610IT-T-XS lH13-P628 in all direction. and after the test.
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- I I 3 - 1 O O O Specification No. PO-2876
SUMMARY
OF Page D51 of 5( .
Vendor: Transmation EQUIPMENT QUALIFICATION Rev. oo Wm. II . Zimmer Project No. 4130-00 Date Y-/f"A/
Equipment Description 5$
ia Location Qualification Results Number Method
- 1 __. . - . . .. .
Transmation Thermo- A Aux. Bldg. Resonance Search Resonance frequency are Couple Alarms 1PM08J Uniaxial Blac Sweep found in the horizontal Model: 610A-E(A-X-5)- Frequency '/ :mge . 5-35 IIz direction at 8 ,16 ,1911z .
235 Qualification Tesc All essential instruments Uniaxial Sine Lwell were monitored. No abnorm-Transmation Signal A Aux. Bldg . Frequency Range .5 to alities were detected Converter 1T49-P865 35 IIz. Input acceleratior during and after the test.
Model: S520A-243, 1T49-P866 = 3.0g in all directions.
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i i i i i O O O Specification No. PO 2949
SUMMARY
OF Page D.54 of Sg .
Vendor: C.S. Gordon EQUIPMENT QUAL.IFICATION Rev. Oo Wm. !! . Zimmer Y~/[~[/
Project No. 4130-00 Date Equipment Nj Qualification Number Description ia Location Method Results n
CS Gordon Thermocalples A Reactor Qualification Method Based on the analycis and Model: 404-3107-050 Bidg. Static Analysis the design of the thermo-Maximum acceleration used: couple supports the niaxi-7.5g horiz. mum combined stress is 2.259 vert. 9,479 psi (max, allowable
= 30,000 psi) e
i r 1 O O O Specification No. B/M
SUMMARY
OF Page D55 of g'e '
Vendor: Refer Below EQUIPMENT QUALIFICATION Rev. OO wm. II . Zimmer Project No. 4130-00 Date V- / f- A/
. (; C 1:quipment c 1 Qua1ification Number
""U E 5U" fd I'oca tion Method Results 4 rl - _ _ _ .
GE Electrical Indica- A Aux. Bldg . Resonance Search Tests All casential equipment tor Type 180 Vertical lill3-P601 Pseudo Diaxial Sine Sweep were monitored. No ab-Edgewise 1PL67JA Prequency range: 1-33 Itz normalities were deducted 1PL67J11 Quali fication Test during and after the test Pseudo 11iaxial Sine Beat Natural frequencies:
Test at on-half octave 1st SS/v:12311z frey, intervals between 2nd FB/V:2811z 1-33 IIz. Resulting mat. 2nd SS/V:30ll:
acc.: 4.979 in all directions.
Leeds & Northrup Pen A Aux. Bldg. Qualification Tests: All essential equipment Recorder lill3-P601 Diaxial Random Motion were monitored throughout Type: Speedomax Preg. range 1-40 llz the test. No abnormalitle: ,
Mart III TRS enveloped RRS were detected during and Model: 832,833 after the test.
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