Text

Confirms Required Mod to Valve V11-2006 Completed,Resolving Open Issue Identified in Sser 4 (NUREG-0798).Valve Meets Applicable Seismic Qualification Criteria.Addl Sqrt Forms for Equipment Installed & Qualified After Audit Encl
	ML20099H654
Person / Time
Site:	Fermi
Issue date:	11/20/1984
From:	Jens W; DETROIT EDISON CO.
To:	Youngblood B; Office of Nuclear Reactor Regulation
References
	RTR-NUREG-0798, RTR-NUREG-798 EF2-71997, NUDOCS 8411280241
	Download: ML20099H654 (121)
	v • d • e

6 myne H. Jins Vce Pres 4ent Nuclear Operanons Detroit

""~i Edison =400 North Disse Heghaf 6

= * " -

November 20, 1984 EF2-71997 Director of Nuclear Reactor Regulation Attention:

Mr.

B.

J.

Youngblood, Chief Licensing Branch No. 1 Division of Licensing U.

S.

Nuclear Regulatory Commission Washington, D.C.

20555

Reference:

1)

Fermi 2 NRC Docket No. 50-341 2)

Detroit Ed.ison Letter to NRC," Submittal of SQRT List Update and Responses to Open Items", EF2-68287, dated June 22, 1984.

3)

NUREG-0798, Safety Evaluation Report -

Supplement No.

4, dated September, 1984.

Subject:

Seismic Qualification of Equipment

Dear Mr. Youngblood:

Section 3.10 of Reference 3 indicated that as a result of the NRC's review of Reference 2, only Item (2) (c) [as identified in Section 3.10 of Supplement 3 to the SER] remained open.

Edison has reviewed the status of valve Vll-2006 and confirms the required modification has been completed, and the valve now meets the applicable seismic qualification criteria.

This should resolve this remaining issue identified in SSER 4.

In addition, in accordance with SSER 3, item 3.10 (2) (d), and SSER 4, item 3.10.2 (b), attached are additional SQRT forms for equipment installed and qualified after the SQRT audit.

These forms constitute the last set of SQRT forms to be submitted prior to fuel load.

Edison, therefore, confirms that all safety-related equipment currently identified to be installed at time of fuel load is seismically qualified.

As you are aware, Detroit Edison has a seismic qualification program to address future design changes with related Seismic Category I equipment.

Edison will notify you of design changes identified subsequent to this letter and before fuel load, which require the qualification of additional equipment or structures not currently encompassed in Fermi 2 seismic qualification submittals to date.

0 0 000 g

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q IN'

Mr.

B.

J. Youngblood EF2-71997 November 20, 1984 I

Page 2 i

If you have any further questions on this matter, please contact i

Mr.

O.

K. Earle (313) 586-4211.

l Sincerely, i

i

/.

\\

/

cc:

Mr.

P.

M.

Byron Mr. M.

D.

Lynch Mr. A.

Lee USNRC, Document Control Desk Washington, DC 20555 i

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.Mr. B. J. Youngblood EF2-71997 November 20, 1984 Page 3 i

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Qualification Sammary of Equipment I.

Plant Emme: Enrico Fermi Atomic Power Plant - Unit 2 Type :

1.

Utility:

Detroit Edison Company FWR 2.

ESSS:

GE 3.

A/E:

DECO EUR X

II.

Component Esme Annubar Flow Element 1.

Scope:( )NSSS

( X) BOF 2.

Model Ntaber:

ANR 76 3.

Vendor:

Dicttrich f't,nd,r4 corp.

4.

If the component is a cabinet or panel, name and model No. of the devices included:

(See Section VIII) 5.

Physical Description a.

Appearance (See Section II) b.

Dimensions 21.3 7" long, probe 0.813" x 0.813" squa re (approx. )

l c.

Weight 10.5 lbs. (a pprox. )

6.

Ioca tion: Building:

Auxilia ry i

Elevation:

691'-3" 7.

Field Mounting Condition ( ) Bolt (No.

, Size

)

(x) Weld (Iangth 5.7"

)

()

3.

a.

System in which located:

T-46 b.

Functional Description Mensuren flow Is the equipment required for( ) Mot Standby ( ) Cold Shutdown

c.

( X) 30th

( )Neither 9.

Pertinent Referenced Design Specifications IEEE 3_44-1975 J

['

SQRT FORM Page 2 III. Is Equipment Available for Inspection in the Plantf(X)Yes( )No However it is inaccessible.

IV.

Equipment Qualification Method:

( ) Test (X) Analysis

( ) Combination of Test and Analysis Qualification Report *: ER-5109, Rev. A, " Seismic Analysis Qualification Annubar Flow Element Model ANR 76, Jan. 25, 1984 DECO File No. R3-865 Company that Frepared Report: Dieterich Standard Corp.

Company that Reviewed Report Deco V.

Vibration Input 1.

Loads considered: a.(X) Seismic only b.( ) Hydrodynamic only c.( ) Combination of (a) and (b)

I 2.

Method of Combining RRS:( ) Absolute Sun ( )SRSS (X)

N/A other, specify 3.

Required Response Spectra (attach the graphs):

N/A 4.

Desping Corresponding to RRS: OBE N/A SSE N/A 5.

Required Acceleration in Each Direction:( )1FA (X) 5g horizontal 3g vertical other, specify 6.

Were fatigue ef fects or other vibration loads considered?

(X)Yes

( )No If yes, describe loads considered and how they were treated in overall qualification progran:,The st rouhal f requency of the fluid probe system was calculated and was coy ared_with the natural fre-quency of the probe to ensure that the fluid forcing functson would not cause the probe to resonate.

CHOTE:

If more than one report complete items IV through V11 for each report.

21.2

SQRT FORM Page 3 VI.

If Qualification by Test then Canylete*: N/A 1.( ) Single Frequency

( )Nulti-Frequency

( ) ra ndom

( ) sine beat

()

other, specify 2.( ) Single Anis

( )Nulti-Amis 3.

no. of qualification Tests: OBE SSE Cther 4.

Frequency Range:

5.

natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical) :

S/S -

F/ s -

V-6.

Method of Determining Natural Frequencies

( ) lab Test

( )1n-Situ Test

( ) Analysis 7.

TRS enveloping RRS using Multi-Frequency Test ( )Yes ( Attach TRS & RSS Graphs)

( )No 8.

Input g-tevel Test: OBE S/S =

F/ B =

V=

Ssz S/S -

r/a-V-

9.

Imboratory Mounting:

1.( ) Bolt ( No.

. Size

)

( ) Weld (Irngth

) ()

10. Functional operability verified ( )Yes ( )Mo( ) Mot Applicable

11. Test Nesults including modifications made:

12. Other teste performed (such as aging or fragility test, including results):

CNOTE: If quellfication by a combination of test and analysis also complete 1 ten VII.

21.3

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SQRT PORM Page 4 VII. If Qualification by Analysis, then Complete:

1.

Method of Analysis:

( ) Static Analysis (X) Equivalent Static Analysis

( )Dynesic Analysis

( ) Time-Bistory ( ) Response Spectrum 2.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S =Not determinedF/B =

299 HZ V=

299 HZ 3.

Model Type:( )3D

( )2D (X)1D

( ) Finite Elessent( ) Bean ( ) Closed Fo 1s Solution 4.( ) Computer Codes:

Frequency Range and No. of modes considered:

(X) Hand Calculations j

5.

Method of Combining Dynamic Responses:( ) Absolute Sum ( )SRSS

( )0ther:

N/A (specif y) 6.

Damping: OBE - SSE - Basis for the damping used:

N/A 7.

Support Considerations in the model Fixed S.

Critical Structural Elements: Exterior probe and internal tubes Coverning Load or Response Seismic Total Stress A.

Identification Location Cambination Stress Stress Allowable Probe Static Port 1795 2282 18,800 psig inner Tubos Welds 3208 4210 18,800 pelg Man. Critical Maximum Allowable Deflection to 5.

Deflection Location Assure Functional Operability 1.02 x 10"3(n St atic port 5' or 0.715 in.

of probe I

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SQRT PORM Psse 5 Vill. List of Subcomponents N/A Model No. -

Weight -

Mas subcomponent

tacation - If subcom-Was Component operability veri-ponent use actually present or mass fled (Y or N or Neue pre sent simulated?

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fII Page 1 SQRT FORM l

Qualification Summary of Equipment I.

Plant Name: Enrico Fermi Atomic Power Plant - Unit 2 Type:

1.

Utility:

Detroit Edison Company FWE 2.

NSSS:

GE 3.

A/E:

DECO BWE I

II.

Component Name Presure Transmitter 1.

Scope:( )MSSS (X) BOP 2.

Model Number:

ll53GB7 3.

Yeador Rosemount 4.

If the component is a cabinet or panel, name and model No. of the devices included:

(See Section VIII) 5.

Physical Description a.

Appearance (See Gection II) b.

Dimensions 4-1/2" x 4-1/2" x 9" H c.

Weight 13 lbs.

6.

Location: Building:

Reactor Elevation:

Varies 7.

Field Mounting Condition ( ) Bolt (No. 4

, Size 5/16")

( ) Weld (Length

)

()

i 8.

a.

System in which located:

T-49 b.

Functional Description Measurement of Cage Pressure Is the equipment required for( ) Hot Standby ( ) Cold Shutdown c.

(X)Both

( )Neither 9.

Pertinent Referenced Design Specifications IEEE-344-1975

SQRT FORM Page 2 i

III. Is Equipment Available for Inspection in the Plantf(X)Yes( )3o IV.

Equipment Qualification Method:

(X) Test

( ) Analysis

( ) Combination of Test and Analysis Qualification Report *: Rosemount Report 108025, Rev. B, 2/22/83:

g,ualification report for pressure transmitters (No., Title and Date)

Rosemount Model 1153 Series B (DECO #Cl-1689)

Company that Prepared Report:

Rosemount Company that Reviewed Report:

DECO V.

Vibration Input 1.

Loads considered: a.(X) Seismic only b.( )Hydrodynanic only c.( ) Combination of (a) and (b) 2.

Method of Combining RRS:( ) Absolute Sun ( )SRSS

()

N/A other, specify 3.

Required Response Spectra (attach the graphs):See Attachment "A" (Generic Requirement by the vendor) 4.

Damping Corresponding to RRS: OBE 5%

SSE 5%

5.

Required Acceleration in Each Direction:( ) EPA

()

other, specify 6.

Were fatigue effects or other vibration loads considered?

(X)Yes

( )No r

If yes, describe loads considered and how they were treated in overall qualification program:

Sine _ vibration sweep in a limited frequency range _to simulate semi-rigid mounting at field.

CNOTE: If more than one report complete items IV through VII for each report.

l I

l

SQRT FORM Page 3

.N VI.

If Qualification by Test then Complete *:

1.( ) Single Frequency (X) Multi-Frequency

( ) random

( ) sine best

()

other, specify 2.( ) Single 4xis (X) Multi-Azis 3.

No. of Qualification Tests: OBE 5 SSE 1 Other 4.

Frequency Range:

1-33 5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical): RIGID. See note 1 below.

S/S =

F/B =

V=

6.

Method of Determining Natural Frequencies See note 1 below

( ) Lab Test

( )In-Situ Test

( ) Analysis 7.

TRS enveloping RRS using Multi-Frequency Test (X)Yes (Attach TRS & RRS Graphs)

( )Mo See Attachment "A" 8.

Input g-level Test: OBE S/S =

F/B =

V=

N/A SSE S/S =

F/B =

V=

9.

Laboratory Mounting:

1.(X) Bolt (No. 4, Size 5/16) ( ) Weld (Length

) ()

10. Functional operability verified:(X)Yes ( )No ( )Not Applicable

11. Test Results including modifications made:

Satisfactory

12. Other tests performed (such as aging or fragility test, including results):

Aging: Thermal, Functional, Radiation, Seismic.

Results:

Satisfactory CNOTE: If qualification by a combination of test and analysis also complete Item VII.

Item VII. Note 1.

Resonance search was conducted by c low level (approx 0.2g single axis sine sweep from 1 to 60 HZ, in each of three orthogonal axes.

The sweep rate was one octave par minute. The test results are given in Table 16, Page 44 of the O.T.R. (Type Test Report, Vol. 1, Test Results).

?

SQRT FORM Page 4 VII. If Qualification by Analysis, then Complete: N/A 1.

Method of Analysis:

( ) Static Analysis

( ) Equivalent Static Analysis

( ) Dynamic Analysis

( ) Time-History ( ) Response Spectrwt 2.

Natural Frequencies in Each Direction (Side / Side, Front / Bach, Vertical):

S/S -

F/B -

V-3.

Model Type:( )3D

( )2D

( )lD

( ) Finite Element ( ) Beam ( ) Closed Form Solution 4.( ) Computer Codes:

Frequency Range and No. of modes considered:

( ) Hand Calculations 5.

Method of Combining Dynamic Responses:( ) Absolute Sim ( )SRSS

( )Other:

(specify) 6.

Damping: OBE SSE Basis for the damping used:

7.

Support Considerations in the model:

8.

Critical Structural Elements:

Governing Load or Response Seismic Total Stress A.

Identification Location Combination Stress Stress Allowable l

Max. Critical Maximum Allowable Deflection to B.

De flection Location Assure Functional Operability 1

SQRT FORM Page 5 VIII. List of Subcomponents Model No. -

Weight -

Was subcomponent

Location - If subcom-Was Component operability veri-ponent was actually present or mass fied (Y or N or Hage present simulated?

U **)

l t

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- Yes = Yes, N = No, U = Unknown i

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o SQRT FORM 56 page 1 Qualification Summary of Equipment I.

Plant Name: Enrico Fermi Atomic Power Plant - Unit 2 Type:

1.

Utility:

Detroit Edison Company PWR 2.

ESSS:

GE 3.

A/E:

DECO BWR X

II.

Component Name Differential Pressure Transmitter 1.

Scope:( )NSSS

( X) BOP 2.

Model Number:

Veltron/4 - BEJPV 3.

Vendor:

Air Monitor Corporation 4.

If the component is a cabinet or panel, name and model No. of the devices included:

(See Section VIII) 5.

Physical Description a.

Appearance (See Section II) b.

Dimensions c.

Weight 55 lbs (approximately) 6.

Location: Building:

Auxiliary Elevation:

3rd Floor 7.

Field Mounting Condition (X) Bolt (No.

2

, Sire 0.281)

( ) Weld (Length

)

(X) Additional silicon adhesive GE RTV-108 T-41 8.

a.

System in which located:

Monitor differential pressure for room b.

Functional Description pressurization (Ref. NUREG 75/087) c.

Is the equipment required for( ) Bot Standby ( ) Cold Shutdown (X ) Both

( )Neither 9.

Pertinent Referenced Design Specifications IEEE 344-1975 w

i SQRT PORM Page 2 III. Is Equipment Available for Inspection in the Plantf(X)Yes( )No

~

IV.

Equipment Qualification Method:

( 4 Test

( ) Analysis

( ) Combination of Test and Analysis Qualification Report *:

lA-57815, IEEE-323 & IEEE-344 Oualification Summary. 1/25/84. DECO File No. Cl-2529. This (No., Title and Date) report is to be used in conjunction with Cl-2530 and Cl-2531.

Company that Prepared Report: Wyle Laboratories for Air Monitor Corp.

Test Report No. 58800 and 58619 Company that Reviewed Report:

DECO V.

Vibration Input 1.

Loads considered:

a.( $ Seismic only b.( ) Hydrodynamic only c.( ) Combination of (a) and (b) 2.

Method of Combining RRS:( ) Absolute Sum ( )SRSS

( )

other, specify 3.

Required Response Spectra (attach the graphs): See Attachments "A" and "B" 4.

Damping Corresponding to RES: OBE SSE 3%

5.

Required Acceleration in Each Direction:( )ZPA (X)

See Attachment "C" other, specify 6.

Were fatigue effects or other vibration loads considered?

( X)Yes

( )No If yes, describe loads considered and how they were treated in overall qualification program: See page 22, Wyle Lab Qualification Plan 57612-1, DECO File Cl-2531.

Operational Cycling Effects.

Aging ettects of mechanical cycling were found to be insignificant.

CNOTE: If more than one report complete items IV through VII for each report.

SQRT FORM Page 3 VI.

If Qualification by Test then Complete *:

~

1.( ) Single Frequency

( X) Multi-Frequency

( X) random

( ) sine beat

()

other, specify 2.( ) Single Axis

( 4 Multi-Axis 3.

No. of Qualification Tests: OBE 5 SSE 1

Other 4.

Frequency Range:

l\\ to 40 HZ 5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

30 HZ combined. See Attachment "D", Transmissibility curve.

S/S =

F/B =

V=

6.

Method of Determining Natural Frequencies Resonance search

( $ Lab Test

( )In-Situ Test

( ) Analysis 7.

TRS enveloping RRS using Multi-Frequency Test ( X)Yes (Attach TRS in RRS Graphs)

( )No 8.

Input g-level Test: OBE S/S =

F/B =

Y=

N/A SSE S/S =

F/B =

V=

See Page 23, Wyle Qualification Plan 57612-1, Rev. A, 9.

Laboratory Mounting:

DECO Cl-2531. Mounting hole pattern of equipment is 1.( X) Bolt (No.

. Size Y(

Nd NngtY"#**) ( )

10. Functional operability verified:( X)Yes ( )No ( )Not Applicable

11. Test Results including modifications made:

Satisfactory

12. Other tests performed (such as aging or fragility test, including results):

Baseline functional, radiation, aging, time-temperature effect, operational cycling effect.

CNOTE: If qualification by a combination of test and analysis also complete Item VII.

SQRT FORM Page 4 VII. If Qualification by Analysis, then Complete:

N/A

~

1.

Method of Analysis:

( ) Static Analysis

( ) Equivalent Static Analysis

( ) Dynamic Analysis

( ) Time-History ( ) Response Spectress 2.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S =

F/B =

V=

3.

Model Type:( )3D

( )2D

( )1D

( ) Finite Element ( ) Beam ( ) Closed Form Solution 4.( ) Computer Codes:

Frequency Range and No. of modes c.onsidered:

( ) Hand Calculations 5.

Method of Combining Dynamic Responses:( ) Absolute Sun ( )SRSS

( )Other:

(specify) 6.

Damping: OBE SSE Basis for the desping used:

7.

Support Considerations in the model:

i 8.

Critical Structural Elements:

Coverning Load or Response Seismic Total Stress A.

Identification Location Combination Stress Stress Allowable Max. Critical Maximum Allowable Deflection to B.

Deflection Location Assure Functional Operability I

j SQRT FORM Page 5 l

YIII. List of Subcomponents l

Model No. -

Weight -

Was subcomponent

Location - If subcour-Was Component operability veri-ponent was actually present or mass fied (7 or E or Bame present simulated?

U **)

IEEE-33 & 344 QUAL IF iCATsca Lyyjay Document No. 1A-57815 1-25-1984 p' age 3 of 19 2.0 IEEE-323 QUALIFICATION (WYLE Report No. 58800)

2.1 DESCRIPTION

OF COMPONENTS a) Electronic Differential Pressure Transducer Manufacturer / Model: Air Monitor Corp., Veltron Series 2000 b) Eiectronic Signal Condit!oner/ Scaling Multiplier Manufacturer / Model: Air Monitor Corp., Factron Series 1500 Note: Two different models of the Factr'on Series (1000

& 1750) were quellfled in the following test. Together these models contain all of the components and systems incorporated in any other single model in the Factron line. Therefore,'their qualification will qualify all Factron models, due to their similarity of construction and components. The Factron 1000 contains all of the components and systems in the Factron 1500, plus the most sensitive system tested, a square rooting circuit, which is not incorporated in the 1500. Since the Factron 1000 is quellfled, the Factron 1500 is considered to be also.

c) Fuse Manufacturer / Model: Bussman/Fusetron FRN-R-1 d) Fuse Block Allen Bradley, 1491-N122 Manuf acturer / Model:

e) Terminal Strip Manufacturer / kodel: General Electric, CR151A2 f) Pneumatic Tubing, Polyeurethane Manufacturer / Mocal:

J.P. Stevens, MP1880 g) Electrical Wiring Manufacturer / Modelt Carol,18 ga. VTW h) Wire Connectors Manufacturer / Model: 'Molex, series 22 I) Bulkhead Connectors Manufacturer / Model: Parker, 01600-7002 j) 20" x 20" NEMA Type 4 Enclosure Manufacturer / Model: Hoffman, A20H20BLP

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FERMI RRS TRA!4SMisslBILITY (ccM81NED SPECTRA, FRoM PGS. 5-4.+ { 5-72 0F W(LE REPORT N8 58800)

p

'56 Page 1 SQRT FORM Qualification Summary of Equipment I.

Plant Name: Enrico Fermi Atomic Power Plant - Unit 2 Type:

1.

Utility:

Detroit Edison Company PWR 2.

NSSS:

GE 3.

A/E:

DECO BWR X

II.

Component Name Pressure Regulator 1.

Scope:( )MSSS (X) BOP 2.

Model Number:

Circle Seal NP20-2 3.

Vendor:

Circle Seal Controls 4.

If the component is a cabinet or panel, name and model No. of the devices included:

(See Section VIII) 5.

Physical Description a.

Appearance (See Section IX) b.

Dimensions See page 6 c.

Weight 5 lbs. approximately 6.

Location: Building:

Reactor Elevation:

2nd and 3rd Floor 7.

Field Mounting Condition ( ) Bolt (No.

Size

)

( ) Weld (Length

)

(X) Male / Female Connector 8.

a.

System in which located:

TSO b.

Functional Description Pressure Regulator for Primary Containment H -02 M nitoring System 2

c.

Is the equipment required for( ) Bot Standby ( ) Cold Shutdown (X)Both

( )Neither 9.

Pertinent Referenced Design Specifications IEEE-344-1975 i

SQRT FORN Page 2 III.

Is Equipment Available for Inspection in the Plantf(X)Yes( )No IV.

Equipment Qualification Method:

(X) Test

( ) Analysis

( ) Combination of Test and Analysis Qualification Report *: Seismic Test Report of Circle Seal Controls Part No. NP20-2 including Test Report #16262 of (No., Title and Date) Environmental Action Testing Corp. DECO File No.

Cl-2585 Com'any that Prepared Report:

Circle Seal Controls p

Company that Reviewed Report:

DECO V.

Vibration Input 1.

Loads considered: a.(X) Seismic only b.( ) Hydrodynamic only c.( ) Combination of (a) and (b) 2.

Method of Combining RRS:( ) Absolute Sun ( )SRSS l

()

i other, specify 3.

Required Response Spectra (attach the graphs): Attachment "A" Generic by Vendor 4.

Damping Corresponding to RES: OBE 1%

SSE 1%

5.

Required Acceleration in Each Direction:( )ZPA

()

n/A other, specify 6.

Were fatigue effects or other vibration loads considered?

l

( )Yes

( )No NOT MENTIONED IN TEST REPORT If yes, describe loads considered and how they were treated in overall qualification program:

C NOTE: If more than one report complete items IV through VII for each report.

I i

SQRT FORM Page 3 VI.

If Qualification by Test then Complete *:

1.( ) Single Frequency (X) Multi-Frequency (X) random

( ) sine beat

()

other, specify 2.( ) Single Axis (X) Multi-Axis 3.

No. of Qualification Tests: OBE 5 SSE 1 Other 4.

Frequency Range:

1 - 35 HZ 5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical): None below 35 HZ, Reference Page 8 of Report S/S =

F/B =

V=

6.

Method of Determining Natural Frequencies Resonance Search

( ) Lab Test

( )In-Situ Test

( ) Analysis 7.

TRS enveloping RRS using Multi-Frequency Test (X)Yes (Attach TRS & RRS At tachment " A" Graphs)

( )Ro 8.

Input g-level Test: OBE S/S =

F/B =

V=

N/A SSE S/S =

F/ B =

V=

9.

Laboratory Mounting:

1.( ) Bolt (No.

, Size

) ( ) Weld (Length

) (X) Bulkhead type fixture

10. Functional operability verified:(X)Yes ( )No ( )Not Applicable 11.

Test Results including modifications made: Satisfactory l

12. Other tests performed (such as aging or fragility test, including results):

N/A CNOTE: If qualification by a combination of test and analysis also complete Item VII.

1

SQRT FORM Page 4 VII. If Qualification by Analysis, then Complete:

1.

Method of Analysis:

( ) Static Analysis

( ) Equivalent Static Analysis

( )Dynasic Analysis

( ) Time-History ( ) Response Spectrum 2.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S =

F/B =

V=

3.

Model Type:( )3D

( )2D

( )1D

( ) Finite Element ( ) Bean ( ) Closed Form Solution 4.( ) Computer Codes:

Frequency Range and No. of modes considered:

( ) Hand Calculations 5.

Method of Combining Dynamic Responses:( ) Absolute San ( )SRSS i

( )Other:

(specify) 6.

Damping: OBE SSE Basis for the desping used:

l 7.

Support Considerations in the model:

8.

Critical Structural Elements:

Governing Load or Response Seismic Total Stress A.

Identification location Combination Stress Stress Allowable Max. Critical Maximum Allowable Deflection to B.

Deflection Location Assure Functional Operability i

I

SQRT FORM Page 5 VIII. List of Subcomponents Model No. -

Weight -

Was subcomponent

Location - If subcoor-Was Component operability veri-ponent was actually present or mass fied (Y or N or Name present simulated?

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s' SQRT FORM 67 Page 1 Qualification Susmary of Equipment I.

Plant Name: Enrico Permi Atomic Power Plant - Unit 2 Type:

1.

Utility:

Detroit Edison Company PWR 2.

NSSS:

GE 3.

A/E:

DECO BWE I

II.

Component Name Differential Pressure Switch 1.

Scope:(X)RSSS

( ) BOP 2.

Model Number:

580A-0 3.

Vendor:

ITT Barton 4.

If the component is a cabinet or panel, name and model No. of the devices included:

(See Section VIII) 5.

Physical Description a.

Appearance (See Section LK) b.

Dimensions See page 6 c.

Weight 15 lbs. approximately 6.

Location: Building:

Reactor Building sub-basement Elevation:

548'-0" 7.

Field Mounting Condition (X) Bolt (No.

4 Size 3/8 )

( ) Weld (Length

)

( )

8.

a.

System in which located:

T-2 3 b.

Punctional Description Differential Pressure Switch for Primary containment Vent System c.

Is the equipment required for( ) Bot Standby ( ) Cold Shutdown

( )Both (X)Neither 9.

Pertinent Referenced Design Specifications IEEE - 344 -1975

SQRT FORM Page 2 III. Is Equipment Available for Inspection in the Plantf(X)Yes( )Ro i

IV.

Equipment Qualification Method:

( X) Test

( ) Analysis

( ) Combination of Test and Analysis Qualification Report *:

R3-580A-9, ITT Barton Qualification Test Report; 580A Series Differential Pressure Switch; 12/83; (No., Title and Date) DECO File No. Cl-2586 (4 Volumes)

Company that Frepared Report:

ITT Barton Company that Reviewed Report:

Seismic Review by DECO V.

Vibration Input 1.

Loads considered: a.(X) Seismic only b.( )Hydrodynesic only c.( ) Combination of (a) and (b) 2.

Method of Combining RRS:( ) Absolute Sun ( )SRSS

( )

N/A other, specify 3

3.

Required Response Spectra (attach the graphs):See Attachments "A" and "B" 4.

Damping Corresponding to RRS: OBE 5%

SSR 5%

5.

Required Acceleration in Rach Direction:( )ZFA

( )

N/A other, specify I

6.

Were fatigue effects or other vibration loads considered?

(X)Yes

( )No If yes, describe loads considered and how they were treated in overall qualification program:

Accelerated aging.

Result:

Satisfactory i

cNOTE: If more than one report complete items IV through VII for each report.

i

e SQRT FORM Fage 3 VI.

If Qualification by Test then Complete *:

1.( ) Single Frequency

( X) Multi-Frequency

( )randan

( ) sine best

()

other, specify 2.( ) Single Axis (X)Nulti-Axis 3.

No. of Qualification Tests: OBE 5 SSE 1 Other 4.

Frequency Range:

1 to 100 HZ 5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical): Resonance search indicated resonance above 40HZ in all directions (Page IV-17, Volume 2 of Report)

S/S =

F/ B =

V=

6.

Method of Determining Natural Frequencies Resonance Search (X) Lab Test

( )1n-Situ Test

( ) Analysis 7.

TRS enveloping RRS using Multi-Frequency Test ( )Yes (Attach TRS & RRS Graphs)

( )No 8.

Input g-level Test: OBE S/S =

F/B =

V=

SSE S/S =

F/B =

V=

9.

Laboratory Mounting:

1.( ) Bolt (No.

, Size

)

( ) Weld (Length

) (X) Simulation of Actual Mounting

10. Functional operability verified:(X)Yes ( )No ( )Not Applicable

11. Test Results including modifications made:

Satisfactory

12. Other tests performed (such as aging or fragility test, including results):

Aging, Radiation, LOCA. Results satisfactory.

Section 4.13, pages 29 and 30.

Volume 1 of Report.

i i

CNOTE: If qualification by a combination of test and analysis also complete Iten VII.

l SQRT FORM Page 4 VII. If Qualification by Analysis, then Complete:

1.

Method of Analysis:

( ) Static Analysis

( ) Equivalent Static Analysis

( )Dynesic Analysis

( ) Time-History ( ) Response Spectrum 2.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S =

F/B =

V=

3.

Model Type:( )3D

( )2D

( )lD

( ) Finite Element ( ) Beam ( ) Closed Form Solution 4.( ) Computer Codes:

Frequency Range and No. af modes considered:

( ) Hand Calculations 5.

Method of Combining Dynamic Responses:( ) Absolute Sum ( )SRSS

( )Other:

(specify) 6.

Damping: OBE SSE Basis for the damping used:

7.

Support Considerations in the model:

8.

Critical Structural Elements:

Coverning Load or Response Seismic Total Stress A.

Identification Location Combination Stress Stress Allowable Max. Critical Maximum Allowable Deflection to B.

Deflection Location Assure Functional Operability i

l l

f I

SQRT FOitM Page 5 VIII. List of Subcamponents 1

i i

NMel No. -

Weight -

Was subcomponent

Location - If subcom-Was Component operability veri-ponent was actually present or mass fied (Y or N or Name present simulated?

U **)

l I

If Available

- Yes = Yes, N = No, U = Unknown i

\\

l 1

SQRT FORM Page 6 II.

Sketch or drawing installed Bow it has been installed or Bow it will be installed 1

, _mi...,._. mm,

v-

!L,7,' ',", "4"

=_l_-.

5QRknW,E'M.~

=

-4

- * = ' ~ - -

" ' =

r%",(Witan,7,7a.~.,,%

' +*

/

r., m.a:l/

w y/

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f fV fL 4

4. %

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=,

a 1

q $ y _ =j~'

< ur Q t,y.L

(*" o l.

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imm 999,750...

Figure 5-3.

Cu G ir.t Limt..u. L:aain; Mocel 580A-C, I

I I I u-.-

n'.s-.y,.;R..m.. =. =:= -

WIC p_ _--

.eG'. 'l" - '=~W' REF: Qua1ification Report

-r:

2 Volume

l

.e l

i lt, Appendix "A"

)

Figure 11.1 RUN OBEYZ1 Ah 2

10

........i BETA = 0.050 P

ZPA= 4.672 A

?

C C

E L

i y

gg h

r b

\\

0 H

8 19

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8 i

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iiiiii-0 1

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19 19 10 FREQUENCY - H f

Figure 11.2 RUN OED:',

A.

10, i

.....3

.....3 EETA= 6.050 2PA=

5.054 i

A 1

~

C C

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,a L

i gg E

[

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D gg-1 i

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e iiiif i

i e

i.ii.

0 1

le 10 16 -

FREQUEHCY - HZ 19 l --

e Appendix "B"

. t.5 Figure 11.11 RUN SSEYZ1 AH 3

10-BETh= 8.850 r

ZPA=

6.995 l

H C

C f

-M -

E p

it E

R A

~

T I

0 H

0 19

/

G lI

' ~'~

' '~'

10'I 9

1 5

le 10 10 -

FREQUEHCY - H2 Figure 11.12 RUN 55EY 1 A '.

e 10-BETA = 0.050 F

2FA=

9.96J A

C I

C

~

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^

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L 1

10 E

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F i

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8 10

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FREQUEHCY - HI 24 i

SQRT FORM 58 Page i Qualification Summary of Equipsent I.

Plant Name: Enrico Fermi Atomic Power Plant - Unit 2 Type:

1.

Utility:

Detroit Edison Campany PWR 2.

NSSS:

GE 3.

A/E:

DECO BWR I

II.

Component Name See attached table A-C 1.

Scope:( )NSSS (X) BOP 2.

Model Number:

See attached table A-C 3.

Vendor:

See attached table A-C 4.

If the component is a cabinet or panel, name and model No. of the devices included:

(See Section VIII) 5.

Physical Description a.

Appearance (See Section IX) b.

Dimensions Largest component is 8" x 6" x 4".

All other instru-ments are smaller.

c.

Weight All each less than 15 lbs.

6.

Location: Building:

Auxiliary, Reactor, RHR Elevation: All elevations 7.

Field Haunting Condition ( ) Bolt (No.

, Size

)

( ) Weld (Length

)

()

See Attchment D & E 8.

a.

System in which located: T41-00, T41-02, X41-03, T47 b.

Functional Description Various c.

Is the equipment required for( ) Hot Standby ( ) Cold E'hutdown (X)Both

( )Neither 9.

Pertinent Referenced Design Specifications 3071-150 IEEE-344-1975

SQRT FORM Page 2 III.

Is Equipment Available for Inspection in the Plant?(X)Yes( )No IV.

Equipment Qualification Method:

(X) Test

( ) Analysis

( ) Combination of Test and Analysis Nuclear Environmental Qualification Report of Safety Related Qualification Report *: HVAC Equipment for Enrico Fermi Atomic Power Plant, Unit 2 (No., Title and Date) CCL Report #A-610-83, November 15, 1983 Company that Prepared Report: Corporate Consulting and Development Company, LTD.

Company that Reviewed Report:

DECO V.

Vibration Input 1.

Loads considered: a.(X) Seismic only b.( ) Hydrodynamic only c.( ) Combination of (a) and (b) 2.

Method of Combining RRS:( ) Absolute Sun ( )SRSS (X)

N.A.

other, specify 3.

Required Response Spectra (attach the graphs): Figures 3.3 - 3.6 from Report - Attachment F-I 4.

Damping Corresponding to RRS: OBE 2%

SSE 5%

5.

Required Acceleration in Each Direction:( ) ZPA (X)

N.A.

other, specify 6.

Were fatigue effects or other vibration loads considered?

( )Yes

(!)No If yes, describe loads considered and how they were treated in overall qualification program:

I CNOTE: If more than one report complete items IV through VII for each report.

l l

I

SQRT FORM Page 3 VI.

If Qualification by Test then Complete *:

1.( ) Single Frequency (X) Multi-Frequency (X) random

( ) sine beat

( )

other, specify 2.( ) Single Axis (X) Multi-Axis 3.

No. of Qualification Tests: ORE 5 SSE 1 Other

4. - Frequency Range:

1 to 50 HZ 5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

(See Attached Sheets J-L)

S/S S F/B =

V=

6.

Method of Determining Natural Frequencies Low level sine sweep (X) Lab Test

( )1n-Situ Test

( ) Analysis 7.

TNS enveloping RRS using Multi-Frequency Test (X)Yes ( Attach TRS & RRS Graphs)

( )No**ROA 001 (See #11 below) 8.

Input g-level Test: OBE S/S =

F/ B =

V=

N.A.

SSE S/S =

F/B =

V=

9.

Laboratory Mounting:

See attachment D & E 1.( ) Bolt (No.

, Size

) ( ) Weld (Length _

) ( )

10. Functional operability verified:(X)Yes ( )No ( ) Mot Applicable

11. Test Results including modifications made: Test levels did not meet re-

_ quired levels due to limitatiars of the shake table. Refer to ROA 001.

The RRS peak is 33.6 compared to shake table maximum 33.4.

12, other testa performed (such as agir;g or fragility test, including results): NUREG 0588 analysis for potential aging. A recommended schedule for periodic mainteurnce is to be sunplied by MCC panels.

CNOTE: If qualification by a cooliination of test and analysis also complete Item V!i.

~,

SQRT FORM Fage 4 VII. If Qualification by Analysis, then Complete:

N.A.

1.

Method of Analysis:

( ) Static Analysis

( ) Equivalent Static Analysis

( ) Dynamic Analysis

( ) Time-History ( ) Response Spectrum 2.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S =

F/B =

V=

3.

Model Type:( )3D

( )2D

( )1D

( ) Finite Element ( ) Beam ( ) Closed Form Solution 4.( ) Computer Codes:

Frequency Range and No. of modes considered:

( ) Hand Calculations 5.

Method of Combining Dynamic Responses:( ) Absolute Sum ( )SRSS

( )Other:

(specify) l 6.

Damping: OBE SSE Basis for the damping used:

7.

Support Considerations in the model:

8.

Critical Structural Elements:

Coverning Load or Response Seismic Total Stress A.

Identification Location Combination Stress Stress Allowable Max. Critical Maximum Allowable Deflection to B.

Deflection Location Assure Functional Operability

SQRT FORM Page 5 VIII. List of Subcomponents N.A.

Model No. -

Weight -

Was subcomponent

Locatiott - If subcom-Was Component operability veri-ponent was actually present or mass fied (Y or N or Name present simulated?

U **)

If Available j

- Yes = Yes, N = No, U = Unknown

SQRT FORM Page 6 II.

Sketch or drawing installed How it has been installed or How it will be installed

i Table 2.1 Safety-Related Instruments, Seismic I, QA Level I, Class IE I

i i

i l CCL SAMLE l l

l MANUFACTURER l ENVIR01sEiffAI.1 I NO. 1794-I DESCRIPTION AND RANGE /RATillG I

MANUFACTURER l PART NUMBER I

CRITERIA i

1 i

1-1 I

I i

l I

i I

001 1 Terminal Block, 600 V l Allen Bradley l 1492-CA1 i Tele 3.1 l

l l

l I

.l l

002 i Oual Element Fuse /Fuseblock l Fusetron Fuse l Fist l Table 3.1 l

l l

l Suchanan Fuseblock l 358

'l l

l l

l I

I l

1 003 i Control Relay,120 VAC,10 A, 8 Pole i General Electric l CR120A00022AA l Table 3.1 l

l 1

l i

I i

l 004 l Control Rely,125 VOC,10 A, 8 Pole l General Electric I CR120A000041AA I Table 3.1 l

l l

l I

I l

l 005 l Control Relay, Latched 120 VAC,10 A, 8 Pole i General Electric I CA120C00022AA l Table 3.1 l

l l

I l

l l

l 006 i Control Relay,120 VAC,10 A, 8 Pole l

l l General Electric l CR120B08022 1 Table 3.1 l

I l

l 007 l Control Relay,125 VOC,10 A, 9 Pole l General Electric l CR1208009041 1 Table 3.1 l

l 1

l

- 1 I

l l

008 I DC M1111 ammeter, 4 20 meDC i General Electric l D8-40 1 Table 3.2 l

I l

l l 50-103191ME l

l l

1 I

l i

I I

009 I E/P Transducer, 4-20 meDC l Moore Products l EE: 77-16 l Tele 3.2 l

l l

1 010 l Alaru ItHlule, 4-20 maDC l Rochester Instruments l ET-1215 l Table 3.2 l

l l

I i

1 011 l Isolated Signal Transmitter, 4-20 anDC l Rochester Instruments l $C-1302 i Table 3.2 l

l l

t i

1 l

024 + l Pushbuttaa Switch,120 VAC l General Electric l CR2940UW221A2 1 Table 3.2 1

1 025 4 Current Transformer, 10 VA, 40 A Osborne l12207 l Table 3.1 l

- ~~

i h

y I

I Table 2.2 Safety-Related Instruments, Seismic I, QA Level I CCL SAMPLE MANUFACTURER ENVIRONMENTAL NO. 1794-DESCRIPTION AND RANGE / RATING l MANUFACTURER PART NUMBER CRITERIA 1

012 Pilot Valve, 3-30 psig l

ASCO F316044K Table 3.2 013 Receiver Controller, 3-15 psig MCC Powers RC185-0125 Table 3.2 014 Multi-Purpose Relay, 20 psi Input i

MCC Powers 243-0009 Table 3.2 l

l 015 Room Thermostat, 20 psig Input MCC Powers TH-1800 Table 3.3 l

016 i Pressure Gauge, 3-15 psig Input l Ashcroft l 35-1009-AXPR-Table 3.2 1

028-XUC 017 Receiver-Controller, 3-15 psig Input MCC Powers RC 195-0001 Table 3 A 018 l Temperature Transmitter, 3-15 psig MCC Powers 163-3110 Table 3.2 l

l l

8 h

W

/

~

Table'2.3 Safety-Related Instruments, Seismic II/I, QA Level II MANUFACTURER ENVIRONMENTAL CCL SAMPLE NO. 1794-DESCRIPTION AND RANGE / RATING MANUFACTURER PART NUMBER CRITERIA 019 Light, 120 VAC Dialight 51-091-0231-

, N/A 303 Lens 656-125V Lamp I

020 Enclosure, 8" x 6" x 4" Hoffman Type SC N/A Transformer, 120 VAC/24 VAC Jefferson Electric 216-1121 N/A l

021 N/A 1

022 Switching Relay, 3-20 psig MCC Powers 243-0001 023 Current Alarm, 115 VAC, 0-5 A' Rochester Instruments ET-1200 L/U N/A I

I

\\

A R

i b

A rrk a. -v l

Table 4.1 Mounting Details The mounting of the specimen simulated the actual in-service mounting as closely as practical.

~

SOURCE OF HARDWARE l

CCL SAPPLE ICUNTED NO. 1794-DESCRIPTION IN -

POUNTIMI HARDWARE MFR C0fWL I

001 Terminal Block 12 ga 8-32 screws every 18*.

Drill 1

and tap subpanel.

002 Fuse /Fuseblock 12 ga (1) 8-32 screw each end. Drill I

and tap subpanel.

003 AC Relay 12 ga (2) 8-32 self tapping screws, I

top left and bottom right.

004 DC Relay 12 ga (2) 8-32 self tapping screws, I

top lef t and bottom right.

005 Latched AC 414y 12 ga (2) 8-32 self tapping screws, I

top left and bottom right.

006 AC Relay 12 ga (2) 8-32 self tapping screws, I

top left and bottom right.

i l

007 DC Relay 12 ga (2) 8-32 self tapping screws, I

top left ano botten right.

l l

008 DC M1111assnet.;

12 ga (4) 1/4-28 studs 8 nut.

X 00g E/P Transducer 12 ga (4) 1/4-20 bolts. Drill and I

tap subpanel.

010 Alers Module 12 ga (2) 8-32 screws. Drill and tap I

subpanel.

i 011 Isolated Signal 12 ga (2) 8-32 screws. Drill and tap 1

Transmitter subpanel.

012 Solenoid Valve 3/8' (2) 3/8' bulkhead fittings.

1 013 Receiver Co. trailer 12 ga (4) 8-32 screws. Drill and tap I

subpanel.

(Continood)

I

~

l

\\

Antw. - E I

Table 4.1 Mounting Details SOURCE OF MARDWARE

L SAMLE ICUNTED NO. 1794-DESCRIPTION IN MOUNT!fG HARDWARE PFR C0ppi'L 014 hitt-Purpose Relay 12 ga (2) 8-32 screws. Drill and tap I

sub9anel.

015 Room Thermostat 1/8" (2) 8-32 screws. Ort 11 and tap X

subpanel.

016 Teaperature Gauge 12 ga Vendor clamps over 10-32 case I

studs.

017 Receiver Controller 12 ga Mount to sample 1794-020 using X

(4) 6-32 screws, 2 nuts.

018 Teaperature 1/4" (4) 8-32 screws. Ort 11 and tap I

Transmitter subpanel.

019 Light 12 ga Furnished lockwasher and nut.

X 020 Enclosure 12 ga (4) 8-32 screws. Ort 11 and tap I

subpanel.

021 Transformer 12 ga (4) 1/4-20 bolts. Ort 11 and I

tap subpanel.

022 Switching Relay 12 ga (1) 8-32 screw through vendor X

X bracket. Ort 11 and tap subpanel.

023 Current Alans 12 ga (2) 8-32 screws. Ort 11 and I

tap subpanel.

024 Switch 1/4" Furnished lockwasher, (1) gasket X

I and nut. 20* from vertical.

025 Transformer 12 ga (4) 1/4-20 screws, flat and X

lockwasher. Install screws from bottom, mount horizontal.

=

(concluded)

[

F

\\

Arre-a.- p

\\

l l

l N

l SSE PERCENT DIRECTION cet wo.:83-rrv 1rSSE ]

DAMPNG HORIZONTAL N-S LI owa. ev:SFGnn DBEO HORIZONTAL E-W cm. sv: AWM OBE E VERTICAL M om: s-is-as e

g gg m

N 6

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i 2

1 +

n I I F

II t

_ i

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J o o, o, o

o o

'o u on,,

o o

o huomer see Figure 3.3 Vertical OBE RRS Corporate Consuhing & Development Cornpany Ltd.

consuhants constructors e.o. o.. sano;n r.n vra.nei. r.ra. m.rin caroun. stioe eees TF-004-I

.,e--

.......-.-.---------,----,---,-------v---~,---,----,-.r--.--

-w----,----

v r-n.,--

Aww - 9 SSE ]

PERCENT DRECTION cCL No.:93-U94 1/2SSE ]

DAMPNG HORIZONTAL N-S E owo. ev.sram DBEO HORIZONTAL E-W G cm sw 4Ne/

OBE 3 VERTICAL l out s-is-as O

l I

s

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-7

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l I

I.

1 I v II I

I, s1.

n

.. o e no o

o or,,

4 o

e o m no

,em Figure 3.4 Horizontal OBE RRS Corporate Consulting & Development Company Ltd.

consultants constructors I

P.O. Ses 12720,Messerah Trienste Park, North Coronne, 37700999a 1

1 TT-004-1

1 l

A rrk.a. H SSE [

PERCENT DIRECTION cet me.e sPnw 1MESE J DAMPNG HORIZONTAL N-S [ owa. ev:s<r.e-a.

DBEO HORIZONTAL E-W cm. sv: AM OBE ~l 5 2

vERTicAt om: -i t

EE.,-.E E~ =__2M__

I

. _ ~ = _

1

+

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a

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=

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n_:_.n.=___

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a

_ _ = _ =._=

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e

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1 o

o

. o e

o "

o mi, o

o m

m i m o

o

. m e no

,ses l

Figure 3.5 Vertical SSE RRS Corporate Consulting & Developrnent Conwany. Ltd.

consultants constructors e.o. s. inns, n.

.,.n vra nei. p.,6, w.,in c.r.en., arroe sese TF-004-1

b'TiA /l - f SSE 3 PERCENT DIRECTION cet we.:33-nu 1/2SSE ]

DAMPNG HORIZONTAL N-S

@ owa. sv:sm.

DBE O HORIZONTAL E-W @ cow. sy: ANN OBE l VERTICAL O om e-is-as t

n.!

r_ : r.c_ E_ _=

. c -.-

z _.s n- =~

._--'.:=._. --'

=

-=

==.=;

-=2

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_=_.-..-

-. 5: _

= = = -

==-

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~

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~

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_;._.= c.m

'.~_::' - -

~~

1 I I a

1 1 1.

w -

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g

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.=

=:= c..a 2.<

. =. _ =. =. g

2

. g.

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-.:. 5=J"_ J -~

~

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=f-

..- =

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r e

s2 1 _w=. g-a

.--;;; ;nm

_ =. =.=_.

-- ci:z v.

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s,

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_=G_ :

55_2 9.' r. =

-..=5 C

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e_n=

-=

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=.=-=-.u

=

j n

b I l I l

A

] ]

e e

.. o o oi, o

o e o e

' o,,,,

n o

m o o i o.

he== =rsee Figure 3.6 Horizontal SSE RRS Corporate Consulting & Development Company. Ltd.

consultants c e..structors P.O. Sea 12728, Aseearch Trisagte Park, Notth Ceronne, 37709 9994 i

w-cos.:

l L

l acce <r enoe2 pi;t cm w s9 74-summary cf f

' tscottse nu ner ofrection Fig no.

Fig. No.

Description Major aesonances (u P 1

X N-S I.1 E.1

- 002 N300 B31cu 50 Hz 1

Y E-W E.2 f c /cecg,y

.None Below 30 Hz Z

Vertical E.3 None Below 50 H2.

1 2

X N-S 1.1 E.4

- oo 4 36.9. 41.1 2

Y E-W E.5 None Below 50 Hz Z

Vertical E.6 M 4'A r, None Below 50 Hz 2

3 X

N-S I.2 E.7

- 23.1, 39.2 3

Y E-W E.8 y

-o/o None Below 50 Hz 3

Z Vertical E.9 7&,,,,,,7,c 7-

,,,, rec None Below 50 Hz E

m X

N-S i.3 E.10 co 37.3, 41.1, 49.0 4

y E-W E.11

- oo 6 None Below 50 Hz Z

Vertical E.12

, Aur None Below 50 Hz

\\

5 X

N-S I.3 E.13

- 23.3, 37.3, 39.5 41.9, 49.0 5

Y E-W E.14 "7

39.5, 42.3

=

Z Vertical E.15 PC CcW 43.6, 48.6 0

5 o

6 X

N-S I.4 E.16

- 23.1, 36.6, 41.1 3

43.2 x

s

..u >c, y

E-W E.17 39.2, 44.0, 48.6 Z

Vertical E.18

./ C A'd r 44.5 6

-o I

X N-S 1.3 E.19 36.9 E.20 None Below 50 Hz 7

Y E-W

_o,3 r

Z Vertical E.21 None Below 50 Hz g a.os ce t.wrme e*

a X

N-S

!.3 E.22 a

Y E-W E.23

-oo9 37.3, 39.5, 41.9 w*o Z

Vertical E.24 4

,4

, 48.1 a

gg 7,,,

g

Note: These frequencies are cursored approntmations at the equipment's resonant frequencies.

" Note: This frequency represents a system resonance and is Q

not a resonance of the fjature.

e-u

_1__

'l f

Accelerometer Phot 3 FIST MpLa. SJa, MM IWeE8FF CI Locatsse

' Amoer Direction Fig. No.

Fig. No.

Description Major Resonances (Na)*

i 35.9 37.7. 48.6 9

x N-S

~ 1.5 E.25

- o/o 30.1, 34.5. 39.5 9

y E-W E.26 Jac~ Mapa 44.5 40.7. 49.0 9

2 Vertical E.27

- 23.3. 36.9. 41.9 10 X

N-S I.3 E.28 None Below 50 Hz 10 Y

E-W E.29 g

v' pfmfgg h

None Below 50 Hz

.1.0 Z

Vertical E.30 r-m 11 X

N-S I.3 E.31 o72 37.7. 42.3. 49.0 11 Y

E-W E.32 None Below 50 Hz 5' e,<<4,4 11 Z

Vertical E.33 41.5 a

a None Below 50 Hz i

12 X

N-S I.6 E.34

-oco U

None Below 50 Hz 12 Y

E-W E.35

( u c u v,e c Bad Cable h,

None Below 50 Hz 12 Z

Vertical E.36 13 X

i I.6 E.37

-oO/

20.5 N-S V

E.38 None Below 50 Hz 13 l

l E-V N e ^'*R None Below 50 Hz

=

Vertical E.39

,2 Z

g g

E s-14 X

M-S 1.6 E.40

- o/S 20.7 3

f 14 Y

E-w E.41 None Below 50 Hz z

g,y 14 Z

Yertical E.42 None Below 50 Hz

?

g

,,,,_g e

N-S

!.7 E.43

-o/2 20.7

} E-W None Below 50 Hz 16 1

w E.44 15 v

8 "*~ "

None Below 50 Hz 15 I

Vertical E.45

==

16 X

N-S I.7 E.46

-oo/

20.7. 42.3 7

w 16 Y

E-W E.47 30.1, 33.8 16' Z

Vertical E.43 I #**<' " A ~3 -c 'r-None Below 50 Hz These frequencies are Cursored appromlestions at the

Note:

x equipment's resonant frequencies.

P t

This frequency represents a system resonance and is

- Note:

not a resonance of the fiature.

D f

J l

accelero.eter rhoto Pict f:*am m /974-Summary cf teuttaa aw=ner nirzettre rig. no.

Fig. no.

Description nejor aesonances (M )*

17 X

N-S 1.8 E.49 20.7 17 Y

E-W

,o Accel not mounted due to space 5"> ' * #

17 2

Vertical E.50 limitations None Below 50 Hz CD r"

m W

am.

O O

E

=A e-o E

Cm O

w 0

e V

O 4

rt E

O O

>=

U e

N 4<

N 20 ka>

D

r.ote: These frequencies are cursored approstmations at the equipment's risonant frequencies, r-I

. '\\

SQRT FORM Page 1 Qualification Summary of Equipunent I.

Plant Nasse: Enrico Fermi Atomic Power Plant - Unit 2 h

1.

Utility:

Detroit Edison Company PWR 2.

NSSS:

GE 3.

A/E:

DECO BWR I

II.

Component Name Bellows assemblies 1.

Scope:(X)MSSS

( ) BOP 2.

Model Number:

1-1/2" bellows assemblies 3.

Vendor: Johnson Controls, Engineered Piping Systems Division 4.

If the component is a cabinet or panel, name and model No. of the devices included:

(See Section VIII) 5.

Physical Description a.

Appearance (See Section II) b.

Dimensions c.

Weight 6.

Location: Building: Reactor Building, let Floor Elevation:

583'-6" 7.

Field Mounting Condition ( ) Bolt (No.

4 Size 1/2 )

( ) Weld (Length

)

( )

8.

a.

System in which located: CSI (Traversing In-Core Probe System) b.

Functional Description Expansion Joint c.

Is the equipment required for( ) Mot Standby ( ) Cold Shutdown (X)Both

( )Neither 9.

Pertinent Referenced Design Specifications IEEE-344-1975

\\

SQRT FORM _

Fage 2 III. Is Equipment Available for Inspection in the Plantf(X)Yes( )Mo IV.

Equipment Qualification Method:

( ) Test (X) Analysis

( ) Combination of Test and Analysis Qualification Report *: SR-10276, Stress Report, 9-20/84 (No., Title and Date)

Company that Frepared Report:

Johnson Controls Company that Reviewed Report:

DECO V.

Vibration Input 1.

Loads considered:

a.( ) Seismic only b.( ) Hydrodynamic only c.(X) Combination of (a) and (b) 2.

Method of Combining RES:(X) Absolute Sum ( )SRSS

()

other, specify 3.

Required Response Spectra (attach the graphs):

N/A 4.

Desping Corresponding to RES: OBP, N/A SSE N/A 5.

Required Acceleration in Each Direction:( )ZPA

( )

N/A other, specify 6.

Were fatigue effects or other vibration loads considered?

(X)Yes

( )Mo If yes, describe loads considered and how they were treated in overall qualification program:

cNOTE: If more than one report complete items IV through VII for each report.

.s SQRT FORM Page 3 VI.

If Qualification by Test then Complete *:

N/A 1.( ) Single Frequency

( ) Multi-Frequency

( )randon

( ) sine beat

( )

other, specify 2.( ) Single Amis

( ) Multi-Amis 3.

No. of Qualification Tests: OBE SSE Other 4.

Frequency Range:

5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S =

F/B =

V=

6.

Method of Determining Natural Frequencies

( ) Lab Test

( )In-Situ Test

( ) Analysis 7.

TRS enveloping RRS using Multi-Frequency Test ( )Tes ( Attach TRS & RRS Graphs)

( )Mo 8.

Input g-level Test: OBE S/S =

F/B =

V=

SSE S/S =

F/B =

V=

9.

Laboratory Mounting:

1.( ) Bolt (No.

, Size

)

( ) Weld (Length

)( )

10. Functional operability verified:( )Yes ( )No ( ) Mot Applicable

11. Test Results including modifications made:

12. Other tests performed (such as aging or fragility test, including results):

cMou:

If qualification by a combination of test and analysis also complete item VII.

SQRT FORM Page 4

]

l VII. If Qualification by Analysis, then Complete:

1.

Method of Analysis:

( ) Static Analysis (X) Equivalent Static Analysis

( )Dynesic Analysis

( ) Time-Bistory ( ) Response Spectre 2.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S = 560 HZ F/B =

279 HZ V=

$60 HZ 3.

Model Type:(X)3D

( )2D

( )1D

( ) Finite Element ( ) Bean (X) Closed Form Solution 4.( ) Computer Codes:

DESCAL-8 Frequency Range and No. of modes considered:

N/A

( ) Hand Calculations 5.

Method of Combining Dynamic Responses:(X) Absolute Se ( )SRSS

( )0ther:

(specify) 6.

Damping: OBE - SSE - Basis for the damping used:

N/A 7.

Support Considerations in the model:

Both ends rigid 8.

Critical Structural Elements:

Bellows Governing Load or Response Seismic Total Stress Range A.

Identification Location Combination Stress Stress Range Allowable Bellows on the Normal +(OBE/SSE) 153,680 PSI 375,000 PSI Bellows Faulted (LOCA) 457,761 PSI

$50,000 PSI Max. Critical Maximus Allowable Deflection to S.

Deflection Location Assure Functional Operability 0.375" Axial NORMAL +

On the 0.875" (FSAR 3.8.2.3.2.2) 0.125" Lateral (OBE/SSE)

Bellows 0.375" 1.25" Axial FAULTED 0.125" Lateral (LOCA)

i SQItT FORM Page 5 VIII. List of Subcamponents gjg Model No. -

Weight -

Was subcamponent i

Location - If subcour-Was Camponent operability veri-ponent was actually present or mass fled (Y or N or Name present eimulated?

U **)

J i

4 i

l l

I 1

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o If Available

- Yes = Yes, M = No, U = Unknown 4

I

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

,.,s sqRT FonM Page 6 11.

sketch or drawins installed Bow it has been installed k

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SQRT FORM Page 1 Qualification Sumry of Equipment 1.

Plant Nase: Enrico Fermi Atomic Fouer Plant - Unit 2 Type:

1.

Utility:

Detroit Edison Company FWR 2.

NSSS:

GE 3.

A/E:

DECO NWR I

II.

Camponent Name Solenoid Operated Globe Valves 1.

Scope:(X)NSSS

( )BOF 2.

Model Number: 81M-002, 8 2M-003, 81M-004 and 84U-001 J.

Vendor:

Target Rock Corporation 4.

If the component is a cabinet or panel, name and model No. of the devices included:

(See Section VIII) 5.

Physical Description a.

Appearance (See Section II) b.

Dimensions c.

Weight 6.

Location:

Building:

Reactor Building Elevation:

613'-6" T2-B12 7.

Field Mounting Condition ( ) Bolt (No.

Size

)

(X) Weld (3/4" Socket)

(X)

On line 8.

a.

System in which located: Radiation Monitoring System T50-01 b.

Functional Description o Full Open or Full Closed o Not used for throttling c.

Is the equipment required for( ) Hot Standby ( ) Cold Shutdown (X)Both

( )Neither 9.

Pertinent Referenced Design Specifications Deco Spec. 3071-501, 3071-12-PUR-ll6, IEEE-344-1975 i

p

---,-w

SQRT FORM Page 2 III.

Is Equipment Available for Inspection in the Plantf( )Yes( ) No IV.

Equipment Qualification Method:

( ) Test (X) Analysis

( ) Combination of Test and Analysis Qualification Report *: TRC Report No. 3477A (DECO File #Cl-2134)

(No., Title and Date) Design Report for Solenoid Operated Globe Valves, 2/17/83 Com'pany that Prepared Report:

Target Rock Corporation Company that Reviewed Report:

DECO V.

Vibration Input 1.

Loads considered:

a.( ) Seismic only b.( )Hydrodynanic only c.(X) Combination of (a) and (b) 2.

Method of Combining RRS:( ) Absolute Sun (X)SRSS

( )

other, specify 3.

Required Response Spectra (attach the graphs):

N/A 4.

Damping Corresponding to RRS: OBE N/A SSE N/A 5.

Required Acceleration in Each Direction:( )ZPA (X) 5.0g Horiz. Accel.,

3.0g Vert. Accel.

other, specify 6.

Were fatigue effects or other vibration loads considered?

(X)Yes

( )No If yes, describe loads considered and how they were treated in overall qualification program:

Fat igue Requirement s per NB-3545.3 sat is fied.

CNOTE: If more than one report complete items IV through VII for each report.

SQRT FORM Page 3 1

VI.

If Qualification by Test then Complete *:

N/A 1.( ) Single Frequency

( ) Multi-Frequency

( )randon

( laine beat

( )

other, specify 2.( ) Single Axis

( ) Multi-Azis 3.

No. of Qualification Tests: OBE SSE Other 4.

Frequency Range:

5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S =

F/ B =

V=

6.

Method of Determining Natural Frequencies

( ) Lab Test

( )1n-Situ Test

( ) Analysis 7.

TRS enveloping RRS using Multi-Frequency Test ( )Yes ( Attach TRS & RRS Graphs)

( )Mo 8.

Input g-level Test: OBE S/S =

F/ B =

V=

SSE S/S =

F/B =

V=

9.

Laboratory Mounting:

1.( ) Bolt (No.

, Size

)

( ) Weld (Length

) ( )

10. Functional operability verified:( )Yes ( )No ( ) Mot Applicable 11.

Test Results including modifications made:

12. Other tests performed (such as aging or fragility test, including results):

CNOTE:

If qualification by a combination of test and analysis also complete Item VII.

t I

\\

o.'

SQRT FORM Page 4 VII. If Qualification by Analysis, then Complete:

1.

Method of Analysis:

( ) Static Analysis (X) Equivalent Static Analysis

( ) Dynamic Analysis

( ) Time-History ( ) Response Spectrum 2.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S =

162 HZ F/B =

V=

162 HZ 3.

Model Type:(X)3D

( )2D

( )lD

( ) Finite Element (X) Beam ( ) Closed Form Solution 4.( ) Computer Codes:

Frequency Range and No. of modes considered:

(X) Hand Calculations 5.

Method of Combining Dynamic Responses:( ) Absolute Sim ( X) SRSS

( )Other:

(specify) 6.

Damping: OBE - SSE - Basis for the damping used:

N/A 7.

Support Considerations in the model: Assumed simply supported by the pipes 8.

Critical Structural Elements: Well Thickness (see Table C below)

Total Stress A.

Identification Location Stress Allowable 1

81M-003 Body (Fatigue Factor = 0.50797) 1,927 PSI 32,700 PSI

Bonnet, 10,902 PSI 20,000 PSI 81M-004 Body } (Fatigue Factor = 0.43172) <1,927 PSI 42,100 PSI Bonnetj 11,880 PSI 20,000 PSI Max. Critical Maximum Allowable Deflection to B.

Deflection Location Assure Functional Operability 0.0038 81M-003 0.005 0.0038 81M-004 0.005 Wall Thickness (inches)

Body Neck Model No.

Actual Reg'd.

Actual Req'd.

Actual Required 81 M-003 0.617 0.2454 0.5975 0.3924 0.0825 0.0441 81M-004 0.758 0.307 0.5975 0.510 0.0825 0.0441

SQRT FORM Page 5 VIII. List of Subcomponents N/A Model No.

Weight -

Was subcamponent

Location - If subcom-Was Component operability veri-ponent was actually present or mass fied (Y or N or Nm present simulated?

U **)

If Available

- Yes = Yes, N = No, U = Unknown

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Page 1 SQRT FORM Qualification Summary of Equipment I.

Plant Name: Enrico Fermi Atomic Power Plant - Unit 2 Type:

1.

Utility:

Detroit Edison Company PWR 2.

NSSS:

CE 3.

A/E:

DECO BWR I

II.

Component Name PYC0 Thermocouple 1.

Scope:( )MSSS (X) BOP 2.

Model Number:

102-9039-08-6/102-3171-20 3.

Vendor:

PYC0 4.

If the component is a cabinet or panel, name and model No. of the devices included:

(See Section VIII) 5.

Physical Description I

a.

Appearance (See Section II) b.

Dimensions 6" long x 1/4" 0.D.

c.

Weight less than I lb. each 6.

Location:

Building:

Reactor Elevation:

Various 7.

Field Mounting Condition ( ) Bolt (No.

, Size

)

( ) Weld (Length

)

l (X) Pipe mounted or local i

8.

a.

System in which located:

P44 and G33 b.

Functional Description Measure Area Temperature c.

Is the equipment required for( ) Hot Standby ( ) Cold Shutdown (X)Both

( )Neither 9.

Pertinent Referenced Design Specifications IEEE-344-1975 l

SQRT PORM Page 2 III.

Is Equipment Available for Inspection in the Plantf(X)Yes( )No IV.

Equipsent Qualification hthod:

-(X) Test

( ) Analysis

( ) Combination of Test and Analysis Nuclear Qualification Testing of Temperature Measurement Qualification Report *: Devices per IEEE Std. 323-1974 and IEEE Std. 344-1975 (No., Title and Date) 16436-82N Rev. 3 1/31/84 Company that Prepared Report:

Acton Environmental Testing Corp.

Company that Reviewed Report:

DECO V.

Vibration Input 1.

Loads considered: a.(X) Seismic only b.( )Hydrodynasic only c.( ) Combination of (a) and (b) 2.

hthod of Combining RRS:( ) Absolute Sun ( )SRSS (X)

N.A.

other, specify 3.

Required Response Spectra (ettach the graphs):

4.

Damping Corresponding to RES: OBE 5%

SSE 5%

5.

Required Acceleration in Each Direction:( ) ZPA (X)

N.A.

Other, specify i

6.

Were fatigue effects or other vibration loads considered?

( )Yes (X)No If yes, describe loads considered and how they were treated in overall qualification program:

CNOTE: If more than one report complete items IV through VII for each report.

SQRT FORM Page 3 VI.

If Qualification by Test then Complete *:

1.( ) Single Frequency (X) Multi-Frequency

( )randon

( ) sine beat

( )

other, specify 2.( ) Single Axis (X) Multi-Axis 3.

No. of Qualification Tests: OBE 5 SSE 1 Other

4. " Frequency Range:

1 to 50 HZ 5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

No Resonance found from 1 to 50 to 1 HZ S/S =

F/B =

V=

6.

Method of Determining Natural Frequencies Low level sine sweep (X) Lab Test

( )In-Situ Test

( ) Analysis 7.

TRS enveloping RRS using Multi-Frequency Test (X)Tes (Attach TRS & RRS 5MftinGraphs)

( )No 8.

Input g-level Test: OBE S/S =

F/ B =

V=

N/A SSE S/S =

F/B =

V=

9.

Laboratory Mounting:

1.( ) Bolt (No.

, Size

)

( ) Weld (Length

) (X)To simulate actual field utg.

10. Functional operability verified:(X)Yes ( )No ( )Not Applicable 11.

Test Results including modifications made: No anomalies to report during multi-frequency testing 12.

Other tests performed (such as aging or fragility test, including resultr):

Thermal aging performed with no anomalies 1

CNOTE: If qualification by a combination of test and analysis also conplete Item VII.

SQRT FORM Fage 4 VII. If Qualification by Analysis, then Complete:

N/A 1.

Method of Analysis:

( ) Static Analysis

( ) Equivalent Static Analysis

( ) Dynamic Analysis

( ) Time-History ( ) Response Spectre 2.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S =

F/B =

V=

3.

Model Type:( )3D

( )2D

( )lD

( ) Finite Element ( ) Beam ( ) Closed Form Solution 4.( ) Computer Codes:

Frequency Range and No. of modes considered:

( ) Hand Calculations 5.

Method of Combining Dynamic Responses:( ) Absolute Sims ( )SRSS

( )0ther:

(specify) 6.

Damping: OBE - SSE - Basis for the damping used:

7.

Support Considerations in the model:

8.

Critical Structural Elements:

Governing Load l

or Response Seismic Total Stress A.

Identification Location Combination Stress Stress Allowable t

Max. Critical Maximum Allowable Deflection to B.

Deflection location Assure Functional Operability 4

SQRT FORM Page 5 VIII. List of Subcomponents N.A.

Model No.

Weight -

Was subcomponent

Location - If subcom-Was Component operability veri-ponent was actually present or mass fied (Y or N or Nase present aimulated?

U **)

If Available

- Yes = Yes, N = No, U = Unknown l

SQRT FORM Page 6 IX.

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(________

/

f SQRT FORM bE Page 1 Qualification Summary of Equipmeq I.

Plant Name: Enrico Fermi Atomic Power Plant - Unit 2 Type:

1 1.

Utility:

Detroit Edison Company PWR 2.

MSSS:

GE 3.

A/E:

DECO BWR X

f II.

Component Nasee Liquid filled pressure gauges 1.

Scope:(X)MSSS

( ) BOP 2.

Model Number: Ashcroft Model #1279, 316 ES Bourdon Tube 3.

Vendor:

Dresser Instrument Division 4.

If the component is a cabinet or panel, nase ed model No. of the devices included:

(See Section VIII) 5.

Physical Description a.

Appearance (See Section II) b.

Dimensions Dial Size 4-1/2" dia. See page 6 c.

Weight 3-1/2 lbs. (approxi.atelv) 6.

Location: Building: RX Building.

Sub-bas ment Elevation:

545'-0" 7.

Field Nounting Condition ( ) Bolt (No.

, Size

)

( ) Weld (Length

)

~

(X) ___ Threaded mounting 8.

a.

System in which located:

Ell and E21 _.

b.

Functional Description To measure suction pressure for RHR pumps and core spray pumps c.

Is the equipment required for( ) Hot Stardby ( ) Cold Shutdown

( )Both (X)Neither 9.

Pertinent Referenced Design Specificatious None -

Pur. Speci ficat ion 3071-ROO-PUR-ll3

l i

SQRT PORM Page 2 III. Is Equipment Available for Inspection in the Plantf(X)Yes( )No IV.

Equipment Qualification Method:

(X) Tes t

( ) Analysis

( ) Combination of Test and Analysis Qualification Report *: DTB04R74-0892, Dayton T. Brown, Inc. Job No.

400524-00.000 Instrument Seismic Vibration Test Program, 7/23/74 (No., Title and Date)

DECO File No. Cl-2795 Company that Prepared Report: Dayton T. Brown, Inc. for Dresser Industrial Valve and Instrument Division Company that Reviewed Report:

V.

Vibration Input 1.

Loads considered:

a.(X) Seismic only b.( ) Hydrodynamic only c.( ) Combination of (a) and (b) 2.

Method of Combining RRS:( ) Absolute Sun ( )SRSS

( )

N/A other, specify 3.

Required Response Spectra (attach the graphs):

N/A 4.

Damping Corresponding to RRS: OBE SSE N/A 5.

Required Acceleration in Each Direction:( ) ZPA (X) 3G. - Vendor Specified other, specify 6.

Were fatigue effects or other vibration loads considered?

( )Yes (X)No r

If yes, describe loads considered and how they were treated in overall qualification program:

CNOTE: If more than one report complete items IV through VII for each report.

l l

SQRT FORM Page 3 VI.

If Qualification by Test then Complete *:

1.(X) Single Frequency

( ) Multi-Frequency

( ) random

( ) sine beat (X)

Dwell Test other, specify 2.(X) Single Axis

( ) Nulti-Axis 3.

No. of Qualification Tests: OBE SSE N/A Other

4. ' Frequency Range:

1 to 35 HZ 5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical): Resonance at 7, 11 and 16 HZ.

Page 15 of Report.

S/S =

F/B =

V=

6.

Method of Determining Natural Frequencies Resonance Search (X) Lab Test

( )In-Situ Test

( ) Analysis 7.

TRS enveloping RAS using Multi-Frequency Test ( )Tes (Attach TRS & RRS Graphs)

( )No N/A 8.

Input g-level Test: OBE S/S =

F/ B =

V=

Up to 7.5g Combined SSE S/S =

F/B =

V=

9.

Laboratory Mounting: Standard mounting simulating field mounting condition 1.( ) Bolt (No.

, Size

) ( ) Weld (Length

)( )

10. Functional operability verified:(X)Yes ( )No ( ) Mot Applicable 11.

Test Results including modifications made:

Satisfactory i

12.

Other tests performed (such as aging or fragility test, including i

results):

N/A CNOTE: If qualification by a combinatic, of test and analysis also complete Iten VII.

SQRT FORM Page 4 VII. If Qualification by Analysis, then Complete:

N/A 1.

Method of Analysis:

( ) Static Analysis

( ) Equivalent Static Analysis

( ) Dynamic Analysis

( ) Time-History ( ) Response Spectrum 2.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S =

F/B =

V=

3.

Model Type:( )3D

( )2D

( )lD

( ) Finite Element ( ) Beam ( ) Closed Form Solution 4.( ) Computer Codes:

Frequency Range and No. of modes considered:

( ) Hand Calculations 5.

Method of Combining Dynamic Responses:( ) Absolute Sun ( )SRSS

( )Other:

(specify) 6.

Dauping: OBE - SSE - Basis for the damping used: __

7.

Support Considerations in the model:__

8.

Critical Structural Elements:

Coverning Load or Response Seismic Total Stress A.

Identification Location Combination Stress Stress Allowable Max. Critical Maximum Allowable Deflection to I

B.

Se flection Location Assure Functional Operability

)

SQRT FORM Page 5 VIII. List of Subcomponents Model No.

Weight -

Was subcomponent

Location - If subcom-Was Component operability veri-l ponent was actually present or mass fied (Y or N or Came present simulated?

U **)

I

{

l 1

)

e If Available

- Yes = Yes, N = No, U = Unknown

t e

6N Page 6

@' ASH"" CAOFT.

II.

Sketch or dravias installed

.$ [

~'

~ Nx

, T j

i Eow it has been installed 3

. 5E ressur Gauges Eow it will be installed Bunefin LF."1-9e

~'

O e Specifications 1279 :

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1 SQRT FORN 00 Page 1 Qualification Summary of Equiguent I.

Plant Name: Enrico Fermi Atomic Power Pla st___

"Jnit 2 Type:

1.

Utility:

Detroit Edison Company PWR 2.

NSSS:

GE 3.

A/E:

Deco _

BWR I

II.

Component Name 20" 900# Gate Valves with I.imitorque_3MB-3-150 Operator 1.

Scope:( X) MSSS

( ) BOP 2.

Model Number: DECO Valve No. V8-4613 aad V8-4614 3.

Vendor:

TVA ( Anchor Darling) 4.

If the component is a cabinet or par +1, umme and model No. of the devices included:

(See Section VIIll 5.

Physical Description a.

Appearance (See Section 17.)

b.

Dimensions 13-1/2" dia x 50" long n 79"_ht ( Approx)See page 6 c.

Weight 7349 lbs ( Approx) 6.

Location: Building:

Iienctor - Torus Roon Elevation:

5 6? ' L_5 70 '

7.

Field Mounting Conditina ( )Lolt (No.

__, Site

)

(X)W Id (Length

)

( )

8.

a.

System in which loedted:

RHR (Ell) b.

Functional Description Inciste_lgypasses around F017A/B c.

Is the equipment required for( ) Hot Standby ( ) Cold Shutdown

( )Both (X)Neither 9.

Pertinent Referenced Design Specifications l

SQRT PORM Page 2 III. Is Equipment Available for Inspection in the Plantf(X)Yes( )No IV.

Equipment Qualification Method:

( ) Test (X) Analysis

( ) Combination of Yest and Analysis Qualification Report *:

1077.524, Seismic Category I Analysis of 20 inch-900 lb. Carbon Steel Flex Wedge Gate Valves, 3/28/78 (No., Title and Date)

(DECO File No. PI-11045)

Company that Prepared Report:Ananmet Lab. Inc. for Anchor / Darling Valve Co.

Company that Reviewed Report:

Hopper and Associates (HA-4/84-283)

V.

Vibration Input 1.

Loads considered: a.(X) Seismic only b.( ) Hydrodynamic only c.( ) Combination of (a) and (b) 2.

Method of Combining RRS:( ) Absolute Sun ( )SRSS

()

N/A other, specify 3.

Required Response Spectra (attach the graphs):

N/A 4.

Damping Corresponding to RRS: OBE SSE N/A 5.

Required Acceleration in Each Direction:( )ZPA (X) other, specify Sgt = 4.5g, SH2 = 4.5g, Sy = 3.0g SMAX = 7.52g.

Reference Page 8 of Report 6.

Were fatigue effects or other vibration loads considered?

(X)Yes

( )No If yes, describe loads considered and how they were treated in overall qualification program: Valve Body is analyzed for the maximum combination of seismic, operating and pipe reaction loads.

Reference page 34 of report.

C NOTE:

If more than one report complete items IV through VII for each report.

SQRT PDRM Page 3 VI.

If Qualification by Test then Complete *:

N/A 1.( ) Single Frequency

( ) Multi-Frequency

( ) random

( ) sine beat

( )

other, specify 2.( ) Single Axis

( ) Multi-Azis 3.

No. of Qualification Tests: OBE SSE Other

4. ~ Frequency Range:

5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

l S/S =

F/B =

V=

6.

Method of Determining Natural Frequencies

( ) Lab Test

( )In-Situ Test

( ) Analysis 7.

TRS enveloping RRS using Multi-Frequency Test ( )Yes (Attach TRS & RRS Craphs)

( )No 8.

Input g-level Test: OBE S/S =

F/8 =

V=

SSE S/S =

F/B =

V=

9.

Laboratory Mounting:

1.( ) Bolt (No.

, Size

)

( ) Weld (Length

)( )

10. Functional operability verified:( )Yes ( )No ( )Not Applicable 11.

Test Results including modifications made:

12. Other tests performed (such as aging or fragility test, including results):

cNOTE: If qualification by a combination of test and analysis also complete Iten VII.

i

SQRT FORM Page 4 VII. If Qualification by Analysis, then Complete:

1.

Method of Analysis:

j

( ) Static Analysis (X) Equivalent Static Analysis

( ) Dynamic Analysis

( ) Time-History ( ) Response Spectrum 2.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical): 79.52 HZ. Minimum. Reference page 59 of Report.

S/S =

F/ B =

V=

3.

Model Type:( )3D (X)2D

( )1D

( ) Finite Element ( ) Bean ( ) Closed Form Solution 4.( ) Computer Codes:

Frequency Range and No. of modes considered:

(X) Hand Calculations 5.

Method of Combining Dynamic Responses:( ) Absolute Stai ( )SRSS

( )Other:

N/A (specify) 6.

Damping: OBE - SSE - Basis for the damping used:

N/A 7.

Support Considerations in the model: Hinged on both ends of valve body (Page 53 of Report) 8.

Critical Structural Elements:

Valve Body and Bonnet Governing Load or Response Seismic Total Stress A.

Identification Location Combination Stress Stress Allowable l

KSI KS1 KSI Valve Body (Material SA216 WCB) 14.62 17.5 Bonnet (Material SA105) 6.23 17.5 Mhx. Critical Maximum Allowable Deflection to B.

Deflection Location Assure Functional Operability 0.008" Maximum Lateral

>0.008" l

Deflection of Operator

SQRT FORM Page 5 VIII. List of Subcomponents Model No. -

Weight -

Was subcamponent

Location - If subcour-Was Component operability veri-ponent was actually present or mass fied (Y or N or Came present simulated?

U **)

l 0

If Available

- Yes = Yes, N = No, U = Unknown i

i

,[

SQRT FORM Page 6 II.

Sketch or drawing i

Bow it has been installed or Now it will be installed A.N A. M...E T 6.es...

.e es.n

.. =

A N A... M...E.. T 6.e

..e..e ee u

...e TABLE !!f-1 COMPourirr wrisses AFD DINtus!0g3 Center of Mass Cemeenent weinhee Operator Operator (w. Abs.) e 3

stes.,

e.g.

Yoke 8 Stem (w. Abs.)

e 2

oes.e Bennet (v. 1be.)

e Se r.e

.e 3

Velve Body (w. Ibe.)

g e

ette.e Disc (w&. 1be.)

e

%gd.,

8' Yeee 8 Stee total vte.

(tfy. 1be.)

e 74ee.e steenesene m

yg (in.)

e Fe.e.

F2 (in.)

g.,,,

g.. @

mennet F3 un. )

3.,,,

_..g

v. un. >

e

.e p_

,, u.. )

...e.

u.. )

e

{,,e,.e,ed, e y-..

g r, u.. )

e e,,e e

Fg (18.)

e So.a.

e datum Fg um. )

e it.se E

(12.)

e d%.es l,

e, u.. )

,,.es z

e 0.0 m

(in.)

g og g

e. v.:

,1 a

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p. se l

og (in.)

e.ve rigure III.1 S.heastis of Talve Assembly 7

l i

3071-296B.40 051283 l

i

{$a 4.

SQRT FORM Page 1 Qualification Summary of Equipment I.

Plant Name: Enrico Fermi Atomic Power Plant - Unit 2 Type:

1.

Utility:

Detroit Edison Company PWR 2.

ESSS:

CE 3.

A/E:

DECO BWR X

II.

Component Name Battery Charger Area Cooling Units 1.

Scope:( )NSSS (X) BOP 2.

Model Number:

3.

Vendor:

CVI Inc.

4.

If the component is a cabinet or panel, nace and model No. of the devices included:

(See Section VIII) 5.

Preliminary Physical

Description:

a.

Appearance (See dection II)

T4100B043 T4100B044 o

b.

Dimensions 66" x 48" x 36" High 57" x 39" x 33" High c.

Weight 1050 lb.

850 lb.

6.

Location:

Building:

Auxiliary Elevation: T4100B043 - 651'-0"+

T4100B044 - 652'-0".T 7.

Field Mounting Condition (X) Bolt (No.

, Size

)

Hounting bolts are used to anchor the platform to the ceiling.

( ) Weld (Length

)

( )

8.

a.

System in which located: Battery Charger Area Ventilation b.

Functional Description c.

Is the equipment required for( ) Rot Standby ( ) Cold Shutdown (X)Both

( )Neither 9.

Pertinent Referenced Design Specifications 3071-533 Rev. A 3071-337 Rev. A l

l l

SQRT FORN Page 2 III. Is Equipment Available for Inspection in the Plantf( )Yes( )No IV.

Equipment Qualification Method:

( ) Test (X) Analysis

( ) Combination of Test and Analysis Qualification Report *: B9-2463, B9-2477, B9-2479, B9-2478 & B9-2476 (No., Title and Date) Response Spectrum Analysis of Fan / Coil Units No. T4100B043 and T4100B044 Company that Prepared Report:

CVI Incorporated Company that Reviewed Report:

DECO V.

Vibration Input 1.

Loads considered: a.(X) Seismic only b.( ) Hydrodynamic only c.( ) Combination of (a) and (b) 2.

Method of Combining RRS:( ) Absolute Sum (X)SRSS

( )

other, specify 3.

Required Response Spectra (attach the graphs):

Attached 4.

Damping Corresponding to RRS: OBE

.5%

SSE 2%

5.

Required Acceleration in Each Direction:( )ZPA j

( )

other, specify 6.

Were fatigue effects or other vibration loads considered?

( )Yes (X)No If yes, describe loads considered and how they were treated in overall qualification program:

CNOTE: If more than one report complete items IV through VII for each report.

l l

SQRT FORM Page 3 VI.

If Qualification by Test then Complete *:

1.( ) Single Frequency

( ) Multi-Frequency

( ) random

( ) sine beat

( )

other, specify 2.( ) Single Axis

( ) Multi-Axis 3.

No. of Qualification Tests: OBE SSE Other 4.

Frequency Range:

5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S =

F/B =

V=

6.

Method of Determining Natural Frequencies

( ) Lab Test

( )In-Situ Test

( ) Analysis 7.

TRS enveloping RRS using Multi-Frequency Test ( )Tes (Attach TRS & RRS Graphs)

( )No 8.

Input g-level Test: OBE S/S =

F/B =

V=

SSE S/S =

F/B =

V=

9.

Laboratory Mounting:

1.( ) Bolt (No.

, Size

)

( ) Weld (Length

) ()

10. Functional operability verified:( )Yes ( )No ( )Not Applicable

11. Test Results including modifications made:

12.

Other tests performed (such as aging or fragility test, including results):

l cNOTE: If qualification by a combination of test and analysis also complete Item VII.

SQRT FORM Page 4 i

VII.

If Qualification by Analysis, then Complete:

1.

Method of Analysis:

( ) Static Analysis

( ) Equivalent Static Analysis (X)Dynanic Analysis

( ) Time-History (X) Response Spectrum 2.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical):

S/S = 13.3 HZ F/B =

17.4 HZ V=

23.7 HZ 3.

Model Type:(X)3D

( )2D

( )lD (X) Finite Element ( ) Bean ( ) Closed Form Solution 4.( ) Computer Codes:

Stardyne Frequency Range and No. of modes considered:

1-50 HZ No. of modes = 13

( ) Hand Calculations 5.

Method of Coimbining Dynanic Responses:( ) Absolute Sun (X)SRSS

( )Other:

(specify) 6.

Desping: OBE.5 SSE 2 Basis for the danping used:% of Critical (reg,quagg f.(,l Damping

\\ Ik FS AR 7.

Support Considerations in the model: ( Nt4ED) 8.

Critical Structural Elements: Tombstone and Fan Housing Governing Load or Response Seismic Total Stress A.

Identification Location Combination Stress Stress Allowable Element 970 Tombstone SRSS 6045 P5; 13500 OBE (Fan / Coil Unit No. T4100B043)

Element 970 Tombstone SRSS 15033 18900 SSE (Fan / Coil Unit No. T4100B043)

Max. Critical Maximum Allowable Deflection to B.

~ Deflection Location Assure Functional Operability 0.l87 in.(Global XI Direction)

Bottom of Backplate OBE Near outlet 0.203 in.(Global XI Direction)

Bottom of Backplate SSE Near outlet

s SQRT FORM Page 5 VIII. List of Subcamponents Model No. -

Weight -

Was subcamponent

Location - If subcom-Was Component operability veri-ponent was actually present or mass fled (Y or N or Emme_

present simulated?

U **)

t I

l If Available

- Yes = Yes, N = No, U = Unknown l

l

SES/CL/TL-83-006A May 7,1984 Rev.A SQRT FORM Page 6

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SPECTRUM NODE ELEV DIRECT LDCATION e 583-6 VERT AUXILLIARY PUILDING SLAB S E 5-C-te CEL-C-1B is15-6 Amo-A

SQRT FORM

65 Page 1 Qualification Simmary of Equipment I.

Plant Name: Enrico Fermi Atomic Power Plant - Unit 2 Type:

1.

Utility:

Detroit Edison Company FWR 2.

MSSS:

GE 3.

A/E:

Deco NWR X

II.

Camponent Name Various pneumatic control devices. See Attachment 'A' l.

Scope:( )MSSS (X) BOP 2.

Model Number: See Attachment 'A' 3.

Vendor:

See Attachment ' A' 4.

If the component is a cabinet or panel, name and model No. of the devices included:

(See Section VIII) 5.

Physical Description a.

Appearance (See Section II) b.

Dimensions See Attachment 'A' c.

Weight See Attachment 'A' 6.

Location: Building:

Auxiliary Building Elevation:

577'-6" 7.

Field Mounting Condition ( ) Bolt (No.

, Size

)

( ) Weld (Length

)

()

See Attachment ' A' 8.

a.

System in which located:

T41-02 b.

Functional Description Pneumatic controls for operation of damper and its air seal c.

Is the equipment required for( ) Rot Standby ( ) Cold Shutdown (X)Both

( )Neither 9.

Pertinent Referenced Design Specifications IEEE 344-1975 and DECO 3071-296 l

l

SQRT FORM Page 2 III. Is Equipment Available for Inspection in the Plantf(X)Yes( )Bo IV.

~ Equipment Qualification Method:

(X) Test

( ) Analysis

( ) Combination of Test and Analysis Qualification Report *:

10258, Rev. 6, Seismic Qualification Report on Twelve pneumatic cont rol devices, November 5,1984 (No., Title and Date)

Company that Prepared Report:

Farwell and Hendricks, Inc.

Company that Reviewed Report:

DECO V.

Vibration Input 1.

Loads considered: a.(X) Seismic only b.( ) Hydrodynamic only c.( ) Combination of (a) and (b) 2.

Method of Combining RRS:( ) Absolute Stse ( )SRSS

( )

N/A other, specify 3.

Required Response Spectra (attach the graphs): Attachment C and D 4.

Damping Corresponding to RRS: OBE 5%

SSE 5%

5.

Required Acceleration in Each Direction:( )ZPA (X) 5.0 G for SSE EPA other, specify 6.

Were fatigue effects or other vibration loads considered?

(X)Yes

( )30 If yes, describe loMs considered and how they were treated in overall qualification program:

Operational cycling (1500 cycles) with monitoring.

cEOTE: If more than one report complete items IV through VII for each report.

. ~, - -.

SQRT FDEM Page 3 If Qi lificatiop by Test then Complete *:

VI.

g I*

14 )5 ingle frequer,cy (X)hlti-Frequency (X) random

( ) sine best

( )

other, specify 2.( ) Giggle Axis (X) Multi-Axis 3.

No. of Qualification Tests: OBE 5 SSE 1 Other 4.

Frcquen.:y E; sage:

1 to 5011Z 5.

Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical): Not required for the test program S/S =__

F/B =

V=

6.

Method of Determining Natural Frequencies N/A

( ) Lab Test

( )1n-Situ Test

( ) Analysis 7.

TRS enveloping RRS using hiti-Frequency Test (X)Yes ( Attach TRS & RRS Attachment 'C' and 'D' Graphs)

( )No 8.

Input g-level Test : OBE S/S =

F/ B =

V=

N/A SSE S/S =

F/ B =

V=

9.

Laboretary Mounting: See Attachment 'B' 1.( ) Snit (Ma.

, Size

)

( ) Weld (Length

)( )

10. Function.sl operability verified:(X)Yes ( )No ( )Not Applicable

11. Test Results including modifications made:

Satisfactory.

12. Other testa performed (such as aging or fragility test, including results):

Baseline functional, operational cycling prior to seismic test, operational cycling after seismic test, post seismic functional.

St013: If e;ustification by a combination of test and analysis also complete 3 ten VII.

i

SQRT FORM Page 4 VII. If Qualification by Analysis, then Complete:

N/A I.

. 1.

Method of Analysis:

( ) Static Analysis

( ) Equivalent Static Analysis

( ) Dynamic Analysis

( ) Time-History ( ) Response Spectrim l

2.

Natural Frequencies in Each Directiric (Side / Side, Front /Back, Vertical):

S/S =

F/B =

V=

l t

3.

Model Type:( )3D

( )2D

( )1D

( ) Finite Element ( )Beas ( ) Closed Form Solution 4.( ) Computer Codes:

Frequency Range and No. of modes considered:

( ) Hand Calculations 5.

Method of Combining Dynamic Responses:( ) Absolute Sun ( )SRSS

( )Cther:

(specify) i 6.

Damping: OBE - SSE - Basis for the darping used:

7.

Support Considerations in the utdel:

8.

Critical Structural Elements:

Coverning Load or Response Seismic Total Stress A.

Identification Location Combination Stress Stress Allowable Max. Critical Masimum Allowable Deflection to B.

Deflection Location Assure Functional Operability

sQtT FonM Page 5 VIII. List of Subcamponents I.

Model No. -

Weight -

Was subcamponent

Location - If subcamr-Was Camponent operability veri-ponent was actually present or mass fied (Y or N or Eame present simulated?

U **)

1 i

l i

0 If Available

- Yes = Ye s, N = No, U = Unknown i

l i

i f

-,,-,,--,.,.w,,a-,.y-, - - -, -,

,-----.,-,,-~.,,,_.,,,_e.,,,,_n.,n_,-n

,.,,,.w,

.-e e.m, e.

=

l ATTACHMENT ' A" to SQRT Form #65 i

l MT DIMENSION LBS.

FIELD f

COMPONENT VENDOR MODEL.

INCH ( APPROXIMATE)

( APPROX)

MOUNTING

1. Check Valve Parker Hannifin 0.81 x 0.81 x 2.62 tong.

0.4 In line, Brass Fittings to 1/4" l

1 0-400-B-10 Soft Copper

+

(2) 5/16" dia.

2. Filter Fisher Controls bolts; Rzgulator Co.

I 67F-203 (in-3.19 x 3.19 x 9.0 Ht.

f stalled) 67AF-237 (tested) 3.19 x 3.19 x 7.94 Ht.

1.5 l

l

3. 3-Way Fisher Controls 4.12 dia. x 9.19 ht.

4.0 L shaped bracket Switching Co.

l Valve 164A (3-15PSIG)

& (40-100PSIG)

4. Pressure Fisher Controls 2.0 dia.

Brass tee to 1/4" soft Gauge Co.

4 (0-60PSIG)

J512 copper j

1-1/2" dia.

(4) 7/16"-14THD

5. Actuator G.H. Bettis CB-525-SR 8-3/4 dia. x 27-11/16 Ig.

60.0 bolts CB-725-SR 8-3/4 dia. x 27-3/4 Ig.

92.0 i

(2) 1/4" thru

6. 3-Way Valve WABC0 i

Manual with-2MA-1A cud 2-1/2 w x 2-7/16 ht x 0.5 bolts l

out lugs 2CA-1A (without 1-1/2 th.

roller) l 4

I i

i r

, ATTACHMENT

'B' 10258.0PG5 o

TABLE

1.1 DESCRIPTION

OF TEST SPECIEN(5) Als MOUNTING C

Test l

~

Specimen I.D.

Device Mounting Orientation CV-1 Parker Hannifin Check In Line Connection - Brass Horizontal Valve C-400-B-10 Fittingc to 1/4" Soft Copper CV-2 Same as CV-1 In Line Connection - Brass Vertical Fittings to 1/4" Soft Copper PVC-1 Fisher 67AF-237 2-5/16" Diameter Bolts -

Horizontal Filter Regulater Side of Regulator to Fixture PCV-2 Same as PCV-1 2-5/16" Diameter Bolts -

Vertical Side of Regulator to Fixture SWV-1 Fisher 164A-47(40-100 L-Shaped Bracket (Supplied Horizontal i

psig Spring Range) with Unit) to fixture 3 Way Switching Valve SWV-2 Fisher 164A-17 L-Shaped Bracket (Supplied Vertical (3-15 psig Spring) with Unit) to Fixture 3 Way Switching Valve PI-7 Fisher J512 Pressure Connect to Stainless Steel Horizontal Tee i

Gauge 0-40 psig 1 1/2" Stainless Steel Tee 1/4" Sof Copper Dia. Back Mounted PI-4 Fisher JS12 Pressure Connect to Stainless Steel Vertical Tee Gauge 0-60 peig 1 1/2" Stainless Steel Tee to 1/4" Soft Cooper Dia. Back Mounted ACT-1 Bettis CB-725-SR-80 Bolt to Fixture with 4-1/2"-

Vertical Actuator 13 THO. SAE Grade 5 Bolts ACT-2 Bettis CB-525-SR-80 Bolt to Fixture with 4-7/16" Horizontal Actuator 14 THD SAE Crade 5 Bolts

SWV-3 WABC0 2 CA-1A(P58721) 2-1/4" Thru Bolts to fixture Vertical Manual 3 Way Valve with CAM Roller Re-moved

'SWV-4 dABCO 2 MA-1 A(P58719) 2-1/4" Thru Bolts to Fixture Horizontal 1

functionally the same Refer to Appendix 0, the P58719 is functionally the sene as the P58718 but is supplied with lugs for various operating i

kits. The P58721 is a P58719 supplied with a two-director cam roller operator kit.

Test items were purchased by Farwell & Hendricks, Inc. as commerical grade components.

Model numbers are corrected from list provided by Detroit Edison and j

verified with Larry Reissnen on 10-15-84

ATTACHMENT 'C' Test Plan / Procedure No.10258, Rev. 0 82 l

l l

D 250 %

E 5

/

x i

/

\\

10 0 %

i

/

A 25%

i 2

3 5

10 2

3 5

80 0 2

3 5

1000 FREouENCY HI 5% oAMPING A

0 E

G OBE #1

.63 g's 6.25 g's 6.25 g's

2.5 g's 1 Hz 4 Hz 16 Hz 33 Hz OBE #2 - #5 will be increased to the following approximate l

fl a t.

Portion (0-E) Levels OBE #2 7.50 gs OBE #3 8.75 g s OBE #4 10.00 gs OBE #5 11.25 g s SSE 1.25 g's 12.5 g's 12.5 g's 5.0 g's 1 Hz 4 Hz 16 Hz 33 HZ REQUIRED RESPONSE SPECTRA d

ATTECHMENT

'D' F.

CHANNEL - A 2PA=

4.98 Get 10.08

_-4-+

--o.

~"

_. <y.

._i_

r

. _ _ q.

..;. i 4 4 g

l f'

)V i-

. q ACC C'S

?f

'!!/

,rf t

t

[I l

1 0.198 0.501 LOGIS FREQ 50.12

$ HOCK RESPONSE 5)8 % Daeo Abs Acc 01-NOV-84 12:14:40 192580.E.2ND50t08ESY,Z 13 Octave Maxi-Max

?

Free Aspl Free Aepi Free Aeol 8.63 8.11 3.16 5.23 15.85 6.53 0.79 8.25 3.98 8.94 19.95 5.69 1.00 9.60 5.01 S.32 25.12 5.27 1.26 1.81 6.31 7.87 31.62 5,08 1.58 1.62 7.94 8.04 39.81

.4.27 2.90 2.27 18.99 7.86 50.12 4.18 2.51 3.19 12.59 7.50 FIGURE 6.2 I

TEST RESPONSE SPECTRA l

i o

e SQtT pons Page 6 II.

Sketch or drawins installed h Hanninn CorporaHon Manatrol Now it has been installed 520 Tomes Avenue Control Valves w.

or Phone:M 322431 Catalog 3000-2 Now it will be installed i

l i

i Check Valves "".e*kv.i.iu

"*'aa' Series C and CS ch ini,o

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subpiet+ mounted series es

gygg, Inline-mounted sof te$ C C2T 18 27 Nm o u t 15 M 2 00 f So s:

01006 Check valve cam

,e to mm Ost i 20 s.

2 62 es st 0 4 e 25 C4JO tio it UNF 20 SAE si Cae 22 3 312 e 79 7 O S C 25 Cen0 34it NrTF 100 4 25 di 2751 0096 0 S C 2)

C820 SW te UNF 28 SAE 8; 112( 28 di 350(089'

1306, C300 1/214 NPTR 125 t 31 Si 344 f 47 et 1306i C1020 7414 UNF 29 SAE tot 125 f 31a>

4 001901 Si 202>

C1200 3414 Nm 1 Soi 3811 3 se i to 4, 20ee C1220 1 trio 12 UNF 26 SAE 121 150 e 3816 4 42(117 3i 2 0 e 9, C1420 141412 Lee Saf 14>

2 00i 90 0+

6 00 r127 On 3 3 ft Si Cie00 1111/2 NPTF 175( 44 si 6 001127 Di 1311 Si C1820 161612 UN SAE te 2JS e $7 Ji 6 821942 h 3 3 si le C2000 114111/2 NPTF 2JS( $721 6 421942 h SJ Q 9 C2020 14412 UN SAE 206 2 75i GB 9, 6 to rie6 ti 42Gt C2400 11/21112 NFTF 2 FS( 00 m 5 821942 M 0 4 O Di C2420 17412 UN SAE foi 3 00( 76 21 7 29(184 2' 44091 C3200 2-111/2 NFTF 390183 M 6 $0196511 1S 4 & 16 C3220 91/212 UDe SAE 32) 4 00 (101 Si 0000296 15 4 & 11

SQRT FORM Fage 6 A II.

Sketch or drawing installed fl5HEg+

yfBressure Regulators

' = = ri = = => nw iu - -

1 Bow it has been installed en rmgsi m..

Sphem0Resteur4B

_A -

+ + - - '

Old Cat.o.g Isiemese C 67 7

em. ambas 1 tus egge se. um Weg.e Ptug R e Spreeg te.o v..,..

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$7US 40f'psus and tessumpt 4 l

As Ouses Tyyne 200 puse att Onner Fspes Ah n and teenart er tre.s asus titus r'

[

l WILIT Tys.s $7FT. S?FTR. 977..und

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STYR 20p.e furenatus

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01 feufft en sus est.s t Ras tapessfas see emass 4 us ep.e e

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es c etze s

T 57F or T 57FR S dhe.eemaried.nserust tus tutus FBear mie.es.m e aura massTu atar.

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pr

_a Model 67F-203 has been installed.

I f"

3

~ ~

flowever, this model is now discon-e 5-f%

%~.

l tinued by the manufacturer.

I

=

j Model 67AF has been tested for sim a

. " T - ~~ '.

e Ei

)

ilarity. Besidm Model 67FR-224 WT r..

j was previously qualified per MCC

?

- - - + - - '

I

.. b

,,j 7"

Powers Report No. 44870-1,

' " ~ ~ ~ ~ ~

December 17, 1979, DECO File

"**"*"~'"*"#***

~~IJ No. B9-2455 an part af a control F,-+ 8 8 '~a o = 'a.a' r**'a' o=' = ra==

Re1ay pane 1 with components.

See Page 6 D.

l

. m.

-.-~.-.m-

=as sQtT rotM Page 6B Ix.

sketch or drawing installed 67 SeriesSmaD- 'lume Fisher Controls Pressure Regu rs Bow it has been installed P.

(;

r.-

& amadini&~;"

September 1980 Bulletin 71.1:6:

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r.

l muusu iee asnem

-so en

(

nar. ins. tee.t 1w re we, meneeemies u

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aanstam man.

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sanees an saa - a,m m,.

t unsuum Jw

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eme.

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6

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panese so,e, p e me,i s., evne,,,es,,

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1 N

Model 67AP-237 has been tested to O

3 l

q qualify the installed Model 67F-203 by similarity. 67F series has been l

j discontinued by the manufacturer.

l j

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M.

MMM ee _

ese pawns.ee e as a u.e em -

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sQRT poet Fase 6c II.

sketch or dravias installed 7, g i

g Bow it has been installed

'v a - ' " *

" d ' " *^

SHms Switching Valves 1

i i

March 1979 l Ballere 71 7.164

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SQRT 70mt Page 6 D II.

Sketch or drawing festalled gl5HERs'

- 1..

ma i t.u m

.c Bow it will be lastalled Fisher Gauges 00Cember 1972 l &s0gte 11,3:50 b

0 m*2%.lWA. MS Reg 1"/2ef 15' Old Catalog Number PI 50 BerlesJ5DO Gauges s moo e mos m,io i. mie e,.n ow.ie

.= 7 4

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SQRT FORM Page 6 E II.

Sketch or drawing installed _

^

'~~

g Bow it has been installed CB. Series:

or Pneumatic Actuators Cata% #20.001A i

i Bow it will be installed y:

4 b

4 i

l l

t I

i i

l D6menelons

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l

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ML20099H654

Contents

Text

Reference:

Subject:

Dear Mr. Youngblood:

=

2.1 DESCRIPTION

SUMMARY

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==

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.

Description:

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1.1 DESCRIPTION

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