ML20204H259
| ML20204H259 | |
| Person / Time | |
|---|---|
| Site: | Waterford  |
| Issue date: | 03/16/1999 |
| From: | Margotta K, Neyman G, Wills R ABB COMBUSTION ENGINEERING NUCLEAR FUEL (FORMERLY |
| To: | |
| Shared Package | |
| ML20204H122 | List: |
| References | |
| STD-100-237, NUDOCS 9903290040 | |
| Download: ML20204H259 (13) | |
Text
.
PROCEDURE FOR THE MODIFICATION OF REACTOR COOLANT SYSTEM PRESSURE BOUNDARY FOR THE INSTALLATION OF MECHANICAL NOZZLE SEAL ASSEMBLIES (MNSA)
FOR WATERFORD NUCLEAR GENERATING STATION UNITS 3 i Procedure No: STD-100-237, REV. 00 l
ABB Combustion Engineering Nuclear Operations l Chattanooga, Tennessee 1
Prepared By: 8,dh
~ == 2 Date: 3'l2 - f f O.S.NEYMARf ProjectManager Approved Bydd Date:d 12-91 R.L. Wills, Supervisor, NSSS Projects Approved By: KEA) M arc 47'S PM TNH d.2d+1. - 1 Date: 3-/2'f7 ~
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Approved By: ( .
, Date: 3[I3-f99 R. Tals Manager, Field Quality 11sk k: : k the property ofABB Combustion Emineerms Naelear Operations (ABB CENO), Cluntmoooga, Tennessee, ami k to be need onlyfor alw purpoons of the agreenannt with ABB CENO persmant to whkh it is fwnished
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. ,ihi i TABLE OF CONTENTS SECTION PAGE i
1.0 REFERENCES
3 1
2.0 - PREREQUISITES 4 1
3.0 PROCEDURE 5 3.1 HOT LEG RTD NOZZLE PREPARATION 6 3.2 HOT LEG PDT NOZZLE PREPARATION 8 3.3 HOT LEG SAMPLE NOZZLE PREPARATION 11 1
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1.0 REFERENCES
1.1 ABB CE Drawing No. E-MNSAWFD-228-001, Latest Revision, " Hot Leg RTD Mechanical Nozzle Seal Assembly".
1.2 ABB CE Drawing No. E-MNSAWFD-228-002, Latest Revision, " Hot Leg PDT MNSA".
1.3 ABB CE Drawing No. E-MNSAWFD-228-003, Latest Revision, " Hot Leg sampling MNSA" 1.4 ABB~CENO Procedure No: C-NOME-EP-0189, " Engineering Procedure for the Installation of the Mechanical Nozzle Seal Assemblies for Waterford Unit 3.
_ . . _ _ _ _ _ _ . . _ _ . _ . . _ _ __ _ _ _ ___~ _ _ _. _ _ _ ___._ _._ _.
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d e [of I3 qT 2.0 2.1 The Reactor Coolant System (RCS) is cooled down and available for work.
2.2 All necessary work platforms and scaffolds have been erected at the work area.
2.3 Compressed air,90 psig minimum, lighting and other services have been run to the work area.
2.4 Resistance Te+sare Detectors (RTD's) to be worked have been electrically disconw~i and the sensing elements removed from the instrument well. .
2.5 In=d=*ing material has been removed to the component shell surface in the vicinity of the nozzle or RTD to be worked. Insulation should be removed for-a minimu n of a 12" radius around the nozzle.
2.6 Other interference items have been removed or moved back from the work site to the maximum extent possible. Other insemwne lines or connections that could be easily damaged should be moved or protected as required.
2.7 Remove all loose foreign material from the base of the nozzle or RTD and the component shell surface in the area where the seal assembly will be mounted.
Particular attention should be paid to the area at the base of the nozzle or RTD where the seal gasket material will be placed.
2.8 Check all drillsprior to use to ensure the 29/64" diameter is correct.
2.9 The following additional tools are required for the installation of the work fixtures and modifications to the basic components to accept the MNSA.
2.9.1 Waterford approved cutting fluid for drilling ad tapping attachment boltholes.
2.9.2 Assorted small hand tools for installation of drill fixtures. l 2.9.7 Vacuum cleaner for chip removal.
2.9.4 Instruments fbr measuring drilled holes. Both hole depth and diameter measurunents will be required. Long handled snap gages (%" to 1" capacity) are suggested t'or the diameter checks.
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. Page 5 of 13 gAN 3.ib- i 3.0 PROCEDURE j NOTE: !
Should conniets be noted between dimensions and tolerances as stated on the I referenced drawings and limits used la this procedure, the requirements of the referenced drawings shall take precedence over limits in this procedure. Ensure the proper revision of the drawing is utilized. Actual installation of the Mechanical Nozzle Seal Assembly (MNSA) is provided in Reference 1.4.
This procedure is intended to provide a general sequence of steps for the preparation of the RCS pressure boundary to accept the Mechanical Nozzle Seal Assemblies. The locations applicable to this procedure are the various hot leg nozzles (RTD, PDT, and sample nozzles). The steps for the ymy-eion of the RCS pressure boundary for all the seal assemblies are essentially the same. Due to the variation in the nozzle diameters and i the surface geometry at the different locations, unique fixtures are required in order to I ensure proper orientation of the seal assemblies to that location.
A separate drilling fixture is provided for each type or size of nozzle. The drill motor and drill stand is common to all the fixtures.
The general sequence for the modification of the component surface to accept the MNSA is as follows:
- 1) Remove interference items and insulation from the area to be worked.
- 2) Clean the surface around the nozzle of all loose material
- 3) Mount and align the drill fixture to the nozzle. I
- 4) Drill and tap the first hole.
- 5) Lock the fixture into position by installing a bolt into the tapped hole.
- 6) Drill and tap the remaining mounting holes.
- 7) Remove the drilling fixture.
- 8) Insta11the MNSA. l Details for the accomplishmem of the individual steps should be perfected in a mockup prior to the actual nwQcations.
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3.1 HOT I FG RTD NOz7s.F PREPARATION The Hot Leg RTD Nozzle drilling fixture is a split plate assembly that mounts around and ,
clamps to the large boss at the top of the RTD. The fixture halves are bolted together using !
shoulder bolts and/or d/ vel pinned to maintain their alignment. The fixture halves are match !
marked. A mounting plate for the drill stand is attached to either side of the fixture. The mounting plate is indexed to the centerline of the drill bushing holes. A drill stand is attached to i the mounting plate. The drill motor and sliding plate is attached to the drill stand. There is a i sliding collar around one leg of the drill stand that is used as a drill stop to control the depth of ;
the holes to be drilled in the component shell. l Ensure the shell surface around the nozzle is clean and free of dirt, loose scale, or other foreign ;
material. Report any scoring or gouges on the shell or nozzle surface in the sealing area to ABB l CENO for disposition prior to installation. Ensure the area on the nozzle where the drilling fixture will attach is free of all foreign material and raised metal that would interfere with fit of 1 the fixture.
NOTE All machining operations shall be done in accordance with the requirements of Ref.1.1.
3.1.0 If necessary loosen the clamp bolts and separate the fixture halves so that it will pass over the head of the RTD nozzle. Ensure the mating surfaces of the fixture halves are clean and free of burrs. Tighten the fixture bolts to bring the halves together. Alternate between the fixture bolts while tightening to prevent binding of the dowel pins.
3.1.1 Align the fixture to 'l RTD nozzle to position the MNSA mounting holes by placing a e level on the upper surface of the fixture. Rotate the fixture until it is level. Move the fixture out slightly from the component shell such that it is not in contact with the component surface. This will ensure the fixture is aligned to the nozzle and not binding on the surface. His will also ensure maximum contact and grip of the clamping surface.
Tighten the nozzle clamp. Ensure the clamp is tight and the fixture does not rotate around the nozzle. l l
CAUTION Until the first hole is drilled and tapped and a stop bolt is installed to lock the clamp in ,
position, care should be exercised to prevent the fixture from rotating on the nozzle. l 3.1.2 Attach the mounting plate to either side of the fixture. Ensure the mating surfaces are free ofdirt, chips or burrs.
3.1.3 Attach the drill stand to the mounting plate. Mount the drill motor and slide plate to the drill stand. Do not tighten the slide plate mounting bolts. Ensure the mating surfaces are free of dirt, chips or burrs.
a 3.1.4 Install a 29/64" drill bushing into the fixture plate hole nearest the drill stand. Install a 29/64" drill bit into the drill motor. Ensure the drill bit is fully ih into the drill chuck.
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gne bushing. Tighten the drill motor clamp bolts when satisfled with the alignment.
3.1.6 Recheck the alignment of the fixture to the nozzle and adjust as required. Ensure the nozzle clamp is tight.
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3.1.7 Insert the drill bit into the bushing until the drill point makes contact with the cc-mg=:
l shell. On the back leg of the drill stand, position the drill stop collar approximately 0.985" ,
- below the movable drill stand plate. l 4
'; WARNING THE MAXIMUM DEPTH OF THE FINISHED HOLE MUST NOT EXCEED 1.12 KNCH.
i 3.1.8 Start the drill notor and drill into the component until the movable drill stand plate makes l contact with the drill stop collar. The drill bit should be backed out of the bushing
- periodically during the drilling operation to clear any chips that may accumulate in the j hole. Check to see that the hole is clear of chips prior to reinserting the drill bit into the hole. DO NOT EXCEED A MAXIMUM HOLE DEPTH OF 1.12 INCH.
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3.1.9 Remove the drill bit from the drill motor. Remove the 29/64" drill bushing from the
- fixture. Check to ensure the drilled hole is free of chips and other debris.
1 l 3.1.10 Install a tap bushing into the fixture. Tap the drilled hole using a 1/2"X20 UNF plug tap inserted through the bushing and into the hole until the tap bottorns in the hole. The holes may require tapping using both a plug tap and then a bottom tap to get the required number i of threads. It will probably not be possible to use the bottom tap in the hole until the drill 1 fixture is removed from the nozzle. The number of full threads should be checked prior to
! using the bottom tap. If there are sufficient threads after using the plug tap, it is not
! necessary to use the bottom tap. The minimum fully threaded depth is 0.68" (13 %" full
] threads).
3.1.11 After tapping the hole is complete, remove the tap bushing. Check and ensure the hole is 4
fme ofchips or other debris.
1 3.1.12 install a 1/2" drill bushing into the fixture and thread a 1/2" X 20 UNF bolt through the
! bushing and into the tapped hole to lock the fixture in place and prevent any mtation. The j bolt should only be finger tight in the hole.
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- 3.1.13 Move the drill stand to the other attachment point the p plate and drill the next hole as described in Steps 3.1.4 thru 3.1.g g 3.1.14 Move the mounting plate to the other side of the f and drill the remaining holes as described in steps 3.1.3 thru 3.1.y g,g,99 4- 3.1.15 Remove the drill stand, motor and m=*ia
- plate from the fixture plate.
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"/C"J^"F ^^ ^^ ;,1. . . ^0 d 3 Page 8 of 13 3-[m.91/A 3,g ff 3.1.16 Ensure the remaining drilled holes are free of chips and debris. Using the tap bushing, tap the remaining drilled holes using a 1/2" x 20 UNF plug tap inserted through the bushing until the tap bottoms in the hole. The holes may require tapping using both a plug tap and )
then a bo:som tap to get the required number of threads. It will probably not be possible to use the bottom tap in the hole until the drill fixture is removed from the nozzle. The number of full threads should be checked prior to using the bottom tap. If there are sufficient threads after using the plug tap, it is not necessary to use the bottom tap. The minimum fully threaded depth is 0.68" (13 %" full threads).
3.1.17 Remove the fixture from the RTD nozzle.
3.1.18 Ensure the tapped holes are free of chips and other debris. Inspect holes for final depth and length of thread. Threads are to be checked using a 1/2" X 20 UNF 2B GO - NO GO plug gage. The GO end of the gage shall be inserted into the hole a minimum of 13 %"
turns (0.68"). The NO GO end should not enter more than 3 turns. Record inspection results as required by the appropnate Quality Assurance requirements. Report any nonconformance to ABB CENO for disposition prior to installation of the MNSA.
3.1.19 Install the Hot Leg RTD MNSA per Ref.1.4 3.2 HOT LEG PDT NOZZLE PREPARATION The Hot Leg PDT Nozzle drilling fixture is a split plate assembly that mounts around and clamps to the nozzle below the upper boss. The fixture halves are bolted together using shoulder bolts to maintain their alignment. The fixture halves are match marked. The mounting plate for the drill stand can be attached to any side of the fixture. The mounting plate is indexed to the centerline of the drill bushing holes. A drill stand is attached to the mounting plate. The drill motor and sliding plate is attached to the drill stand. There is a sliding collar around one leg of the drill stand that is used as a drill stop to control the depth of the holes to be drilled in the component shell.
Ensure the shell surface around the nozzle is clean and free of dirt, loose scale, or other foreign material. Report any scoring or gouges on the shell or nozzle surface in the sealing area to ABB CENO for disposition prior to installation. Ensure the area on the nozzle where the drilling fixture will attach is free of all foreigr. material and raised metal that would interfere with fit of the fixture. l NOTE I AH unschining g "-- shnu be done in accordance with the requirements of Ref.1.2.
4 3.2.0 La-- the fixture clamp and separate the fixture halves so that it can be placed around the base of the PDT nozzle. Ensure the mating surfaces of the fixture halves are clean and free of burrs. Tighten the fixture bolts to bring the halves together. Altemate between the fixture bolts while tigh*=iag to preventhiadias.
3.2.1 Align the fixture to the PDT nozzle to position the MNSA mounting holes b e placing a level on the upper surface of the fixture. Rotate the fixture until it is level. Move the fixture out slightly from the component shell such that it is not in contact with the
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- component surface. This will ensure the fixture is aligned to the nozzle and not binding on i the surface. This will also ensure maximum contact and grip of the clamping surface.
Tighten the nozzle clamp. Ensure the clamp is tight and the fixture does not rotate around the nozzle.
CAUTION Until the first hole is drilled and tapped and a stop bolt is installed to lock the clamp in position, care should be exercised to prevent the fixtare from rotating on :he nozzle.
3.2.3 Attach the mounting plate to any side of the fixture. Ensure the mating surfaces are free of dirt, chips or burrs.
3.2.4 Attach the drill stand to either of the mounting plate drill stand locations with two (2) shoulder bolts. Mount the drill motor and slide plate to the drill stand. Do not tighten the slide plate mounting bolts. Ensure the mating surfaces are free of dirt, chips or burrs.
3.2.5 Install a 29/64" drill bushing into the fixture plate nearest the drill stand. Install a 29/64" drill bit into the drill motor. Ensure the drill bit is fully inserted into the drill chuck. j 3.2.6 Adjust the position of the drill motor until the drill bit passes freely in and out of the drill bushing. Tighten the drill motor clamp bolts when satisfied with the alignment.
3.2.7 Recheck the alignment of the fixture to the nozzle and adjust as required. Ensure the
-nozzle clamp is tight.
3.2.8 Insert the drill bit into the bushing until the drill point makes contact with the component shell. On the back leg of the drill stand, position the drill stop collar approximately 0.985" below the movable drill stand plate.
WARNING THE MAXIMUM DEFTH OF THE FINISHED HOLE MUST NOT EXCEED 1.12 INCH.
.;.9 Start the drill motor and drill into the component until the movable drill stand plate makes contact with the drill stop collar. The drill bit should be backed out of the bushing periodically during the dnlling operation to clear any chips that may accumulate in the hole. Check to see that the hole is clear of chips prior to reinserting the drill bit into the hole. DO NOT EXCEED A MAXIMUM HOLE DEFTH OF 1.12 INCH.
3.2.10 Remove the drill bit fhan the drill motor. Remove the 29/64 " drill bushing from the fixture. Check to ensure the drilled hole is free of chips and other debris.
3.2.11 Install a tap bushing into the fixture. Tap the drilled hole using a 1/2"X20 UNF plug tap inserted through the bushing and into the hole until the tap bottoms in the hole. The holes may require tapping using both a plug tap and then a bottom tap to get the required number of threads. It will probably not be possible to use the bottom tap in the hole until the drill fixture is removed from the nozzle. 'Ibe number of full threads should be checked prior to using the bottom tap. If there are sufBcient threads after using the plug tap, it is not necessary to use the bottom tap. The minimum fully threaded depth is 0.68" (13 %" full threads).
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3.2.12 After tapping the hole is complete, remove the tap bushing. Check and ensure the hole is free of chips or other debris.
3.2.13 Install a 1/2" drill bushing into the fixture and thread a 1/2" X 20 UNF bolt through the bushing and into the tapped hole to lock the fixture in place and prevent any rotation. The bolt should only be finger tight in the hole.
3.2.14 Move the drill stand, drill and mounting plate to the other attachment points as required to drill the remaining holes as described in steps 3.2.4 thru 3.2.10. i 3.2.15 Remove the drill stand, motor and mounting plate from the fixture plate.
3.2.16 Ensure the remaining drilled holes are free of chips and debris. Using the tap bushing, tap l the remaining ddlled holes using a 1/2" x 20 UNF plug tap inserted through the bushing l until the tap bottoms in the hole. The holes may require tapping using bo;h a plug tap and then a bottom tap to get the required t. umber of threads. It will probably not be possible to ;
use the bottom tap in the hole until the drill fixture is retcoved from the nozzle. The number of full threads should be checked prior to using the bottom tap. If there are sufficient threads after using the plug tap, it is not necessary to use the bottom tap. 'Ihe minimum fully threaded depth is 0.68" (13 %" full threads).
3.2.17 Remove the fixture from the PDT nozzle.
3.2.18 Ensure the tapped holes are free of chips and other debris. Inspect holes for final depth
' and length of thread. Threads are to be checked using a 1/2" X 20 UNF 2B GO - NO GO plug gage. The GO end of the gage shall be inserted into the hole a minimum of 13 %"
turns (0.68"). The NO GO end should not enter more than 3 turns. Record inspectior resu:ts as required by the appropriate Quality Assurance requirements. Report any nonconformance to ABB CENO for disposition prior to i=*=Hation of the MNSA.
3.2.19 Install the Hot Leg PDT MNSA per Ref.1.4
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HOT r EG SAMPI E NO77r.F ppFPARATION. 3
) 3.3 i
1 The Hot Leg Sample Nozzle drilling fixture is a split plate assembly that mounts around and clamps to the nozzle below the upper boss. The fixture halves are bolted together using shoulder bolts to maintain their alirws. The fixture halves are match marked. A mounting plate for the drill stand can be attached to any side of the fixture. The mounting plate is indexed to the centerline of the drill bushing holes. A drill stand is attached to the mounting plate. The drill motor and sliding plate is attached to the drill stand. There is a sliding collar around one leg of the drill stand that is used as a drill stop to control the depth of the holes to be drilled in the
.omponent shell.
j Ensure the shell surface around the nozzle is cleau and free of dirt, loose scale, or other foreign i material. Report any scoring or gouges on the shell or nozzle surf ~; 'It the sealing area to ABB
- CENO for disposition prior to installation. Ensure the area ou uw nozzle where the drilling l fixture will attach is free of all foreign material and raised metal that would interfere with fit of
- the fixture.
I N.QIE 1 All machining operations shall be done in accordance with the requirements of Ref.1.3.
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l' 3.3.0 Loosen the fixture clamp and separate the fixture halves so that it can be placed around the base of the Sample Nozzle. Ensure the mating surfaces of the fixture halves are clean j
and free of burrs. Tighten the fixture bolts to bring the halves together. Alternate between l
. the fixm bolts while tightening to prevent any binding.
l 3.3.1 Align the fixture to the Sample Nozzle to position the MNSA mounting holes. Rotate the l
. fixture until one side of the fixture plate is parallel to the long axis of the sample line.
2 Move the fixture out slighay from the component shell such that it is not in contact with
) the component surface. This will ensure the fixture is aligned to the nozzle and not binding on the surface. This will also ensure maximum contact and grip of the clamping l surface. Tighten the nozzle clamp. Ensure the clamp is tight and the fixture does not i rotate around the nozzle.
I CAUTION
- Until the first hele is driBed and tapped and a stop bolt is installed to lock the clamp in j position, care should be exercised to prevent the fixture from rotating on the nozzle.
3.3.3 Attach the mounting plans to any accessible side of the fixture. Ensure the mating surfaces l
are free of dirt, chips or burrs.
i 3.3.4 Attach the drill stand to either of the mounting plate drill stand locations with two (2) j shoulder bolts. Mount the drill motor and slide plate to the drill stand. Do not tighten the slide plate mounting bolts. Ensure the mating surfaces are free of dirt, chips or burrs.
I 3.3.5 Install a 29/64" drill bushing into the fixture plate nearest the drill stand. Install a 29/64" i drill bit into the drill motor. Ensure the drill bit is fully inserted into the drill chuck.
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+[9 cf 3.3.6 Adjust the position of the drill motor until the drill bit passes freely in and out of the drill bushing. Tighten the drill motor clamp bolts when satisfied with the alignment.
3.3.7 Recheck the alignment of the fixture to the nozzle and adjust as required. Ensure the nozzle clamp is tight.
3.3.8 Insert the drill bit into the bushing until the drill point makes contact with the component shell. On the back leg of the drill stand, position the drill stop collar approximately 0.985" below the movable drill stand plate.
WARNING THE MAXIMUM DEPTH OF THE FINISHED HOLE MUST NOT EXCEED 1.12 INCH.
3.3.9 Start the drill motor and drill into the component until the movable drill stand plate makes contact with the drill stop collar. The drill bit should be backed out of the bushing periodically during the drilling operation to clear any chips that may accumulate in the hole. Check to see that the hole is clear of chips prior to reinsertmg the drill bit into the hole. DO NOT EXCEED A MAXIMUM HOLE DEPTH OF 1.12 INCH.
3.3.10 Remove the drill bit from the drill motor. Remove the 29/64 " drill bushing from the fixture. Check to ensure the drilled hole is free of chips and other debris.
3.3.11 Install a tap bushing into the fixture. Tap the drilled hole using a 1/2"X20 UNF plug tap inserted through the bushing and into the hole until the tap bottoms in the hole. The holes may require tapping using both a plug tap and then a bottom tap to get the required number of threads. It will probably not be possible to use the bottom tap in the hole until the drill fixture is removed from the nozzle. The number of full threads should be checked prior 'o
., using the bottom tap. If there are sufficient threads after using the plug tap, it is not necessary to use the bottom tap. The minimum fully threaded depth is 0.68" (13 %" full threads).
3.3.12 After tapping the hole is complete, remove the tap bushing. Check and ensure the hole is free of chips or other debris.
.13 Install a 1/2" drill bushing into the fixture and thread a 1/2" X 20 UNF bolt through the bushing and into the tapped hole to lock the fixture in place and prevent any rotation. The bolt should only be finger tight in the hole.
3.3.14 Move the drill stand drill, and mounting plate to the other attachment point as required to drill the remaining holes as described in steps 3.3.5 thru 3.3.10.
3.3.15 Remove the drill stand, motor, and mounting plate from the fixture plate.
3.3.17 Ensure the remaining drilled holes are free of chips and debris. Using the tap bushing, tap the remaining drilled holes using a 1/2" x 20 UNF plug tap inserted through the bushing until the tap bottoms in the hole. The holes may require tapping using both a plug tap and then a bottom tap to get the required number of threada, it will probably not be possible to use the bottom tap in the hole until the drill fixture is removed from the nozzle. The numWr of full threads should be checked prior to using the bottom tap. If there are
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, 3-lG 9 7 i sufHeient threads after using the plug tap, it is not necessary to use the bottom tap, The I minimum fhlly threaded depth is 0.68" (13 %" full threads). i l
3.3.18 Remove tbs fixture from the Sample Nozzle.
3.3.19 Ensure the tapped holes are free of chips and other debris. Inspect holes for final depth and length of thread. Threads are to be checked using a 1/2" X 20 UNF 2B GO - NO GO plug gsge. The GO end of the gage shall be inserted into the hole a minimum of 13 %"
tums (0.68"). The NO GO end should not enter more than 3 turns. Record inspection rer L s required by the appropriate Quality Assurance requirements. Report any nowar!9rmance to ABB CENO for disposition prior to installation of the MNSA.
3.3.20 Install the Hot Leg Sample Nozzle MNSA per Ref.1.4 ,
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O 9 Ref. Test Request TS070A ABB/ COMBUSTION ENGINEERING Project No. 2.007241 PRIMARY SYSTEMS TEST REPORT FOR MNSA HYDROSTATIC AND THERMAL CYCLE TESTS ere,. red er b
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= ddn Temung Semces nov,m er Vtul 0 Unliep m 6/15f91 K. H. Hashager, Supemear l Temung Semcas ,
wor C1 '0 P. M Manager -4g.Dase:
7/3/r7 Prunary Symeme The tems descr4ed is e report me accepted as mesang the objecoves and inaruccom in the redwegQgs request and test precedens, Cosatanet Easmeer: K. V
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'Dess Prmoed Ne m s / Si m Dese ofIssue: O 3 /97 4
TR PENG 042, Rev. 00 Page1ofl' e 0 ' f '
Raf. Tm RapenTS010A ABB/ COMBUSTION ENGINEfJUNG Project No. 2007241 PlUMARY SYSTEMS I RECORD OF REVISIONS NUMBER DATE PAGES l PREPARED BY APPROVALS INVOLVED 00 07/03/97 All F. V. Rossano K. H. Hashager P. Laombruna K. V. Marpaa ee- ee l
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Ref. Test Regasst TS074A ABB/ COMBUSTION ENGINEEJUNG Protect No. 2007241
- PRIMARY SYSTEMS 2
! TABLE OF CONTENTS
! SECTION DESCRIPTION PAGE NO.
1.0 INTRODUCTION
4 i 2.0 OBJECTIVE 4 1 3.0
SUMMARY
4 TEST APPARATUS 4 4.0 4.1 Autocisw 5
} 5
- 4.2 . Seal Aman-hl- '
Test Measurement Equiposat 5 3
4.3 5
j 5.0 TEST SETUP 6
j 6.0 PERFORMANCE OF THETEST 7
! 6.1 Hydrostanc Test Theraud Cycle Test 8 l 6.2 7.0 POST TEST INSPECTION AND DATA REDUCTION 9
}
9
) 8.0 DOCUMENTATION AND QUALTTY ASSURANCE REQUIREMENTS l
9.0 REFERENCES
10
' LIST OF FIGURES i
! FIGURE NUMBER TTTLE PAGE NO , l 11
! 1 TEST FACILfrY SCHEMATIC !
SKETCH OF PRESSURIZER BOTTOM HEAD SEAL ARRANGEMENT 12
! 2 13
) 3 SKETCH OF HOT LEG RTD NOZZLE SEAL ARRANGEMENT 4 4 PHOTOGRAPH OF PRESSURIZER BOITOM SEAL 14 l
15 l 5 PHOTOGRAPH OF HOT LEG RTD NOZZLE SEAL i
e LIST OF TABLES TABLE NUMBER TIT 12 PAGE NO.
l I 1 LIST NTESTINSTRUMENTS ,Q6 i
ATTACHMENT Desen RalasedTesungm Pass 17 LISTOF APPENDICES PAGES.
APPENDDC NO Tm2 i A HOT LEO RTD DATA SHEETS AND CHARTS Al-A17 51-B16 i B PRESSURIZER BOTT(N NOEZI2 DATA SHEETS AND CHARTS C1 C11
- C CALIBRATION CERTIFICATIONS AND DATA SHEETS i
i 4 TR-PENG442, Rev. 00 Page 3 of17 i
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Ref. Test Request T507pA ABB/ COMBUSTION ENGINEERING Protect No. 2007241 ~
PRIMARY SYSTEMS i
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1.0 INTRODUCTION
j The Structural Integnty and Testing Group (TS) of CE Nuclear Operanons (CENO) was requessed, via Reference 9.1, to vertfy the integnty of the MNSA (Mechamcal Nozzle Seel Assembly) semi clamp
====mhhas for Field Services, Mechamcal Engineering,(FSME). The test requirements are contained in l
l Rohrences 9.1 and 9.2. Only the hydrostanc test and thermal cycle nest are covered by this procedure This report presents the obpectives, presents a description of the test hardmere, authnas the test l procedures, presents the test results, and lists the h=mmiaa requirements for the test. Copies of data sheets are contaaned in the appendices of this report.
I Per Retrences 9.1 and 9.11 Quahty Assurance (QA) requaremsets Gw Demgs Venficanon (Secteam 3.6 l
of Retrence 9.3) were apphesbie to this test programa.
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! 2.0 OBJECTIVE j
The otpoetne of this test mes to quahfy one MNSA seal clamp hr an instnuneet nomde located a the l
bosom of a PWR pressunaar and one MNSA seat clamp hr a Hot Les RTD nossie. Speedle
{ '
requiremeens more to =====hla the seal clamps, perform a room temperstme hydrostanc test of each l
assembly, portra a thennal cycle test (each test consisting of three cycles) of each assembly, and to l
' compises the test h with a test report.
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! 3,0
SUMMARY
f The <pahnemiam teattag of the MNSA seals mes perhnned Bean June 10,1997 through June 17,1997, using the auencisves loused in Budding 5 of ABB/CENO's test &cabases. Bodt seal ====hhas were subsected to hydnumme teenas a 3,175 Puis,150 Paig and to a thenmal cycle test Dom room temperature up to 650 7,110 T and 2,500 Paig,150 Peig, The seal ====hhas were them examened er any indlemens that boric acid had leaked past the semis. There were ao ages banc acid leakass timed during the peut test ======miaa and the seal =====hH== are considered to h4 sucessdally compasandthis spanhSemnon test.
4.0 TERF AFFARATIE The test apparases commesed of the hilouseg -- ,---- -
- Amancisves capable doperanas a up 2,800 Paig a 650T.
- Instrumasses to moamor and record the test parasseenL
- Mock-ups of the NSSS pasare homedenes and the MNSA classy seal ====hana=
TR-PENG 042, Asv. 00 Page 4 et17
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Ref. Test Request TS070A ABB/ COMBUSTION ENGINEERING Propet No. 2007241 PRIMARY SYSTEMS 41 Autoclave The autoclave is a vessel capable of mantaining high temperature, high pressure water. The l Structural Intagnty and Testing Group of ABB/CENO has several of these autoclaves. They are capable of using typical NSSS chemistry and obtenning prunary system temperatures and ,
pressures. Autoclaves 5 A and 6A were used for this test. These are 5" insula d=. mar by 36' (
long autoclaves designed to operses at up to 1800 Paig at 650*F. Higher operating pressures are (
allowable at lower temperseures. The hydrostanc test at 3,175 Paig was performed at roona temperature and mes within the operating capabdity of thsee autoclaves. A schemanc of the autoclave arrangement for the thermal cycle test, is shown in Figure 1. Additional desenption of the sutoclave esctlities is ena*= sand in Reference 9.4 41.Stlst Assembhas l FSME prtmded two mock-ups of the NSSS pressure boundary in place of the normal autoclave **
hand. They also primded all MNSA cimap seal P These items are desenbod by .. .
Redsrences 9.6,9.7, and 9.8. No special tools mers needed der the assembly and Aa====any g the MNSA riemps Cahbraced torque wrenches were used to most the requiremsats af Raderence ,,,,,
9.10.
4.3 Test Measurement Equspment Table I contans a list of test instruments. The pressure recorder and the thor ===pla recorder were part of the auencisve rocen fhalman Tta pressure recorders were 24 hour2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> circular chart devices. The tempersare recorder mes a ca=*a=== multi chamast etnp chart recorder Calibraced thor ===pI== nere used to record the tempermure of the meest la the auenciave.
These tastruments were calibrated and the calibramos recente ressened in sourdance with Radstence 9.5. TS pavided calibreed torque wrenches Air the asonably of the MW Capses of calibratens dets shoes are e==*==aad in Appendix C.
5.0 TEST SETUP The seasy of the aulacisme was the r==ra==*= lay ofTS. The general ansegnannt of the suancieve was as shoma la Figue 1. The muser used mes planned te be desaneralised maner tar the hydrostusse teses and borased mener (assemelly 1200 PPM beric acid in Di motor) thr the thanaal cycle sense. Huoever, to save sene schedule time, the beric acid saluden mes aise used 9er two of the hydmetene tsees on the Het las LD noszie seal and both of the hydrostanc tests on the boscen noszie seal The innreceors da To assembfy of the MNSA seat cismsps were prodded hp FSME in Redaeace 9.10.
All of the asseawt, 4the seal ~==pa==== were portarused under the direction of FSME pomommet TR-PENO 042 Ray. 00 Page 5 of17 r-- -- . . _ _ - - - . - - _ . - - . - - - - _ _ . - - - - - - - - - - - - - - _ - - - - - - - - -
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. . i Ref. Test Raquest TS010A ABB/ COMBUSTION ENGINEEEUNG Project No. 2007h t PRIMARY SYSTEMS Excepoons to Reference 9.10 were noted on a copy of the reference and a listed here. For the Hot tag RTD MNSA, the test assembly started at Secuan 7.1.5 of Reference 9.10. The followtng secuon numbers are thxn Reference 9.10-Secuan 7.2.3: It was necessary to tit the RTD nozzle to install the compression collar.
Secuan 7.2.9 The bolts were torquod to 35 R4. to set the seal, thea laanmaart and retorquad to 30 A-h Secnos 7.2.14: It was not necessary to toad the washer taba due to the short durataos of this test prograss and the absence of siedle==* vibrance.
For the Bottom Pressunser MNSA, the test assembly stoned with Sectica 6.1.4 of Radersace 9.10. The following secnon numbers are Boat Raderence 9.10'.
Secuca 6.2.4: It mes necessary to rubce the dismisest of the ahn=ld=r bolt tom: 0.76&* to 0.74#*.. -
fbr one inch above the threads in order to fit isso the holes in the test mock-up.
Secues 6.2.7: It mes necessary to aquet the lamer flangs using the 1/2 inch hex boks ter align ===* bedore torquag the shoulder screes to IC A-h Secnos 6.2.8: The compression collar reqaired runachamLg to increase the innde a=== mar in the upper region. A 0.050 inch thick shim was also iammilarl betseem the Gratal seal and the compreemos collar.
Sechos 6.2.20: It was not necemary to band the mesher tabs des to the short chirance of this test program and the sheence of asadicant vibranen.
Aw 6.e FEammasApcz orTuaTEST ,
All tuules mas pertamed by gemidled personnet, or persons worhag under the direenos d qashfied
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perseenal, per Radusase 9.9. The tilloonas i, - ~ reqaireuseas were the some for each of the two MNEA seat siemps tened. The compenset being tested mes id==ediad on the dets shoom usesL There were as serial sambers Sur any of the test compensam.
The gaaeral operanos spadelines Air sesocieve operanos, gives in Reemence 9.4, were tailseed Air the set up of the mencime. Prior to the MNSA seat monas, ai! Senas comescar,as were chedad, to the atteet a poemble, to venfy that they more not likely to pnmde a leakags path chenas the test.
TR PENG 042, Esv. 00 Pass 6af17
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Ref. Test Raquest TS010A ABB/ COMBUSTION ENGINFJJtING Protect No. 2007241 PRIMARY SYSTEMS All woned parts and seal surface metal parts wre clean and od free. The seal clamps ute assembled por instruenons supphed by FSME. Some minor adjuarmants are required to the assembly procedures. I These adjustments were recorded onto a copy dthe assembly procockare and onto Data Sheet 1. Copies of data sheets are contsnad in the appendices to this report. The data for the Hot Les RTD seal are contmaad in Appendax A and the data for the pressurtzer bottom seal are contatned in Appendix 5.
l 6.1 Hydrostatac Test I
For tEis test phase, the rupture disk was removed toat each autoclave and the accumulsors were isolmed toe the ausaclaves with valves. Four triai were pe fonned on the Hot Les RTD noczle and two trials were performed on the pressur:ser bonom oozzia The hydrostanc pressure reqmroment was 3,175, t 50, Psig, at ambient temperatus. The presses should not decay by more than 50 Paig, if any decay d more thea 50 Pais ces not be aanbuted to leakage home other than the test seat, the test meuld have been comedered a thilure.
6,1.1 Hot Lea Mock-up For the initial two test trials the ausoclave was Siled math plais denumerahand seest.
The test aan==Wy was vented at the top to allow gases to escape Rosa the autoclave and ,
seal regicas. The system was sealed aher it mes Slied and veseed.
The Srst test had a leakage rate of about 150 Psi over 19 =naaman The pressee was released and the autocisve head out was retorquad to a lugher torque value,120 A-lb.
The daranon of the second test was 16 mamman and the pressee damy was 15 Pai, withis the acceptadde limsts Fouommag the second trial, whsch mes istaedy considered sucesssad, the suencien was drmand and reaned with boric acid solanon, in preparassos der the thennel cy.ie teses.
D a..e .e .rm.i c,.is to some - was ste es.i i reglen. Aasr some Aar===a= it was decided to recheck the aghtnaes of the semi assembly and to repeat the hydrostanc test since there mes the poembihtyb the
=
mesume mes die to a leek that had not been deessted fouemmag the second G tests. Ces 1/2" bok was famed to be less that the 30 8 k tongue that was innauy appiimL AB of the 1/2 inch boMs mars instiauy retighammed to 35 8 k to set the seal, loosened, and resarquod to 30 A-k The byskaamme test mes repened un'ag the horic acid solunos is the amencisve. This third te. lassed 29 emmunes, and the decay was 50 Pui. Whde this us wittua the secopimble liames, it us deaded to resorges the auencisw I head and repost the test for a longer duranen.
A Asunk test ses porturened, while the ymesure mes ==an==ad ihr as sitended penod, l of 3 heers. Over this 3 hour3.472222e-5 days <br />8.333333e-4 hours <br />4.960317e-6 weeks <br />1.1415e-6 months <br /> period, there mes a 100 Puis decoy in presses, but no signs TR-PENG.042. Rev. 00 Pugs 7 d17
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Ref. Test Request TS020A ABB/ COMBUSTION ENGINEERING I Project No. 2007241 PRIMARY SYSTEMS i
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ofleakage kom the seal area. The seal interface was checked penodically, with stnpa of
- paper slipped into the mock up, between the lower flange and the autoclave head. No traces of moisture were found and the test was considered successful. (Note that the
! MNSA was newt disassembled after the irutial assembly pnor to the first hydrostatic i test and completing thermal cycle test).
J 1
A copy of Data Sheet 2 was completed h each hydrostanc test tnal. Copies of these
} . data sheets and of the pressure recorder chart are contmaad in Appendix A.
i
! 61.2 R a.n- -izar MNSA I l To save some program test time, it was decided to perfona this hydrostanc test with the
{
banc acid solution required ihr tte thennal cycle test. The first hydrossanc test ansept l
i faled at 1,600 Psi. The syness was AM and it appeared that the Granal asel i
ring was not sufBciently _ _
FSME decided to make some maddir=r-a to the seal compramos collar and to iammil_ _
a 0.050 inch thick shim besmeen the compreemos collar and the GraAnl semi ring. The '
, seal was reassembled with a new Graeol seat nas and the moddled P A "
hydrostanc test was perfbnned at 3,175 Puig, wrth a duratnam of 26 annuses, dunas l
1 which the presses decay was less than 50 Psi. The crevices botness presounzer mock-I up and seal lamer flangs were checiced ihr signs of moisture, and some mes fbund.
- A copy of Data Sheet 2 was completed fbr each test. The test hardners was theri
! prepared Air the thennel cycle test Copees of the dets sheses and of the preemre recorder charte are coasassed in the Appendix 5 of this report l
l 6.2 Thannel CvciaTest
- MD i
This test mes partinued on each assembly folloemag successed ea= rima = of the
' test.
Esah anesteve comammed the 2,200 PPM boric acid solution tem the pronous mas.
i Abses 500 edtillears of solanon were drained hem each system to allow as initial er pocist at j
- the any of ensk assoclave. The rupase disk was insemiled, along with vast lines, and naa==3*-
! linen,11te 8== mes procharged with nitrogen gun, i
l All bess up and ecol dam rases were in accontence with the operating spadshnes, Radmence 9.4.
Hans up of the auencime ses liamond to 1507/ hour. Each annociarm was vested ensi the top l
i dunas the firm thennel cycle as between 2507 and 3007 to remove crygsa ham the sysess.
1
\
4 A total of three (3) thenmal cycles were requued ist entdt seal asambly. A thenmal cycle ses dediand as beenas tfee asocime Domi mobsent (less than 2007) to 6507, t 107, and 3 TR PENG 042, Rev. 00 Pugs 8 cf17 i
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4 Ret Test RequestTS070A ABB/ COMBUSTION ENGINEERING Project No. 2007241 PRIMARY SYSTEMS estabhsiung a pressure of 2.500, t 50. Psig, and then allowing the system to cool to less than 200*7. The elevated temperature / pressure had to be held for at least 60 minutes. The Srst cycle started flrom room temperature The remaining cycles started from where the autoclave cooled overnight.
Pressure inchcation was not a reliable method to identify leakage while hat. Therefore, visual evenannas were performed. A mirror was used to look for any steem wisps. (Note: leakage tiram locations other than the test seal clamp amuld not how invahdmeed the test if the integrity of the test seal could hsw been d==anawaned.) Furthermore, resuhind depomis of boric acid outade i l
of the seal may also have been indranans of a leak. Thorn were no observed leaks 6can either of the test naarnannts dunng any of the cycles.
A copy of Data Sheet 3 mes completed ihr each assembly fbr each thermal cycle. Copass of the Hot lag RTD MNSA dets sheets and recorder charts are aa=*==aad ic Appenda A. Copees of the pressunzer honoma nasale MNSA desa sheets and recorder charts are amaad in Appeedbt 5.
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7.0 POST TEST INSPECTION AND DATA REDUCTION At the conciumos of the test, the asel clamps more inspected, disassenhied and ======ad FSME , !
procedures more fbliowed. Repressetatives of FSME sere present tr the di-M All seat boundary men --aad to desenmas if any boric acid solution leaked past the seal innerhees. Thors more no signs of banc acid crystals catside of the seat boundary funned by the Grahd seal ihr other amamenWy Therefore, the semi specumens have inet the y reqaremones of Retrence 9.1.
8.0 DOCUMENTATION AND QUALTTY ASSURANCE REQUREMENTS Quakey Assurance, as Demos Venficanon, mes regmund fbr this pmgrani per Rahrence 9.1. The regeusessess unre a test procedure, controlled tastruments, and a test report as specdled in QF 3.6 of QPM-101, Raderence 9.3. A*
- 4 11 bis report documnet pasemes a desenption of the test, repons the test suuroement data, consatas rehumans to suppernas desa, and provides a list of instnuments used. Copees of dass sheses, reconfer chans and emitsation desa sheses are included la the appsoscos of this test report. T - of any test nouses se Qualisy Records and/or SCE is the . ", of the Cogssammt Eastseenas Groep.
FSME The dass and daa====*=aam ressasson pened will be Gwe (5) years a8er issue of this test report.11te angsmal copies dthese documens will be retaused in the T5 Group Ales tr that penotL Copses of the test procedme and inst repen will be essa to the Cogusant Engineer.
TR-PENG 042, Rev. 00 Pugs 9of17
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1 Ret Tts' Request T5078A ABB/ COMBUSTION ENGINEERING Propet No. 2007241 PRIMARY SYSTEMS Calibrance dess for thoes instruments controlled per Reference 9.5, will be stored per the requirements of l Reference 9.5. j
9.0 REFERENCES
9.1 Test Raquest TS070A, Supplements 00 and 01.
9.2 S-NOME WTR-0007, Rev. 00, Test Raqmrements for the San Cao6e MNS A Clamps for Presswust Insuunent Nozzles and RTD Hot Lag Nozzles.
9.3 QPM 101, Psvision 01.
9.4 00000 PENG 006, Rev. 00, Autoclave Operating Gedehnes.
9.5 MISC-PENG IPQP.007, Rev. 01, Quality Prograni Plan hr Enguesering Operances Control of Meeswtag and Test Equi tunaa*
9.6 Drawing E MNSA 228,005, Rev. 02, MNSA Amoclave Test Fixtmos.
s 9.7 Drawtag E MNSA-228,006, Rev. 01, Pressurtzer Level Autocisve Assy.
9.8 Drawing E MNSA-228,007, Rev. 01 Hot Las RTD Associsve Assy.
9.9 Inter Ot5ce Memo PENG 96 501, Assessment of Test Personnel Certdicates ibt 1997.
9.10 S3-NOME EP.0124, Rev. 00, Enguesering Procedure ihr the iameaalanna of the Mechancel Nozzle Seal Am ihr SONGS Unit 3.
9.11 PP 2007241, Rev. 00, Propect Plan fbr MNSA Clamp Analysis and Testing, p
- /
TR PENG.042, Rev. 00 Peps 10 of17
. . 1 Ref. Test Request T5070A ABB/ COMBUSTION ENGINEERING Project No. 2007241 PRIMARY SYSTEMS
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2 TopPlase 7 SputPacking 11 Hsu Hd Cap Sc w, short l 3 UpperFlangs 8 TieRod 12 RatesmerWasher(1/2") i 4 Imer Flangs 9 Ham Nut 13 Han HdCap Screw,long 5 CounpressonCouar 10 Ratsamer Washar(3/8") 15 Spener 6 PadnagRatanner 16 Preemers!avel Anancism Test Pistese l Figure 2. Skssch of Prussartner Bonomi Head Semi Arrangsasset I
. TR.PDi 042, Rev. 00 Page 12 of17 i
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444 _r,u_i.m-a-s.ae Ja da-saws .a e A,ia -. 5..e._.a ---..an 4.ungA We d _e__44 4-4-A a _d r-, m_,4-4J 4 J a h _a uA_rma 4ME.,.e4,i.A3.am.J J d ,4u_g,__AA_.m.3,t_.A_4p.m_i. J2-a_,a .J2a4_As._
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Ref. Test Request TS070A ABB/ COMBUSTION ENGINEERING Project No. 2007241 PRIMARY SYSTEMS 9
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@ HOT LIG RTD AUTOCLAW ASesunty 2 TopPhar 8 Tiered 3 UpperFlames 9 Hsu Nut i
4 LonerFlames to Ratanser Washer (3/8")
5 Compnumou Collar 11 Hem HdCap Screw i 6 Packmaslung 12 RamaserWasher(112")
i 7 SplitPacknag 13 HattagRTD AmassieveFW Figene 3. Shusch r* Hot Ig RTD Nousie Sami Arrangsmassa TR-PENG 042. Rev. 00 Pues 13 af17
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Ret Test Request TSOIDA AB5/ COMBUSTION ENGINEERING Project No. 2007241
! PRIMARY SYSTEMS i
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5 i Figure 4. Photograph of Pressunser Bottom Seal l
N' MA h. 00 Pap 14 of17 i
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Ref. Test Request T5020A ABB/ COMBUSTION ENGINEERING Project No. 2007241
< PRIMARY SYSTEMS i
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l Ref. Test Request TS070A ABB/ COMBUSTION ENGINEERING Project No. 2007241 PRD4ARY SYSTEMS l
Table 1 List of Test Instruments 5ystem Pressure Honeywell circular recorder Honeywell circular recorder.
Attachedto Ausaclave 5A. Attached to Autoclave 6A.
Laborasory identatication EL-964. l Laboratory identification EL-963.
Model Y702Cl(P3)-134 000 2274. Model Y7C;Cl(P3) 134 0042274.
l Cahbrated range 43500 Psig, Cahbraced range 0 3500 Psig.
Cahbraced 06/02/97 and dus 12/02/97. Cahbrated 06/02/97 and due 12/02/97.
Syseen:Temporanue Yokogsom strip chart recorder Model HR 1300.
Calibrated rangs 41000T.
Calibraced 03/13/97 and due 09/13/97.
Laboraeory idaaaneneian CL-0142.
Temperatus Sensors: Projects Inc. Timyian SST sheethodType J. ,
Attached to Autoclave 5 A. Attached to Autoclave 6A.
Cahbraced Range 100T to 7007. Cabbrated Rangs 100T eo 7001.
Calibrased 05/06/96 and due 12/ L3/97.* Calibrated 05/07/96 and des 12/10/97?
Laborseory uianaAemnaa CL-1018. Laboratory id==hAcanaa CL 1008.
- The TCs used more TCs that had been previously cabbrated and stored ihr theurs use. Per Rs6mence 9.5, the calibrance pened can be extended for this type d sensor for the normal calibranca poned Ibilemmag first use. This test see the first uso d these devices. Both TCs more abbrataos checend 06/19/97 and ibund to meet the accuracy reqmransene dt 57.
mw Torque Wrenches:,Prsee Rangs 4250 h Rames: 4150 fb lh.
Nihrmand 04/16/97 and des 04/16/98. Cahbrated 05/20/97 and due 11/20/97.
Labasseeryidammaamaan ME 25. Laborneory utmanacanan CL 1031.
Copies dthe calairanos data shoom Air the above instrumenes are casemand in Appendix C.
Peps 16 d17 TR-PENG 042 Rev. 00
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1 Ref. Test Request T5079A ABB/ COMBUSTION ENGINEERING Project No. 2007241 PRIMARY SYSTEMS r - = ' - f Tesdag Checklist TEST REPORT Docussest
Title:
Test Report For MNSA Hydrostatic sed l Thermal Cycle Tests 1
Document Number: TR-PENG 042 Revisies: 00 Yes N/A l Is the test purpose stated? @
2 Are the w procedmalined? C!i[
3 Are the ten resuhslined? 8 4 i. ine te. reque. oomb uu . ine te repo cw. p 7 g 5 Has the test repost been signed and dated by the author? S _ , . .
6 Has prwisi. been made fu append by the manager ofthe to.ing 5 -
oW7 7 Has prwision been made for a ==ta==.* of acceptance by the Cognizant Y Engineer?
ce==ents/Re rkn Amo" Reviewed byt" Kad R Haaliaser !G k #6 Hd( [/2[/A7 a-n.e.t n - (
TR-PENG 042,itsv. 00 Pass 17 of17
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Ret Test RaquesTS070A ABB/ COMBUSTION ENGINEEJLING Ptoject No. 2007241 l PRIMARY SYSTEMS NUN PERMANENT QUALITY RECORD CERTIFICATE OF CALIBRATION
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Ref. Test Request 5070A ABB/COMSUSTION ENGINEERING Preject No. 2007241 PRIMARY SYSTEMS ') l
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fyE {l:10,9 , ./f4 coman or muco u,o courmen omves Ok J - f-h reanevus. cona.ect u rets,~ons mones.seen i Pnscis40N msmow. A TORQUE CALIBRATION CERTIFICATE REPORT NUMBER: 213012 PO Nassber: 45676KP l l ~ DATE OF CALIBRATION: 5/20/97 CUSTOMER: ABB Combusuon Engmeerms L.tuBRATION INSTRUMENT: Torque Wrench,150 Mbs. U OE U" # 7) S/N:CL 1031 MAKE: Proto 153668 .. . PRECENT OF RANCE 20 % 40 % 60 % 80 % 100 % CLOCKWISE
- INDICATED 30'Ibe. 60*Ibs. 90'!bs. 120'Ibs. I50'Ibs.
WRENCH TORQUE: 30'Ibs. 60'Ibs. 90'Ibs. 120*!bs. 149'Ibs. ACTUAL TORQUE: COUNTERCLOCKMSE INDNATED WREhCH TORQUE: ACTUAL TORQUE: Amw i PROCEDUREt #32 s # TEMPERATURE / HUMIDITY:68*/41% THIS INS'IRUMENT WAS CALIBRATED USING MASTER CALIBRATOR SERIAL NO. 5217 CALIBRATED ON &l7/96 DUE: &l?/98 TRACEABLE TO THE NIST THROUGH NIST TEST NO. MMAP 822/LA Ob __ CALIBRATIOh TECHNICIAN mat. ANSI Biff.14 Raf. Federal Spes. GGG-W.408 Ms.w.aaerr Ca m rostos h to A Mb.'. Set.1 Essemseed levelof sesersey b 21% TR MG 041 Re. 00 Page C11 dC11 m}}