ML20153B499
| ML20153B499 | |
| Person / Time | |
|---|---|
| Site: | Perry  |
| Issue date: | 06/02/1986 |
| From: | Bosworth B CLEVELAND ELECTRIC ILLUMINATING CO. |
| To: | |
| Shared Package | |
| ML20153B440 | List: |
| References | |
| SP-1E68-001-ADD, SP-1E68-1-ADD, NUDOCS 8803220193 | |
| Download: ML20153B499 (65) | |
Text
{{#Wiki_filter:l l TEST ADDENDUM l NO 6208 Rev. 2/85 TEST PROCEDURE NO. REY. TEST ADCENOLN No. lb$auptcLi W lE69- col I 60l TEST TITLE 6% TEM. UlBiztViioid She#4t TE5T heibtub' CHECK ONE/ hTESTEXCEPTIONIm.EMENTATION/ CLOSEOUT l l RETEST l l OTHER PERRY NUCLEAR POWER PLANT
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RECORD OF APPROVAL ACCEPTANCE TESTS OPA.Y PREOPEP.ATIONAL / SPECIAL TESTS ONLY PREPARED By: DATE PREPARED B , CAT l CECO *E'OED APPROVAL SY LTE: CATE RECOWENCE T DA E APPROVED BY GSE-NTS: Il I TPRC: CATE lDATE PM IWi l 23A APPR D AT TPR I _ 0@h3d'JR5ENCE- DM' \ DATE
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m e. . . .a MEMDRANDUM __ i "4ff@P nocu CC300 rRoM Blair Bosworth DATE May 22, 1986 GG.R.Leidich PHoNc 6179 acoM TS-15 I susaccT Test Report for SP lE68-001 Rev. ! , Addendum #l. I i l A. OBJECTIVES l l The objective of this addendum was to verify by visual observation that steady state and transient induced vibration was within acceptable lir_its for E12 system
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i piping running in the Fuel Pool Cooling Assist "B" mode. ) B. ACCEPTANCE CRIT.RIA VERIFIED It was verified tlat the subject vibration levels were within acceptable limits. j Overall, all acce,itance criteria were satisfied. C. DEFICIENCIES None D. CONCLUSIONS 7__ (,) Piping vibration levels for the E12 system running in the Fuel Fool Cooling Assist "B" mode are acceptable. E. RECOMMENDATIONS System Operating Instruction SOI E-12 was used for s test and gB'[c[dateas written. There are no recommendations. ,M Y y-BB/kg
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\ 1 Lj PtFP NO, 6261 Rev. 5/83 PREOPERATIONAL / ACCEPTANCE TESTING RELEASE FOR TEST CONTROL FORM PROCEDURE TITLE sp% h TI At d6Cl b Eh@b PROCEDURE NUMiER REY [d
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'. Rev.: 4 /^g 10CFR50.59 Applicability Check Attachment 1 Forms PAP-0305-1 s#F> 4 I. Description of Item to be Evaluated:
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- 5. Yes No % Is there an effect on the environ =ent or change to the Environmental Protection Plan? Reason:
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- REVIEWD BY
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- DATE 9- S~~
** APPROVD B LE DATE RMAN DATEY!4T APPROVED BY APPROVAL AT TPRC MEETIfiG MI--
NO. CSE, NTS OCS ' DATE , CONCURRENC . * .
- i b "d % ATE M7/M CHANGE .
ENTERED CHANGE . DATE ENTERED y A]l- JG ' DATE Y 2'T
- Minor test changes shall be reviewed by the Test Coordinator.
prior to release do not require Test Coordinator Review. Test chanEes written
** Minor change to preoperational test may be signed, by NTS. CSE O r-- .- -. ..... .
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- PARAGRAPH 7.1 ACCEMANCE CRITCRIA TABLE NEF d-1 PNPP Q Q PRE- FUEL LOAD BOP SYSTEMS VISUAL VIBRATION ACCEPTABLE CRITERIA ALLOWABLE RELATIVE DISPLACEMENTS NOMINAL -
TYPE SIZE LENGTH OF SPAN IN FEET WELD INCHES L Minimum 6 9 12 15 18 21 24 27 3/4" 10 f L:3.8' 25 56 Socket 1" 10 0 L 4.2' 20 44 Welded 1 -1/4" 10 0 L:4.7' 16 35 - SPAN LENGTHS Pipe 1-1/2" 10 # L:5.0' 14 31 ARE NOT 2" 10 e L:5.7' 11 25 44 EXPECTED IN THIS REGION - 2-1/2" 10 @ L=3.9' 24 54 96 3" 10 @ L:4.2' 20 45 80 4" 10 0 L:4.9' 15 34 60 94 6"
- 24 40 63 90 Full Penet. 8"
- 17 30 SD 68 92 Oirth 10"
- 14 24 38 54 74 Butt 12" ' ' 11 20 31 45 61 80 Welded 14" *
- 17 27 39 53 69 Pipe 16" ' ' 15 23 34 46 60 18" *
- 13 21 30 41 53 68 20" *
- 12 19 27 37 48 61 22" *
- 11 17 25 33 44 55 24" ' ' 10 16 23 31 40 51 NOTES: ,
(1) Tabular values are fort (a) Mid-span deflections in the plane of the end supports (b) Steady state operation (c) Displacements given in mils (1 mil = .001 inch) peak to peak (d) Simple span of straight pipe ~ (e) Carbon Steel pipe (f) Schedule 40 wall thickness and greater (g) End points of the span at rigid supports: struts, anchors or I equipment connections (h) Long radius elbows (i) At least one socket welded fitting or one full penetration girth butt weld in the span or at end point of the span (j) Pipe tests at low temperatures where pipe stresses from ther=al effects will not be significant and themal pipe growth will not affect the nominal assumed 1/32" minimum clearance at pipe supports other than rigid struts, anchors and equipment.
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, Rsv. 1 St4E (-L (2) A Maximum Allowable Visual (MAV) displace =;nt will be determined for each pipe span surveyed visually. If pipe motion is not observed by the Oualified Piping Engineer (OPE) at the =aximum observing distance (MCD)
(_ , the vibration is acceptable. Lj (3) Determine MOD by dividing MAV by a factor of between 2 and 3, to be determined on-site prior to testing by the CPE, consistent with the visual acuity of designated surveyors. (4) Determine MAV by one of the following methods: (a) For the case of both en,ds of the pipe span supported rigidly aith either rigid struts, anchors, or equipment connections, use the expression: MAV CF x SF x DF x TV where: CF = configuration factor, or product of all applicable factors - see notes 5 or 6 below SF = steel factor - see note 7 DF = dynamic factor - see note 8 TV = tabular value from the above for corresponding pipe si:e and span length. (b) For the case of only one end of the piping span supported rigidly with either a rigid strut, an anchor or an equipment connection. Use the higher of the following two values: (1) MAV = 25 mils; or (ii) MAV = CF x SF x DF x TV (")'N (c) For the case of neither end of the piping span supported rigidly with either a rigid strut, or anchor or an equipment connection, . use the higher of the following two values: (1) MAV = 40 mils; or (ii) MAV = CF x SF x DF x TV (5) Configuration factors (CF) for socket welded piping sizes 3/4" through 2", inclusive (a) Si=ple span of straight pipe including at least CF = 1.0 one socket welded fitting within the span or at either end. (b) No socket welded fitting at either end or within CF = 4.0 the span. (c) Cantileve r CF = 10.0 b (d) One elbow in run, motion out of plane 2/L3 <.5, CF = 2.7 measure at center of long les L). (m) u> _ $sn - -_._. - b i e"d. nl ' ;;/:,, ,,,,JJ r , a ' &c
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Cont'd-(5) b (e) One elbow in run, motion out of plane 2/L 3 g.5, CF = 8.0 m measure at elbow (v ) (f) Guided Cantilever CF = 4.0 (6) Configuration factors (CF) for full penetration girth butt welded pipe sizes 2-1/2" through 24", inclusive. (a) Simple span of straight pipe including at least CF = 1.0 one full penetration girth butt weld within the span
. or at either end. ,
(b) No full penetration girth butt weld within the span CF = 1.8 or at either end. (c) Cantilever CF = 10.0 (d) Guided Cantilever CF = 1.25 (e) One elbow in run, motion in plane CF = 0.3 (f) One elbow ir run, motion out of plane '2/L) (.5, CF = 1.0 measure at center of long leg Lj. L (g) One elbow in run, motion out of plane 2/L) 1 5, CF = 2.5 measure at albow x -(h) Two elbow in the span joined within one pipe diameter CF = 0.2 of each other - motion in plane of elbows ( (i) A single short radius schedule 40 elbow in run, CF = 0.7 pipe sises 12" through 24" inclusive. (7) Steel factor (SF) (a) For carbon steel CF = 1.0 (b) For stainless steel CF = 2.0 (8) Dynamic Factor (DF) (a) For steady state DF = 1.0 (b) For transients DF = 2.0
- (9) If pipe motion, estimated to be greater than MAV, is observed by the OPE l at the MOD then the Relative Displacement'(RD) must be determined at mid-gay The RD is the mid-span measured peak-to-peak displacements minus the versge of the end point measured peak to peak displacement along the axis of interest.
... (a) If RD(MAV the vibration is acceptable O
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SP IE6 ti-001 Rav. I h.kbE bL Cont'd (9) (b) If RD) MAV the OPE will take the necessary steps to resolve the p( #/ condition in accordance with the procedures of paragraph 6.1c.6 for steady state testing or 6.2c8 for transient testing. ( (10) The stop test limit is = HAV x 2.5. (11) The asterisks (*) in the table above appear where continuous operating stresses in short spans cannot be inferred using peak to peak relative displacements at mid-span using hand-held instrumentation. (12) Interpolation of span length dithin the table is permissible. (13) This table and the above accompanying notes cannot be used to detemine overall piping stresses due to high frequency ( 2100 HZ) vibration. Refer to paragraph 6.1c.3/6.2c.4 as applicable for additional testing details. (This table has less stringent requirements than the previous
- table in Addendum D)
(14) In all cases vibration readings must be parallel to the axis of the supports acting.as the end points of the span. s 6 Sg o
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SP 1E68-001 R ,v . 1 L,Tk//tibA #1 SYSTEM VIBRATION SPECIAL TEST PROCEDURE 1.0 OBJECTIVES , 1.1 To verify that transient induced pipe vibrations and steady state vibrations during acceptance, preoperational and other system testing are within acceptable limits for selected BOP piping, designated as follows:
- a. ASME Code Class 1, 2, and 3 piping systems.
- b. High-energy piping systems inside seis=ic Category I structures.
- c. High-energy portions of systems whose f ailure could reduce the functioning of seismic Category 1 plant features to an unaccep-table safety level.
l l d. Seismic Category 1 portions of moderate-energy piping systems 1 located outside containment. NOTE: In the context of this procedure, BOP piping means piping other than recirculation and main steam piping. 1.2 To demonstrate that small attached piping, test connections, branch line connections and instrument connections were not in resonance with the major sources of vibration in their respective syste=s during steady state and transient vibration testing. l l l 1.3 To desc r.. crate that during steady state and transient vibration l testing, evidence of excessive stressos due to high frequency vibration including weld cracks, loose nuts and bolts, loose l threaded connections and flow instabilities was not found. l o/ i v r-;y3-.3,,.,
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Rsv. 1 Tai Mcf cd "i 1.4 To demonstrate that for spring hangers identified as being within the scope of piping for transient vibration testing, at the com-pletion of testing, on a system by system basis, spring hangers were inspected and hangers were within the hot and cold setpoints. 1.5 To demonstrate that for snubbers identified as being within the scope of piping for transient vibration testing, at the completion of testing, on a system by system basis, snubbers were inspected and no evidence of snubber damage was found. NOTE: Thermal Expansion Preoperational testing, as outlined in Test Specification TS-E68, will be performed in Test Procedure SP-1E68-002, System Thermal Expansion Special Test Procedure. During Post Fuel Load testing, piping and restraint response to thermal expansion as well as certain dynamic and steady state responses will b demonstrated for selected systems, as identified in Test Specifica-tion P99, Post Fuel Load BOP System Vibraticn Testing i Acceptance Test. Portions of systems identified in this 1 procedure which cannot be properly monitored due to operating constraints shall be deferred to P99, utilizing
- a test exception.
2.0 REFERENCES
i 2.1 The Cleveland Electric Illuminating Co., Perry Nuclear Power Plant i Units 1 and 2, Final Safety Analysis Report, Table 3.2-1, Chapter 1 3.9.2 and Chapter 14.2.12.4.1, Amendment - 27. 2.2 U.S. Nuclear Regulatory Commission Regulatory Guide 1.68 - Initial l Test Programs for Vater Cooled Nuclear Power Plants, Revision 2, August 1978. l 2.3 ANSI /ASME OM3-1982, Requirements for Preoperational and Initial l'k<s Start-Up Vibration Testing of Nuclear Power Plant Piping Systems.
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. 2.4 GAI Flow Diagrams:
rm SYSTEM ( DRAVING NO. jtEV. cicas nvil=6 'B21) D-302-605 D-302-606 C Reactor Water rculation (B33) D-30 1 D 602 D-302-603 B C gh D-302-604 B M l.t4-EG Control Rod Drive ' raulics (C11) 2-871 G D-302 ' G St y Liquid Control (C41) D-302-691 C
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Residual Heat Removal (E12) D-302-641 , 4- M D-302-642 -ft- 6\ D-302-643 1,- M
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3c" Pr-serre core Spray (I22) D-302-705 - High Pre re Core Spray (E22) D-302-701 K
~)' Leak Detection Sy m (E31) 2-964 C yh b
Reactor Core Isolation Coo ) D-302-631 E Nb D 302-632 E l N SL Reactor Water Cle up (G33) 2-671 F D-302- G Re - r Water Clean-up Filter D-302-675 G us iu.a.11 . (G36) - Fuel Pool Cooling and Clean-up (G41) D 002-001 X D - 0 02 - 0;'. "
. D-302-655 -F- 7 Suppression Pool Clean-up (G42) D-302-681 -2, Es
""--:nt i:2 ?::'. ". du- (C' ", O 102.-000 Control an Humidification (M.
uter Room D-913-41 B hk g Combustible Gas Control 5-1 D-302-831 H t N., 2-832 H Main R eat Extraction and D-302-121 F
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" . ed eter L;;h:;; C;;tr:1 (N27) D-302-971 i D-302-082 Con sate Transfer and Storage (P11)' D-302-102 L Service ater (P41) D-302-212 L
Emergency osed Cooling (P42) D-302-621 F D-302-62 D D-352- 1 H Nuclear Closed Co ling (P43) D-3 .-611 F D- 02-612 E
-302-613 E g
Emergency Service Water P45) D-302-791 G M3 D-302-7,92 G (.14- % Control Complex Chilled Wate. (P ) D-913-001 R D-913-002 K Emergency Service Water Scr en ' D-302-214 J Wash (P49)
} Safety-Related Instrum .t Air (P57) D-302-271 B Auxiliary Steam (P6 p 1. 302-053 G
/
Standby Diesel Ge'nerator Starting D-3 -351 G Air (R44) Standby Dies'el Generator Fuel D-302-352 G Oil (R45) HPCS Die el Generator Fuel Oil (R45) D-302-356 A Stan4by Diesel Generator Exhaust, D-302-355 C Int ke and Crankcase (E22, R48) tandby Diesel Generator Lube D-302-353 B
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( TPI-28, Conduct of Preoperational and Acceptance t ests, Rev. d., RS e> q "$ ~ A 2.7 TPI-7, Test Procedure Preparation, Revie~w and Approval, Rev. .. g
) 2.8 TPI-29, Test Results Review and Approval, llev. -t--
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SP 1E68-001 , Rev. 1 TuitAdA~du~ *1 2.9 Test Specification TS-E68 System Vibration Preoperational Testing, approved date November 16, 1983; Addendum A, approved 3/5/84; Addendum B, approved 7/30/84; Addendum C, approved 2/11/85. Ab(% b op cM( t/,G/85; 4ideada E,egeve4( 4/Z'/Cf 2.10 Test Specification TS-P99 Post Tuel Load BOP Systers Vibration Acceptance Test, preliminary issue date August 30, 1983. 2.11 ANSI /ASME OM4-1982 Examination and Performance Testing of buclear Power Plant Dynamic Restraints.
- 2. 12. 1/ibeden and Therma.l blc pld.ce..kcAh Modif oritid Di<gramsr -
0-3cN.yl 5 Aut I Ra A, Shed 2 Rev B, Sheef 3 Ra. A 7 0 3cs-d Ra. , J Lt3 swTen onmATM rk9thcTic4 soI E-l't. , he L. d-l 3.0 TEST EQUIPMENT F'.h4 3 L. %L, 3.1 Portable vibration monitor, Vibrametrics Model MSD with model 1020 accelerometer (or EQUAL). NOTE: The type of vibration monitor and associated equip =ent to be used shall be determined by the STE at the time of '\- testing. This determination shall be based on particular test equipment applications and types of data required to be taken. Vibration monitoring equipment actually used shall not be inferior to test equipment specified. 4.0 LIMITS AND PRECAI."TIONS 4.1 The System Test Engineer / Leader is aware of all major construction and maintenance activities in the testing area. 4.2 Periodic inspections of pipe support components should be performed during testing to detect possible component malfunction. Oil leaks, j bent shafts, deteriorating grouting around anchor bolts, etc., are
- , all symptoms of impending component f ailure. Pipe support compo-i nents exhibiting these symptoms shall be repaired and the cause for the malfunction analysed.
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SP 1E68-001 R:v. 1 , K.,fhk/ctItw. #$ 4.3 Numerous pump / motor starts and stops may be required to conduct testing in Sections 6.1 and 6.2. To prevent excessive heat buildup and possible motor damage, manufacturer's limitations for successive motor starts shall be adhered to. , 4.4 Test personnel shall obcerve test hold / termination criteria con-tained in this procedure. Otherwise, piping and equipment da= age may result. Test personnel shall be qualified and assigned by Gilbert Associates, Inc. 5.0 PREREQUISITES NOTE: Obtain necessary copies of the Prerequisite Checklist Sheet, Attachment No. 2,, and sign off each step as is completed. 5.1 Enter the following on the Prerequisite Checklist Sheet:
- a. System Name
- b. System MPL No.
- c. Date 5.2 An initial walkdown of the system, or applicable portions thereof, has been co=pleted and the following ite=s have been verified:
- a. Piping is supported and restrained in conformance with design drawings. The Qualified Piping Engineer may approve selected supports / restraints not to be installed /co:plete based on his l evaluation of effect on test. Ince=plete/not installed supports are docu=ented on the memorandum from NCES.
(Ref. 5.3) l
- b. No obstructions to pipe movement exist other than designed, (including snuWr surrogates) 1 6 - ~ r. - ., . . ~ .
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- c. Suspension components are correctly installed and free of damage,
- d. Pipe support components are unblocked and free to operate,
- e. Spring hangers are cold set with cold position marked.
- f. Insulation is removed where required.
5.3 A memorandum describing the status of system supports at time of testing has been received from NCES Piping Engineering. NOTE: See 5.2.a 5.4 Complete the Test Equipment Calibration Signoff Sheet, Attachment 7. 5.5 Experienced test personnel are available and have been familiarized with the sections of piping / support components they are to observe and the acceptance criteria for those piping / support components.
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L 5.6 Safety and jurisdictional tagging has been completed, as applicable. 5.7 Briefing conducted per Reference 2.6. 5.8 Communications have been established between the control room and the Qualified Piping Engineer performing piping observations. 5.9 The system being monitored is capable of being operated in the modes specified for steady state und transient vibration testing. 5.10 During steady state and transient vibration testing, a Qualified Piping Engineer (QPE) of Gilbert Associates, Inc. shall observe vibration testing and review test results.
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SP 1E68-001 Rtv. 1 7~WI h/tndm #1
.- 5.11 Authority is obtained from the Unit Supervisor / Test Coordinator to start the test.
6.0 'ITST PROCEDURE 6.1 , Steady State vibrs. tion Testing CAttrION: FAILURE TO OBSERVE TEST HOLD / TERMINATION CRITERIA CON-TAINED IN THESE INSTRUCTIONS MAY RESULT IN SEVERE PIPING AND EQUIPMEh7 DAMAGE.
- a. Obtain necessary copies of Data Sheet No. 1, Attachment No. 3.
NOTE: Testing is conducted on a system by system basis, , however, for the testing of large systems more than one data sheet may be necessary. gb b. Record the following on Data Sheet No. 1, Attachment 3. b
- 1) Date and time of test.
- 2) System Name and MPL No.
,NCI : For steady state testing, the system should be in a normal operating valve lineup. Running equipment should be in a normal operating configuration.
- 3) Equipment running at time of test.
- 4) System flow rate.
- 5) Verification that system flow is within 10% of design conditions, as determined by the E68 system Test Engineer.
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- 6) Piping section(s) monitored.
- 7) System valve lineup.
- c. Using the following test instructions, inspect piping iden-tified in Section 6.1.d of this procedure and record results on Data Sheet No. 1.
- 1) During acceptance, preoperational and other system testing, visually inspect identified piping to ensure that piping vibrations are within acceptance criteria limits.
NOTE: Piping which connects to a nonmonitored system shall be inspected to the end of identified piping scope. The end of piping scope shall constitute an end point r>f the piping span.
- 2) During visual observation, attention shall be given to small attached piping, test connections, branch line i
connections and instrument connections to ensure that they f are not in resonance with the c:ajor sources of vibration in their respective systems. Branch line connections shall be inspected to the point where the pipe has been restrained in the three orthogenal directions unless l otherwise specified.
, NOTE: Flow control valves, restricting orifices, and other components which produce a large differ-ential pressure are sources of high frequency vibration.
l .
- 3) For high frequency vibrations (2100 Hz), piping stresses cannot be determined by using enly the Paragraph 7.1 Acceptance Criteria Table (Attachment 1). In conjunction with monitoring overall piping displacements, inspect piping subject to high frequency vibration for evidence of._.
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t damage or impending damage. Evidence of excessive stresses due to high frequency vibration include items such as: a) Surface cracks in welds or fluid leakage at welds, b) Loose nuts and bolts: Packing nuts Valve stem nuts Valve bonnet nuts and bolts Valve actuator nuts and bolts Valve limit switch clamp nuts and bolts c) Loose instrumentation line/ valve actuator air 13na threaded connections. d) High noise levels due to possible cavitation or other# flow instabilities.
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i 4) Observe piping for excessive movements in other than the plane of support. Excessive movements shall be do:umented and brought to the attention of the Qualified Piping Engineer. Although no specific acceptance criteria exists for movements in other than the plane of support, exces-l sive movements include items such as: a) Piping movements in close proximity t_o.other p'iping and/or plant structures:' ' b) Piping movements which place piping support compo-nents in close proximity to -other' piping and/or plant structures. c) Piping movements to the extent that piping and/or
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support co=ponents may be permanent 1s distorted.
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d) Piping movements which are cyclic in nature during steady state flow conditions. e) Piping movements which are caused by and do not subside within five (5) seconds subsequent to a change in system flow rate or other transient.
- 5) For testing systems equipped with multiple pumps in parallel:
Piping should be inspected while operating various com-binations of parallel pumps as maximum vibrations may occur at one particular operating pu=p combination. Exa=ple: A system has three 50% capacity parallel pumps, A, B, & C. Test as follows:
- 1. Operate each pump singularly.
l h ['N (_,) 2. Operate combinations of pumps; A & B, A & C, and B & C. I NOTE: To minimize the number of pump starts and stops required to perform vibration testing, transient vibration testing of pump starts and stops should be conducted while placing the system in various pump operating configurations.
- 6) When visual inspection detects questionable vibration, such vibration shall be investigated as follows:
a) Vibration shall be monitored with a portable vibra-tion monitor and recorded on Data Sheet No. 3 (Attachment 5). 9 '
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SP 1E68-001 Rsv. 1 [es,Y IkdbCbNLG" % b) As required, the portion of the test during which questionable vibrations originated shall be repeated. Retesting shall be in compliance with applicable CEI administrative procedures. c) During the course of equipment monitoring and/or repeat tests, take regular vibration readings to determine compliance with acceptance criteria. If trends indicate that vibration levels are increasing and/or that acceptance criteria may be violated, increase the frequency at which vibration readings are taken. d) Once it has been determined that acceptance criteria
, have been violated ( the Qualified Piping Engineer shall be notified as soon as possible.
- 7) The Qualified Piping Engineer shall determine if a test
- hold is required. If so, the following corrective actions will be taken: l i a) Installation Inspection - a walkdown of the piping and pipe support components will be performed to identify any obstruction or improperly operating support co=ponents. The source of the excitation must be identified to determine whether it is related l to equipment failure. Action is taken to correct any I discrepancies prior to repeating the test. b) Instrumentation Inspection - the instrument cali-bration is checked and discrepancies are corrected. Additional instrumentation is added if necessary, c) If items 7)a) and 7)b) above identify discrepancies that could account for failure to satisfy acceptance criteria, the test is repeated after completion of {O , 12 - Q*;* ; * ;;(, { 9, ,, j ( C W00036 'y t y *p e ..w .- _. -
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%sfbdclbtkuw W1 the necessary corrective action and Data Sheet No. 4 (Attachment 6).
- 8) Assemble, for each system tested,_ Prerequisite Checklist Sheets, Data Sheets and other test records generated as a result of testing and identify those records as part of the test package for that system.
- 9) the System Test En On a system ANb TricbycWune.D systeo basis,5 h f14 EL6#Nceq,(QPc)gineer (STE)"shall signify, by signature in the space provided, satisfactory completion of required Steady State Vibration Testing for piping identified in Section 6.1d. of this procedure.
- d. Piping to be visually inspect,ed,for steady state vibrations during acceptance, preoperational and other system testing is identified as follows:
TEST SATISFACTORILY < 7~ TEM PIPING TO BE MONITORED COMPLETED /
- 1) Nuclear oiler (B21) 15-1" lines from vessel to first
! three way support. / STE Signature Date
/
QPE Signature Date g
- 2) Reactor Water a. All scellaneou small bore M Recirculation (B33) piping % ofefe'cire, pu=p li4-$
- suction an 'disch. piping i and valves. /
i
-STE Signature Date l
/
QPE Signature Date
- b. Both 4" lines from recire.
l pump suctions to G33 sys. / l 1 STE Sigha ure Date
- l. QPE Signature Date s l8 !.. ., _ ,, ; y l - -- ~ . . -
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Test Addendum #I T f'- 6.1. d 10" branch line (of f of 10" Fuel Pool Cooling
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/ / s a PG QPE Signature Date lO l -
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haust silencer D008 and to e' 36 ne and D012. - STE Sigpature Date
/ k[A QPE Signature Date g
- g. If test of standby sal 1 N'N generator C001A ated piping indicates a ration problem, test CO related piping also. /
STE Signatu Date QPE Signature Date
- e. System tested is to be restored to the configuration specified by the Unit Supervisor.
. 6.2 Tran.tient Vibration Testing .
CAlTTION: FAILURE TO OBSERVE TEST HOLD / TERMINATION CRITERIA CON-TAINED IN THESE INSTRUCTIONS MAY RESULT IN SEVERE PIPING
)
t AND EQUIPMENT DAMAGE. ? O lt l NOTE: Unless otherwise specified, transients should be Ilmited to normal operating transients expected over the life of the plant.
- a. Obtain necessary copies of Data Sheet No. 2, Attachment No. 4.
. NOTE: Testing is conducted on i system by system basis, however, for testing of large systems more than one i
data sheet may be necessary, i
- b. Record the following on Data Sheet No. 2:
l
- 1) Date and time of test.
- 2) System name and MPL number.
- 3) Equipment running prior to transient test.
- 4) Transient (s) to be monitored.
- ;,,.2 .
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.. 5) System valve lineup.
C,vi c. Using the following test instructions, inspect piping during the transients specified in Section 6.2d of this procedure and record results on Data Sheet No. 2:
- 1) . During acceptance, preoperational and other systems testing, visually inspect identified piping to ensure that piping vibrations are within acceptance criteria limits.
- 2) Only that portion of piping identified in Section 6.1d need be inspected unless otherwise specified in Section 6.2d. The extent of this observation shall be at the discretion of the QPE.
- 3) During observation of each'of the transients identified in Section 6.2d., attention shall be given to small attached piping, test connections, branch line connections and
, instrument connections to ensure that they are not in resonance with the major sources of vibretion in their respective systems. Branch line connections shall be inspected to the point where the piping has been restrained in the three orthogonal directions, unless otherwise specified. ! 4) Flow control valves, restricting orifices, and other 1 components which produce a large differential pressure are sources of high frequency vibration. For high frequency vibrations (2:100 Hz), piping stresses cannot be determined by using only the Paragraph 7.1 Acceptance Criteria Table (Attachment 1). In conjunction with monitoring overall i i
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SP 1E68-001 Rav. 1 M MMe,n Luw D piping . displacements, inspect piping subject to high -
) frequency vibration for evidence of damage or impending
() damage. Evidence of excessive stresses due to high frequency vibration include items such as: a) Surface cracks in welds or fluid leakage at welds. b) Loose nuts and bolts: Packing nuts Valve Stem nuts Valve bonnet nuts and bolts Valve actuator nuts and bolts Valve limit switch clamp nuts and bolts l c) Loose instrumentation line/ valve actuator air line threaded connections. l'
) d) High noise levels due to possible cavitation or other flow instabilities.
[) e
- 5) Observe piping for excessive movements in other than the plane of support. Excessive movements shall be documented and brought to the attention of the Qualified Piping Engineer. Although no specific acceptance criteria exist for movements in other than the plane of support, exces-sive movements include items such as:
1 I - a) Piping movements in close proximity to other piping and/or plant structures. b) Piping movements which place piping support-compo-nents in close proximity to other piping anc/or plant structures.
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- , c) Piping movements to the extent that piping and/or support components may be permanently distorted.
d) Piping movements which are cyclic in nature during
. steady state flow conditions.
I e) Piping movements which are caused by and do not subside within five (5) seconds subsequent to a change 'in system flow rate or other transient.
- 6) For testing systems equipped with multiple pumps in parallel:
l Piping should be inspected while operating various com-binations of parallel pumps. Unless otherwise specified, transients should be limited to normal operating tran-sients expected over the life of the plant.
- Example: A system has two 100*. capacity parallel pumps, A&B. Test as foll'ows:
i
- 1. With both pumps off, start pump A.
- 2. With A pump running, start B pump and stop A pump.
- 3. Stop B pump.
NOTE: To minimize the number of pump starts and stops required to perform vibration testing, steady state vibration testing of various operating configurations should be conducted in conjunc-tion with transient vibration tests.
- 7) During piping system transients, observe pipe support
) corrponents identified as being within the scope of piping
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for transient vibration testing. Verify that spring hangers remain between their hot and cold setpoints at the end of each transient and that there is no evidence that snubbers became fully extended or retracted, nor is there v2sual evidence that the snubber was damaged.
- 8) When visual inspection detects questionable vibration, such vibration shall be investigated as follows:
a) As required, the portion of the test during which questionable vibrations originated shall be repeated. Retesting shall be in compliance with applicable CEI administrative procedures. b) During retesting, piping shall be monitored beyond the first rigid support from the component initiating the transient to determine that piping vibrations beyond that point are within acceptable limits. v l c) During the course of equipment monitoring and/or repeat tests, take regular vibration readings to determine compliance with acceptance criteria. d) Once it has been determined that acceptance criteria have been violated, the Qualified Piping Engineer l shall be notified as soon as possible. 1 e) Vibration shall be monitored with suitable transient ' recording instrumentation and recorded on Data Sheet No. 3 (Attachment 5). g
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- 9) The Qualified Piping Engineer shall determine if a test hold is required. If so, the following corrective action will be taken:
a) Installation Inspection - a walkdown of the piping and pipe support components t'ill be performed to identify any obstruction or improperly operating support components. The source of the excitation must be identified to determine whether it is related to equipment fan u.e. Action is taken to correct any discrepancies prior to repeating the test. b) Instrumentation Inspection - the instrument cali-bration is checked and discrepancies are corrected. Additional instrum,entation is added if necessary, c) If items 9)a) and 9)b) above identify discrepancies that could account for failure to comply with accep-tance criteria, the test is repeated after completion of the necessary corrective action and Data Sheet l No. 4 (Att;.chment 6).
- 10) Assemble, for each system tested, Prerequisite Checklist Sheets, Data Sheets and other test records generated as a result of testing and identify those records as part of the test package for that system.
11) On a s stem by4d system basis the System Test Eng -, b TtM AUF @ Pi /mG G6tucER CQPcineer j (STE)' all signify, by signature in the space pr)ovided, satisfactory co=pletion of required Transient Vibration l Testing for transients identified in Section 6.2d of this procedure. J. T ra.,w.d s + c L . m o a , + c r e_ d 1 .4 i a cue pfu.s ca , - l . .. pn.egecc.4, cal aaA oHw m Je.n h.b i ,9 a ee. U l) 1
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- 6.2.d Pump IE12-C001B start and stop with the E12 system aligned in the Fuel Pool Cooling Assi "B" mode. , h /rf 2Pk) g g STE Si ature Date
. , scO#S 'E
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QPE Signature Date IO31 l b) Generator 1R43-C001B /_ _ STE S2 re Datc l l QPE Signature Date
- e. System tested is to be restored to the configuration specified by the Unit Supervisor. I 7.0 ACCEPTANCE CRITERIA 7.1 Piping steady-state and transient vibrations at the center of the span were within the peak-to peak limitations of the enclosed, Attachment 1, Paragraph 7.1 Acceptance Criteria Table for selected
}
BOP piping designated as follows: ' a
- a. ASME Code Class 1, 2 and 3 piping systems,
- b. High-energy piping systems inside seismic Category I struc-tures.
- c. High-energy portions of systems whose failure could reduce the functioning of seismic Category I plant features to an unaccep-table safety level,
- d. Seismic Category I portions of oderate-energy piping systems located outside containment.
7.2 Small attached piping, test connections, branch line connections and instrument connections were not in resonance with the major sources of vibration in their respective systems during steady state and transient vibration testing. [ . .. - - . -
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SP 1E68-001 Rav. 1 l*3k YbG U U. 7.3 During steady state and transient vibration testing, evidence of excessive stresses due to high frequency vibration including weld cracks, loose nuts and bolts, loose threaded connections and flow instabilities was not found. , 7.4 .7or spring hangers identified as being within the scope of piping for transient vibration testing, at the completion of testing, on a
~
system by system basis, spring hangers were inspected and hangers were within the hot and cold setpoints. 7.5 For snubbers identified as being within the scope of piping for transient vibration testing, at the completion of testing, on a system by system basis, snubbers were inspected and no evidence of snubber damage was found NOTE: Satisfying the requirements of Paragraph 7.1 demonstrates snubbers do not become fully extended or retracted during I transient vibration testing.
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- - - Rav. I PARAGRAPH 7.1 ACCEPTANCE CRITERIA TABLE Mf dhn Q TNFP
(~'a PRE- FUEL LOAD BOP SYSTEMS VISUAL VIBRATION ACCEPTABLE CRITE3IA () ALLOWABLE RELATIVE DISPLACEMENTS NOMINAL TYPE SIZE LENGTH OF SPAN IN FEET WELD INCHES L Minimum 6 9 12 15 18 21 24 27 3/4" 10 e L=3.8' 25 56 Socket 1" 10 0 L=4.2' 20 44 Welded 1-1/4" 10 0 L:4.7' 16 35 - SPAN LENGTHS Pipe 1-1/2" 10 e L=5.0' 14 31 ARE NOT 2" to e L=5.7' 11 25 44 EXPECTED IN THIS REGION - 2-1/2" 10 0 L=3.9' 24 54 96 3" 10 @ L=4.2' 20 45 80 4" 10 0 L:4.9' 15 34 60 94 Full 6"-
- 24 40 63 90 Penet. 8"
- 17 30 ff 68 92 Girth 10"
- 14 24 38 54 74 a 20 80 Butt 12" 11 31 45 61 Welded 14" *
- 17 27 39 53 69 Pipe 16" ' '
15 23 34 46 60 18" *
- 13 21 30 41 53 68 l
d 20" *
- 12 19 27 37 48 61 l
. 22" ' ' 11 17 25 33 44 55 24" ' ' 10 16 23 31 40 51 NOTES: .
(1) Tabular values are for: (a) Mid-span deflections in the plane of the end supports (b) Steady state operation (c) Displacements given in mils (1 mil = .001 inch)' peak to peak (d) Si=ple span of straight pipe (e) Carbon Steel pipe _ (f) Schedule 40 wall thickness and greater (g) End points of the span at rigid supports: struts, anchors or l equipment connections (h) Long radius elbows (1) At least one socket welded fitting or one full penetration girth butt weld in the span or at end point of the span (j) Pipe tests at low temperatures where pipe stresses from thermal effects will not be significant and themal pipe growth will not affect the nominal assumed 1/32" minicum clearance at pipe supports other than rigid struts, anchors and equipment. l*=o l
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S? IE6@cc( Rev. 1 T'ddd('c,d<,5. (2) A Maximum Allowable Visual (MAV) displacement will be determined for each pipe span surveyed visually. If pipe motion is not observed by the /7\
/ Oualified Piping Engineer (OPE) at the maximum observing distance (MOD)
\ the vibration is acceptable.
(3) Determine MOD by dividing MAV by a factor of between 2 and 3, to be detarmined on-site prior to testing by the OPE, consistent with the visual acuity of designated surveyors. (4) Determine MAV by one of the following methods: (a) For the case ,of both en,ds of the pipe span supported rigidly with either rigid struts, anchors, or equipment connections, use the expression: MAV = CF x SF x DF x TV where: CF = configuration factor, or product of all applicable factors - see notes 5 or 6 below SF = steel factor - see note 7 DF = dynamic factor - see note 8 TV = tabular value from the above for corresponding pipe size and span length. (b) For the case of only one end of the piping span supported rigidly with either a rigid strut, an anchor or an equipment connection. Use the higher of the following two values: fN (i) MAV = 25 mils; or . N_,/ (ii) MAV = CF x SF x DF x TV 1 l (c) For the case of neither end of the piping span supported rigidly with either a rigid strut, or anchor or an equipment connection, . use the higher of the following two values: l (1) MAV = 40 mils; or (ii) MAV = CF x SF x DF x TV (5) Configuration factors (CF) for socket welded piping sizes 3/4" through 2", inclusive (a) Simple span of straight pipe including at least CF = 1.0 one socket welded fitting within the span or at either end. l (b) No socket welded fitting at either end or within CF = 4.0 i the span. l (c) Cantilever CF = 10.0 (d) One elbow in run, motion out of plane '2/L3 <.5, CF = 2.7 measure at center of long les L j . r3 .
- 56a -
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Cont'd (5) * (e) One elbow in run, motion out of plane 2/L A.5, CF = 8.0 measure at elbow 3 / z_ (Vh (f) Guided Cantilever CF = 4.0 (6) Configuration factors (CF) for full penetration girth butt welded pipe sizes 2-1/2" through 24", inclusive. (a) Simple span of straight pipe including at least CF = 1.0 one full penetration girth butt weld within the span
, or at either end. .
f.b ) No full penetration girth butt weld within the span CF = 1.8 or at either end. (c) Cantilever CF = 10.0 (d) Guided Cantilever CF = 1.25 (e) One elbow in run, motion in plane CF = 0.3 b (f) One elbow in run, motion out of plane 2/L <.5, CF = 1.0 measure at center of long les L;. b (g) One elbow in run, motion out of plane 2/L 15, 3 CF = 2.5 measure at elbcw
-(h) Two elbow in the span joined within one pipe diameter CF = 0.2 / \ of each other - motion in plane of elbows V
(1) A single short radius schedule 40 elbow in run, CF = 0.7 pipe sises 12" through 24" inclusive. (7) Steel factor (SF) (a) For carbon steel CF = 1.0 (b) For stainless steel CF = 2.0 (8) Dynamic Factor (DF) (a) For steady state DF = 1.0 (b) For transients DF = 2.0 (9) If pipe motion, estimated to be greater than MAV, is observed by the OPE at the MOD then tne Relative Displacement (RD) must be determined at mid-span. The RD is the mid-span measured peak-to-peak displacements minus the average of the end point measured peak to peak displacement along the axis of interest.
.. (a) If jD( MAV the vibration is acceptable r- - - 3~ .- . . . , . ~
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SP IE66-UUl Rev. I Nf hi t.s I Cont'd (9) (b) If RD) MAV the OPE will take the necessary steps to resolve the / \ [,,,} condition in accordance with the procedures of paragraph 6.1c.6
- Ns/ for steady state testing or 6.2c8 for transient testing.
(10) The stop test limit is = MAV x 2.5. (11) The asterisks (*) in the table above appear where continuous operating stresses in short spans cannot be inferred using peak to peak relative displacements at mid-span using hand-held instrumentation. (12) Interpolation of span length dithin the table is permissible. (13) This table and the above accompanying notes cannot be used to determine overall piping stresses due to high frequency ( 2100 HZ) vibration. Refer to paragraph 6.1c.3/6.2c.4 as applicable for additional testing details. (This table has less stringent requirements than the previous table in Addendum D) l (14) In all cases vibration readings cu3t be parallel to the axis of the supports acting .aus the end points of the span. O a i l I l t ['
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e SP 1E68-001 Rev. 1 9 6 f .*(., (d h - (% Test Identification No: Alf d Y.C3 f- 27-$6 O Retest? Tes No) AITACHMDTI 2 PREREOUISITE CRECKLIST SHEET 5.1. a. System Name 17C9 b dL NGAF YL M IdL
- b. System MPL No. IEIL
- c. Date C-7 7 - b'l 5.2 Initial Systen Walkdosm
- a. Piping Supports and Restraints h[L3 / b - 2 7-5c., ~
Initials Date
- b. Pipe Movenent Obstructions (including snubber surrogates) blTb / D U-bb Initials Date 3
- c. Suspension Components Undamaged 323 / f-11-h
/% Initials Date
- d. Pipe Support Components Free to Operate 3l'Cb /f-27,h Initials Date
- e. Spring Hanger Cold Settings 3?M /_ { ~27-Q Initials Date
- f. Insulation Removed Where Required M / (-22-)b Initials Date 5.3 Hanger Status Memo Received
[7h / $ 7.7.-$h Initials Date ( 5'. 4 Test Equipment Available and Calibrated [M Initials Date
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- a. Make & Model IbMCIIllvsM.D
- b. MPL No. l 70" hN7
.c. Calibration Due Date 7- D '
5.5 Test Personnel k / [-7 7-b Initials Date ! 5.6 Tagging Coepleted 3}?2% Initials Date
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SP 1E68-001 Rr.v. 1 T:ct LdcIncittw % Test Identification No: k(!k D@ S-M-bb ATIACEMENT 2 (Cont'd) PREREOPISITE CHECKLIST SHEET 5.7 Briefing Conducted hRE2 / s-7 7- sC, Initials Date 5.8 Communications Established MYS / 5'-77-SL Initials Date 5.9 Monitored System capable of Operating Modes Mi2N3 /s '27 $ l. Initials Date 5.10 Qualified Piping Engineer Available h[3 /,( A 7 - b(', Initials Date 5.11 Authority to Start Test s
@N/5-77-h Initials Date l
l l Prerequisite Checklist Sheet Reviewed by: l l [L . Y7aM System Test Engineer Signature
/ Date L 77-(
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o SP 1E68-001 Rev. 1
%% ( f.c[c[ct Ltu-Test Identification No: MN I'U' Retest? Yes No AITACHMENT 3 SYSTEM VIBRATION PREOPERATIONAL TESTING , STEADY STATE DATA SHEET NO. 1 Paragraph 6.1 STEADY STATE TESTING Documentation of Steady State Visual Inspection Results Date: C-W-M System Name: NelfD AL /-lt:4T}Ztatet),\L_
Time: D 6 '5D System M?L No.: l E I'7_ e I l Identify Running Equipment: SELY LJM Elfh PbiEldtd System Flow Rate (gpm): _7W o bha ' System Flow Rate Within 10% of Expected Normal Operating Flow Rate: Yes No
/( _
l (,)/ Piping Section(s) Monitored: , GEG l& W 1 1
'"*I "d_****[$yN *(('rp n{E FucL ?ce' kw N 6 ANI Y #N l Satisfactory Visual Inspection Results Obtained: bTes l
No (If No, cceplete l and attach Data Sheet 3.) System vibration inspection results werehisfactohunsatisfactory per Section 7.0: m t b iSMT STE Signature Date L
.,~ /5A tl4 Gilbert QPE Signature l 5 22- FC Date 3
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n SP 1E68-001 Rsv. 1 Test Identification No: Mfk D3 G77-b Retent? Yes No u ATTACHMENT 4 SYSTEM VIBRATION PREOPERATIONAL TESTING TRANSIENT DATA SHEET NO. 2 Paragraph 6.2 TRANSIENT TESTING Documentation of Transient Visual Inspection Results Date: f-7 2- S b- System Name: k%IDCIkL I4 ear km-0A-t -.- Time: 69 % System MPL No.: / E l ~L Running Equipment: % E' LiN E O 'l3 E W (Prior to start . of test) Transient (s) Monitored:
) 1. lEll.- bxR$ GTAYZT 77 @ 4.
1
- 2. 5.
l ! 3. 6. Specify Systen Valve Lineup: 5 % % AN T2M M NtM b 'C M ElLA (CL 6f4L(Mb kVt5.[ "U$"hl(N>(" Satisfactory Visual (Non-instrumented) Inspection Results Obtained: d Yes No (If No, complete and attach Data Sheet 3.) Systemvibrationinspectionresultswerekstisfactc3/unsatisfactoryper k , j q,.77 Q STE Signature Date
.Gilbert h / QPE Signature fc / / Cl?-k l... Date ) For unsatisfactory results. Data Sheet 4 is attached. ,
i s-
. t .. . ,000059
SP 1E68-001 Rsv. 1
'T (A Lu - $
'est Identification No: h 4 M S-17-@,
Retest? Yes Ws M% s/kW rs
^27^C"*E"T 5 p2R s-n-sL SYSTDi VIBRATION PREOPERATIONAL TESTING INSTRIMENT RESULTS DATA FEEET NO. 3 TRANSIENT OR STEADY STATE TESTING Docueentation of Instrumented Inspection Results Date: System Name:
Time: System MPL No.: Vibration Monitor Used: Name and Model: MPL No. Cal. Due Date Pickup Location (include counting method): Condition Monitored (transient or steady state, piping section monitored, - equipnent involved): Data:
. Data Recorded by: /
Signature Date
. I -
0 0 0 :3 ')
SP IE68-001
, Rav. 1 Tcsf eA l etufuse #1 Test Identification Nor d A M 5-77-6 M s b kTE- f M U b(A Fett $ fs TEL E ATTACRMENT 6 gg g,7),4 SYSTDi VIBRATION PREOPERATIONAL TESTING TEST FAILURE EVALUATICN DAYA SHEET NO. 4 System Name & MPL:
Nature of Failure (attach test data sheete):
)
l. l Recedial Action Taken: l Retest Required: Yes No
/~
Gilbert QPE Signature Date O , . _ _ . . , '
-:0 u0 6 3
Y lG$ W \ T&-e 1 I T(si ) cat LM ArnicdMeur 7 TEST EQUIPMENT CALIBRATION SIGNOFF SHEET l [ PNPP No. 6 2 70 Rev.5/ 8 5 CALIBRATION STATUS , (SEE NOTE 2 FOR CAL. STATUS SYMBA) l l INSTR M NT M ER/ INSTRUMENT DESCRIPTION 1 2 SERIAL NLNBER CA BRAT ON VERIrIE0/0 ATE (MODEL/NAME) VERIr!EDIDATE (SEE NOTE 1) uw guqn \hBeknewes Msh 9-r- et, WR s-D - Q-l l { NOTE: 1. INSERT SYMBOL "(AC)* AT BOTTOM OF B0x FOR ALL TEST INSTRWENTS USED TO VERIFY ACCEPTANCE CRITERIA IN PREOCERATIONAL OR SPECIAL TESTS.
* * ' ' ~
- 2. CALIBRATION STATUS SYMBOLS ARE AS FOLL0nS:
I ALL *AC' INSTR WENTS HAVE BEEN CALIBRATED nITHIN APPDOX. 6 MONTHS OF START OF TFST. n STE MAY ORANT VARI ANCE TO "6 MONTH
- RECUIREWNT AS LONO AS CALIBRATICN OUE DATE IS NOT EXCEEDED OURINO USE OF THE INSTRLHENT. -
"~
- 2. ALL *AC" "NSTRUM".NTS ARE IN CAL. AFTER TEST COWLETION.
-G3' 00062
rei, nn-CHANGE AND EXCEPTION LIST s,tf _ l _ . ,,o. ,. ,,,, UNIT TEST PROCEDURE NO. GEVISION FILL IN ONLY IF APPLICABLE TEST A00!NOUM NO. g dbl 7 TP-hflLQM- { (
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PERRY NUCLEAR POWER PLANT
- NUCLEAR TEST SECTION Cat.NCE NLNBER - C-CESCRIPTION OF CwANCE b Akl[E N NN 2 b N#O bN U (i3 CdAut,E 64i 87eM6 L7 Fhhu 4 To P< e 6,
[D KbD TETE 1? ELE [ ( L h<, Ruad5 i ' 5%TC:n TTEtt ATIL6 2%STlwcTieu 5 O I E 17 , kc o . 7 FStC COWITwCNTS ArFECTED YES NO TEST C*ANCE CLASS rICATION MAJOR HINOA. DEASON rCa C*AN",E f ivUb RETblN3bEb e l - r04 ACCEPTANCE TEST ONLY FOR PPEOPERATIONAL AND SPECIAL TESTS ONLY _7 CC .* 0 ! N A T DA CtTE OAICINATOA >
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- C *E ,g C*t.N;E ENTERED CATE 9 g rc4C Mre44 e IDEA 05 AL lT TPAC MMNO NO. Shy 7 fe - 4L-005 CONCUAEENCE tt. T E hjh'd h? b h W ALD M 3 0
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' Minor cha";e to a cre:;eratic al cr s:e:isi test ray te si;"e: ty CSE, HTS.
;lGINATOR: PROMPTLY SEND COPY OF APPROVED TEST CHANGE TO NTS RECORDS, S210.
HINGAS- AT LTE Acep0.t.. w;.rA i- t.' ME. U S DA TPAC Cnt.Isut.N AroRO.A., AS EEMEO.
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TEST CHANGE FORM UNIT TEST PROCEDURE NO. REVISION FILL IN ONLY IF APPLICABLE 8UE k 7p, cp gg - @ g l REPEFJ0cwANCE NO. TEST AOCENouv NO. OfMM( M() l PERRY NUCLEAR POWER PLANT
- NUCLEAR TEST SECTION CHANGE NUMBER - C-OIP bN N 1 /ONS D b 3d NllIIN K . ddf7tYEC I DESfr DNOFbNCEttNE (2co 'ZtN, seco LEU 6 L Fiz<M th v e ro 'Trw I' (t y 61J W MbL 71 meo unm e m re n rr meme m, A -r zu we nawu exmc TEST CHANCE CLASSIFICATION MA;0R v 1 NCc .
FSAR COWITMENTS ArFECTED YES NO EEASON FOR CHANOE N Y I E L E - 4 FOR ACCEPT ANCE TEST ONLY FCC PAECCERATICML AND SPECI AL TESTS CNLY a-_ _. CATE ORIGINAT0d s ,i, [4 . CATE j ORIGINATOR (_ 4.cs . Wh 97[-$6 1
- REVIEnED By TEST COORDINATOR DATE
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CATE ApoA 'LTE CalE ADPROVED BY LTE
, f d'7. S'b h APPROVED BY CSE, NTS CATE e ,
A " #*'f4 " '##' #" '# " "' CATE APPR0 VAL'AT_TPRF MEETIN6No. CHANGE ENTERED
>YL 8t - /03 f.& %,.)L.0 S CONCURAENCE f,) t*. (7O WAAfA1d CATE S * *y> b I 'W OC - McW '
'b
- The Test Coordinator shall only revien minor test cha"ges initiated for testing a:tivities covered in TF1-;S.
" Minor cha~ge to a preccerational or special test way te signed by CSE, NTS.
~ 71NATOR: PROMPTLY SEND COPY OF APPROVED TEST CHANGE TO NTS RECORDS. S210.
kJ MINORS- Al LTE APPROVAL MAJOR $.AT CSE, NTS OR TPRC CHAIRMAN APPRD'. AL, AS RECUIDED.
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