ML20009C529
| ML20009C529 | |
| Person / Time | |
|---|---|
| Site: | McGuire, Mcguire |
| Issue date: | 07/02/1981 |
| From: | Sniezek J NRC OFFICE OF INSPECTION & ENFORCEMENT (IE) |
| To: | Eisenhut D Office of Nuclear Reactor Regulation |
| Shared Package | |
| ML20009C444 | List: |
| References | |
| NUDOCS 8107210197 | |
| Download: ML20009C529 (29) | |
Text
{{#Wiki_filter:r, peg'o,, UNITED STATES '3 y NUCLEAR REGULATORY COMMISSION o 34 Ll WASHINGTON D. C. 20555 \\ *- / JUL 2 1981 ; MEMORANDUM FOR: Darrell G. Eisenhut, Director, Division.of Licensing, NRR Richard H. Vollmer, Directoy, Division of Engineering, NRR Y. FROM: James H. Sniezek, Director, Division of Resident and Regional Reactor inspectipy, IE'
SUBJECT:
SANDIA CONNECTOR TEST RESULTS Forwarded for your information is a preliminary IE Inspection Report covering a recently completed environmental test by the-Sandia National Laboratory of an electrical penetration assembly (EPA) supplied by the Duke Power Company. The specific EPA was one of a batch of assemblies procurred from the D. G. O'Brien Company for installation in the Catawba plant. Similar units are installed in the McGuire plant. Testing resulted in a failure (electrical grounding).of three of the 208 individual conduchrs passing through the connector ass 'mbly. Thirteen of the remaining ccnducturs also showed a reduction in resistance to ground but maintained electrical continuity. The failtfre (as analyzed to have been caused by the extrusion of grommet sealing material which stripped insulation from the conductors and exposed the conductor to a metallic plug sleeve. The extrusion mechanism is attributed to the elevated temperatures utilized in the accelerated aging process. We believe that the test results are inconclusive regarding the connector assembly suitability for service since the installed assemblies will not be exposed to the elevated aging temperatures during actual service life. Under lower temperature conditions, induced stresses in the assembled unit are lower; thereby, extrusion of the grommet material would not be expected to occur. Previous qualification tests provide adequate assurance that the c.-trusion mechanism should not cause failure during or following postulated LOCA conditions. The D@.e Power Company is currently initiating additional tests to further confira that the failure mechanism was caused by the accelerated aging process and to further confirm that with proper adjustments that the EPA is suitable fcr its intended service. IE plans to monitor these tests. 1M Jatnes H. Sniezek,fj;irector Dfvision of Resident and Regional Reactor Inspection Office of Inspection and Enforcement
Enclosure:
As stated i 0107210197 810708 PDR ADOCK 05000369 1 0 PDR
e 2-JUL 2 1981 'D.-G. Eisenhut R. H. Vollmer cc/w enclosure: V. Stello, IE R. B. Minogue,.RES Z. Rosztoczy, NRR W.' Farmer, RES D. Sullivan, RES R. Birkel, NRR K. Jabbour, NRR J. P. O'Reilly, RII U. Potarovs, RIV R. Tedesco, NRR-E. Adensam, NRR 4 i r. 1 i e t i a- ? 4 1 y-.-- ,y-, ,my_,,+,-w----- ,,, = - - - r
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-n. .~- I Date: June :26,1981 r
- To
- 61. ' R. Rutherford 4
- '.t From:
- 0. G. Mcdonald y
J. R. Agee f
Subject:
Preliminary Assessmept of D. G. O'Brien, Type K, Electrical Penetraedon Assembly (EPA) The purpose of this memorandum is to provide a pre-11minary description and assessment o.f tne failures wnich occurred'during the verification. test of. the suoject EPA.~. On June 23, 1981 a meeting'was held with representatives of StiL, Duke Power Ccmpany (DPC),' O. G. O'Brien, and Brand Rex Cable Co. to devise a disassembly procedure for.the r. test specimen. The purpose of the procedure is to identify, isolate and determine the cause of f ailures which occurred during the test. This procedure, Attachment A, was revised on June 29 ani 25 as the result of information ootai,ned as the disassembly progressed. Secuence of Events 1. The. EPA was, received by SNL and a visual inspection i- [ was performed. Each connector (coupling) ring required .[ approximately one-quarter (1/4). turn re-torquing to achieve tne specified twenty-five (25) ft-lbs torque. i 2. Pre-test insulation resistance (IR) measurements were taken to estaolish baseline data. The readings were in the 9 range of 10 ohms. j. l [ s-
v. .s. ii. R. Rutherford, 3. The EPA,. including the cable connector assemolies, 0 was' aged for one-hundred-sixty-eight (168) hours at 150 C. All the connectors required approximately one (1) turn of re-torquing subsequent to the accelerated thermal aging: process. 4. Post thermal aging IR measurements were taken. The 9 readings were in the range of 10 ohms. Post radiation (approximately 240 hours at.75 MR/hr) IR measurements were approximately one-half the post thermal aging In values. Also, about one-sixth turn of re-torquing was applied prior to the accident sequence. i 5 The harsh environment portion of the test was initiated i with 600V AC applied to all the circuits. Approximately three (3) hour's into the test, at 120 C saturated steam, the 600V AC was removed and functional measurements (continuity and IR readings) were taken on all circuits. Initially, twelve (12) of the 104 circuits exhibited low or erratic r ead ing s. The 600V AC could not be re-established on two (2) of these circuits which were, pin "J" of connector assembly Nos. 10 & 15, and pin "K" of connector assembly dos. 1 & 12. l Both circuits drew excessive current which tripped the 600v i t-AC power supply. b
i ti. R. Rutherford -3 ~ x 6. Prior to_ completion of^the test a; third failure occurred. .The-f ailure was on pin "G" of connector assembly Nos. 3 & 13 and required removal-of the 600V AC. s.
- tr, d 7.
FinalIR readings, prior to' termination -of tne test, were taken on all circuits.. TN readings were in the range of l' 06 7 to 10 ohms. Of the" initial. thirteen (13) circuits with IR readings of less than 106 ohms, seven (7) recovered, exhibiting readings' greater than-5 x '106 ohms. Three (3) of the remaining six (6) were the previously identified short circuits which required removal of the 600V AC.
- 8. 'All circuits, excluding the three (3) short circuits r.
mentioned above, were energized with 600V AC with leakage in tne range of 0.4 to 0.8 milliamps (ma) during the current test. 9. The test was concluded and the following actions were 4 performed: a. All immersign heaters were turned off. b. The water in the test chamber was pumped out and the test was vented to atmosphere. The 600V AC power supply was disconnected. c. 10. Approximately twenty-four ( 24 ) hours after termination of the test, IR and continuity measurements were't'aken. Only-seventeen (17) circuits had readings greater than 106 ohms, L t t - re-w- --,r r r,,,e- ~. -,, - e t
o.: Y.~ .W. R. Rutherford 4-- .and twenty-five (25 circuits could withstand the 600V AC while drawing less than five-(5) ma.of currene. Disassembly Procedure Attachment A provides the detailed disassembly procedure used by the SNL staf f. to isolate the failures and provide detailed information to assist in determining the causes.of the f ailures. The acceptance criteria identified in the test plan was' that the circuits be capable of maintaining 600V AC. power and periodic IR readings greater than 5 x 10 6-ohr.s. A orief summary of the actions required by the procedure T is: 1. Examination of the external connectors 1 2. Removal of the test chamber cover. 3. Performance of hi-pot testing of all circuits with the ' cable submerged in water to assure that no shorts existed in the internal jumper cables. 4. Letailed examination of the failed circuits. S. Removal of the remaining -internal cable connector assemblies. t O 3 m ---,,~m-m.-
3, m W. R. Rutherford e m Preliminary Find'ings Attachments B through E provide details of circuit arrangementc, connector pairs, cable connectdr assemblies, ./ and test ' set-up details. 'f Attachment B identifies [the failed circuits which include the three (3) circuits'that appeared to be shorted. Determination was made to concentrate on the connector pair assemblies, which include the apparedt shor t circuits and also somc circuits exhibiting low IR readings. Attachment C identifies the connector pair assemblies. 4 The external cable and connector assemblies were disconnected and eliminated as a source of the f,aulps., The test chamber lid was then removed, exposing the test specimen. Tne j unction box which housed the caole connector assemblies was removed. The cables were then submerged in water and a hi-pot was performed to determine if my faults existed in the cable portion of the assemolies. No faults were found. The next step was to isolate the location of the fault which would be in one (1) of the connectors of the connector ^ pair assembly, or one (1) of the modules to which the connectors are mated. Attachment E provides a view of a connector pair and its mating penetration modules. The faults were isolated to indi-vidual connectors with one (1) exception; pin "G" on module exhibited a low IR reading. e,-
-{, v. ii. R. Rutherford Attachment D identifies the component parts rf the connector. It was determined that the cable grommet, which provides the seal for the back portion of the connector, was where the f aults were occurring. One (1) of the connector assembliet was dried overnight in a vacuum oven to determine if a direct snort existed or if the apparent direct short was-the result of moisture ingress. All the low IR readings on that connector improved with the exception of the pin assumed to be shorted. This pin exhibited a low IR reading, indicating a partial but not direct short. During the removal of the connector cable assemblies from the modules, it was noted that the connectors which connected to t-he inner ring of modules (11 through 16) had moisture on the connector faces.
- However, with tne exception of the modules, the surfaces of the pene-tration modules appeared to be dry.
It should also be noted that the' outer ring of a.ocules (1 through 10) had no moisture at the connector faces. See Attachment C for the module locations. Assumed Causes Tne failure me'chanism appears to be the cable grommet which provides tne rear seal. The grommet materia] is a Dow Chemical Co. RTV silicone. It appears that the re-torquing of the connectors identified in the " Sequence of Events" section, resulted in ex-truding the silicone material and displacing the cable conductor insulating material (XLPE, cross-linked polyethylene) resulting in exposed or partially exposed conductors near the crass plug
a ~ ^ 7.) 7,. S' 4. R. Rutherford, \\ sleeve. The initial thickness of the grommet was 250 mils. Measurements taken indicate tb1 grommets were compretssed to about 150 mils after the re-torquing. As pre,v,iously noted, tne connectors required.a full tur.g, of tor'quing (60 mils) y-after the accelerated aging process. sanclusions As identified above, the ext'rusion of tne cable grommet material, resulting in a weak point or bare wires in the caole conductors, was the probable cause of the f ailures. It was noted that during the disassembly that some cable clamps had broken and the rear connector coupling rings were loose. How-e'v e r, the broken clamps did not contribute to any of the failures. The loose rear coupling rings were' nod the probrble path for the moisture ingress at the interface of the cable connector and . cod ul e. It is assumed the path for the moisture ingress was through the rear of the connector as the result of the rear seal failure. Follow-Up Actions SNL will perform the following: 1. Record IR reading on all cable connector assemblies, coth wet and' dry. ( 2. Evacuate EPA module No.3 and determine if the low IR i i reading on pin "G* is the result of moisture. l
3.;. ,e- ~q "t if.* p. : (fii W. R. RutherCord 3. Perform IR readings on remaining modules. 4. Provide' dimension /durometer measurements of the-silicone grommet at the penetration module inter-face SNL requested that D. G. O'Brien provide detailed infor-mation on.the materials, tolerances, and assemoly of the connectors. SNL also indicated that a preliminary report will be provided.by July 15, 1981. We indicated to SNL and Duke Power Co. (DPC) representative that a meeting will be' held at NRC headquat ters following the receipt of the SNL report. r. Copy to: 'D. G. Mcdonald (2) 4440 G. R. Otey 4445 L. O. Cropp 4445 L. L. Bonzon (3) J G 4 l 6 t-
..e N. y% c;2.5 cmoly Procsdura for Catawba Fenetration/ Connector Assembly Dated: June 25,1981 ~ Pavised: ~0une 24, 1981 Rvvised: June 25, 1981 N Completed - 1. ' Take Insulation Resistance (IR) readings (at 500V DC) while still at tsmperature (about 109 C).,. 2 2, Take IR readings when the uni,t reaches room temperature. 3. Take' IR readings again before star ting disassembly. Y ?' 4. Disconnect #2 (14-pin) outboard-connector. r A. Cut cable 2-3 feet above the connector 8. Check and record forward torque before removing the connector C. Take pictures documenting status 5. Disassemble #2 outboard connector A. Document status, condition 1 B. Hilberg disassembles, to detecmine condition 6. Check reverse torque on all outboard connectors. 7. Disconnect all outboard connectors. 8. Take IR readinge of all suspect pins / connectors. 9. 'Open test chamber, per form IR measur tments and hi-pot tests on suspect pins / connector-(limit to 600V AC and increase slowly) remove inboard junction box. 10. Visually inspect and document status of inboard connectors and cabling; note any abnormalities. 11. Suspend cables only in suitable water bath (e.g., the test enamber) to do low hi-pot tests and IR measurements. The cable clamps shall not be submerged. I 12. Perform IR measurements and hi-pot tests on suspect pins / connectors. A. Limit hi-pot tests to 600V AC to prevent further damage; increase slowly B. Watch for flashes or bubbling in water as voltage is l l .. U
p ~-- c. ,. Dated:. June 23, 1981 Revised: June 24, 1981 Revised: June 25, 1;e 81 Completed 13. Remove cables from water bath. .14. Remove cable clamps from inboard connectors; do not spread cables. A. Perform visuals and document B. Perform IR measurements and hi-pot. tests (up to 600V AC and increase slow 3y) on suspect pins. (Attempt to detect ground connection in clamps) 15. Spread cables and repeat step 14. 16. Cut conductors' (at middle of loop) and perform IR measurements on the suspect pins; this procedure will isolate the damc;ed connector modules. 17. Check and record forward torque on #2 inboard connector. 18. Remove #2 inboard connector ( this is deemed a " good" connector). r A. Visually inspect receptac1'e, re' cord and document observations B. Do immediate IK measurement on module / penetration C. Bag and tape the receptacle to prevent moisture dryout of face 19. Disassemble #2 inboard connector. A. Visually inspect cor moisture intrusion on sealing surface B. Check for* damage; take pictures C. Hilberg disassembles, to determine condition D. Compare to #2 outboard connector condition. (Determine general condition of connector for use in further dis-assembles) 20. Measure reverse torque on #10 (or #15) inboard connector depending on previous steps. This is start of disassembly .of a deemed " bad" connector.
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ac. . Dated: June 23, lydl ~ Re /.i sed : June 24, 1981 - Re,ised: June 25, 1981-Completed
- 21. -Remove #10 (or #15)-inboard ~ connector.
A. Visually inspect receptacle, recor'dand document observations 7 ,j g* B. Do immediate.IR.measurem,ents on module / penetration Bag' and tape the re<c$eptacle-tof prevent moisture C. dryout of face 22. Perform IR measurement on #10 - (or #15) inboard connector. A. If shor ted,- dry i'n vacuum ov'en at low temperature, for.a period of time._ Repeat IR measurement 2-B. If not' shorted, perform disassembly l 23. Disassemble ~ #10 (or #15) connector A. Visually inspect for moisture intrusion on sealing surfaces r. S. Check for damage; take pictures 1 C. Hilberg disassembles, to determine condition D. Check for:- l - =oisture between g rommet and insulation - deformation of the conductors at grommet - grommet condition f - other physical damage 24. Fepeat steps 20-23 on #15 inboard connector. 25. Repe'at steps 20-23 on the #3 inboard connector; as deemed necessary (some parts of 20-23 may be omitted). 26. F.epe a t steps 20-23 on #13 inboard connector; as deemed necessary L (some par ts. of 20-23 may be omitted). i f 7 1 v--w---,e =. + + - -- w w r,
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?[*_ NN.. ,*y J. -Dated: June'23, 1981 Revised: June 24, 1981 Revised: June 25, 1981 Completed ~ 27. Repeat steps 20-23 on il inboard connector; as deemed necessary (some parts of 20-23 may be omitted). s - 28. Repeat steps 20-23 on #12 inboard connector; as deemed necessary (some parts of 20-23 may be omitted). 29.- Remove all other inboard connectors; perform vicual inspections, document all observations, bag and saye all pieces. e 4 ~ r O d l
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